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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  27986.17
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   132.3
   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 3574)
    ---------------------------------------
 
    Vector Time (GMT): 2014/325/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         555117.61                 A    =         6787081.54  meter
     Y    =       -4579382.83  meter          E    =           .0018984
     Z    =       -4996036.51                 I    =           51.86089
     XDOT =       6632.920350                 Wp   =           66.02129
     YDOT =       3147.038352  meter/sec      RA   =           38.65447  deg
     ZDOT =      -2146.530787                 TA   =          183.06898
                                              MA   =          183.08064
                                              Ha   =            227.717  n.mi
                                              Hp   =            217.056
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1821251.99                 X    =          630553.84
     Y    =      -15024221.88  feet           Y    =        -4572753.22  meter
     Z    =      -16391195.89                 Z    =        -4993156.65
     XDOT =      21761.549705                 XDOT =        6607.663883
     YDOT =      10324.928975  feet/sec       YDOT =        3221.070809  meter/sec
     ZDOT =      -7042.423842                 ZDOT =       -2114.369416
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15069494.18                 X    =         4593181.82
     Y    =        1544769.16  feet           Y    =          470845.64  meter
     Z    =      -16378019.97                 Z    =        -4992020.49
     XDOT =      -9657.960227                 XDOT =       -2943.746277
     YDOT =      20960.329995  feet/sec       YDOT =        6388.708582  meter/sec
     ZDOT =      -6905.883312                 ZDOT =       -2104.913234
  
  
    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   14325.60809216  .00016717  00000-0  10270-3 0  9004
    2 25544  51.6465  39.1502 0006798  51.3816 308.7943 15.51298731 35759
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14325.60809216   =   yrday.fracday
    Element set:     900
    Inclination:       51.6465  deg
    RA of node:        39.1502  deg
    Eccentricity:     .0006798     
    Arg of perigee:    51.3816  deg
    Mean anomaly:     308.7943  deg
    Mean motion:   15.51298731  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3575
    Checksum:              317
 
 
    Coasting Arc #2 (Orbit 3590)
    ---------------------------------------
 
    Vector Time (GMT): 2014/326/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1057966.17                 A    =         6785892.32  meter
     Y    =        4212571.27  meter          E    =           .0009274
     Z    =        5205568.43                 I    =           51.83189
     XDOT =      -6798.336791                 Wp   =           79.12922
     YDOT =      -3309.287015  meter/sec      RA   =           33.69933  deg
     ZDOT =       1296.093182                 TA   =          358.45975
                                              MA   =          358.46261
                                              Ha   =            227.768  n.mi
                                              Hp   =            216.786
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3471017.63                 X    =        -1130281.09
     Y    =       13820771.88  feet           Y    =         4200335.82  meter
     Z    =       17078636.59                 Z    =         5200253.40
     XDOT =     -22304.254563                 XDOT =       -6767.122457
     YDOT =     -10857.240864  feet/sec       YDOT =       -3385.135955  meter/sec
     ZDOT =       4252.274218                 ZDOT =        1263.142676
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13961724.77                 X    =        -4255533.71
     Y    =       -2988976.48  feet           Y    =         -911040.03  meter
     Z    =       17055139.62                 Z    =         5198406.56
     XDOT =       9681.555323                 XDOT =        2950.938063
     YDOT =     -21753.126702  feet/sec       YDOT =       -6630.353019  meter/sec
     ZDOT =       4112.407520                 ZDOT =        1253.461812
  
  
    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   14326.63877582  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6457  34.0341 0006981  54.9885 305.1921 15.51373411 35918
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14326.63877582   =   yrday.fracday
    Element set:     901
    Inclination:       51.6457  deg
    RA of node:        34.0341  deg
    Eccentricity:     .0006981     
    Arg of perigee:    54.9885  deg
    Mean anomaly:     305.1921  deg
    Mean motion:   15.51373411  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3591
    Checksum:              312
 
 
    Coasting Arc #3 (Orbit 3605)
    ---------------------------------------
 
    Vector Time (GMT): 2014/327/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1624648.81                 A    =         6785367.71  meter
     Y    =       -3893838.29  meter          E    =           .0021162
     Z    =       -5332220.43                 I    =           51.80465
     XDOT =       6840.840109                 Wp   =           77.52679
     YDOT =       3398.027686  meter/sec      RA   =           28.74059  deg
     ZDOT =       -393.969307                 TA   =          188.69688
                                              MA   =          188.73361
                                              Ha   =            227.704  n.mi
                                              Hp   =            216.734
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5330212.64                 X    =         1693972.63
     Y    =      -12775060.02  feet           Y    =        -3875282.48  meter
     Z    =      -17494161.51                 Z    =        -5324159.80
     XDOT =      22443.701145                 XDOT =        6804.247958
     YDOT =      11148.384798  feet/sec       YDOT =        3474.321819  meter/sec
     ZDOT =      -1292.550221                 ZDOT =        -360.825439
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13078248.93                 X    =         3986250.27
     Y    =        4669186.49  feet           Y    =         1423168.04  meter
     Z    =      -17459012.42                 Z    =        -5321506.99
     XDOT =      -9449.566449                 XDOT =       -2880.227854
     YDOT =      22122.388915  feet/sec       YDOT =        6742.904141  meter/sec
     ZDOT =      -1151.881871                 ZDOT =        -351.093594
  
  
    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   14327.60501175  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6466  29.2372 0006994  57.9366 302.2463 15.51396886 36066
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14327.60501175   =   yrday.fracday
    Element set:     902
    Inclination:       51.6466  deg
    RA of node:        29.2372  deg
    Eccentricity:     .0006994     
    Arg of perigee:    57.9366  deg
    Mean anomaly:     302.2463  deg
    Mean motion:   15.51396886  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3606
    Checksum:              321
 
 
    Coasting Arc #4 (Orbit 3621)
    ---------------------------------------
 
    Vector Time (GMT): 2014/328/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2244049.64                 A    =         6785194.71  meter
     Y    =        3576438.01  meter          E    =           .0010058
     Z    =        5304171.16                 I    =           51.77548
     XDOT =      -6819.992776                 Wp   =           62.51845
     YDOT =      -3470.017605  meter/sec      RA   =           23.77895  deg
     ZDOT =       -540.310150                 TA   =           32.65656
                                              MA   =           32.59441
                                              Ha   =            227.781  n.mi
                                              Hp   =            216.438
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7362367.59                 X    =        -2309641.81
     Y    =       11733720.51  feet           Y    =         3550976.49  meter
     Z    =       17402136.37                 Z    =         5293110.62
     XDOT =     -22375.304383                 XDOT =       -6778.058653
     YDOT =     -11384.572194  feet/sec       YDOT =       -3546.048680  meter/sec
     ZDOT =      -1772.671096                 ZDOT =        -573.339654
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12274329.37                 X    =        -3741215.59
     Y    =       -6549027.39  feet           Y    =        -1996143.55  meter
     Z    =       17354252.58                 Z    =         5289576.19
     XDOT =       9156.602858                 XDOT =        2790.932551
     YDOT =     -22276.670559  feet/sec       YDOT =       -6789.929187  meter/sec
     ZDOT =      -1912.833899                 ZDOT =        -583.031772
  
  
    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   14328.63562950  .00016717  00000-0  10270-3 0  9034
    2 25544  51.6452  24.1200 0007192  61.7924 298.3953 15.51473546 36225
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14328.63562950   =   yrday.fracday
    Element set:     903
    Inclination:       51.6452  deg
    RA of node:        24.1200  deg
    Eccentricity:     .0007192     
    Arg of perigee:    61.7924  deg
    Mean anomaly:     298.3953  deg
    Mean motion:   15.51473546  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3622
    Checksum:              303
 
 
    Coasting Arc #5 (Orbit 3636)
    ---------------------------------------
 
    Vector Time (GMT): 2014/329/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2882669.53                 A    =         6785793.73  meter
     Y    =       -3330882.59  meter          E    =           .0019856
     Z    =       -5178675.21                 I    =           51.74946
     XDOT =       6649.768672                 Wp   =           88.44910
     YDOT =       3485.830408  meter/sec      RA   =           18.81572  deg
     ZDOT =       1464.868283                 TA   =          195.63392
                                              MA   =          195.69533
                                              Ha   =            227.672  n.mi
                                              Hp   =            216.455
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9457577.20                 X    =         2944858.64
     Y    =      -10928092.48  feet           Y    =        -3298298.65  meter
     Z    =      -16990404.22                 Z    =        -5164520.59
     XDOT =      21816.826352                 XDOT =        6603.179128
     YDOT =      11436.451471  feet/sec       YDOT =        3559.931838  meter/sec
     ZDOT =       4805.998305                 ZDOT =        1497.059392
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11779583.71                 X    =         3590417.12
     Y    =        8495915.56  feet           Y    =         2589555.06  meter
     Z    =      -16929371.93                 Z    =        -5160072.56
     XDOT =      -8720.794272                 XDOT =       -2658.098094
     YDOT =      21904.875621  feet/sec       YDOT =        6676.606089  meter/sec
     ZDOT =       4942.580365                 ZDOT =        1506.498495
  
  
    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   14329.60180363  .00016717  00000-0  10270-3 0  9047
    2 25544  51.6461  19.3228 0007151  64.3865 295.8025 15.51492561 36375
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14329.60180363   =   yrday.fracday
    Element set:     904
    Inclination:       51.6461  deg
    RA of node:        19.3228  deg
    Eccentricity:     .0007151     
    Arg of perigee:    64.3865  deg
    Mean anomaly:     295.8025  deg
    Mean motion:   15.51492561  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3637
    Checksum:              306
 
 
    Coasting Arc #6 (Orbit 3652)
    ---------------------------------------
 
    Vector Time (GMT): 2014/330/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3545381.01                 A    =         6786752.92  meter
     Y    =        3093796.85  meter          E    =           .0014245
     Z    =        4882039.15                 I    =           51.72207
     XDOT =      -6382.084037                 Wp   =           63.47230
     YDOT =      -3518.678863  meter/sec      RA   =           13.85014  deg
     ZDOT =      -2393.289077                 TA   =           50.00895
                                              MA   =           49.88398
                                              Ha   =            227.720  n.mi
                                              Hp   =            216.157
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11631827.48                 X    =        -3603428.65
     Y    =       10150252.12  feet           Y    =         3053825.25  meter
     Z    =       16017188.81                 Z    =         4864675.22
     XDOT =     -20938.595922                 XDOT =       -6330.637089
     YDOT =     -11544.221992  feet/sec       YDOT =       -3589.759670  meter/sec
     ZDOT =      -7851.998284                 ZDOT =       -2424.167848
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11391572.99                 X    =        -3472151.45
     Y    =      -10533070.87  feet           Y    =        -3210480.00  meter
     Z    =       15942517.01                 Z    =         4859279.18
     XDOT =       8386.310215                 XDOT =        2556.147354
     YDOT =     -21210.568216  feet/sec       YDOT =       -6464.981192  meter/sec
     ZDOT =      -7982.975370                 ZDOT =       -2433.210893
  
  
    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   14330.63235636  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6447  14.2046 0007295  68.1752 292.0175 15.51576082 36531
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14330.63235636   =   yrday.fracday
    Element set:     905
    Inclination:       51.6447  deg
    RA of node:        14.2046  deg
    Eccentricity:     .0007295     
    Arg of perigee:    68.1752  deg
    Mean anomaly:     292.0175  deg
    Mean motion:   15.51576082  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3653
    Checksum:              302
 
 
    Coasting Arc #7 (Orbit 3667)
    ---------------------------------------
 
    Vector Time (GMT): 2014/331/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4171972.81                 A    =         6788322.00  meter
     Y    =       -2937975.24  meter          E    =           .0015627
     Z    =       -4491001.61                 I    =           51.69739
     XDOT =       5966.306814                 Wp   =           92.72190
     YDOT =       3526.478276  meter/sec      RA   =            8.88536  deg
     ZDOT =       3244.528906                 TA   =          209.93628
                                              MA   =          210.02573
                                              Ha   =            227.632  n.mi
                                              Hp   =            216.185
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13687574.84                 X    =         4226331.84
     Y    =       -9639026.39  feet           Y    =        -2891017.41  meter
     Z    =      -14734257.26                 Z    =        -4470602.72
     XDOT =      19574.497420                 XDOT =        5910.668506
     YDOT =      11569.810618  feet/sec       YDOT =        3592.886157  meter/sec
     ZDOT =      10644.779876                 ZDOT =        3273.377572
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11326247.30                 X    =         3452240.18
     Y    =       12431809.60  feet           Y    =         3789215.57  meter
     Z    =      -14646675.52                 Z    =        -4464306.70
     XDOT =      -8069.989228                 XDOT =       -2459.732717
     YDOT =      20002.527435  feet/sec       YDOT =        6096.770362  meter/sec
     ZDOT =      10767.095602                 ZDOT =        3281.810740
  
  
    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   14331.59847011  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6453   9.4073 0007295  70.8689 289.3252 15.51587880 36682
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14331.59847011   =   yrday.fracday
    Element set:     906
    Inclination:       51.6453  deg
    RA of node:         9.4073  deg
    Eccentricity:     .0007295     
    Arg of perigee:    70.8689  deg
    Mean anomaly:     289.3252  deg
    Mean motion:   15.51587880  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3668
    Checksum:              336
 
 
    Coasting Arc #8 (Orbit 3683)
    ---------------------------------------
 
    Vector Time (GMT): 2014/332/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4782721.04                 A    =         6790046.52  meter
     Y    =        2781454.53  meter          E    =           .0018500
     Z    =        3923640.90                 I    =           51.67186
     XDOT =      -5431.252573                 Wp   =           77.84440
     YDOT =      -3587.229215  meter/sec      RA   =            3.91905  deg
     ZDOT =      -4057.466406                 TA   =           54.64489
                                              MA   =           54.47213
                                              Ha   =            227.593  n.mi
                                              Hp   =            215.930
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15691342.00                 X    =        -4832528.35
     Y    =        9125507.00  feet           Y    =         2727692.46  meter
     Z    =       12872837.58                 Z    =         3900286.07
     XDOT =     -17819.070121                 XDOT =       -5371.025694
     YDOT =     -11769.124722  feet/sec       YDOT =       -3647.628151  meter/sec
     ZDOT =     -13311.897657                 ZDOT =       -4083.704624
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11319290.48                 X    =        -3450119.74
     Y    =      -14280588.41  feet           Y    =        -4352723.35  meter
     Z    =       12772685.58                 Z    =         3893114.57
     XDOT =       8030.241055                 XDOT =        2447.617474
     YDOT =     -18429.858683  feet/sec       YDOT =       -5617.420927  meter/sec
     ZDOT =     -13423.065752                 ZDOT =       -4091.350441
  
  
    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   14332.62895866  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6443   4.2885 0007336  74.2506 285.9454 15.51678374 36840
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14332.62895866   =   yrday.fracday
    Element set:     907
    Inclination:       51.6443  deg
    RA of node:         4.2885  deg
    Eccentricity:     .0007336     
    Arg of perigee:    74.2506  deg
    Mean anomaly:     285.9454  deg
    Mean motion:   15.51678374  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3684
    Checksum:              341
 
 
    Coasting Arc #9 (Orbit 3698)
    ---------------------------------------
 
    Vector Time (GMT): 2014/333/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5302532.40                 A    =         6791949.98  meter
     Y    =       -2696581.13  meter          E    =           .0012046
     Z    =       -3285197.02                 I    =           51.64720
     XDOT =       4780.959400                 Wp   =           78.92683
     YDOT =       3657.379396  meter/sec      RA   =          358.95484  deg
     ZDOT =       4731.726609                 TA   =          243.01553
                                              MA   =          243.13859
                                              Ha   =            227.570  n.mi
                                              Hp   =            215.882
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17396759.84                 X    =         5348250.65
     Y    =       -8847050.94  feet           Y    =        -2637029.10  meter
     Z    =      -10778205.45                 Z    =        -3259326.86
     XDOT =      15685.562336                 XDOT =        4716.721020
     YDOT =      11999.276235  feet/sec       YDOT =        3710.483950  meter/sec
     ZDOT =      15524.037430                 ZDOT =        4754.796022
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11562672.42                 X    =         3524302.56
     Y    =       15798719.13  feet           Y    =         4815449.59  meter
     Z    =      -10667350.00                 Z    =        -3251408.28
     XDOT =      -8162.471879                 XDOT =       -2487.921429
     YDOT =      16483.636677  feet/sec       YDOT =        5024.212459  meter/sec
     ZDOT =      15621.674519                 ZDOT =        4761.486393
  
  
    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   14333.59501293  .00016717  00000-0  10270-3 0  9083
    2 25544  51.6444 359.4911 0007446  77.7451 282.4533 15.51692657 36991
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14333.59501293   =   yrday.fracday
    Element set:     908
    Inclination:       51.6444  deg
    RA of node:       359.4911  deg
    Eccentricity:     .0007446     
    Arg of perigee:    77.7451  deg
    Mean anomaly:     282.4533  deg
    Mean motion:   15.51692657  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3699
    Checksum:              338
 
 
    Coasting Arc #10 (Orbit 3714)
    ---------------------------------------
 
    Vector Time (GMT): 2014/334/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5762976.80                 A    =         6793658.22  meter
     Y    =        2583412.72  meter          E    =           .0020654
     Z    =        2482106.61                 I    =           51.62177
     XDOT =      -4010.601591                 Wp   =           96.25699
     YDOT =      -3808.223313  meter/sec      RA   =          353.98943  deg
     ZDOT =      -5312.367632                 TA   =           55.92925
                                              MA   =           55.73336
                                              Ha   =            227.441  n.mi
                                              Hp   =            215.725
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18907404.19                 X    =        -5803494.20
     Y    =        8475763.51  feet           Y    =         2518740.81  meter
     Z    =        8143394.40                 Z    =         2454012.19
     XDOT =     -13158.141703                 XDOT =       -3941.913026
     YDOT =     -12494.170975  feet/sec       YDOT =       -3852.688365  meter/sec
     ZDOT =     -17429.027664                 ZDOT =       -5331.683959
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11734761.11                 X    =        -3576755.19
     Y    =      -17133851.77  feet           Y    =        -5222398.02  meter
     Z    =        8023084.06                 Z    =         2445436.02
     XDOT =       8707.540234                 XDOT =        2654.058263
     YDOT =     -14219.064946  feet/sec       YDOT =       -4333.970995  meter/sec
     ZDOT =     -17510.626399                 ZDOT =       -5337.238926
  
  
    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   14334.62543798  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6438 354.3718 0007387  80.4611 279.7375 15.51774004 37155
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14334.62543798   =   yrday.fracday
    Element set:     909
    Inclination:       51.6438  deg
    RA of node:       354.3718  deg
    Eccentricity:     .0007387     
    Arg of perigee:    80.4611  deg
    Mean anomaly:     279.7375  deg
    Mean motion:   15.51774004  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3715
    Checksum:              334
 
 
    Coasting Arc #11 (Orbit 3729)
    ---------------------------------------
 
    Vector Time (GMT): 2014/335/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6091036.79                 A    =         6794964.99  meter
     Y    =       -2513994.47  meter          E    =           .0014180
     Z    =       -1650588.55                 I    =           51.59511
     XDOT =       3183.887500                 Wp   =           60.46847
     YDOT =       3993.669088  meter/sec      RA   =          349.02563  deg
     ZDOT =       5710.337754                 TA   =          281.46816
                                              MA   =          281.62737
                                              Ha   =            227.438  n.mi
                                              Hp   =            215.571
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19983716.50                 X    =         6126714.30
     Y    =       -8248013.36  feet           Y    =        -2445681.04  meter
     Z    =       -5415316.77                 Z    =        -1620912.11
     XDOT =      10445.825130                 XDOT =        3111.253355
     YDOT =      13102.588873  feet/sec       YDOT =        4028.867196  meter/sec
     ZDOT =      18734.703918                 ZDOT =        5725.628467
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12011739.86                 X    =         3661178.31
     Y    =       18012675.69  feet           Y    =         5490263.55  meter
     Z    =       -5288281.88                 Z    =        -1611868.32
     XDOT =      -9512.601249                 XDOT =       -2899.440861
     YDOT =      11819.428727  feet/sec       YDOT =        3602.561876  meter/sec
     ZDOT =      18799.096472                 ZDOT =        5729.964605
  
  
    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   14335.59143264  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6434 349.5741 0007544  85.2745 274.9268 15.51812367 37309
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14335.59143264   =   yrday.fracday
    Element set:     910
    Inclination:       51.6434  deg
    RA of node:       349.5741  deg
    Eccentricity:     .0007544     
    Arg of perigee:    85.2745  deg
    Mean anomaly:     274.9268  deg
    Mean motion:   15.51812367  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3730
    Checksum:              321
 
 
    Coasting Arc #12 (Orbit 3745)
    ---------------------------------------
 
    Vector Time (GMT): 2014/336/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6323269.84                 A    =         6795759.32  meter
     Y    =        2373679.72  meter          E    =           .0019391
     Z    =         687865.05                 I    =           51.56768
     XDOT =      -2263.047747                 Wp   =          113.05853
     YDOT =      -4266.700633  meter/sec      RA   =          344.05982  deg
     ZDOT =      -5953.491495                 TA   =           59.50986
                                              MA   =           59.31852
                                              Ha   =            227.288  n.mi
                                              Hp   =            215.535
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20745635.95                 X    =        -6352684.40
     Y    =        7787663.11  feet           Y    =         2302804.33  meter
     Z    =        2256775.10                 Z    =          657075.60
     XDOT =      -7424.697333                 XDOT =       -2186.247684
     YDOT =     -13998.361656  feet/sec       YDOT =       -4291.577939  meter/sec
     ZDOT =     -19532.452410                 ZDOT =       -5964.298804
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12027631.17                 X    =        -3666021.98
     Y    =      -18626392.06  feet           Y    =        -5677324.30  meter
     Z    =        2125029.08                 Z    =          647708.86
     XDOT =      10767.233131                 XDOT =        3281.852658
     YDOT =      -9236.497316  feet/sec       YDOT =       -2815.284382  meter/sec
     ZDOT =     -19577.671075                 ZDOT =       -5967.274144
  
  
    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   14336.62179430  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6435 344.4543 0007441  87.3292 272.8712 15.51859103 37467
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14336.62179430   =   yrday.fracday
    Element set:     911
    Inclination:       51.6435  deg
    RA of node:       344.4543  deg
    Eccentricity:     .0007441     
    Arg of perigee:    87.3292  deg
    Mean anomaly:     272.8712  deg
    Mean motion:   15.51859103  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3746
    Checksum:              309
 
 
    Coasting Arc #13 (Orbit 3761)
    ---------------------------------------
 
    Vector Time (GMT): 2014/337/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6405507.18                 A    =         6795699.94  meter
     Y    =       -2237854.54  meter          E    =           .0018716
     Z    =         245761.61                 I    =           51.53778
     XDOT =       1356.660732                 Wp   =           64.17744
     YDOT =       4579.867479  meter/sec      RA   =          339.09367  deg
     ZDOT =       5995.348078                 TA   =          298.47212
                                              MA   =          298.66052
                                              Ha   =            227.216  n.mi
                                              Hp   =            215.353
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21015443.50                 X    =         6428861.46
     Y    =       -7342042.47  feet           Y    =        -2166093.44  meter
     Z    =         806304.48                 Z    =          276935.84
     XDOT =       4450.986655                 XDOT =        1276.222769
     YDOT =      15025.811939  feet/sec       YDOT =        4594.588532  meter/sec
     ZDOT =      19669.777160                 ZDOT =        6001.743473
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11969770.14                 X    =         3648385.94
     Y    =       18762894.86  feet           Y    =         5718930.35  meter
     Z    =         939659.15                 Z    =          286408.11
     XDOT =     -12264.496015                 XDOT =       -3738.218385
     YDOT =       6788.648442  feet/sec       YDOT =        2069.180045  meter/sec
     ZDOT =      19696.120572                 ZDOT =        6003.377550
  
  
    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   14337.65212199  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6430 339.3359 0007505  93.0250 267.1760 15.51928291 37622
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14337.65212199   =   yrday.fracday
    Element set:     912
    Inclination:       51.6430  deg
    RA of node:       339.3359  deg
    Eccentricity:     .0007505     
    Arg of perigee:    93.0250  deg
    Mean anomaly:     267.1760  deg
    Mean motion:   15.51928291  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3762
    Checksum:              309
 
 
    Coasting Arc #14 (Orbit 3776)
    ---------------------------------------
 
    Vector Time (GMT): 2014/338/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6373812.28                 A    =         6794962.89  meter
     Y    =        1983708.86  meter          E    =           .0014948
     Z    =       -1253589.04                 I    =           51.50726
     XDOT =       -407.283836                 Wp   =          120.16867
     YDOT =      -4955.341268  meter/sec      RA   =          334.12380  deg
     ZDOT =      -5830.099721                 TA   =           73.47081
                                              MA   =           73.30666
                                              Ha   =            227.112  n.mi
                                              Hp   =            215.358
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20911457.60                 X    =        -6389431.22
     Y    =        6508231.18  feet           Y    =         1912345.51  meter
     Z    =       -4112824.95                 Z    =        -1284590.47
     XDOT =      -1336.233057                 XDOT =        -323.520555
     YDOT =     -16257.681326  feet/sec       YDOT =       -4959.427081  meter/sec
     ZDOT =     -19127.623755                 ZDOT =       -5831.875121
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11451575.21                 X    =        -3490440.12
     Y    =      -18638657.62  feet           Y    =        -5681062.84  meter
     Z    =       -4245389.06                 Z    =        -1293994.58
     XDOT =      14099.964553                 XDOT =        4297.669196
     YDOT =      -4347.797391  feet/sec       YDOT =       -1325.208645  meter/sec
     ZDOT =     -19134.194083                 ZDOT =       -5832.102356
  
  
    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   14338.61802625  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6436 334.5356 0007436  94.5553 265.6448 15.51947638 37775
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14338.61802625   =   yrday.fracday
    Element set:     913
    Inclination:       51.6436  deg
    RA of node:       334.5356  deg
    Eccentricity:     .0007436     
    Arg of perigee:    94.5553  deg
    Mean anomaly:     265.6448  deg
    Mean motion:   15.51947638  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3777
    Checksum:              339
 
 
    Coasting Arc #15 (Orbit 3792)
    ---------------------------------------
 
    Vector Time (GMT): 2014/339/14:07:07.165
    Vector Time (MET): N/A
    Weight (LBS)     : 914609.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6202823.64                 A    =         6793410.55  meter
     Y    =       -1695199.04  meter          E    =           .0020698
     Z    =        2167034.35                 I    =           51.47494
     XDOT =       -463.721576                 Wp   =           80.58819
     YDOT =       5352.027370  meter/sec      RA   =          329.15116  deg
     ZDOT =       5472.653789                 TA   =          303.50418
                                              MA   =          303.70178
                                              Ha   =            226.976  n.mi
                                              Hp   =            215.244
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20350471.27                 X    =         6210791.83
     Y    =       -5561676.64  feet           Y    =        -1625790.66  meter
     Z    =        7109692.75                 Z    =         2197186.47
     XDOT =      -1521.396246                 XDOT =        -550.119512
     YDOT =      17559.144916  feet/sec       YDOT =        5346.358237  meter/sec
     ZDOT =      17954.900883                 ZDOT =        5470.191614
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10704496.10                 X    =         3262730.41
     Y    =       18128387.29  feet           Y    =         5525532.45  meter
     Z    =        7238576.95                 Z    =         2206318.26
     XDOT =     -16050.742328                 XDOT =       -4892.266262
     YDOT =       2259.736347  feet/sec       YDOT =         688.767638  meter/sec
     ZDOT =      17943.325844                 ZDOT =        5469.125717
  
  
    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   14339.64828953  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6436 329.4167 0007426  99.8374 260.3616 15.52020677 37939
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14339.64828953   =   yrday.fracday
    Element set:     914
    Inclination:       51.6436  deg
    RA of node:       329.4167  deg
    Eccentricity:     .0007426     
    Arg of perigee:    99.8374  deg
    Mean anomaly:     260.3616  deg
    Mean motion:   15.52020677  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3793
    Checksum:              340
 
             

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