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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  19375.04
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.423
   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 
   ------------------------------------------------------------------------
   263/11:28:05.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.4  
   000/00:00:00.000           0.0               0.0              219.9  
   
 
 
    Coasting Arc #1 (Orbit 2533)
    ---------------------------------------
 
    Vector Time (GMT): 2014/258/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4075211.09                 A    =         6794314.86  meter
     Y    =       -3888849.00  meter          E    =           .0007808
     Z    =       -3806384.17                 I    =           51.72174
     XDOT =       6007.899973                 Wp   =           84.08893
     YDOT =      -2177.632861  meter/sec      RA   =           11.43457  deg
     ZDOT =      -4214.060961                 TA   =          141.40893
                                              MA   =          141.35310
                                              Ha   =            227.694  n.mi
                                              Hp   =            219.970
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13370115.11                 X    =        -4012931.98
     Y    =      -12758690.95  feet           Y    =        -3934072.71  meter
     Z    =      -12488137.05                 Z    =        -3826029.44
     XDOT =      19710.957918                 XDOT =        6052.274834
     YDOT =      -7144.464767  feet/sec       YDOT =       -2110.200845  meter/sec
     ZDOT =     -13825.659321                 ZDOT =       -4184.767435
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11772080.74                 X    =         3588130.21
     Y    =       14173414.10  feet           Y    =         4320056.62  meter
     Z    =      -12571005.83                 Z    =        -3831642.58
     XDOT =     -19442.052595                 XDOT =       -5925.937631
     YDOT =       4015.663471  feet/sec       YDOT =        1223.974226  meter/sec
     ZDOT =     -13700.631762                 ZDOT =       -4175.952561
  
  
    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   14258.52404156  .00016717  00000-0  10270-3 0  9004
    2 25544  51.6469  11.8400 0001959 112.9946 247.1411 15.50292224 25349
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14258.52404156   =   yrday.fracday
    Element set:     900
    Inclination:       51.6469  deg
    RA of node:        11.8400  deg
    Eccentricity:     .0001959     
    Arg of perigee:   112.9946  deg
    Mean anomaly:     247.1411  deg
    Mean motion:   15.50292224  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2534
    Checksum:              287
 
 
    Coasting Arc #2 (Orbit 2549)
    ---------------------------------------
 
    Vector Time (GMT): 2014/259/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3957040.96                 A    =         6793153.69  meter
     Y    =        3701279.93  meter          E    =           .0012430
     Z    =        4089303.90                 I    =           51.68820
     XDOT =      -6195.902364                 Wp   =          104.53153
     YDOT =       2356.936828  meter/sec      RA   =            6.48199  deg
     ZDOT =       3849.363299                 TA   =          305.62039
                                              MA   =          305.73611
                                              Ha   =            227.534  n.mi
                                              Hp   =            219.918
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12982417.86                 X    =         3895493.79
     Y    =       12143306.85  feet           Y    =         3745186.30  meter
     Z    =       13416351.36                 Z    =         4108376.85
     XDOT =     -20327.763663                 XDOT =       -6240.496637
     YDOT =       7732.732375  feet/sec       YDOT =        2287.401196  meter/sec
     ZDOT =      12629.144683                 ZDOT =        3819.156010
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11681056.93                 X    =        -3560386.15
     Y    =      -13318799.87  feet           Y    =        -4059570.20  meter
     Z    =       13496815.84                 Z    =         4113829.47
     XDOT =      20080.063010                 XDOT =        6120.403205
     YDOT =      -4901.186638  feet/sec       YDOT =       -1493.881687  meter/sec
     ZDOT =      12500.200014                 ZDOT =        3810.060964
  
  
    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   14259.55540441  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6474   6.7281 0001962 114.0110 246.1246 15.50361194 25501
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14259.55540441   =   yrday.fracday
    Element set:     901
    Inclination:       51.6474  deg
    RA of node:         6.7281  deg
    Eccentricity:     .0001962     
    Arg of perigee:   114.0110  deg
    Mean anomaly:     246.1246  deg
    Mean motion:   15.50361194  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2550
    Checksum:              272
 
 
    Coasting Arc #3 (Orbit 2564)
    ---------------------------------------
 
    Vector Time (GMT): 2014/260/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3782469.92                 A    =         6792175.54  meter
     Y    =       -3567365.88  meter          E    =           .0010349
     Z    =       -4380576.17                 I    =           51.65371
     XDOT =       6355.837478                 Wp   =           76.56845
     YDOT =      -2540.118463  meter/sec      RA   =            1.52675  deg
     ZDOT =      -3423.941333                 TA   =          158.67205
                                              MA   =          158.62889
                                              Ha   =            227.579  n.mi
                                              Hp   =            219.903
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12409678.22                 X    =        -3721018.32
     Y    =      -11703956.29  feet           Y    =        -3609320.67  meter
     Z    =      -14371969.07                 Z    =        -4398801.26
     XDOT =      20852.485163                 XDOT =        6400.401644
     YDOT =      -8333.721991  feet/sec       YDOT =       -2468.794491  meter/sec
     ZDOT =     -11233.403324                 ZDOT =       -3392.957215
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11365803.22                 X    =         3464296.82
     Y    =       12632715.29  feet           Y    =         3850451.62  meter
     Z    =      -14448848.50                 Z    =        -4404009.02
     XDOT =     -20589.352176                 XDOT =       -6275.634543
     YDOT =       5844.117124  feet/sec       YDOT =        1781.286899  meter/sec
     ZDOT =     -11101.124740                 ZDOT =       -3383.622821
  
  
    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   14260.52229171  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6474   1.9361 0001887 115.7289 244.4057 15.50346519 25659
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14260.52229171   =   yrday.fracday
    Element set:     902
    Inclination:       51.6474  deg
    RA of node:         1.9361  deg
    Eccentricity:     .0001887     
    Arg of perigee:   115.7289  deg
    Mean anomaly:     244.4057  deg
    Mean motion:   15.50346519  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2565
    Checksum:              304
 
 
    Coasting Arc #4 (Orbit 2580)
    ---------------------------------------
 
    Vector Time (GMT): 2014/261/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3591967.63                 A    =         6791058.87  meter
     Y    =        3445608.02  meter          E    =           .0010202
     Z    =        4614042.76                 I    =           51.61970
     XDOT =      -6497.631853                 Wp   =          114.67324
     YDOT =       2760.268384  meter/sec      RA   =          356.56790  deg
     ZDOT =       2987.678567                 TA   =          305.46572
                                              MA   =          305.56089
                                              Ha   =            227.409  n.mi
                                              Hp   =            219.866
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11784670.69                 X    =         3530757.64
     Y    =       11304488.27  feet           Y    =         3485433.92  meter
     Z    =       15137935.58                 Z    =         4631342.95
     XDOT =     -21317.689807                 XDOT =       -6542.528010
     YDOT =       9055.998634  feet/sec       YDOT =        2687.356914  meter/sec
     ZDOT =       9802.095037                 ZDOT =        2956.004826
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10977152.90                 X    =        -3345836.20
     Y    =      -11998233.95  feet           Y    =        -3657061.71  meter
     Z    =       15210900.96                 Z    =         4636282.61
     XDOT =      21017.067177                 XDOT =        6406.002075
     YDOT =      -6934.440734  feet/sec       YDOT =       -2113.617536  meter/sec
     ZDOT =       9666.848615                 ZDOT =        2946.455458
  
  
    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   14261.55361679  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6477 356.8238 0001906 115.9913 244.1434 15.50415499 25813
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14261.55361679   =   yrday.fracday
    Element set:     903
    Inclination:       51.6477  deg
    RA of node:       356.8238  deg
    Eccentricity:     .0001906     
    Arg of perigee:   115.9913  deg
    Mean anomaly:     244.1434  deg
    Mean motion:   15.50415499  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2581
    Checksum:              323
 
 
    Coasting Arc #5 (Orbit 2595)
    ---------------------------------------
 
    Vector Time (GMT): 2014/262/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 912103.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3359926.43                 A    =         6790225.30  meter
     Y    =       -3387087.48  meter          E    =           .0013066
     Z    =       -4843915.54                 I    =           51.58544
     XDOT =       6593.404371                 Wp   =           77.62655
     YDOT =      -2974.182748  meter/sec      RA   =          351.60679  deg
     ZDOT =      -2496.728700                 TA   =          167.78002
                                              MA   =          167.74829
                                              Ha   =            227.469  n.mi
                                              Hp   =            219.838
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11023380.67                 X    =        -3298271.45
     Y    =      -11112491.75  feet           Y    =        -3424316.14  meter
     Z    =      -15892111.36                 Z    =        -4860087.39
     XDOT =      21631.904103                 XDOT =        6638.300579
     YDOT =      -9757.817414  feet/sec       YDOT =       -2900.200272  meter/sec
     ZDOT =      -8191.367125                 ZDOT =       -2464.589665
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10425042.21                 X    =         3177552.86
     Y    =       11582286.23  feet           Y    =         3530280.84  meter
     Z    =      -15960286.28                 Z    =        -4864695.26
     XDOT =     -21245.658567                 XDOT =       -6475.676731
     YDOT =       8037.795556  feet/sec       YDOT =        2449.920085  meter/sec
     ZDOT =      -8054.110465                 ZDOT =       -2454.892870
  
  
    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   14262.52046843  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6475 352.0319 0001818 117.6760 242.4575 15.50400458 25962
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14262.52046843   =   yrday.fracday
    Element set:     904
    Inclination:       51.6475  deg
    RA of node:       352.0319  deg
    Eccentricity:     .0001818     
    Arg of perigee:   117.6760  deg
    Mean anomaly:     242.4575  deg
    Mean motion:   15.50400458  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2596
    Checksum:              304
 
 
    Coasting Arc #6 (Orbit 2610)
    ---------------------------------------
 
    Vector Time (GMT): 2014/263/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3181700.87                 A    =         6792410.08  meter
     Y    =       -4230684.62  meter          E    =           .0009981
     Z    =       -4266565.69                 I    =           51.56328
     XDOT =       6620.605078                 Wp   =          110.96947
     YDOT =       1363.031805  meter/sec      RA   =          346.71168  deg
     ZDOT =       3588.922559                 TA   =          195.79076
                                              MA   =          195.82191
                                              Ha   =            227.415  n.mi
                                              Hp   =            219.870
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10438651.15                 X    =         3249498.41
     Y    =      -13880198.89  feet           Y    =        -4194726.22  meter
     Z    =      -13997918.92                 Z    =        -4250944.32
     XDOT =      21721.145270                 XDOT =        6587.437523
     YDOT =       4471.889125  feet/sec       YDOT =        1436.882678  meter/sec
     ZDOT =      11774.680312                 ZDOT =        3621.003658
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12679483.78                 X    =        -3864706.66
     Y    =       11947103.44  feet           Y    =         3641477.13  meter
     Z    =      -13930703.63                 Z    =        -4246078.47
     XDOT =     -19736.129644                 XDOT =       -6015.572315
     YDOT =      -7070.256330  feet/sec       YDOT =       -2155.014129  meter/sec
     ZDOT =      11910.893317                 ZDOT =        3630.440283
  
  
    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   14263.48730189  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6477 347.2391 0001899 117.4348 242.6996 15.50462957 26118
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14263.48730189   =   yrday.fracday
    Element set:     905
    Inclination:       51.6477  deg
    RA of node:       347.2391  deg
    Eccentricity:     .0001899     
    Arg of perigee:   117.4348  deg
    Mean anomaly:     242.6996  deg
    Mean motion:   15.50462957  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2611
    Checksum:              340
 
 
    Coasting Arc #7 (Orbit 2626)
    ---------------------------------------
 
    Vector Time (GMT): 2014/264/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3355119.79                 A    =         6793492.42  meter
     Y    =        4397374.29  meter          E    =           .0012742
     Z    =        3934163.59                 I    =           51.53677
     XDOT =      -6397.262279                 Wp   =           85.18685
     YDOT =      -1262.760360  meter/sec      RA   =          341.74716  deg
     ZDOT =      -4031.924474                 TA   =           47.06153
                                              MA   =           46.95470
                                              Ha   =            227.451  n.mi
                                              Hp   =            219.791
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11007610.85                 X    =        -3423153.74
     Y    =       14427081.00  feet           Y    =         4359475.29  meter
     Z    =       12907360.85                 Z    =         3917699.09
     XDOT =     -20988.393303                 XDOT =       -6363.080595
     YDOT =      -4142.914567  feet/sec       YDOT =       -1334.108106  meter/sec
     ZDOT =     -13228.098668                 ZDOT =       -4062.918195
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13109177.85                 X    =         3995677.41
     Y    =      -12620653.37  feet           Y    =        -3846775.15  meter
     Z    =       12836537.35                 Z    =         3912576.59
     XDOT =      19136.682243                 XDOT =        5832.860748
     YDOT =       6247.842688  feet/sec       YDOT =        1904.342451  meter/sec
     ZDOT =     -13359.697430                 ZDOT =       -4072.035777
  
  
    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   14264.51857252  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6476 342.1268 0001899 115.8653 244.2693 15.50478263 26271
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14264.51857252   =   yrday.fracday
    Element set:     906
    Inclination:       51.6476  deg
    RA of node:       342.1268  deg
    Eccentricity:     .0001899     
    Arg of perigee:   115.8653  deg
    Mean anomaly:     244.2693  deg
    Mean motion:   15.50478263  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2627
    Checksum:              330
 
 
    Coasting Arc #8 (Orbit 2641)
    ---------------------------------------
 
    Vector Time (GMT): 2014/265/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3484288.17                 A    =         6794498.70  meter
     Y    =       -4602008.43  meter          E    =           .0006953
     Z    =       -3591452.77                 I    =           51.51074
     XDOT =       6132.458699                 Wp   =          101.75346
     YDOT =       1195.988846  meter/sec      RA   =          336.78184  deg
     ZDOT =       4422.856013                 TA   =          215.79781
                                              MA   =          215.84444
                                              Ha   =            227.312  n.mi
                                              Hp   =            219.823
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11431391.65                 X    =         3552936.06
     Y    =      -15098452.86  feet           Y    =        -4562661.55  meter
     Z    =      -11782981.51                 Z    =        -3574359.18
     XDOT =      20119.615153                 XDOT =        6097.144276
     YDOT =       3923.847921  feet/sec       YDOT =        1264.369155  meter/sec
     ZDOT =      14510.682458                 ZDOT =        4452.560684
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13391511.10                 X    =        -4081732.58
     Y    =       13454915.51  feet           Y    =         4101058.25  meter
     Z    =      -11709454.56                 Z    =        -3569041.75
     XDOT =     -18356.371657                 XDOT =       -5595.022081
     YDOT =      -5548.790837  feet/sec       YDOT =       -1691.271447  meter/sec
     ZDOT =      14636.802893                 ZDOT =        4461.297522
  
  
    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   14265.48537084  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6473 337.3344 0001824 119.6787 240.4545 15.50509020 26424
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14265.48537084   =   yrday.fracday
    Element set:     907
    Inclination:       51.6473  deg
    RA of node:       337.3344  deg
    Eccentricity:     .0001824     
    Arg of perigee:   119.6787  deg
    Mean anomaly:     240.4545  deg
    Mean motion:   15.50509020  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2642
    Checksum:              309
 
 
    Coasting Arc #9 (Orbit 2657)
    ---------------------------------------
 
    Vector Time (GMT): 2014/266/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3602295.09                 A    =         6795572.65  meter
     Y    =        4798144.33  meter          E    =           .0014557
     Z    =        3176232.57                 I    =           51.48612
     XDOT =      -5852.150908                 Wp   =           96.79375
     YDOT =      -1201.836138  meter/sec      RA   =          331.81466  deg
     ZDOT =      -4804.340754                 TA   =           46.48335
                                              MA   =           46.36247
                                              Ha   =            227.287  n.mi
                                              Hp   =            219.733
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11818553.44                 X    =        -3671110.49
     Y    =       15741943.33  feet           Y    =         4757476.84  meter
     Z    =       10420710.53                 Z    =         3158565.19
     XDOT =     -19199.970169                 XDOT =       -5814.938721
     YDOT =      -3943.031950  feet/sec       YDOT =       -1267.071342  meter/sec
     ZDOT =     -15762.272816                 ZDOT =       -4832.679207
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13607813.90                 X    =         4147661.68
     Y    =      -14279090.03  feet           Y    =        -4352266.64  meter
     Z    =       10344717.60                 Z    =         3153069.92
     XDOT =      17482.031823                 XDOT =        5328.523300
     YDOT =       5112.418748  feet/sec       YDOT =        1558.265234  meter/sec
     ZDOT =     -15882.573973                 ZDOT =       -4841.008547
  
  
    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   14266.51660423  .00016717  00000-0  10270-3 0  9081
    2 25544  51.6471 332.2217 0001797 117.3655 242.7678 15.50543619 26584
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14266.51660423   =   yrday.fracday
    Element set:     908
    Inclination:       51.6471  deg
    RA of node:       332.2217  deg
    Eccentricity:     .0001797     
    Arg of perigee:   117.3655  deg
    Mean anomaly:     242.7678  deg
    Mean motion:   15.50543619  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2658
    Checksum:              319
 
 
    Coasting Arc #10 (Orbit 2672)
    ---------------------------------------
 
    Vector Time (GMT): 2014/267/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3664186.33                 A    =         6796593.76  meter
     Y    =       -5017395.76  meter          E    =           .0005829
     Z    =       -2757871.49                 I    =           51.46172
     XDOT =       5553.365883                 Wp   =           72.41677
     YDOT =       1245.897142  meter/sec      RA   =          326.84649  deg
     ZDOT =       5122.389908                 TA   =          256.33867
                                              MA   =          256.40358
                                              Ha   =            227.222  n.mi
                                              Hp   =            219.770
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12021608.69                 X    =         3733416.63
     Y    =      -16461272.17  feet           Y    =        -4976033.78  meter
     Z    =       -9048134.81                 Z    =        -2739902.34
     XDOT =      18219.704342                 XDOT =        5514.138125
     YDOT =       4087.589048  feet/sec       YDOT =        1307.779922  meter/sec
     ZDOT =      16805.741169                 ZDOT =        5149.272096
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13623682.77                 X    =        -4152498.51
     Y    =       15207919.02  feet           Y    =         4635373.72  meter
     Z    =       -8970828.66                 Z    =        -2734308.57
     XDOT =     -16520.355204                 XDOT =       -5035.404266
     YDOT =      -4839.617877  feet/sec       YDOT =       -1475.115529  meter/sec
     ZDOT =      16919.834176                 ZDOT =        5157.165457
  
  
    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   14267.48336835  .00016717  00000-0  10270-3 0  9096
    2 25544  51.6462 327.4288 0001750 120.5729 239.5594 15.50549718 26739
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14267.48336835   =   yrday.fracday
    Element set:     909
    Inclination:       51.6462  deg
    RA of node:       327.4288  deg
    Eccentricity:     .0001750     
    Arg of perigee:   120.5729  deg
    Mean anomaly:     239.5594  deg
    Mean motion:   15.50549718  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2673
    Checksum:              339
 
 
    Coasting Arc #11 (Orbit 2688)
    ---------------------------------------
 
    Vector Time (GMT): 2014/268/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3713765.30                 A    =         6797462.28  meter
     Y    =        5212462.13  meter          E    =           .0015552
     Z    =        2267863.50                 I    =           51.43951
     XDOT =      -5247.971797                 Wp   =          109.03505
     YDOT =      -1371.006984  meter/sec      RA   =          321.87676  deg
     ZDOT =      -5417.238956                 TA   =           45.67918
                                              MA   =           45.55178
                                              Ha   =            227.142  n.mi
                                              Hp   =            219.656
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12184269.37                 X    =        -3782792.91
     Y    =       17101253.71  feet           Y    =         5170546.78  meter
     Z    =        7440497.06                 Z    =         2249653.93
     XDOT =     -17217.755241                 XDOT =       -5205.935345
     YDOT =      -4498.054408  feet/sec       YDOT =       -1429.458960  meter/sec
     ZDOT =     -17773.093688                 ZDOT =       -5442.630826
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13563439.63                 X    =         4134136.40
     Y    =      -16065561.31  feet           Y    =        -4896783.09  meter
     Z    =        7362142.35                 Z    =         2243980.99
     XDOT =      15517.833595                 XDOT =        4729.835680
     YDOT =       4868.258437  feet/sec       YDOT =        1483.845172  meter/sec
     ZDOT =     -17880.820789                 ZDOT =       -5450.074177
  
  
    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   14268.51456458  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6462 322.3155 0001739 117.9214 242.2113 15.50607022 26890
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14268.51456458   =   yrday.fracday
    Element set:     910
    Inclination:       51.6462  deg
    RA of node:       322.3155  deg
    Eccentricity:     .0001739     
    Arg of perigee:   117.9214  deg
    Mean anomaly:     242.2113  deg
    Mean motion:   15.50607022  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2689
    Checksum:              291
 
 
    Coasting Arc #12 (Orbit 2703)
    ---------------------------------------
 
    Vector Time (GMT): 2014/269/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3701969.32                 A    =         6798323.48  meter
     Y    =       -5413213.91  meter          E    =           .0007922
     Z    =       -1784574.70                 I    =           51.41742
     XDOT =       4949.347022                 Wp   =           50.42290
     YDOT =       1532.253967  meter/sec      RA   =          316.90585  deg
     ZDOT =       5640.933410                 TA   =          289.95007
                                              MA   =          290.03538
                                              Ha   =            227.151  n.mi
                                              Hp   =            219.693
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12145568.63                 X    =         3770895.00
     Y    =      -17759888.16  feet           Y    =        -5371430.95  meter
     Z    =       -5854903.86                 Z    =        -1766422.66
     XDOT =      16238.015163                 XDOT =        4904.442937
     YDOT =       5027.079944  feet/sec       YDOT =        1587.350464  meter/sec
     ZDOT =      18506.999378                 ZDOT =        5664.867685
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13278021.12                 X    =        -4047140.84
     Y    =       16956753.78  feet           Y    =         5168418.55  meter
     Z    =       -5776765.54                 Z    =        -1760758.14
     XDOT =     -14535.378898                 XDOT =       -4430.383488
     YDOT =      -5067.084613  feet/sec       YDOT =       -1544.447390  meter/sec
     ZDOT =      18608.495230                 ZDOT =        5671.869346
  
  
    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   14269.48129438  .00016717  00000-0  10270-3 0  9110
    2 25544  51.6454 317.5219 0001715 119.6624 240.4698 15.50589065 27048
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14269.48129438   =   yrday.fracday
    Element set:     911
    Inclination:       51.6454  deg
    RA of node:       317.5219  deg
    Eccentricity:     .0001715     
    Arg of perigee:   119.6624  deg
    Mean anomaly:     240.4698  deg
    Mean motion:   15.50589065  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2704
    Checksum:              322
 
 
    Coasting Arc #13 (Orbit 2719)
    ---------------------------------------
 
    Vector Time (GMT): 2014/270/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3681520.36                 A    =         6798808.39  meter
     Y    =        5572073.62  meter          E    =           .0015464
     Z    =        1233666.39                 I    =           51.39792
     XDOT =      -4655.489481                 Wp   =          121.06242
     YDOT =      -1776.025690  meter/sec      RA   =          311.93367  deg
     ZDOT =      -5824.735643                 TA   =           45.49688
                                              MA   =           45.37060
                                              Ha   =            227.039  n.mi
                                              Hp   =            219.558
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12078478.88                 X    =        -3749547.80
     Y    =       18281081.44  feet           Y    =         5530524.27  meter
     Z    =        4047461.90                 Z    =         1215615.90
     XDOT =     -15273.915621                 XDOT =       -4606.988409
     YDOT =      -5826.855937  feet/sec       YDOT =       -1827.815907  meter/sec
     ZDOT =     -19110.025077                 ZDOT =       -5847.233678
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12929896.42                 X    =         3941032.43
     Y    =      -17706736.96  feet           Y    =        -5397013.43  meter
     Z    =        3969733.39                 Z    =         1209974.74
     XDOT =      13578.606870                 XDOT =        4138.759374
     YDOT =       5574.852587  feet/sec       YDOT =        1699.215068  meter/sec
     ZDOT =     -19205.368114                 ZDOT =       -5853.796201
  
  
    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   14270.51245351  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6457 312.4081 0001773 118.8675 241.2654 15.50662512 27201
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14270.51245351   =   yrday.fracday
    Element set:     912
    Inclination:       51.6457  deg
    RA of node:       312.4081  deg
    Eccentricity:     .0001773     
    Arg of perigee:   118.8675  deg
    Mean anomaly:     241.2654  deg
    Mean motion:   15.50662512  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2720
    Checksum:              285
 
 
    Coasting Arc #14 (Orbit 2734)
    ---------------------------------------
 
    Vector Time (GMT): 2014/271/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3601966.05                 A    =         6799304.80  meter
     Y    =       -5719074.12  meter          E    =           .0011071
     Z    =        -701604.28                 I    =           51.37866
     XDOT =       4392.513250                 Wp   =           49.06010
     YDOT =       2046.931443  meter/sec      RA   =          306.96040  deg
     ZDOT =       5933.896545                 TA   =          303.34580
                                              MA   =          303.45173
                                              Ha   =            227.091  n.mi
                                              Hp   =            219.582
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11817473.92                 X    =         3669058.58
     Y    =      -18763366.54  feet           Y    =        -5678419.54  meter
     Z    =       -2301851.30                 Z    =         -683942.59
     XDOT =      14411.132710                 XDOT =        4340.472102
     YDOT =       6715.654340  feet/sec       YDOT =        2095.761011  meter/sec
     ZDOT =      19468.164517                 ZDOT =        5955.108471
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12365356.67                 X    =        -3768960.71
     Y    =       18416272.74  feet           Y    =         5613279.93  meter
     Z    =       -2225755.14                 Z    =         -678410.17
     XDOT =     -12746.602821                 XDOT =       -3885.164540
     YDOT =      -6222.915586  feet/sec       YDOT =       -1896.744670  meter/sec
     ZDOT =      19557.990669                 ZDOT =        5961.275556
  
  
    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   14271.47914852  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6452 307.6141 0001756 118.5584 241.5744 15.50635134 27355
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14271.47914852   =   yrday.fracday
    Element set:     913
    Inclination:       51.6452  deg
    RA of node:       307.6141  deg
    Eccentricity:     .0001756     
    Arg of perigee:   118.5584  deg
    Mean anomaly:     241.5744  deg
    Mean motion:   15.50635134  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2735
    Checksum:              305
 
 
    Coasting Arc #15 (Orbit 2750)
    ---------------------------------------
 
    Vector Time (GMT): 2014/272/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3522893.58                 A    =         6799287.06  meter
     Y    =        5806771.01  meter          E    =           .0014080
     Z    =         109913.26                 I    =           51.36186
     XDOT =      -4146.181409                 Wp   =          131.82174
     YDOT =      -2392.927169  meter/sec      RA   =          301.98588  deg
     ZDOT =      -5984.964906                 TA   =           46.99127
                                              MA   =           46.87337
                                              Ha   =            226.967  n.mi
                                              Hp   =            219.463
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11558049.82                 X    =        -3588098.34
     Y    =       19051085.98  feet           Y    =         5767011.16  meter
     Z    =         360607.80                 Z    =           92640.39
     XDOT =     -13602.957380                 XDOT =       -4090.041522
     YDOT =      -7850.810923  feet/sec       YDOT =       -2438.979093  meter/sec
     ZDOT =     -19635.711634                 ZDOT =       -6004.970189
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11778419.42                 X    =         3590062.24
     Y    =      -18916907.32  feet           Y    =        -5765873.35  meter
     Z    =         286154.08                 Z    =           87219.76
     XDOT =      12008.343531                 XDOT =        3660.143108
     YDOT =       7148.095198  feet/sec       YDOT =        2178.739416  meter/sec
     ZDOT =     -19720.348051                 ZDOT =       -6010.762086
  
  
    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   14272.51027041  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6457 302.4999 0001864 122.1334 237.9998 15.50708337 27512
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14272.51027041   =   yrday.fracday
    Element set:     914
    Inclination:       51.6457  deg
    RA of node:       302.4999  deg
    Eccentricity:     .0001864     
    Arg of perigee:   122.1334  deg
    Mean anomaly:     237.9998  deg
    Mean motion:   15.50708337  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2751
    Checksum:              314
 
 
    Coasting Arc #16 (Orbit 2765)
    ---------------------------------------
 
    Vector Time (GMT): 2014/273/11:28:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929559.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3394440.91                 A    =         6799233.83  meter
     Y    =       -5867577.24  meter          E    =           .0013619
     Z    =         449345.29                 I    =           51.34546
     XDOT =       3950.198358                 Wp   =           57.21617
     YDOT =       2751.374038  meter/sec      RA   =          297.01046  deg
     ZDOT =       5962.210904                 TA   =          307.64248
                                              MA   =          307.76598
                                              Ha   =            227.004  n.mi
                                              Hp   =            219.458
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11136617.16                 X    =         3457618.43
     Y    =      -19250581.50  feet           Y    =        -5829265.12  meter
     Z    =        1474229.94                 Z    =          465989.12
     XDOT =      12959.968366                 XDOT =        3890.175411
     YDOT =       9026.817710  feet/sec       YDOT =        2795.212574  meter/sec
     ZDOT =      19561.059395                 ZDOT =        5981.254631
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11017167.07                 X    =        -3358032.52
     Y    =       19313579.47  feet           Y    =         5886779.02  meter
     Z    =        1546014.72                 Z    =          471225.29
     XDOT =     -11479.371891                 XDOT =       -3498.912552
     YDOT =      -8151.780762  feet/sec       YDOT =       -2484.662776  meter/sec
     ZDOT =      19641.548474                 ZDOT =        5986.743975
  
  
    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   14273.54137451  .00016717  00000-0  10270-3 0  9150
    2 25544  51.6454 297.3863 0001838 120.5404 239.5928 15.50695802 27661
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14273.54137451   =   yrday.fracday
    Element set:     915
    Inclination:       51.6454  deg
    RA of node:       297.3863  deg
    Eccentricity:     .0001838     
    Arg of perigee:   120.5404  deg
    Mean anomaly:     239.5928  deg
    Mean motion:   15.50695802  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2766
    Checksum:              325
 
             

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