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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  22604.21
   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 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 2237)
    ---------------------------------------
 
    Vector Time (GMT): 2014/239/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3900425.41                 A    =         6796997.19  meter
     Y    =        4524544.59  meter          E    =           .0015859
     Z    =        3225677.50                 I    =           51.99624
     XDOT =      -2359.597224                 Wp   =           78.83735
     YDOT =      -5479.462322  meter/sec      RA   =          105.80633  deg
     ZDOT =       4815.650273                 TA   =          318.24684
                                              MA   =          318.36775
                                              Ha   =            228.706  n.mi
                                              Hp   =            220.105
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12796671.29                 X    =        -3966399.16
     Y    =       14844306.38  feet           Y    =         4480558.94  meter
     Z    =       10582931.43                 Z    =         3206569.29
     XDOT =      -7741.460710                 XDOT =       -2321.541886
     YDOT =     -17977.238590  feet/sec       YDOT =       -5505.635609  meter/sec
     ZDOT =      15799.377536                 ZDOT =        4804.280775
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18733025.77                 X    =         5709826.25
     Y    =        5908598.19  feet           Y    =         1800940.73  meter
     Z    =       10500898.94                 Z    =         3200674.00
     XDOT =     -12952.063389                 XDOT =       -3947.788921
     YDOT =      12969.503205  feet/sec       YDOT =        3953.104577  meter/sec
     ZDOT =      15751.867957                 ZDOT =        4801.169353
  
  
    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   14239.44313729  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6450 106.4047 0003599  50.7667 309.3803 15.50012572 22381
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14239.44313729   =   yrday.fracday
    Element set:     900
    Inclination:       51.6450  deg
    RA of node:       106.4047  deg
    Eccentricity:     .0003599     
    Arg of perigee:    50.7667  deg
    Mean anomaly:     309.3803  deg
    Mean motion:   15.50012572  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2238
    Checksum:              294
 
 
    Coasting Arc #2 (Orbit 2252)
    ---------------------------------------
 
    Vector Time (GMT): 2014/240/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3667337.62                 A    =         6796053.42  meter
     Y    =       -4518978.54  meter          E    =           .0008180
     Z    =       -3518524.53                 I    =           52.00172
     XDOT =       2543.779302                 Wp   =           72.86841
     YDOT =       5602.682980  meter/sec      RA   =          100.87603  deg
     ZDOT =      -4550.765109                 TA   =          148.16796
                                              MA   =          148.11849
                                              Ha   =            228.555  n.mi
                                              Hp   =            220.103
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12031947.56                 X    =         3734689.05
     Y    =      -14826045.08  feet           Y    =        -4477591.78  meter
     Z    =      -11543715.65                 Z    =        -3500545.19
     XDOT =       8345.732619                 XDOT =        2503.045757
     YDOT =      18381.505841  feet/sec       YDOT =        5630.900945  meter/sec
     ZDOT =     -14930.331721                 ZDOT =       -4538.507384
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18502071.86                 X    =        -5639431.50
     Y    =       -4902032.36  feet           Y    =        -1494139.46  meter
     Z    =      -11466479.89                 Z    =        -3494983.07
     XDOT =      12897.907854                 XDOT =        3931.282314
     YDOT =     -13926.746122  feet/sec       YDOT =       -4244.872218  meter/sec
     ZDOT =     -14879.068927                 ZDOT =       -4535.140209
  
  
    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   14240.41021608  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6456 101.6130 0003510  52.5600 307.5869 15.50053528 22532
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14240.41021608   =   yrday.fracday
    Element set:     901
    Inclination:       51.6456  deg
    RA of node:       101.6130  deg
    Eccentricity:     .0003510     
    Arg of perigee:    52.5600  deg
    Mean anomaly:     307.5869  deg
    Mean motion:   15.50053528  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2253
    Checksum:              257
 
 
    Coasting Arc #3 (Orbit 2268)
    ---------------------------------------
 
    Vector Time (GMT): 2014/241/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3425622.53                 A    =         6795234.16  meter
     Y    =        4489502.85  meter          E    =           .0014527
     Z    =        3766329.52                 I    =           52.00382
     XDOT =      -2770.750045                 Wp   =           86.93906
     YDOT =      -5721.432790  meter/sec      RA   =           95.94535  deg
     ZDOT =       4286.436389                 TA   =          317.81690
                                              MA   =          317.92859
                                              Ha   =            228.660  n.mi
                                              Hp   =            219.956
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11238919.06                 X    =        -3493866.14
     Y    =       14729340.05  feet           Y    =         4450814.13  meter
     Z    =       12356724.14                 Z    =         3749522.18
     XDOT =      -9090.387287                 XDOT =       -2727.387796
     YDOT =     -18771.104953  feet/sec       YDOT =       -5752.174229  meter/sec
     ZDOT =      14063.111512                 ZDOT =        4273.082417
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18158715.55                 X    =         5534776.50
     Y    =        3912568.22  feet           Y    =         1192550.79  meter
     Z    =       12284471.94                 Z    =         3744307.05
     XDOT =     -12740.662768                 XDOT =       -3883.354012
     YDOT =      15012.390946  feet/sec       YDOT =        4575.776760  meter/sec
     ZDOT =      14007.211435                 ZDOT =        4269.398045
  
  
    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   14241.44174958  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6453  96.5017 0003573  56.0368 304.1122 15.50069007 22695
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14241.44174958   =   yrday.fracday
    Element set:     902
    Inclination:       51.6453  deg
    RA of node:        96.5017  deg
    Eccentricity:     .0003573     
    Arg of perigee:    56.0368  deg
    Mean anomaly:     304.1122  deg
    Mean motion:   15.50069007  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2269
    Checksum:              292
 
 
    Coasting Arc #4 (Orbit 2283)
    ---------------------------------------
 
    Vector Time (GMT): 2014/242/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3232970.57                 A    =         6794243.78  meter
     Y    =       -4415377.28  meter          E    =           .0010291
     Z    =       -4037859.45                 I    =           52.00374
     XDOT =       2996.115701                 Wp   =           67.23932
     YDOT =       5817.410344  meter/sec      RA   =           91.01438  deg
     ZDOT =      -3966.603434                 TA   =          161.64738
                                              MA   =          161.61022
                                              Ha   =            228.467  n.mi
                                              Hp   =            219.999
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10606858.83                 X    =         3301718.67
     Y    =      -14486145.92  feet           Y    =        -4378840.08  meter
     Z    =      -13247570.37                 Z    =        -4021986.76
     XDOT =       9829.775923                 XDOT =        2950.109871
     YDOT =      19085.991942  feet/sec       YDOT =        5850.657252  meter/sec
     ZDOT =     -13013.790793                 ZDOT =       -3952.161013
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17727353.68                 X    =        -5403297.40
     Y    =       -3146271.71  feet           Y    =         -958983.62  meter
     Z    =      -13179298.34                 Z    =        -4017050.13
     XDOT =      12470.484302                 XDOT =        3801.003615
     YDOT =     -16061.923989  feet/sec       YDOT =       -4895.674432  meter/sec
     ZDOT =     -12953.284381                 ZDOT =       -3948.161079
  
  
    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   14242.40879325  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6458  91.7099 0003423  56.8925 303.2554 15.50109103 22846
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14242.40879325   =   yrday.fracday
    Element set:     903
    Inclination:       51.6458  deg
    RA of node:        91.7099  deg
    Eccentricity:     .0003423     
    Arg of perigee:    56.8925  deg
    Mean anomaly:     303.2554  deg
    Mean motion:   15.50109103  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2284
    Checksum:              301
 
 
    Coasting Arc #5 (Orbit 2299)
    ---------------------------------------
 
    Vector Time (GMT): 2014/243/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3041808.26                 A    =         6793388.94  meter
     Y    =        4318066.85  meter          E    =           .0012746
     Z    =        4261935.03                 I    =           52.00076
     XDOT =      -3259.520705                 Wp   =           94.62085
     YDOT =      -5904.967820  meter/sec      RA   =           86.08269  deg
     ZDOT =       3646.009046                 TA   =          318.21304
                                              MA   =          318.31030
                                              Ha   =            228.597  n.mi
                                              Hp   =            219.831
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9979685.89                 X    =        -3110570.93
     Y    =       14166885.99  feet           Y    =         4283667.24  meter
     Z    =       13982726.46                 Z    =         4246990.98
     XDOT =     -10693.965567                 XDOT =       -3210.958893
     YDOT =     -19373.254002  feet/sec       YDOT =       -5941.146077  meter/sec
     ZDOT =      11961.971935                 ZDOT =        3630.293159
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17209366.96                 X    =         5245415.05
     Y    =        2434524.68  feet           Y    =          742043.12  meter
     Z    =       13918412.52                 Z    =         4242332.13
     XDOT =     -12083.314130                 XDOT =       -3682.994147
     YDOT =      17209.305450  feet/sec       YDOT =        5245.396301  meter/sec
     ZDOT =      11896.071200                 ZDOT =        3625.922502
  
  
    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   14243.44028950  .00016717  00000-0  10270-3 0  9047
    2 25544  51.6459  86.5983 0003530  60.5850 299.5653 15.50123991 23006
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14243.44028950   =   yrday.fracday
    Element set:     904
    Inclination:       51.6459  deg
    RA of node:        86.5983  deg
    Eccentricity:     .0003530     
    Arg of perigee:    60.5850  deg
    Mean anomaly:     299.5653  deg
    Mean motion:   15.50123991  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2300
    Checksum:              307
 
 
    Coasting Arc #6 (Orbit 2314)
    ---------------------------------------
 
    Vector Time (GMT): 2014/244/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2908006.78                 A    =         6792412.31  meter
     Y    =       -4187202.50  meter          E    =           .0012700
     Z    =       -4501461.97                 I    =           51.99497
     XDOT =       3515.031684                 Wp   =           67.17066
     YDOT =       5956.071926  meter/sec      RA   =           81.15023  deg
     ZDOT =      -3272.062770                 TA   =          169.97052
                                              MA   =          169.94515
                                              Ha   =            228.370  n.mi
                                              Hp   =            219.896
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9540704.67                 X    =         2976479.59
     Y    =      -13737541.03  feet           Y    =        -4154300.73  meter
     Z    =      -14768576.00                 Z    =        -4487168.69
     XDOT =      11532.256182                 XDOT =        3464.062911
     YDOT =      19540.918391  feet/sec       YDOT =        5995.094089  meter/sec
     ZDOT =     -10735.114075                 ZDOT =       -3255.111413
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16664870.41                 X    =        -5079452.50
     Y    =       -1959818.17  feet           Y    =         -597352.58  meter
     Z    =      -14707043.32                 Z    =        -4482706.80
     XDOT =      11552.037609                 XDOT =        3521.061063
     YDOT =     -18267.871020  feet/sec       YDOT =       -5568.047087  meter/sec
     ZDOT =     -10663.974482                 ZDOT =       -3250.379422
  
  
    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   14244.40729773  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6460  81.8063 0003340  60.8984 299.2501 15.50167292 23152
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14244.40729773   =   yrday.fracday
    Element set:     905
    Inclination:       51.6460  deg
    RA of node:        81.8063  deg
    Eccentricity:     .0003340     
    Arg of perigee:    60.8984  deg
    Mean anomaly:     299.2501  deg
    Mean motion:   15.50167292  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2315
    Checksum:              302
 
 
    Coasting Arc #7 (Orbit 2330)
    ---------------------------------------
 
    Vector Time (GMT): 2014/245/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2785186.84                 A    =         6791606.57  meter
     Y    =        4036063.96  meter          E    =           .0010621
     Z    =        4690779.39                 I    =           51.98690
     XDOT =      -3801.023007                 Wp   =          100.99502
     YDOT =      -5996.421769  meter/sec      RA   =           76.21691  deg
     ZDOT =       2895.069809                 TA   =          320.32942
                                              MA   =          320.40707
                                              Ha   =            228.521  n.mi
                                              Hp   =            219.725
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9137752.09                 X    =        -2852898.31
     Y    =       13241679.64  feet           Y    =         4004539.84  meter
     Z    =       15389696.16                 Z    =         4677084.69
     XDOT =     -12470.547924                 XDOT =       -3747.750441
     YDOT =     -19673.299767  feet/sec       YDOT =       -6038.629251  meter/sec
     ZDOT =       9498.260529                 ZDOT =        2876.734700
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16068430.63                 X    =         4897657.66
     Y    =        1567703.00  feet           Y    =          477835.88  meter
     Z    =       15330726.83                 Z    =         4672805.54
     XDOT =     -10903.693265                 XDOT =       -3323.445707
     YDOT =      19385.842870  feet/sec       YDOT =        5908.804907  meter/sec
     ZDOT =       9421.248077                 ZDOT =        2871.596414
  
  
    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   14245.43875631  .00016717  00000-0  10270-3 0  9066
    2 25544  51.6462  76.6948 0003470  64.8009 295.3501 15.50177493 23313
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14245.43875631   =   yrday.fracday
    Element set:     906
    Inclination:       51.6462  deg
    RA of node:        76.6948  deg
    Eccentricity:     .0003470     
    Arg of perigee:    64.8009  deg
    Mean anomaly:     295.3501  deg
    Mean motion:   15.50177493  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2331
    Checksum:              313
 
 
    Coasting Arc #8 (Orbit 2345)
    ---------------------------------------
 
    Vector Time (GMT): 2014/246/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2724989.91                 A    =         6790720.59  meter
     Y    =       -3865795.53  meter          E    =           .0014995
     Z    =       -4886903.10                 I    =           51.97545
     XDOT =       4068.696500                 Wp   =           70.74061
     YDOT =       5988.889452  meter/sec      RA   =           71.28195  deg
     ZDOT =      -2470.149565                 TA   =          175.06844
                                              MA   =          175.05366
                                              Ha   =            228.277  n.mi
                                              Hp   =            219.786
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8940255.60                 X    =         2791754.51
     Y    =      -12683056.22  feet           Y    =        -3834949.85  meter
     Z    =      -16033146.65                 Z    =        -4873503.20
     XDOT =      13348.741797                 XDOT =        4013.424107
     YDOT =      19648.587441  feet/sec       YDOT =        6034.079090  meter/sec
     ZDOT =      -8104.165240                 ZDOT =       -2450.519010
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15513164.27                 X    =        -4728412.47
     Y    =       -1405890.02  feet           Y    =         -428515.28  meter
     Z    =      -15975452.55                 Z    =        -4869317.94
     XDOT =      10100.353341                 XDOT =        3078.587698
     YDOT =     -20351.033595  feet/sec       YDOT =       -6202.995040  meter/sec
     ZDOT =      -8021.645683                 ZDOT =       -2444.997604
  
  
    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   14246.40572851  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6456  71.9023 0003276  65.2713 294.8778 15.50227074 23466
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14246.40572851   =   yrday.fracday
    Element set:     907
    Inclination:       51.6456  deg
    RA of node:        71.9023  deg
    Eccentricity:     .0003276     
    Arg of perigee:    65.2713  deg
    Mean anomaly:     294.8778  deg
    Mean motion:   15.50227074  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2346
    Checksum:              313
 
 
    Coasting Arc #9 (Orbit 2361)
    ---------------------------------------
 
    Vector Time (GMT): 2014/247/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2683700.92                 A    =         6790056.79  meter
     Y    =        3680122.58  meter          E    =           .0008362
     Z    =        5029443.96                 I    =           51.96250
     XDOT =      -4356.714331                 Wp   =          104.11635
     YDOT =      -5970.445144  meter/sec      RA   =           66.34612  deg
     ZDOT =       2039.115904                 TA   =          326.12171
                                              MA   =          326.17509
                                              Ha   =            228.433  n.mi
                                              Hp   =            219.633
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8804793.03                 X    =        -2749084.67
     Y    =       12073892.97  feet           Y    =         3649746.35  meter
     Z    =       16500800.39                 Z    =         5016248.04
     XDOT =     -14293.682189                 XDOT =       -4299.532931
     YDOT =     -19588.074618  feet/sec       YDOT =       -6018.844925  meter/sec
     ZDOT =       6690.012810                 ZDOT =        2018.090926
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14945694.47                 X    =         4555447.68
     Y    =        1341931.23  feet           Y    =          409020.64  meter
     Z    =       16443999.58                 Z    =         5012131.07
     XDOT =      -9196.273086                 XDOT =       -2803.024036
     YDOT =      21333.275100  feet/sec       YDOT =        6502.382251  meter/sec
     ZDOT =       6601.560777                 ZDOT =        2012.155725
  
  
    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   14247.43714841  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6457  66.7906 0003387  69.2391 290.9122 15.50231205 23627
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14247.43714841   =   yrday.fracday
    Element set:     908
    Inclination:       51.6457  deg
    RA of node:        66.7906  deg
    Eccentricity:     .0003387     
    Arg of perigee:    69.2391  deg
    Mean anomaly:     290.9122  deg
    Mean motion:   15.50231205  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2362
    Checksum:              306
 
 
    Coasting Arc #10 (Orbit 2376)
    ---------------------------------------
 
    Vector Time (GMT): 2014/248/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2706116.76                 A    =         6789353.64  meter
     Y    =       -3492156.59  meter          E    =           .0016815
     Z    =       -5170317.44                 I    =           51.94596
     XDOT =       4612.847215                 Wp   =           76.58501
     YDOT =       5896.819207  meter/sec      RA   =           61.40767  deg
     ZDOT =      -1569.010758                 TA   =          178.31875
                                              MA   =          178.31309
                                              Ha   =            228.190  n.mi
                                              Hp   =            219.673
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8878335.84                 X    =         2770081.20
     Y    =      -11457206.67  feet           Y    =        -3461537.70  meter
     Z    =      -16962983.74                 Z    =        -5157016.09
     XDOT =      15134.013173                 XDOT =        4554.186453
     YDOT =      19346.519709  feet/sec       YDOT =        5948.074964  meter/sec
     ZDOT =      -5147.673091                 ZDOT =       -1546.745267
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14486004.95                 X    =        -4415334.31
     Y    =       -1478553.45  feet           Y    =         -450663.09  meter
     Z    =      -16905762.03                 Z    =        -5152876.27
     XDOT =       8151.598918                 XDOT =        2484.607350
     YDOT =     -22096.731058  feet/sec       YDOT =       -6735.083627  meter/sec
     ZDOT =      -5053.932264                 ZDOT =       -1540.438554
  
  
    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   14248.40408368  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6444  61.9973 0003231  70.4678 289.6822 15.50286890 23772
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14248.40408368   =   yrday.fracday
    Element set:     909
    Inclination:       51.6444  deg
    RA of node:        61.9973  deg
    Eccentricity:     .0003231     
    Arg of perigee:    70.4678  deg
    Mean anomaly:     289.6822  deg
    Mean motion:   15.50286890  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2377
    Checksum:              334
 
 
    Coasting Arc #11 (Orbit 2392)
    ---------------------------------------
 
    Vector Time (GMT): 2014/249/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2752845.51                 A    =         6788921.89  meter
     Y    =        3295097.98  meter          E    =           .0006397
     Z    =        5253409.37                 I    =           51.92891
     XDOT =      -4877.014733                 Wp   =           99.80864
     YDOT =      -5814.793938  meter/sec      RA   =           56.46848  deg
     ZDOT =       1089.416951                 TA   =          339.78037
                                              MA   =          339.80570
                                              Ha   =            228.334  n.mi
                                              Hp   =            219.547
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9031645.37                 X    =        -2815006.50
     Y    =       10810688.90  feet           Y    =         3263966.73  meter
     Z    =       17235595.05                 Z    =         5239885.37
     XDOT =     -16000.704504                 XDOT =       -4816.921864
     YDOT =     -19077.407933  feet/sec       YDOT =       -5868.995786  meter/sec
     ZDOT =       3574.202596                 ZDOT =        1065.871832
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14053710.03                 X    =         4283570.82
     Y    =        1713341.68  feet           Y    =          522226.54  meter
     Z    =       17177457.44                 Z    =         5235689.03
     XDOT =      -7040.207426                 XDOT =       -2145.855223
     YDOT =      22835.824023  feet/sec       YDOT =        6960.359162  meter/sec
     ZDOT =       3475.004382                 ZDOT =        1059.181335
  
  
    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   14249.43546350  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6444  56.8851 0003289  74.2845 285.8668 15.50287226 23939
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14249.43546350   =   yrday.fracday
    Element set:     910
    Inclination:       51.6444  deg
    RA of node:        56.8851  deg
    Eccentricity:     .0003289     
    Arg of perigee:    74.2845  deg
    Mean anomaly:     285.8668  deg
    Mean motion:   15.50287226  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2393
    Checksum:              331
 
 
    Coasting Arc #12 (Orbit 2407)
    ---------------------------------------
 
    Vector Time (GMT): 2014/250/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2859235.86                 A    =         6788495.01  meter
     Y    =       -3113714.09  meter          E    =           .0017860
     Z    =       -5327097.09                 I    =           51.90855
     XDOT =       5094.343792                 Wp   =           83.78276
     YDOT =       5675.864768  meter/sec      RA   =           51.52612  deg
     ZDOT =       -583.060668                 TA   =          180.65803
                                              MA   =          180.66038
                                              Ha   =            228.109  n.mi
                                              Hp   =            219.559
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9380695.07                 X    =         2919718.61
     Y    =      -10215597.39  feet           Y    =        -3081402.63  meter
     Z    =      -17477352.65                 Z    =        -5313060.28
     XDOT =      16713.726351                 XDOT =        5033.328625
     YDOT =      18621.603570  feet/sec       YDOT =        5732.491799  meter/sec
     ZDOT =      -1912.928701                 ZDOT =        -558.462179
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13786457.06                 X    =        -4202112.11
     Y    =       -2096002.74  feet           Y    =         -638861.64  meter
     Z    =      -17417063.47                 Z    =        -5308720.95
     XDOT =       5828.799737                 XDOT =        1776.618160
     YDOT =     -23299.381231  feet/sec       YDOT =       -7101.651399  meter/sec
     ZDOT =      -1809.227222                 ZDOT =        -551.452457
  
  
    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   14250.40236086  .00016717  00000-0  10270-3 0  9110
    2 25544  51.6430  52.0909 0003210  76.5252 283.6256 15.50346583 24085
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14250.40236086   =   yrday.fracday
    Element set:     911
    Inclination:       51.6430  deg
    RA of node:        52.0909  deg
    Eccentricity:     .0003210     
    Arg of perigee:    76.5252  deg
    Mean anomaly:     283.6256  deg
    Mean motion:   15.50346583  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2408
    Checksum:              279
 
 
    Coasting Arc #13 (Orbit 2423)
    ---------------------------------------
 
    Vector Time (GMT): 2014/251/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2991973.95                 A    =         6788375.58  meter
     Y    =        2930135.38  meter          E    =           .0005593
     Z    =        5337891.75                 I    =           51.88849
     XDOT =      -5305.887682                 Wp   =           84.56267
     YDOT =      -5534.169207  meter/sec      RA   =           46.58337  deg
     ZDOT =         64.301664                 TA   =            4.82929
                                              MA   =            4.82389
                                              Ha   =            228.232  n.mi
                                              Hp   =            219.457
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9816187.51                 X    =        -3050446.52
     Y    =        9613305.05  feet           Y    =         2896350.91  meter
     Z    =       17512768.22                 Z    =         5323214.94
     XDOT =     -17407.767985                 XDOT =       -5243.921334
     YDOT =     -18156.723119  feet/sec       YDOT =       -5593.156593  meter/sec
     ZDOT =        210.963465                 ZDOT =          38.677889
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13579831.98                 X    =         4139132.79
     Y    =        2561890.27  feet           Y    =          780864.16  meter
     Z    =       17449788.06                 Z    =         5318695.40
     XDOT =      -4602.079882                 XDOT =       -1402.713948
     YDOT =      23703.818787  feet/sec       YDOT =        7224.923966  meter/sec
     ZDOT =        102.880311                 ZDOT =          31.357919
  
  
    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   14251.43369924  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6434  46.9784 0003211  80.0826 280.0687 15.50346990 24249
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14251.43369924   =   yrday.fracday
    Element set:     912
    Inclination:       51.6434  deg
    RA of node:        46.9784  deg
    Eccentricity:     .0003211     
    Arg of perigee:    80.0826  deg
    Mean anomaly:     280.0687  deg
    Mean motion:   15.50346990  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2424
    Checksum:              306
 
 
    Coasting Arc #14 (Orbit 2438)
    ---------------------------------------
 
    Vector Time (GMT): 2014/252/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3174690.23                 A    =         6788299.37  meter
     Y    =       -2779672.22  meter          E    =           .0017896
     Z    =       -5332977.62                 I    =           51.86575
     XDOT =       5456.608864                 Wp   =           91.61065
     YDOT =       5340.203939  meter/sec      RA   =           41.63753  deg
     ZDOT =        465.709885                 TA   =          182.82370
                                              MA   =          182.83382
                                              Ha   =            228.035  n.mi
                                              Hp   =            219.441
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10415650.36                 X    =         3231442.94
     Y    =       -9119659.50  feet           Y    =        -2743854.18  meter
     Z    =      -17496645.73                 Z    =        -5317417.30
     XDOT =      17902.260051                 XDOT =        5394.225669
     YDOT =      17520.354129  feet/sec       YDOT =        5400.874528  meter/sec
     ZDOT =       1527.919571                 ZDOT =         492.064896
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13577722.19                 X    =        -4138489.72
     Y    =       -3103135.64  feet           Y    =         -945835.74  meter
     Z    =      -17429933.53                 Z    =        -5312643.74
     XDOT =       3338.146442                 XDOT =        1017.467035
     YDOT =     -23796.916035  feet/sec       YDOT =       -7253.300008  meter/sec
     ZDOT =       1639.138974                 ZDOT =         499.609559
  
  
    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   14252.40055784  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6425  42.1839 0003229  83.2164 276.9354 15.50407252 24397
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14252.40055784   =   yrday.fracday
    Element set:     913
    Inclination:       51.6425  deg
    RA of node:        42.1839  deg
    Eccentricity:     .0003229     
    Arg of perigee:    83.2164  deg
    Mean anomaly:     276.9354  deg
    Mean motion:   15.50407252  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2439
    Checksum:              299
 
 
    Coasting Arc #15 (Orbit 2454)
    ---------------------------------------
 
    Vector Time (GMT): 2014/253/09:14:47.654
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3381869.54                 A    =         6788551.49  meter
     Y    =        2633250.21  meter          E    =           .0006672
     Z    =        5259253.24                 I    =           51.84327
     XDOT =      -5587.173513                 Wp   =           70.39820
     YDOT =      -5152.577555  meter/sec      RA   =           36.69149  deg
     ZDOT =      -1009.670456                 TA   =           29.26140
                                              MA   =           29.22405
                                              Ha   =            228.138  n.mi
                                              Hp   =            219.352
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11095372.50                 X    =        -3436611.53
     Y    =        8639272.33  feet           Y    =         2595126.59  meter
     Z    =       17254767.84                 Z    =         5242691.29
     XDOT =     -18330.621761                 XDOT =       -5524.236301
     YDOT =     -16904.782005  feet/sec       YDOT =       -5214.705180  meter/sec
     ZDOT =      -3312.567113                 ZDOT =       -1036.658537
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13656475.72                 X    =         4162493.80
     Y    =        3699770.79  feet           Y    =         1127690.14  meter
     Z    =       17183820.80                 Z    =         5237628.58
     XDOT =      -2125.354733                 XDOT =        -647.808123
     YDOT =      23808.968361  feet/sec       YDOT =        7256.973557  meter/sec
     ZDOT =      -3426.501379                 ZDOT =       -1044.397620
  
  
    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   14253.43185366  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6431  37.0714 0003189  86.4867 273.6649 15.50410740 24554
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14253.43185366   =   yrday.fracday
    Element set:     914
    Inclination:       51.6431  deg
    RA of node:        37.0714  deg
    Eccentricity:     .0003189     
    Arg of perigee:    86.4867  deg
    Mean anomaly:     273.6649  deg
    Mean motion:   15.50410740  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2455
    Checksum:              311
 
             

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