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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  37673.69
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   133.2
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.252
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 3977)
    ---------------------------------------
 
    Vector Time (GMT): 2014/351/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1445190.11                 A    =         6793036.69  meter
     Y    =       -6372841.44  meter          E    =           .0017198
     Z    =        1840999.57                 I    =           51.29878
     XDOT =       4503.555582                 Wp   =           90.38057
     YDOT =       2653.822351  meter/sec      RA   =          269.73200  deg
     ZDOT =       5605.556120                 TA   =          289.95216
                                              MA   =          290.13732
                                              Ha   =            226.013  n.mi
                                              Hp   =            215.538
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4741437.38                 X    =         1507402.25
     Y    =      -20908272.45  feet           Y    =        -6356332.63  meter
     Z    =        6040024.82                 Z    =         1848170.96
     XDOT =      14775.444824                 XDOT =        4446.314989
     YDOT =       8706.766244  feet/sec       YDOT =        2703.863711  meter/sec
     ZDOT =      18390.932151                 ZDOT =        5627.295035
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20441449.41                 X    =         6230553.78
     Y    =        6434248.63  feet           Y    =         1961158.98  meter
     Z    =        6071785.24                 Z    =         1850680.14
     XDOT =      -9434.036876                 XDOT =       -2875.494440
     YDOT =      12389.153881  feet/sec       YDOT =        3776.214103  meter/sec
     ZDOT =      18483.127926                 ZDOT =        5633.657392
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14351.56073791  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6460 270.2430 0007236 142.4564 217.7094 15.52357720 39780
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14351.56073791   =   yrday.fracday
    Element set:     900
    Inclination:       51.6460  deg
    RA of node:       270.2430  deg
    Eccentricity:     .0007236     
    Arg of perigee:   142.4564  deg
    Mean anomaly:     217.7094  deg
    Mean motion:   15.52357720  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3978
    Checksum:              303
 
 
    Coasting Arc #2 (Orbit 3992)
    ---------------------------------------
 
    Vector Time (GMT): 2014/352/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1781920.20                 A    =         6790709.73  meter
     Y    =        5880731.85  meter          E    =           .0011433
     Z    =       -2886957.76                 I    =           51.29380
     XDOT =      -4386.118888                 Wp   =          134.42487
     YDOT =      -3782.500713  meter/sec      RA   =          264.74134  deg
     ZDOT =      -5017.896206                 TA   =           78.59387
                                              MA   =           78.46546
                                              Ha   =            225.795  n.mi
                                              Hp   =            215.534
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5846194.90                 X    =        -1833523.45
     Y    =       19293739.67  feet           Y    =         5860516.93  meter
     Z    =       -9471646.20                 Z    =        -2895739.10
     XDOT =     -14390.153833                 XDOT =       -4319.120555
     YDOT =     -12409.779243  feet/sec       YDOT =       -3831.174196  meter/sec
     ZDOT =     -16462.914063                 ZDOT =       -5039.041060
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18865872.94                 X    =        -5750318.07
     Y    =       -7055059.68  feet           Y    =        -2150382.19  meter
     Z    =       -9510175.49                 Z    =        -2898701.49
     XDOT =      12818.425158                 XDOT =        3907.055988
     YDOT =     -12054.083311  feet/sec       YDOT =       -3674.084593  meter/sec
     ZDOT =     -16552.375369                 ZDOT =       -5045.164013
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14352.52634385  .00016717  00000-0  10270-3 0  9019
    2 25544  51.6470 265.4418 0007234 146.3768 213.7844 15.52430452 39930
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14352.52634385   =   yrday.fracday
    Element set:     901
    Inclination:       51.6470  deg
    RA of node:       265.4418  deg
    Eccentricity:     .0007234     
    Arg of perigee:   146.3768  deg
    Mean anomaly:     213.7844  deg
    Mean motion:   15.52430452  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3993
    Checksum:              313
 
 
    Coasting Arc #3 (Orbit 4008)
    ---------------------------------------
 
    Vector Time (GMT): 2014/353/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2118408.85                 A    =         6788078.13  meter
     Y    =       -5232591.74  meter          E    =           .0016904
     Z    =        3763100.24                 I    =           51.28898
     XDOT =       4284.992247                 Wp   =          116.89690
     YDOT =       4772.060576  meter/sec      RA   =          259.74647  deg
     ZDOT =       4201.188722                 TA   =          288.40544
                                              MA   =          288.58916
                                              Ha   =            225.664  n.mi
                                              Hp   =            215.566
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6950160.28                 X    =         2158483.40
     Y    =      -17167295.74  feet           Y    =        -5208678.58  meter
     Z    =       12346129.40                 Z    =         3773488.13
     XDOT =      14058.373515                 XDOT =        4210.903301
     YDOT =      15656.366720  feet/sec       YDOT =        4819.563518  meter/sec
     ZDOT =      13783.427565                 ZDOT =        4221.825229
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16806826.88                 X    =         5122720.83
     Y    =        7709200.81  feet           Y    =         2349764.41  meter
     Z    =       12391387.13                 Z    =         3776894.80
     XDOT =     -15764.635759                 XDOT =       -4805.060979
     YDOT =      11957.220383  feet/sec       YDOT =        3644.560773  meter/sec
     ZDOT =      13870.549035                 ZDOT =        4227.743346
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14353.55628255  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6466 260.3207 0007256 150.2268 209.9298 15.52484392 40099
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14353.55628255   =   yrday.fracday
    Element set:     902
    Inclination:       51.6466  deg
    RA of node:       260.3207  deg
    Eccentricity:     .0007256     
    Arg of perigee:   150.2268  deg
    Mean anomaly:     209.9298  deg
    Mean motion:   15.52484392  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4009
    Checksum:              316
 
 
    Coasting Arc #4 (Orbit 4023)
    ---------------------------------------
 
    Vector Time (GMT): 2014/354/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2554334.18                 A    =         6785191.98  meter
     Y    =        4384228.06  meter          E    =           .0012632
     Z    =       -4513729.16                 I    =           51.28740
     XDOT =      -4139.373182                 Wp   =          104.24253
     YDOT =      -5628.495648  meter/sec      RA   =          254.74628  deg
     ZDOT =      -3134.976175                 TA   =          134.16468
                                              MA   =          134.06078
                                              Ha   =            225.415  n.mi
                                              Hp   =            215.531
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8380361.48                 X    =        -2581243.45
     Y    =       14383950.33  feet           Y    =         4355513.85  meter
     Z    =      -14808822.71                 Z    =        -4526202.73
     XDOT =     -13580.620675                 XDOT =       -4060.897603
     YDOT =     -18466.193072  feet/sec       YDOT =       -5674.345697  meter/sec
     ZDOT =     -10285.354904                 ZDOT =       -3154.894733
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14109440.43                 X    =        -4300557.44
     Y    =       -8743571.10  feet           Y    =        -2665040.47  meter
     Z    =      -14862818.41                 Z    =        -4530187.05
     XDOT =      18253.479371                 XDOT =        5563.660512
     YDOT =     -11887.304795  feet/sec       YDOT =       -3623.250501  meter/sec
     ZDOT =     -10369.270804                 ZDOT =       -3160.553741
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14354.52181008  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6474 255.5192 0007189 154.1546 205.9966 15.52569391 40242
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14354.52181008   =   yrday.fracday
    Element set:     903
    Inclination:       51.6474  deg
    RA of node:       255.5192  deg
    Eccentricity:     .0007189     
    Arg of perigee:   154.1546  deg
    Mean anomaly:     205.9966  deg
    Mean motion:   15.52569391  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4024
    Checksum:              318
 
 
    Coasting Arc #5 (Orbit 4039)
    ---------------------------------------
 
    Vector Time (GMT): 2014/355/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3009480.07                 A    =         6782997.05  meter
     Y    =       -3439494.64  meter          E    =           .0012429
     Z    =        5008666.54                 I    =           51.28926
     XDOT =       3959.362343                 Wp   =          143.33443
     YDOT =       6280.231351  meter/sec      RA   =          249.74202  deg
     ZDOT =       1921.412497                 TA   =          287.86894
                                              MA   =          288.00446
                                              Ha   =            225.229  n.mi
                                              Hp   =            215.650
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9873622.26                 X    =         3023387.13
     Y    =      -11284431.25  feet           Y    =        -3405763.49  meter
     Z    =       16432633.01                 Z    =         5023319.57
     XDOT =      12990.033934                 XDOT =        3879.507454
     YDOT =      20604.433566  feet/sec       YDOT =        6324.060799  meter/sec
     ZDOT =       6303.846775                 ZDOT =        1940.453269
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11136371.54                 X    =         3394366.05
     Y    =        9936276.77  feet           Y    =         3028577.16  meter
     Z    =       16495752.96                 Z    =         5027905.50
     XDOT =     -20070.763419                 XDOT =       -6117.568690
     YDOT =      11829.998938  feet/sec       YDOT =        3605.783676  meter/sec
     ZDOT =       6383.916514                 ZDOT =        1945.817753
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14355.55166576  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6469 250.3976 0007230 158.6518 201.4937 15.52622062 40406
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14355.55166576   =   yrday.fracday
    Element set:     904
    Inclination:       51.6469  deg
    RA of node:       250.3976  deg
    Eccentricity:     .0007230     
    Arg of perigee:   158.6518  deg
    Mean anomaly:     201.4937  deg
    Mean motion:   15.52622062  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4040
    Checksum:              310
 
 
    Coasting Arc #6 (Orbit 4054)
    ---------------------------------------
 
    Vector Time (GMT): 2014/356/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3555202.88                 A    =         6781649.03  meter
     Y    =        2375335.87  meter          E    =           .0017713
     Z    =       -5278055.71                 I    =           51.29720
     XDOT =      -3657.621947                 Wp   =          108.77690
     YDOT =      -6700.454292  meter/sec      RA   =          244.73390  deg
     ZDOT =       -558.901631                 TA   =          155.89582
                                              MA   =          155.81282
                                              Ha   =            225.034  n.mi
                                              Hp   =            215.589
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11664051.44                 X    =        -3555861.24
     Y    =        7793096.68  feet           Y    =         2335576.18  meter
     Z    =      -17316455.73                 Z    =        -5295327.64
     XDOT =     -12000.072003                 XDOT =       -3579.709107
     YDOT =     -21983.117755  feet/sec       YDOT =       -6740.920495  meter/sec
     ZDOT =      -1833.666770                 ZDOT =        -576.481252
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7818392.08                 X    =        -2383045.91
     Y    =      -11536175.84  feet           Y    =        -3516226.40  meter
     Z    =      -17390557.31                 Z    =        -5300641.87
     XDOT =      21114.067142                 XDOT =        6435.567665
     YDOT =     -11469.310980  feet/sec       YDOT =       -3495.845987  meter/sec
     ZDOT =      -1907.447309                 ZDOT =        -581.389940
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14356.51711758  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6469 245.5955 0007125 162.5790 197.5608 15.52693209 40555
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14356.51711758   =   yrday.fracday
    Element set:     905
    Inclination:       51.6469  deg
    RA of node:       245.5955  deg
    Eccentricity:     .0007125     
    Arg of perigee:   162.5790  deg
    Mean anomaly:     197.5608  deg
    Mean motion:   15.52693209  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4055
    Checksum:              335
 
 
    Coasting Arc #7 (Orbit 4070)
    ---------------------------------------
 
    Vector Time (GMT): 2014/357/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4098923.59                 A    =         6781524.01  meter
     Y    =       -1300778.54  meter          E    =           .0006895
     Z    =        5239215.19                 I    =           51.31137
     XDOT =       3251.101585                 Wp   =          140.86424
     YDOT =       6897.006043  meter/sec      RA   =          239.72578  deg
     ZDOT =       -835.796075                 TA   =          317.13335
                                              MA   =          317.18708
                                              Ha   =            224.700  n.mi
                                              Hp   =            215.799
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13447912.05                 X    =         4087714.39
     Y    =       -4267646.14  feet           Y    =        -1255004.92  meter
     Z    =       17189026.23                 Z    =         5259099.64
     XDOT =      10666.343784                 XDOT =        3177.796011
     YDOT =      22627.972582  feet/sec       YDOT =        6932.952178  meter/sec
     ZDOT =      -2742.113108                 ZDOT =        -820.180201
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4525762.83                 X    =         1379452.51
     Y    =       13253119.80  feet           Y    =         4039550.92  meter
     Z    =       17274086.12                 Z    =         5265141.45
     XDOT =     -21448.314888                 XDOT =       -6537.446378
     YDOT =      10793.350381  feet/sec       YDOT =        3289.813196  meter/sec
     ZDOT =      -2676.723973                 ZDOT =        -815.865467
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14357.54689280  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6464 240.4733 0007088 167.6301 192.5026 15.52767918 40716
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14357.54689280   =   yrday.fracday
    Element set:     906
    Inclination:       51.6464  deg
    RA of node:       240.4733  deg
    Eccentricity:     .0007088     
    Arg of perigee:   167.6301  deg
    Mean anomaly:     192.5026  deg
    Mean motion:   15.52767918  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4071
    Checksum:              325
 
 
    Coasting Arc #8 (Orbit 4085)
    ---------------------------------------
 
    Vector Time (GMT): 2014/358/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4673712.36                 A    =         6782826.64  meter
     Y    =         218655.27  meter          E    =           .0016561
     Z    =       -4925540.45                 I    =           51.33220
     XDOT =      -2659.077405                 Wp   =          129.04816
     YDOT =      -6826.729234  meter/sec      RA   =          234.71851  deg
     ZDOT =       2214.876677                 TA   =          162.73465
                                              MA   =          162.67826
                                              Ha   =            224.642  n.mi
                                              Hp   =            215.753
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15333701.95                 X    =        -4651883.67
     Y    =         717372.94  feet           Y    =          166513.25  meter
     Z    =      -16159909.63                 Z    =        -4948191.36
     XDOT =      -8724.007234                 XDOT =       -2593.300711
     YDOT =     -22397.405622  feet/sec       YDOT =       -6856.097166  meter/sec
     ZDOT =       7266.655765                 ZDOT =        2202.118625
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1274778.41                 X    =         -388552.46
     Y    =      -15194668.85  feet           Y    =        -4631335.07  meter
     Z    =      -16256589.35                 Z    =        -4955008.43
     XDOT =      20951.535416                 XDOT =        6386.027995
     YDOT =      -9493.448143  feet/sec       YDOT =       -2893.602994  meter/sec
     ZDOT =       7213.425878                 ZDOT =        2198.652208
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14358.51227202  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6459 235.6702 0007028 171.4574 188.6699 15.52803001 40863
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14358.51227202   =   yrday.fracday
    Element set:     907
    Inclination:       51.6459  deg
    RA of node:       235.6702  deg
    Eccentricity:     .0007028     
    Arg of perigee:   171.4574  deg
    Mean anomaly:     188.6699  deg
    Mean motion:   15.52803001  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4086
    Checksum:              313
 
 
    Coasting Arc #9 (Orbit 4101)
    ---------------------------------------
 
    Vector Time (GMT): 2014/359/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5177623.34                 A    =         6784950.46  meter
     Y    =         788820.16  meter          E    =           .0010421
     Z    =        4302596.06                 I    =           51.35901
     XDOT =       1903.477346                 Wp   =          112.00052
     YDOT =       6561.930564  meter/sec      RA   =          229.71670  deg
     ZDOT =      -3490.661423                 TA   =           13.63862
                                              MA   =           13.61048
                                              Ha   =            224.219  n.mi
                                              Hp   =            215.968
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16986953.22                 X    =         5147517.43
     Y    =        2587992.64  feet           Y    =          846551.10  meter
     Z    =       14116128.79                 Z    =         4327674.79
     XDOT =       6245.004416                 XDOT =        1846.915099
     YDOT =      21528.643584  feet/sec       YDOT =        6582.900444  meter/sec
     ZDOT =     -11452.301255                 ZDOT =       -3481.551704
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1674588.15                 X    =         -510414.47
     Y    =       17012387.69  feet           Y    =         5185375.77  meter
     Z    =       14223002.40                 Z    =         4335171.13
     XDOT =     -19915.154145                 XDOT =       -6070.138983
     YDOT =       7590.776355  feet/sec       YDOT =        2313.668633  meter/sec
     ZDOT =     -11414.573196                 ZDOT =       -3479.161910
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14359.54196962  .00016717  00000-0  10270-3 0  9089
    2 25544  51.6458 230.5472 0006896 175.8815 184.2395 15.52891952 41024
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14359.54196962   =   yrday.fracday
    Element set:     908
    Inclination:       51.6458  deg
    RA of node:       230.5472  deg
    Eccentricity:     .0006896     
    Arg of perigee:   175.8815  deg
    Mean anomaly:     184.2395  deg
    Mean motion:   15.52891952  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4102
    Checksum:              347
 
 
    Coasting Arc #10 (Orbit 4116)
    ---------------------------------------
 
    Vector Time (GMT): 2014/360/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5611286.22                 A    =         6787795.71  meter
     Y    =       -1699371.88  meter          E    =           .0008665
     Z    =       -3432089.51                 I    =           51.38900
     XDOT =       -953.015033                 Wp   =          145.56684
     YDOT =      -6073.255141  meter/sec      RA   =          224.72038  deg
     ZDOT =       4563.914744                 TA   =          174.15344
                                              MA   =          174.14332
                                              Ha   =            224.223  n.mi
                                              Hp   =            216.015
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18409731.70                 X    =        -5575194.65
     Y    =       -5575367.07  feet           Y    =        -1761918.97  meter
     Z    =      -11260136.20                 Z    =        -3459260.40
     XDOT =      -3126.689742                 XDOT =        -907.201373
     YDOT =     -19925.377759  feet/sec       YDOT =       -6083.656418  meter/sec
     ZDOT =      14973.473571                 ZDOT =        4559.396200
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4258848.87                 X    =         1298097.14
     Y    =      -18688155.45  feet           Y    =        -5696149.78  meter
     Z    =      -11375792.65                 Z    =        -3467341.60
     XDOT =      18281.880404                 XDOT =        5572.317147
     YDOT =      -4939.887319  feet/sec       YDOT =       -1505.677655  meter/sec
     ZDOT =      14955.237897                 ZDOT =        4558.356511
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14360.50727656  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6451 225.7432 0006926 180.3327 179.7821 15.52908671 41178
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14360.50727656   =   yrday.fracday
    Element set:     909
    Inclination:       51.6451  deg
    RA of node:       225.7432  deg
    Eccentricity:     .0006926     
    Arg of perigee:   180.3327  deg
    Mean anomaly:     179.7821  deg
    Mean motion:   15.52908671  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4117
    Checksum:              320
 
 
    Coasting Arc #11 (Orbit 4132)
    ---------------------------------------
 
    Vector Time (GMT): 2014/361/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5870752.20                 A    =         6790335.29  meter
     Y    =        2477656.77  meter          E    =           .0016766
     Z    =        2315690.23                 I    =           51.42129
     XDOT =       -168.562263                 Wp   =          130.59415
     YDOT =       5454.961655  meter/sec      RA   =          219.73235  deg
     ZDOT =      -5394.162633                 TA   =           23.49918
                                              MA   =           23.42266
                                              Ha   =            223.912  n.mi
                                              Hp   =            216.143
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19260998.04                 X    =         5831361.39
     Y    =        8128795.19  feet           Y    =         2543087.01  meter
     Z    =        7597408.89                 Z    =         2344113.60
     XDOT =       -553.025797                 XDOT =        -203.345578
     YDOT =      17896.855824  feet/sec       YDOT =        5452.882375  meter/sec
     ZDOT =     -17697.383968                 ZDOT =       -5395.065782
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6402747.25                 X    =        -1951557.36
     Y    =       19854893.51  feet           Y    =         6051771.54  meter
     Z    =        7718290.63                 Z    =         2352534.99
     XDOT =     -16416.523614                 XDOT =       -5003.756398
     YDOT =       1606.325858  feet/sec       YDOT =         489.608122  meter/sec
     ZDOT =     -17702.170380                 ZDOT =       -5395.621532
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14361.53689873  .00016717  00000-0  10270-3 0  9102
    2 25544  51.6453 220.6197 0006862 183.5541 176.5564 15.52977483 41338
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14361.53689873   =   yrday.fracday
    Element set:     910
    Inclination:       51.6453  deg
    RA of node:       220.6197  deg
    Eccentricity:     .0006862     
    Arg of perigee:   183.5541  deg
    Mean anomaly:     176.5564  deg
    Mean motion:   15.52977483  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4133
    Checksum:              334
 
 
    Coasting Arc #12 (Orbit 4147)
    ---------------------------------------
 
    Vector Time (GMT): 2014/362/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5950292.48                 A    =         6792039.17  meter
     Y    =       -3098965.97  meter          E    =           .0004883
     Z    =       -1060849.25                 I    =           51.45121
     XDOT =       1412.496896                 Wp   =           82.54991
     YDOT =      -4713.710544  meter/sec      RA   =          214.74933  deg
     ZDOT =       5870.961727                 TA   =          265.93039
                                              MA   =          265.98621
                                              Ha   =            223.783  n.mi
                                              Hp   =            216.301
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19521956.97                 X    =        -5910043.66
     Y    =      -10167211.19  feet           Y    =        -3165280.93  meter
     Z    =       -3480476.54                 Z    =        -1089657.03
     XDOT =       4634.176169                 XDOT =        1436.582717
     YDOT =     -15464.929606  feet/sec       YDOT =       -4697.780594  meter/sec
     ZDOT =      19261.685456                 ZDOT =        5877.881741
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8056733.65                 X    =         2455692.42
     Y    =      -20462179.95  feet           Y    =        -6236872.45  meter
     Z    =       -3602906.97                 Z    =        -1098166.04
     XDOT =      14360.346509                 XDOT =        4377.033616
     YDOT =       2270.674753  feet/sec       YDOT =         692.101665  meter/sec
     ZDOT =      19292.021364                 ZDOT =        5880.208112
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14362.50213316  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6444 215.8151 0006842 188.6418 171.4618 15.53018705 41485
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14362.50213316   =   yrday.fracday
    Element set:     911
    Inclination:       51.6444  deg
    RA of node:       215.8151  deg
    Eccentricity:     .0006842     
    Arg of perigee:   188.6418  deg
    Mean anomaly:     171.4618  deg
    Mean motion:   15.53018705  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4148
    Checksum:              295
 
 
    Coasting Arc #13 (Orbit 4163)
    ---------------------------------------
 
    Vector Time (GMT): 2014/363/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5754827.30                 A    =         6792414.58  meter
     Y    =        3575801.60  meter          E    =           .0016488
     Z    =        -309367.37                 I    =           51.47894
     XDOT =      -2752.065949                 Wp   =          157.43145
     YDOT =       3921.151357  meter/sec      RA   =          209.77199  deg
     ZDOT =      -5992.352439                 TA   =           25.91086
                                              MA   =           25.82839
                                              Ha   =            223.633  n.mi
                                              Hp   =            216.400
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18880667.00                 X    =         5715916.94
     Y    =       11731632.55  feet           Y    =         3639938.27  meter
     Z    =       -1014984.80                 Z    =         -281505.75
     XDOT =      -9029.087758                 XDOT =       -2766.599873
     YDOT =      12864.669806  feet/sec       YDOT =        3890.294928  meter/sec
     ZDOT =     -19659.948946                 ZDOT =       -6005.756673
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9330842.02                 X    =        -2844040.65
     Y    =       20180990.33  feet           Y    =         6151165.85  meter
     Z    =        -896660.03                 Z    =         -273301.98
     XDOT =     -12384.717024                 XDOT =       -3774.861749
     YDOT =      -6582.288369  feet/sec       YDOT =       -2006.281495  meter/sec
     ZDOT =     -19717.828775                 ZDOT =       -6009.994211
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14363.53167959  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6442 210.6913 0006934 192.4050 167.6932 15.53058476 41642
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14363.53167959   =   yrday.fracday
    Element set:     912
    Inclination:       51.6442  deg
    RA of node:       210.6913  deg
    Eccentricity:     .0006934     
    Arg of perigee:   192.4050  deg
    Mean anomaly:     167.6932  deg
    Mean motion:   15.53058476  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4164
    Checksum:              318
 
 
    Coasting Arc #14 (Orbit 4179)
    ---------------------------------------
 
    Vector Time (GMT): 2014/364/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5309294.38                 A    =         6791041.46  meter
     Y    =       -3896898.58  meter          E    =           .0010410
     Z    =        1648554.36                 I    =           51.50200
     XDOT =       4066.288296                 Wp   =           92.36478
     YDOT =      -3115.450610  meter/sec      RA   =          204.79376  deg
     ZDOT =       5699.785126                 TA   =          285.71044
                                              MA   =          285.82525
                                              Ha   =            223.333  n.mi
                                              Hp   =            216.504
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17418944.82                 X    =        -5273331.87
     Y    =      -12785100.34  feet           Y    =        -3956069.57  meter
     Z    =        5408642.91                 Z    =         1622849.80
     XDOT =      13340.840865                 XDOT =        4073.136157
     YDOT =     -10221.294653  feet/sec       YDOT =       -3069.940733  meter/sec
     ZDOT =      18700.082434                 ZDOT =        5719.554986
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10225106.87                 X    =         3116612.57
     Y    =      -19065508.82  feet           Y    =        -5811167.09  meter
     Z    =        5299567.01                 Z    =         1615308.02
     XDOT =      10573.774613                 XDOT =        3222.886502
     YDOT =      10921.890458  feet/sec       YDOT =        3328.992212  meter/sec
     ZDOT =      18785.006081                 ZDOT =        5725.669854
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14364.56118430  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6432 205.5657 0006920 197.2101 162.8817 15.53160181 41808
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14364.56118430   =   yrday.fracday
    Element set:     913
    Inclination:       51.6432  deg
    RA of node:       205.5657  deg
    Eccentricity:     .0006920     
    Arg of perigee:   197.2101  deg
    Mean anomaly:     162.8817  deg
    Mean motion:   15.53160181  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4180
    Checksum:              289
 
 
    Coasting Arc #15 (Orbit 4194)
    ---------------------------------------
 
    Vector Time (GMT): 2014/365/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4541574.23                 A    =         6788492.70  meter
     Y    =        4105845.74  meter          E    =           .0008502
     Z    =       -2923029.43                 I    =           51.52174
     XDOT =      -5317.114553                 Wp   =          168.64045
     YDOT =       2319.769772  meter/sec      RA   =          199.81452  deg
     ZDOT =      -5013.487549                 TA   =           44.75127
                                              MA   =           44.68271
                                              Ha   =            223.153  n.mi
                                              Hp   =            216.631
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14900177.92                 X    =         4509523.24
     Y    =       13470622.51  feet           Y    =         4156453.56  meter
     Z    =       -9589991.56                 Z    =        -2901044.76
     XDOT =     -17444.601551                 XDOT =       -5318.305765
     YDOT =       7610.793215  feet/sec       YDOT =        2260.304013  meter/sec
     ZDOT =     -16448.449963                 ZDOT =       -5039.319986
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10962384.43                 X    =        -3341334.78
     Y    =       16884237.02  feet           Y    =         5146315.44  meter
     Z    =       -9496819.41                 Z    =        -2894630.56
     XDOT =      -8998.098026                 XDOT =       -2742.620278
     YDOT =     -15136.293115  feet/sec       YDOT =       -4613.542141  meter/sec
     ZDOT =     -16559.133725                 ZDOT =       -5047.223959
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14365.52631125  .00016717  00000-0  10270-3 0  9146
    2 25544  51.6422 200.7614 0006776 200.9664 159.1212 15.53194499 41955
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14365.52631125   =   yrday.fracday
    Element set:     914
    Inclination:       51.6422  deg
    RA of node:       200.7614  deg
    Eccentricity:     .0006776     
    Arg of perigee:   200.9664  deg
    Mean anomaly:     159.1212  deg
    Mean motion:   15.53194499  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4195
    Checksum:              305
 
 
    Coasting Arc #16 (Orbit 4210)
    ---------------------------------------
 
    Vector Time (GMT): 2014/366/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3534305.39                 A    =         6785225.50  meter
     Y    =       -4206628.66  meter          E    =           .0011313
     Z    =        3980914.82                 I    =           51.54075
     XDOT =       6364.502460                 Wp   =          136.08309
     YDOT =      -1576.617605  meter/sec      RA   =          194.82935  deg
     ZDOT =       3969.708632                 TA   =          272.44586
                                              MA   =          272.57538
                                              Ha   =            222.886  n.mi
                                              Hp   =            216.735
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11595490.14                 X    =        -3506341.10
     Y    =      -13801275.12  feet           Y    =        -4245995.51  meter
     Z    =       13060744.14                 Z    =         3963813.34
     XDOT =      20880.913583                 XDOT =        6362.376086
     YDOT =      -5172.629939  feet/sec       YDOT =       -1505.457811  meter/sec
     ZDOT =      13023.978453                 ZDOT =        4000.621024
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11565097.18                 X    =         3525041.62
     Y    =      -13894707.22  feet           Y    =        -4235106.76  meter
     Z    =       12988428.02                 Z    =         3958872.86
     XDOT =       7687.648966                 XDOT =        2343.195405
     YDOT =      18742.390020  feet/sec       YDOT =        5712.680478  meter/sec
     ZDOT =      13156.243844                 ZDOT =        4010.023124
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14366.55574005  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6416 195.6354 0006795 205.7308 154.3507 15.53258720 42111
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14366.55574005   =   yrday.fracday
    Element set:     915
    Inclination:       51.6416  deg
    RA of node:       195.6354  deg
    Eccentricity:     .0006795     
    Arg of perigee:   205.7308  deg
    Mean anomaly:     154.3507  deg
    Mean motion:   15.53258720  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4211
    Checksum:              309
 
 
    Coasting Arc #17 (Orbit 4225)
    ---------------------------------------
 
    Vector Time (GMT): 2014/367/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2254258.18                 A    =         6782030.77  meter
     Y    =        4247819.33  meter          E    =           .0007881
     Z    =       -4787782.32                 I    =           51.56046
     XDOT =      -7152.340923                 Wp   =          107.77525
     YDOT =        861.429933  meter/sec      RA   =          189.83902  deg
     ZDOT =      -2609.194614                 TA   =          136.48537
                                              MA   =          136.42315
                                              Ha   =            222.666  n.mi
                                              Hp   =            216.761
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7395860.16                 X    =         2229847.83
     Y    =       13936415.12  feet           Y    =         4272891.85  meter
     Z    =      -15707947.25                 Z    =        -4776890.46
     XDOT =     -23465.685444                 XDOT =       -7148.767541
     YDOT =       2826.213692  feet/sec       YDOT =         781.468027  meter/sec
     ZDOT =      -8560.349783                 ZDOT =       -2643.930617
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12253145.18                 X    =        -3734758.65
     Y    =       10010974.41  feet           Y    =         3051345.00  meter
     Z    =      -15662146.89                 Z    =        -4773822.37
     XDOT =      -6500.836767                 XDOT =       -1981.455047
     YDOT =     -21551.448932  feet/sec       YDOT =       -6568.881634  meter/sec
     ZDOT =      -8708.843682                 ZDOT =       -2654.455554
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14367.52079339  .00016717  00000-0  10270-3 0  9163
    2 25544  51.6407 190.8299 0006693 207.7862 152.2934 15.53320839 42268
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14367.52079339   =   yrday.fracday
    Element set:     916
    Inclination:       51.6407  deg
    RA of node:       190.8299  deg
    Eccentricity:     .0006693     
    Arg of perigee:   207.7862  deg
    Mean anomaly:     152.2934  deg
    Mean motion:   15.53320839  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4226
    Checksum:              335
 
 
    Coasting Arc #18 (Orbit 4241)
    ---------------------------------------
 
    Vector Time (GMT): 2014/368/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -839266.78                 A    =         6780081.22  meter
     Y    =       -4233722.42  meter          E    =           .0007716
     Z    =        5230313.08                 I    =           51.58501
     XDOT =       7591.014454                 Wp   =          182.48038
     YDOT =       -194.686767  meter/sec      RA   =          184.84431  deg
     ZDOT =       1052.993839                 TA   =          257.38014
                                              MA   =          257.46643
                                              Ha   =            222.502  n.mi
                                              Hp   =            216.875
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2753499.93                 X    =         -817268.78
     Y    =      -13890165.44  feet           Y    =        -4242985.14  meter
     Z    =       17159819.82                 Z    =         5226289.13
     XDOT =      24904.903064                 XDOT =        7587.512266
     YDOT =       -638.736113  feet/sec       YDOT =        -109.818797  meter/sec
     ZDOT =       3454.704197                 ZDOT =        1089.860932
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12993925.48                 X    =         3960548.49
     Y    =       -5678159.52  feet           Y    =        -1730703.02  meter
     Z    =       17143345.04                 Z    =         5225291.57
     XDOT =       5367.232444                 XDOT =        1635.932449
     YDOT =      23262.502537  feet/sec       YDOT =        7090.410773  meter/sec
     ZDOT =       3612.211302                 ZDOT =        1101.002005
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14368.55014507  .00016717  00000-0  10270-3 0  9174
    2 25544  51.6404 185.7035 0006600 211.9145 148.1608 15.53329702 42423
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14368.55014507   =   yrday.fracday
    Element set:     917
    Inclination:       51.6404  deg
    RA of node:       185.7035  deg
    Eccentricity:     .0006600     
    Arg of perigee:   211.9145  deg
    Mean anomaly:     148.1608  deg
    Mean motion:   15.53329702  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4242
    Checksum:              291
 
 
    Coasting Arc #19 (Orbit 4256)
    ---------------------------------------
 
    Vector Time (GMT): 2014/369/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -694606.45                 A    =         6779479.37  meter
     Y    =        4193437.61  meter          E    =           .0012693
     Z    =       -5291415.96                 I    =           51.61557
     XDOT =      -7619.241079                 Wp   =          121.69725
     YDOT =       -471.699319  meter/sec      RA   =          179.84825  deg
     ZDOT =        620.940779                 TA   =          154.27093
                                              MA   =          154.20774
                                              Ha   =            222.168  n.mi
                                              Hp   =            216.834
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2278892.55                 X    =         -715743.25
     Y    =       13757997.40  feet           Y    =         4185552.38  meter
     Z    =      -17360288.59                 Z    =        -5294841.16
     XDOT =     -24997.510103                 XDOT =       -7616.416430
     YDOT =      -1547.569943  feet/sec       YDOT =        -556.886883  meter/sec
     ZDOT =       2037.207281                 ZDOT =         583.935000
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13892654.99                 X    =        -4234481.24
     Y    =         968089.97  feet           Y    =          295073.82  meter
     Z    =      -17375626.69                 Z    =        -5296091.02
     XDOT =      -4024.580019                 XDOT =       -1226.691990
     YDOT =     -23707.750162  feet/sec       YDOT =       -7226.122250  meter/sec
     ZDOT =       1879.195329                 ZDOT =         572.778736
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14369.51512223  .00016717  00000-0  10270-3 0  9180
    2 25544  51.6404 180.8973 0006637 214.9970 145.0752 15.53437080 42570
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14369.51512223   =   yrday.fracday
    Element set:     918
    Inclination:       51.6404  deg
    RA of node:       180.8973  deg
    Eccentricity:     .0006637     
    Arg of perigee:   214.9970  deg
    Mean anomaly:     145.0752  deg
    Mean motion:   15.53437080  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4257
    Checksum:              314
 
 
    Coasting Arc #20 (Orbit 4272)
    ---------------------------------------
 
    Vector Time (GMT): 2014/370/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2187869.97                 A    =         6780895.60  meter
     Y    =       -4110798.52  meter          E    =           .0002105
     Z    =        4927330.42                 I    =           51.65202
     XDOT =       7237.774011                 Wp   =          143.50130
     YDOT =       1143.987394  meter/sec      RA   =          174.85591  deg
     ZDOT =      -2260.516826                 TA   =          328.57094
                                              MA   =          328.58352
                                              Ha   =            221.942  n.mi
                                              Hp   =            216.998
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7178051.08                 X    =         2209740.36
     Y    =      -13486871.78  feet           Y    =        -4086210.47  meter
     Z    =       16165782.21                 Z    =         4938011.35
     XDOT =      23745.977725                 XDOT =        7235.424396
     YDOT =       3753.239481  feet/sec       YDOT =        1224.911935  meter/sec
     ZDOT =      -7416.393785                 ZDOT =       -2225.363042
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14792275.76                 X    =         4508685.65
     Y    =        3620599.62  feet           Y    =         1103558.76  meter
     Z    =       16212109.01                 Z    =         4941450.83
     XDOT =       2350.382662                 XDOT =         716.396635
     YDOT =      22917.328104  feet/sec       YDOT =        6985.201606  meter/sec
     ZDOT =      -7266.383608                 ZDOT =       -2214.793724
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14370.54439241  .00016717  00000-0  10270-3 0  9194
    2 25544  51.6403 175.7708 0006602 219.3778 140.6895 15.53466924 42731
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14370.54439241   =   yrday.fracday
    Element set:     919
    Inclination:       51.6403  deg
    RA of node:       175.7708  deg
    Eccentricity:     .0006602     
    Arg of perigee:   219.3778  deg
    Mean anomaly:     140.6895  deg
    Mean motion:   15.53466924  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4273
    Checksum:              329
 
 
    Coasting Arc #21 (Orbit 4287)
    ---------------------------------------
 
    Vector Time (GMT): 2014/371/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3583832.99                 A    =         6783552.41  meter
     Y    =        3984014.42  meter          E    =           .0008012
     Z    =       -4167030.14                 I    =           51.69429
     XDOT =      -6420.777815                 Wp   =          158.64778
     YDOT =      -1856.021049  meter/sec      RA   =          169.87028  deg
     ZDOT =       3742.632634                 TA   =          149.88329
                                              MA   =          149.83720
                                              Ha   =            221.664  n.mi
                                              Hp   =            216.916
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11757982.26                 X    =        -3607875.18
     Y    =       13070913.46  feet           Y    =         3943803.54  meter
     Z    =      -13671358.72                 Z    =        -4184497.62
     XDOT =     -21065.544014                 XDOT =       -6417.726249
     YDOT =      -6089.307903  feet/sec       YDOT =       -1927.805557  meter/sec
     ZDOT =      12278.978458                 ZDOT =        3711.449373
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15633703.80                 X    =        -4765152.92
     Y    =       -7913363.95  feet           Y    =        -2411993.33  meter
     Z    =      -13746670.55                 Z    =        -4189985.18
     XDOT =       -136.874540                 XDOT =         -41.719360
     YDOT =     -20857.477973  feet/sec       YDOT =       -6357.359286  meter/sec
     ZDOT =      12146.032948                 ZDOT =        3702.110843
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14371.50929403  .00016717  00000-0  10270-3 0  9207
    2 25544  51.6414 170.9642 0006514 222.6541 137.4107 15.53560932 42884
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14371.50929403   =   yrday.fracday
    Element set:     920
    Inclination:       51.6414  deg
    RA of node:       170.9642  deg
    Eccentricity:     .0006514     
    Arg of perigee:   222.6541  deg
    Mean anomaly:     137.4107  deg
    Mean motion:   15.53560932  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4288
    Checksum:              295
 
 
    Coasting Arc #22 (Orbit 4303)
    ---------------------------------------
 
    Vector Time (GMT): 2014/372/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4747414.06                 A    =         6786848.34  meter
     Y    =       -3766312.46  meter          E    =           .0009973
     Z    =        3041685.46                 I    =           51.73621
     XDOT =       5248.984758                 Wp   =          125.34578
     YDOT =       2620.537433  meter/sec      RA   =          164.89495  deg
     ZDOT =      -4941.923534                 TA   =           19.81080
                                              MA   =           19.77209
                                              Ha   =            221.343  n.mi
                                              Hp   =            217.114
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15575505.46                 X    =         4774401.83
     Y    =      -12356668.18  feet           Y    =        -3713073.06  meter
     Z    =        9979283.00                 Z    =         3064812.54
     XDOT =      17221.078601                 XDOT =        5243.296890
     YDOT =       8597.563756  feet/sec       YDOT =        2679.203450  meter/sec
     ZDOT =     -16213.659890                 ZDOT =       -4916.438980
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16133366.01                 X    =         4917449.96
     Y    =       11532688.12  feet           Y    =         3515163.34  meter
     Z    =       10078755.58                 Z    =         3072004.70
     XDOT =      -2679.251619                 XDOT =        -816.635893
     YDOT =      17839.256106  feet/sec       YDOT =        5437.405261  meter/sec
     ZDOT =     -16105.179663                 ZDOT =       -4908.858761
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14372.53848160  .00016717  00000-0  10270-3 0  9212
    2 25544  51.6411 165.8374 0006500 227.5263 132.5341 15.53605502 43044
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14372.53848160   =   yrday.fracday
    Element set:     921
    Inclination:       51.6411  deg
    RA of node:       165.8374  deg
    Eccentricity:     .0006500     
    Arg of perigee:   227.5263  deg
    Mean anomaly:     132.5341  deg
    Mean motion:   15.53605502  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4304
    Checksum:              280
 
 
    Coasting Arc #23 (Orbit 4318)
    ---------------------------------------
 
    Vector Time (GMT): 2014/373/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5616831.93                 A    =         6789406.91  meter
     Y    =        3435888.86  meter          E    =           .0002081
     Z    =       -1650217.02                 I    =           51.77734
     XDOT =      -3774.602839                 Wp   =          354.84862
     YDOT =      -3421.453954  meter/sec      RA   =          159.92934  deg
     ZDOT =       5725.298678                 TA   =          347.12535
                                              MA   =          347.13066
                                              Ha   =            221.108  n.mi
                                              Hp   =            217.104
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18427926.29                 X    =        -5646819.36
     Y    =       11272601.26  feet           Y    =         3372910.19  meter
     Z    =       -5414097.84                 Z    =        -1677574.87
     XDOT =     -12383.867581                 XDOT =       -3763.873812
     YDOT =     -11225.242631  feet/sec       YDOT =       -3463.604233  meter/sec
     ZDOT =      18783.788315                 ZDOT =        5706.988554
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16129497.67                 X    =        -4916270.89
     Y    =      -14325259.24  feet           Y    =        -4366339.02  meter
     Z    =       -5531610.47                 Z    =        -1686034.87
     XDOT =       6062.658311                 XDOT =        1847.898253
     YDOT =     -14047.669669  feet/sec       YDOT =       -4281.729715  meter/sec
     ZDOT =      18706.094750                 ZDOT =        5701.617680
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14373.50330574  .00016717  00000-0  10270-3 0  9226
    2 25544  51.6428 161.0310 0006371 231.0451 129.0134 15.53686151 43191
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14373.50330574   =   yrday.fracday
    Element set:     922
    Inclination:       51.6428  deg
    RA of node:       161.0310  deg
    Eccentricity:     .0006371     
    Arg of perigee:   231.0451  deg
    Mean anomaly:     129.0134  deg
    Mean motion:   15.53686151  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4319
    Checksum:              271
 
 
    Coasting Arc #24 (Orbit 4334)
    ---------------------------------------
 
    Vector Time (GMT): 2014/374/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6117175.15                 A    =         6790377.04  meter
     Y    =       -2927804.93  meter          E    =           .0012478
     Z    =          82356.41                 I    =           51.81001
     XDOT =       2116.056673                 Wp   =          163.13021
     YDOT =       4245.490534  meter/sec      RA   =          154.97062  deg
     ZDOT =      -6028.261474                 TA   =           15.98455
                                              MA   =           15.94521
                                              Ha   =            220.739  n.mi
                                              Hp   =            217.171
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20069472.27                 X    =         6149059.86
     Y    =       -9605659.22  feet           Y    =        -2859220.43  meter
     Z    =         270198.21                 Z    =          112149.51
     XDOT =       6942.443154                 XDOT =        2097.708040
     YDOT =      13928.774717  feet/sec       YDOT =        4269.051196  meter/sec
     ZDOT =     -19777.760741                 ZDOT =       -6018.026668
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15301317.40                 X    =         4663841.54
     Y    =       16150438.27  feet           Y    =         4922653.58  meter
     Z    =         398049.12                 Z    =          121325.37
     XDOT =      -9907.781887                 XDOT =       -3019.891919
     YDOT =       9885.161695  feet/sec       YDOT =        3012.997285  meter/sec
     ZDOT =     -19734.717440                 ZDOT =       -6015.141876
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14374.53240864  .00016717  00000-0  10270-3 0  9233
    2 25544  51.6423 155.9038 0006293 236.8660 123.1889 15.53766998 43351
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14374.53240864   =   yrday.fracday
    Element set:     923
    Inclination:       51.6423  deg
    RA of node:       155.9038  deg
    Eccentricity:     .0006293     
    Arg of perigee:   236.8660  deg
    Mean anomaly:     123.1889  deg
    Mean motion:   15.53766998  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4335
    Checksum:              338
 
 
    Coasting Arc #25 (Orbit 4350)
    ---------------------------------------
 
    Vector Time (GMT): 2014/375/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6229612.16                 A    =         6789268.39  meter
     Y    =        2232958.91  meter          E    =           .0007594
     Z    =        1500718.07                 I    =           51.83661
     XDOT =       -400.273104                 Wp   =           63.25024
     YDOT =      -5016.431788  meter/sec      RA   =          150.01417  deg
     ZDOT =       5783.300819                 TA   =          313.08642
                                              MA   =          313.14995
                                              Ha   =            220.482  n.mi
                                              Hp   =            217.212
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20438360.11                 X    =        -6261408.49
     Y    =        7325980.67  feet           Y    =         2163117.53  meter
     Z    =        4923615.70                 Z    =         1470378.90
     XDOT =      -1313.231967                 XDOT =        -372.241289
     YDOT =     -16458.109541  feet/sec       YDOT =       -5020.751239  meter/sec
     ZDOT =      18974.084053                 ZDOT =        5781.424411
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13549895.34                 X    =        -4130008.10
     Y    =      -17001791.85  feet           Y    =        -5182146.16  meter
     Z    =        4793533.01                 Z    =         1461068.86
     XDOT =      13869.734898                 XDOT =        4227.495197
     YDOT =      -5687.906467  feet/sec       YDOT =       -1733.673891  meter/sec
     ZDOT =      18966.901404                 ZDOT =        5781.111548
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14375.56146790  .00016717  00000-0  10270-3 0  9241
    2 25544  51.6438 150.7766 0006276 239.6847 120.3685 15.53838470 43513
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14375.56146790   =   yrday.fracday
    Element set:     924
    Inclination:       51.6438  deg
    RA of node:       150.7766  deg
    Eccentricity:     .0006276     
    Arg of perigee:   239.6847  deg
    Mean anomaly:     120.3685  deg
    Mean motion:   15.53838470  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4351
    Checksum:              338
 
 
    Coasting Arc #26 (Orbit 4365)
    ---------------------------------------
 
    Vector Time (GMT): 2014/376/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5952348.37                 A    =         6786380.68  meter
     Y    =       -1303546.59  meter          E    =           .0004639
     Z    =       -2980635.83                 I    =           51.85394
     XDOT =      -1260.893348                 Wp   =          198.09250
     YDOT =       5673.163720  meter/sec      RA   =          145.05435  deg
     ZDOT =      -5001.317433                 TA   =           15.87530
                                              MA   =           15.86077
                                              Ha   =            220.272  n.mi
                                              Hp   =            217.297
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19528701.99                 X    =         5980961.26
     Y    =       -4276727.64  feet           Y    =        -1236823.55  meter
     Z    =       -9778988.95                 Z    =        -2951651.19
     XDOT =      -4136.789198                 XDOT =       -1299.943919
     YDOT =      18612.741865  feet/sec       YDOT =        5658.845283  meter/sec
     ZDOT =     -16408.521763                 ZDOT =       -5007.537376
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10674220.77                 X    =         3253502.49
     Y    =       16974518.78  feet           Y    =         5173833.33  meter
     Z    =       -9654840.70                 Z    =        -2942795.44
     XDOT =     -17637.236551                 XDOT =       -5375.829701
     YDOT =       1746.566626  feet/sec       YDOT =         532.353508  meter/sec
     ZDOT =     -16436.069289                 ZDOT =       -5009.713919
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14376.52617171  .00016717  00000-0  10270-3 0  9255
    2 25544  51.6436 145.9697 0006179 245.0866 114.9645 15.53879321 43665
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14376.52617171   =   yrday.fracday
    Element set:     925
    Inclination:       51.6436  deg
    RA of node:       145.9697  deg
    Eccentricity:     .0006179     
    Arg of perigee:   245.0866  deg
    Mean anomaly:     114.9645  deg
    Mean motion:   15.53879321  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4366
    Checksum:              344
 
 
    Coasting Arc #27 (Orbit 4381)
    ---------------------------------------
 
    Vector Time (GMT): 2014/377/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5334558.14                 A    =         6782473.54  meter
     Y    =         180011.42  meter          E    =           .0006358
     Z    =        4184312.05                 I    =           51.86794
     XDOT =       2731.825094                 Wp   =          138.20153
     YDOT =      -6110.634079  meter/sec      RA   =          140.08706  deg
     ZDOT =       3737.787063                 TA   =          273.45818
                                              MA   =          273.53090
                                              Ha   =            219.822  n.mi
                                              Hp   =            217.167
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17501831.16                 X    =        -5356500.32
     Y    =         590588.65  feet           Y    =          120234.21  meter
     Z    =       13728057.91                 Z    =         4158344.62
     XDOT =       8962.680754                 XDOT =        2781.795909
     YDOT =     -20048.012071  feet/sec       YDOT =       -6079.805657  meter/sec
     ZDOT =      12263.080916                 ZDOT =        3751.179017
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6807891.53                 X    =        -2075045.34
     Y    =      -16228144.71  feet           Y    =        -4946338.51  meter
     Z    =       13616989.20                 Z    =         4150458.31
     XDOT =      20712.708241                 XDOT =        6313.233472
     YDOT =       1671.501521  feet/sec       YDOT =         509.473663  meter/sec
     ZDOT =      12321.377981                 ZDOT =        3755.556009
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14377.55514392  .00016717  00000-0  10270-3 0  9261
    2 25544  51.6444 140.8418 0006182 249.6911 110.3577 15.53975390 43829
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14377.55514392   =   yrday.fracday
    Element set:     926
    Inclination:       51.6444  deg
    RA of node:       140.8418  deg
    Eccentricity:     .0006182     
    Arg of perigee:   249.6911  deg
    Mean anomaly:     110.3577  deg
    Mean motion:   15.53975390  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4382
    Checksum:              324
 
 
    Coasting Arc #28 (Orbit 4396)
    ---------------------------------------
 
    Vector Time (GMT): 2014/378/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4436335.92                 A    =         6779176.74  meter
     Y    =        1125913.55  meter          E    =           .0006477
     Z    =       -5006780.30                 I    =           51.88086
     XDOT =      -3937.405446                 Wp   =           74.27982
     YDOT =       6233.876075  meter/sec      RA   =          135.11206  deg
     ZDOT =      -2087.471647                 TA   =          175.46472
                                              MA   =          175.45885
                                              Ha   =            219.521  n.mi
                                              Hp   =            217.275
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14554907.89                 X    =         4447736.99
     Y    =        3693942.08  feet           Y    =         1175587.34  meter
     Z    =      -16426444.56                 Z    =        -4985201.79
     XDOT =     -12917.996871                 XDOT =       -3996.681341
     YDOT =      20452.349327  feet/sec       YDOT =        6189.514041  meter/sec
     ZDOT =      -6848.660259                 ZDOT =       -2106.742661
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2019771.57                 X    =          615626.37
     Y    =       14980918.96  feet           Y    =         4566184.10  meter
     Z    =      -16334357.13                 Z    =        -4978712.05
     XDOT =     -22679.132539                 XDOT =       -6912.599598
     YDOT =      -4498.828192  feet/sec       YDOT =       -1371.242833  meter/sec
     ZDOT =      -6932.132322                 ZDOT =       -2112.913932
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14378.51976656  .00016717  00000-0  10270-3 0  9274
    2 25544  51.6444 136.0349 0006083 255.0506 104.9974 15.54008786 43973
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14378.51976656   =   yrday.fracday
    Element set:     927
    Inclination:       51.6444  deg
    RA of node:       136.0349  deg
    Eccentricity:     .0006083     
    Arg of perigee:   255.0506  deg
    Mean anomaly:     104.9974  deg
    Mean motion:   15.54008786  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4397
    Checksum:              341
 
 
    Coasting Arc #29 (Orbit 4412)
    ---------------------------------------
 
    Vector Time (GMT): 2014/379/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3352393.83                 A    =         6777431.56  meter
     Y    =       -2509948.14  meter          E    =           .0003814
     Z    =        5331770.95                 I    =           51.89824
     XDOT =       4809.599452                 Wp   =          246.39722
     YDOT =      -5965.995814  meter/sec      RA   =          130.13058  deg
     ZDOT =        214.196186                 TA   =          201.55998
                                              MA   =          201.57604
                                              Ha   =            219.181  n.mi
                                              Hp   =            216.938
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10998667.41                 X    =        -3349977.56
     Y    =       -8234737.98  feet           Y    =        -2547423.39  meter
     Z    =       17492686.84                 Z    =         5315491.50
     XDOT =      15779.525762                 XDOT =        4874.914673
     YDOT =     -19573.477080  feet/sec       YDOT =       -5911.846553  meter/sec
     ZDOT =        702.743393                 ZDOT =         237.718777
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3284258.63                 X    =         1001042.03
     Y    =      -13431723.81  feet           Y    =        -4093989.42  meter
     Z    =       17423493.57                 Z    =         5310680.84
     XDOT =      23177.824863                 XDOT =        7064.601018
     YDOT =       6716.586035  feet/sec       YDOT =        2047.215423  meter/sec
     ZDOT =        804.369496                 ZDOT =         245.171822
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14379.54865217  .00016717  00000-0  10270-3 0  9289
    2 25544  51.6450 130.9060 0006024 260.1360  99.9113 15.54106841 44131
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14379.54865217   =   yrday.fracday
    Element set:     928
    Inclination:       51.6450  deg
    RA of node:       130.9060  deg
    Eccentricity:     .0006024     
    Arg of perigee:   260.1360  deg
    Mean anomaly:      99.9113  deg
    Mean motion:   15.54106841  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4413
    Checksum:              294
 
 
    Coasting Arc #30 (Orbit 4427)
    ---------------------------------------
 
    Vector Time (GMT): 2014/380/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952853.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2174068.17                 A    =         6778152.62  meter
     Y    =        3881506.23  meter          E    =           .0008083
     Z    =       -5120933.75                 I    =           51.92106
     XDOT =      -5325.151453                 Wp   =          115.98964
     YDOT =       5238.112948  meter/sec      RA   =          125.15025  deg
     ZDOT =       1708.197115                 TA   =          170.46985
                                              MA   =          170.45450
                                              Ha   =            218.855  n.mi
                                              Hp   =            216.818
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7132769.58                 X    =         2155378.22
     Y    =       12734600.50  feet           Y    =         3905713.76  meter
     Z    =      -16800963.76                 Z    =        -5110417.82
     XDOT =     -17470.969334                 XDOT =       -5391.627254
     YDOT =      17185.409934  feet/sec       YDOT =        5178.191893  meter/sec
     ZDOT =       5604.321244                 ZDOT =        1682.167325
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8731419.33                 X    =        -2661336.61
     Y    =       11759913.92  feet           Y    =         3584421.76  meter
     Z    =      -16756657.67                 Z    =        -5107429.26
     XDOT =     -21929.499633                 XDOT =       -6684.111488
     YDOT =      -8450.049625  feet/sec       YDOT =       -2575.575126  meter/sec
     ZDOT =       5492.077792                 ZDOT =        1673.985311
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14380.51319303  .00016717  00000-0  10270-3 0  9299
    2 25544  51.6451 126.0987 0005845 264.4045  95.6441 15.54172233 44284
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14380.51319303   =   yrday.fracday
    Element set:     929
    Inclination:       51.6451  deg
    RA of node:       126.0987  deg
    Eccentricity:     .0005845     
    Arg of perigee:   264.4045  deg
    Mean anomaly:      95.6441  deg
    Mean motion:   15.54172233  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4428
    Checksum:              307
 
             

Curator: Kim Dismukes | Responsible NASA Official: Amiko Kauderer | Updated: 06/08/2009
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