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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15269.8125
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   68.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.626
   ET - UTC  (sec) :   68.18
   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 
   ------------------------------------------------------------------------
   234/03:38:33.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              226.8  
   000/00:00:00.000           0.0               0.0              222.3  
   
   235/16:24:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              226.9  
   000/00:00:00.000           0.0               0.0              222.2  
   
   236/05:30:52.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.1  
   000/00:00:00.000           0.0               0.0              221.9  
   
   239/14:44:31.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.5  
   000/00:00:00.000           0.0               0.0              221.3  
   
   240/02:16:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.7  
   000/00:00:00.000           0.0               0.0              221.1  
   
 
 
    Coasting Arc #1 (Orbit 2537)
    ---------------------------------------
 
    Vector Time (GMT): 2019/233/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 937174.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5953041.03                 A    =         6799187.29  meter
     Y    =        2844792.76  meter          E    =           .0011021
     Z    =       -1611961.62                 I    =           51.88955
     XDOT =       -833.906153                 Wp   =          356.07489
     YDOT =       4998.715409  meter/sec      RA   =           36.59038  deg
     ZDOT =       5750.471305                 TA   =          346.36909
                                              MA   =          346.39882
                                              Ha   =            226.597  n.mi
                                              Hp   =            222.469
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19530974.51                 X    =         5928617.28
     Y    =        9333309.58  feet           Y    =         2911227.25  meter
     Z    =       -5288588.00                 Z    =        -1583103.52
     XDOT =      -2735.912574                 XDOT =        -917.673716
     YDOT =      16399.984938  feet/sec       YDOT =        4988.921869  meter/sec
     ZDOT =      18866.375672                 ZDOT =        5746.216928
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11848023.51                 X    =        -3611277.56
     Y    =      -18153873.79  feet           Y    =        -5533300.73  meter
     Z    =       -5157518.95                 Z    =        -1572011.77
     XDOT =       9658.171194                 XDOT =        2943.810580
     YDOT =     -11649.637636  feet/sec       YDOT =       -3550.809551  meter/sec
     ZDOT =      18846.504157                 ZDOT =        5744.414467
  
  
    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   19233.50307464  .00016717  00000-0  10270-3 0  9004
    2 25544  51.6408  37.2388 0007281 309.5568  50.4939 15.50385689 25389
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19233.50307464   =   yrday.fracday
    Element set:     900
    Inclination:       51.6408  deg
    RA of node:        37.2388  deg
    Eccentricity:     .0007281     
    Arg of perigee:   309.5568  deg
    Mean anomaly:      50.4939  deg
    Mean motion:   15.50385689  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2538
    Checksum:              327
 
 
    Coasting Arc #2 (Orbit 2548)
    ---------------------------------------
 
    Vector Time (GMT): 2019/234/03:38:33.000
    Vector Time (MET): N/A
    Weight (LBS)     : 937174.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4342360.43                 A    =         6798412.97  meter
     Y    =        4797767.34  meter          E    =           .0012692
     Z    =        2056614.35                 I    =           51.87092
     XDOT =      -4871.001186                 Wp   =           35.98844
     YDOT =       2019.960360  meter/sec      RA   =           33.40679  deg
     ZDOT =       5565.027715                 TA   =          346.65835
                                              MA   =          346.69188
                                              Ha   =            226.780  n.mi
                                              Hp   =            222.251
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14246589.35                 X    =         4278397.83
     Y    =       15740706.50  feet           Y    =         4845969.07  meter
     Z    =        6747422.42                 Z    =         2077552.40
     XDOT =     -15980.975021                 XDOT =       -4920.258669
     YDOT =       6627.166536  feet/sec       YDOT =        1965.214084  meter/sec
     ZDOT =      18257.964945                 ZDOT =        5541.246622
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19362226.76                 X    =         5901606.72
     Y    =        8634284.27  feet           Y    =         2631729.85  meter
     Z    =        6842234.17                 Z    =         2085512.98
     XDOT =     -11405.287288                 XDOT =       -3476.331565
     YDOT =      11174.593843  feet/sec       YDOT =        3406.016203  meter/sec
     ZDOT =      18149.515577                 ZDOT =        5531.972348
  
  
    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   19234.21210678  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6423  33.7287 0007647 314.5140  45.5385 15.50380337 25490
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19234.21210678   =   yrday.fracday
    Element set:     901
    Inclination:       51.6423  deg
    RA of node:        33.7287  deg
    Eccentricity:     .0007647     
    Arg of perigee:   314.5140  deg
    Mean anomaly:      45.5385  deg
    Mean motion:   15.50380337  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2549
    Checksum:              298
 
 
    Coasting Arc #3 (Orbit 2563)
    ---------------------------------------
 
    Vector Time (GMT): 2019/235/03:38:33.000
    Vector Time (MET): N/A
    Weight (LBS)     : 937174.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4359085.70                 A    =         6797541.32  meter
     Y    =       -4586337.30  meter          E    =           .0002556
     Z    =       -2486759.69                 I    =           51.84069
     XDOT =       5128.128121                 Wp   =          332.65932
     YDOT =      -1982.425214  meter/sec      RA   =           28.46713  deg
     ZDOT =      -5328.609280                 TA   =          235.06334
                                              MA   =          235.08735
                                              Ha   =            226.945  n.mi
                                              Hp   =            222.037
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14301462.27                 X    =        -4295396.71
     Y    =      -15047038.40  feet           Y    =        -4634727.57  meter
     Z    =       -8158660.40                 Z    =        -2507779.74
     XDOT =      16824.567326                 XDOT =        5175.798399
     YDOT =      -6504.019731  feet/sec       YDOT =       -1924.812345  meter/sec
     ZDOT =     -17482.313910                 ZDOT =       -5303.583032
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19257047.19                 X    =        -5869547.98
     Y    =       -7651728.24  feet           Y    =        -2332246.77  meter
     Z    =       -8253854.60                 Z    =        -2515774.88
     XDOT =      12070.956940                 XDOT =        3679.227675
     YDOT =     -11628.605693  feet/sec       YDOT =       -3544.399015  meter/sec
     ZDOT =     -17368.205034                 ZDOT =       -5293.828894
  
  
    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   19235.17896763  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6433  28.9367 0007704 317.7620  42.2936 15.50392030 25644
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19235.17896763   =   yrday.fracday
    Element set:     902
    Inclination:       51.6433  deg
    RA of node:        28.9367  deg
    Eccentricity:     .0007704     
    Arg of perigee:   317.7620  deg
    Mean anomaly:      42.2936  deg
    Mean motion:   15.50392030  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2564
    Checksum:              314
 
 
    Coasting Arc #4 (Orbit 2571)
    ---------------------------------------
 
    Vector Time (GMT): 2019/235/16:24:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 937174.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4363966.29                 A    =         6790625.56  meter
     Y    =       -2066831.57  meter          E    =           .0005663
     Z    =       -4778377.02                 I    =           51.80233
     XDOT =       5250.508104                 Wp   =           70.51231
     YDOT =       4885.460271  meter/sec      RA   =           25.79538  deg
     ZDOT =       2686.436801                 TA   =          225.97412
                                              MA   =          226.02079
                                              Ha   =            226.894  n.mi
                                              Hp   =            222.162
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14317474.72                 X    =         4409964.50
     Y    =       -6780943.48  feet           Y    =        -2017773.40  meter
     Z    =      -15677089.96                 Z    =        -4757066.86
     XDOT =      17226.076457                 XDOT =        5182.438070
     YDOT =      16028.412962  feet/sec       YDOT =        4943.794525  meter/sec
     ZDOT =       8813.769033                 ZDOT =        2711.776437
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7490342.46                 X    =        -2283056.38
     Y    =       14067846.85  feet           Y    =         4287879.72  meter
     Z    =      -15579887.07                 Z    =        -4748749.58
     XDOT =     -22320.752501                 XDOT =       -6803.365362
     YDOT =      -2012.520337  feet/sec       YDOT =        -613.416199  meter/sec
     ZDOT =       8928.585297                 ZDOT =        2721.432799
  
  
    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   19235.69462492  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6438  26.3787 0007418 316.9241  43.1337 15.50416771 25722
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19235.69462492   =   yrday.fracday
    Element set:     903
    Inclination:       51.6438  deg
    RA of node:        26.3787  deg
    Eccentricity:     .0007418     
    Arg of perigee:   316.9241  deg
    Mean anomaly:      43.1337  deg
    Mean motion:   15.50416771  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2572
    Checksum:              318
 
 
    Coasting Arc #5 (Orbit 2580)
    ---------------------------------------
 
    Vector Time (GMT): 2019/236/05:30:52.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952577.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3547364.70                 A    =         6789381.93  meter
     Y    =        2818121.52  meter          E    =           .0009333
     Z    =        5059617.84                 I    =           51.78299
     XDOT =      -6093.649066                 Wp   =          358.33046
     YDOT =      -4231.338407  meter/sec      RA   =           23.10073  deg
     ZDOT =      -1906.544052                 TA   =          110.18950
                                              MA   =          110.08909
                                              Ha   =            227.119  n.mi
                                              Hp   =            221.860
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11638335.63                 X    =        -3603190.83
     Y    =        9245805.52  feet           Y    =         2778140.17  meter
     Z    =       16599796.05                 Z    =         5042250.58
     XDOT =     -19992.286963                 XDOT =       -6036.619230
     YDOT =     -13882.343855  feet/sec       YDOT =       -4299.162975  meter/sec
     ZDOT =      -6255.065788                 ZDOT =       -1936.006163
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         584459.43                 X    =          178143.23
     Y    =       14940609.45  feet           Y    =         4553897.76  meter
     Z    =       16520460.08                 Z    =         5035436.23
     XDOT =     -21862.677275                 XDOT =       -6663.744034
     YDOT =       7952.345805  feet/sec       YDOT =        2423.875001  meter/sec
     ZDOT =      -6388.706287                 ZDOT =       -1947.277676
  
  
    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   19236.27473932  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6449  23.5060 0007896 320.8831  39.1748 15.50437349 25811
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19236.27473932   =   yrday.fracday
    Element set:     904
    Inclination:       51.6449  deg
    RA of node:        23.5060  deg
    Eccentricity:     .0007896     
    Arg of perigee:   320.8831  deg
    Mean anomaly:      39.1748  deg
    Mean motion:   15.50437349  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2581
    Checksum:              324
 
 
    Coasting Arc #6 (Orbit 2595)
    ---------------------------------------
 
    Vector Time (GMT): 2019/237/05:30:52.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952577.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3770752.72                 A    =         6790167.27  meter
     Y    =       -2824074.24  meter          E    =           .0007344
     Z    =       -4894708.39                 I    =           51.75366
     XDOT =       6085.992300                 Wp   =           65.98752
     YDOT =       3982.822382  meter/sec      RA   =           18.14997  deg
     ZDOT =       2396.292369                 TA   =          227.46197
                                              MA   =          227.52400
                                              Ha   =            227.338  n.mi
                                              Hp   =            221.740
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12371235.94                 X    =         3825827.71
     Y    =       -9265335.45  feet           Y    =        -2781598.95  meter
     Z    =      -16058754.56                 Z    =        -4876257.91
     XDOT =      19967.166337                 XDOT =        6029.363125
     YDOT =      13067.002564  feet/sec       YDOT =        4050.563528  meter/sec
     ZDOT =       7861.851603                 ZDOT =        2425.718228
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -439318.85                 X    =         -133904.39
     Y    =      -15537059.42  feet           Y    =        -4735695.71  meter
     Z    =      -15974489.07                 Z    =        -4869024.27
     XDOT =      20989.656700                 XDOT =        6397.647362
     YDOT =      -8794.425028  feet/sec       YDOT =       -2680.540749  meter/sec
     ZDOT =       7995.343900                 ZDOT =        2436.980821
  
  
    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   19237.24159795  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6444  18.7132 0007878 325.2106  34.8529 15.50407099 25960
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19237.24159795   =   yrday.fracday
    Element set:     905
    Inclination:       51.6444  deg
    RA of node:        18.7132  deg
    Eccentricity:     .0007878     
    Arg of perigee:   325.2106  deg
    Mean anomaly:      34.8529  deg
    Mean motion:   15.50407099  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2596
    Checksum:              330
 
 
    Coasting Arc #7 (Orbit 2611)
    ---------------------------------------
 
    Vector Time (GMT): 2019/238/05:30:52.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952577.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4021052.66                 A    =         6790955.31  meter
     Y    =        2846746.47  meter          E    =           .0010848
     Z    =        4675893.24                 I    =           51.72394
     XDOT =      -6023.493724                 Wp   =           17.29457
     YDOT =      -3750.564886  meter/sec      RA   =           13.19795  deg
     ZDOT =      -2884.699483                 TA   =          101.43441
                                              MA   =          101.31255
                                              Ha   =            227.446  n.mi
                                              Hp   =            221.440
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13192430.00                 X    =        -4075299.62
     Y    =        9339719.38  feet           Y    =         2801476.76  meter
     Z    =       15340857.07                 Z    =         4656229.00
     XDOT =     -19762.118517                 XDOT =       -5967.094022
     YDOT =     -12305.002908  feet/sec       YDOT =       -3817.608386  meter/sec
     ZDOT =      -9464.237148                 ZDOT =       -2913.822207
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         311766.61                 X    =           95026.46
     Y    =       16245621.19  feet           Y    =         4951665.34  meter
     Z    =       15251067.40                 Z    =         4648525.34
     XDOT =     -20030.506024                 XDOT =       -6105.298236
     YDOT =       9429.942974  feet/sec       YDOT =        2874.246618  meter/sec
     ZDOT =      -9596.368099                 ZDOT =       -2924.972996
  
  
    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   19238.27291114  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6438  13.6013 0007988 328.7983  31.2693 15.50440746 26126
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19238.27291114   =   yrday.fracday
    Element set:     906
    Inclination:       51.6438  deg
    RA of node:        13.6013  deg
    Eccentricity:     .0007988     
    Arg of perigee:   328.7983  deg
    Mean anomaly:      31.2693  deg
    Mean motion:   15.50440746  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2612
    Checksum:              313
 
 
    Coasting Arc #8 (Orbit 2626)
    ---------------------------------------
 
    Vector Time (GMT): 2019/239/05:30:52.000
    Vector Time (MET): N/A
    Weight (LBS)     : 952577.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4227486.74                 A    =         6791963.96  meter
     Y    =       -2929499.96  meter          E    =           .0006071
     Z    =       -4437670.04                 I    =           51.69414
     XDOT =       5930.494184                 Wp   =           50.01549
     YDOT =       3519.547874  meter/sec      RA   =            8.24391  deg
     ZDOT =       3333.028500                 TA   =          253.63001
                                              MA   =          253.69676
                                              Ha   =            227.629  n.mi
                                              Hp   =            221.366
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13869707.16                 X    =         4281486.49
     Y    =       -9611220.36  feet           Y    =        -2881923.18  meter
     Z    =      -14559284.90                 Z    =        -4417003.71
     XDOT =      19457.001917                 XDOT =        5874.507054
     YDOT =      11547.073078  feet/sec       YDOT =        3585.553701  meter/sec
     ZDOT =      10935.132874                 ZDOT =        3361.700317
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -452765.36                 X    =         -138002.88
     Y    =      -16949274.97  feet           Y    =        -5166139.01  meter
     Z    =      -14464929.71                 Z    =        -4408910.58
     XDOT =      19006.318272                 XDOT =        5793.125809
     YDOT =      -9931.808366  feet/sec       YDOT =       -3027.215190  meter/sec
     ZDOT =      11065.232368                 ZDOT =        3372.682826
  
  
    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   19239.23976875  .00016717  00000-0  10270-3 0  9075
    2 25544  51.6437   8.8083 0007955 331.9401  28.1320 15.50406913 26279
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19239.23976875   =   yrday.fracday
    Element set:     907
    Inclination:       51.6437  deg
    RA of node:         8.8083  deg
    Eccentricity:     .0007955     
    Arg of perigee:   331.9401  deg
    Mean anomaly:      28.1320  deg
    Mean motion:   15.50406913  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2627
    Checksum:              318
 
 
    Coasting Arc #9 (Orbit 2632)
    ---------------------------------------
 
    Vector Time (GMT): 2019/239/14:44:31.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2855484.30                 A    =         6789770.12  meter
     Y    =       -3640020.19  meter          E    =           .0008978
     Z    =       -4975769.71                 I    =           51.67453
     XDOT =       6914.132200                 Wp   =           68.33132
     YDOT =       2484.131249  meter/sec      RA   =            6.34315  deg
     ZDOT =       2156.970845                 TA   =          222.67773
                                              MA   =          222.74750
                                              Ha   =            227.472  n.mi
                                              Hp   =            221.336
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9368386.82                 X    =         2920144.97
     Y    =      -11942323.44  feet           Y    =        -3607726.51  meter
     Z    =      -16324703.76                 Z    =        -4961742.09
     XDOT =      22684.160760                 XDOT =        6875.362861
     YDOT =       8150.036905  feet/sec       YDOT =        2561.233123  meter/sec
     ZDOT =       7076.676000                 ZDOT =        2190.462458
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5871375.48                 X    =        -1789595.24
     Y    =       14071435.59  feet           Y    =         4288973.57  meter
     Z    =      -16260484.74                 Z    =        -4956195.75
     XDOT =     -22973.463043                 XDOT =       -7002.311535
     YDOT =      -1256.644095  feet/sec       YDOT =        -383.025120  meter/sec
     ZDOT =       7228.816749                 ZDOT =        2203.343345
  
  
    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   19239.62651089  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6440   6.8886 0007518 332.4665  27.6087 15.50420552 26331
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19239.62651089   =   yrday.fracday
    Element set:     908
    Inclination:       51.6440  deg
    RA of node:         6.8886  deg
    Eccentricity:     .0007518     
    Arg of perigee:   332.4665  deg
    Mean anomaly:      27.6087  deg
    Mean motion:   15.50420552  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2633
    Checksum:              321
 
 
    Coasting Arc #10 (Orbit 2640)
    ---------------------------------------
 
    Vector Time (GMT): 2019/240/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -662154.23                 A    =         6788171.35  meter
     Y    =        4169858.54  meter          E    =           .0008025
     Z    =        5316495.35                 I    =           51.65323
     XDOT =      -7614.531322                 Wp   =          353.73397
     YDOT =       -786.580705  meter/sec      RA   =            3.98083  deg
     ZDOT =       -323.686131                 TA   =           99.39925
                                              MA   =           99.30851
                                              Ha   =            227.678  n.mi
                                              Hp   =            221.053
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2172422.02                 X    =         -734557.70
     Y    =       13680638.26  feet           Y    =         4162048.97  meter
     Z    =       17442570.06                 Z    =         5313103.11
     XDOT =     -24982.058142                 XDOT =       -7603.597367
     YDOT =      -2580.645357  feet/sec       YDOT =        -871.670614  meter/sec
     ZDOT =      -1061.962373                 ZDOT =        -360.647460
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         -89720.68                 X    =          -27346.86
     Y    =       13871728.27  feet           Y    =         4228102.78  meter
     Z    =       17426693.20                 Z    =         5311656.09
     XDOT =     -24055.867856                 XDOT =       -7332.228522
     YDOT =       1421.673841  feet/sec       YDOT =         433.326187  meter/sec
     ZDOT =      -1230.069146                 ZDOT =        -374.925076
  
  
    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   19240.14216674  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6437   4.3349 0007953 335.5524  24.5248 15.50435038 26414
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19240.14216674   =   yrday.fracday
    Element set:     909
    Inclination:       51.6437  deg
    RA of node:         4.3349  deg
    Eccentricity:     .0007953     
    Arg of perigee:   335.5524  deg
    Mean anomaly:      24.5248  deg
    Mean motion:   15.50435038  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2641
    Checksum:              301
 
 
    Coasting Arc #11 (Orbit 2655)
    ---------------------------------------
 
    Vector Time (GMT): 2019/241/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         884450.42                 A    =         6788460.95  meter
     Y    =       -4192920.34  meter          E    =           .0013010
     Z    =       -5274350.80                 I    =           51.62142
     XDOT =       7588.011460                 Wp   =           63.23938
     YDOT =        542.418841  meter/sec      RA   =          359.02057  deg
     ZDOT =        848.561669                 TA   =          214.84759
                                              MA   =          214.93284
                                              Ha   =            227.854  n.mi
                                              Hp   =            220.860
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2901740.23                 X    =          956890.48
     Y    =      -13756300.32  feet           Y    =        -4182624.83  meter
     Z    =      -17304300.52                 Z    =        -5269878.55
     XDOT =      24895.050721                 XDOT =        7577.260267
     YDOT =       1779.589372  feet/sec       YDOT =         627.213226  meter/sec
     ZDOT =       2783.994977                 ZDOT =         885.394509
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         554859.40                 X    =          169121.14
     Y    =      -14073629.16  feet           Y    =        -4289642.17  meter
     Z    =      -17283512.51                 Z    =        -5268014.61
     XDOT =      23775.334298                 XDOT =        7246.721894
     YDOT =      -2657.753503  feet/sec       YDOT =        -810.083268  meter/sec
     ZDOT =       2951.534660                 ZDOT =         899.627764
  
  
    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   19241.10902117  .00016717  00000-0  10270-3 0  9106
    2 25544  51.6446 359.5423 0007953 340.5154  19.5691 15.50412096 26568
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19241.10902117   =   yrday.fracday
    Element set:     910
    Inclination:       51.6446  deg
    RA of node:       359.5423  deg
    Eccentricity:     .0007953     
    Arg of perigee:   340.5154  deg
    Mean anomaly:      19.5691  deg
    Mean motion:   15.50412096  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2656
    Checksum:              298
 
 
    Coasting Arc #12 (Orbit 2671)
    ---------------------------------------
 
    Vector Time (GMT): 2019/242/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1143067.30                 A    =         6788795.53  meter
     Y    =        4244186.06  meter          E    =           .0010390
     Z    =        5174756.63                 I    =           51.58905
     XDOT =      -7528.057471                 Wp   =            7.32368
     YDOT =       -322.844404  meter/sec      RA   =          354.05878  deg
     ZDOT =      -1387.720872                 TA   =           96.10039
                                              MA   =           95.98200
                                              Ha   =            227.966  n.mi
                                              Hp   =            220.640
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3750220.81                 X    =        -1215577.65
     Y    =       13924494.94  feet           Y    =         4230998.28  meter
     Z    =       16977548.00                 Z    =         5169027.85
     XDOT =     -24698.351284                 XDOT =       -7517.147194
     YDOT =      -1059.200799  feet/sec       YDOT =        -406.967504  meter/sec
     ZDOT =      -4552.890001                 ZDOT =       -1424.262102
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1110736.78                 X    =         -338552.57
     Y    =       14409066.23  feet           Y    =         4391883.39  meter
     Z    =       16951044.97                 Z    =         5166678.51
     XDOT =     -23358.779765                 XDOT =       -7119.756072
     YDOT =       3791.154145  feet/sec       YDOT =        1155.543783  meter/sec
     ZDOT =      -4719.114409                 ZDOT =       -1438.386072
  
  
    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   19242.14032978  .00016717  00000-0  10270-3 0  9111
    2 25544  51.6442 354.4309 0008024 343.2658  16.8227 15.50441897 26724
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19242.14032978   =   yrday.fracday
    Element set:     911
    Inclination:       51.6442  deg
    RA of node:       354.4309  deg
    Eccentricity:     .0008024     
    Arg of perigee:   343.2658  deg
    Mean anomaly:      16.8227  deg
    Mean motion:   15.50441897  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2672
    Checksum:              309
 
 
    Coasting Arc #13 (Orbit 2686)
    ---------------------------------------
 
    Vector Time (GMT): 2019/243/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1343588.65                 A    =         6789428.72  meter
     Y    =       -4342159.43  meter          E    =           .0011564
     Z    =       -5051301.22                 I    =           51.55852
     XDOT =       7417.078323                 Wp   =           66.10484
     YDOT =        101.659455  meter/sec      RA   =          349.09503  deg
     ZDOT =       1893.486152                 TA   =          222.25846
                                              MA   =          222.34763
                                              Ha   =            228.085  n.mi
                                              Hp   =            220.545
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4408099.25                 X    =         1416580.08
     Y    =      -14245929.88  feet           Y    =        -4326726.71  meter
     Z    =      -16572510.57                 Z    =        -5044597.09
     XDOT =      24334.246468                 XDOT =        7406.192939
     YDOT =        333.528396  feet/sec       YDOT =         184.541721  meter/sec
     ZDOT =       6212.224908                 ZDOT =        1929.488486
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1436023.82                 X    =          437700.06
     Y    =      -14877509.99  feet           Y    =        -4534665.05  meter
     Z    =      -16541568.72                 Z    =        -5041870.15
     XDOT =      22738.292929                 XDOT =        6930.631685
     YDOT =      -4865.101573  feet/sec       YDOT =       -1482.882959  meter/sec
     ZDOT =       6376.005843                 ZDOT =        1943.406581
  
  
    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   19243.10718231  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6449 349.6387 0008031 346.5325  13.5610 15.50415328 26874
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19243.10718231   =   yrday.fracday
    Element set:     912
    Inclination:       51.6449  deg
    RA of node:       349.6387  deg
    Eccentricity:     .0008031     
    Arg of perigee:   346.5325  deg
    Mean anomaly:      13.5610  deg
    Mean motion:   15.50415328  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2687
    Checksum:              300
 
 
    Coasting Arc #14 (Orbit 2702)
    ---------------------------------------
 
    Vector Time (GMT): 2019/244/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1574164.11                 A    =         6790080.89  meter
     Y    =        4467190.92  meter          E    =           .0012493
     Z    =        4865771.18                 I    =           51.52886
     XDOT =      -7272.186276                 Wp   =           21.53970
     YDOT =         76.786545  meter/sec      RA   =          344.12898  deg
     ZDOT =      -2409.830807                 TA   =           92.21952
                                              MA   =           92.07646
                                              Ha   =            228.217  n.mi
                                              Hp   =            220.260
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5164580.40                 X    =        -1647635.48
     Y    =       14656138.18  feet           Y    =         4449177.11  meter
     Z    =       15963816.19                 Z    =         4857945.74
     XDOT =     -23858.878859                 XDOT =       -7260.798957
     YDOT =        251.924359  feet/sec       YDOT =          -4.472700  meter/sec
     ZDOT =      -7906.269051                 ZDOT =       -2445.128304
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1819983.53                 X    =         -554730.98
     Y    =       15469729.30  feet           Y    =         4715173.49  meter
     Z    =       15927769.45                 Z    =         4854784.13
     XDOT =     -22003.139607                 XDOT =       -6706.556952
     YDOT =       5762.260695  feet/sec       YDOT =        1756.337060  meter/sec
     ZDOT =      -8066.845441                 ZDOT =       -2458.774491
  
  
    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   19244.13848690  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6452 344.5268 0008172 350.0897  10.0091 15.50454867 27035
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19244.13848690   =   yrday.fracday
    Element set:     913
    Inclination:       51.6452  deg
    RA of node:       344.5268  deg
    Eccentricity:     .0008172     
    Arg of perigee:   350.0897  deg
    Mean anomaly:      10.0091  deg
    Mean motion:   15.50454867  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2703
    Checksum:              309
 
 
    Coasting Arc #15 (Orbit 2717)
    ---------------------------------------
 
    Vector Time (GMT): 2019/245/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1729480.20                 A    =         6791006.23  meter
     Y    =       -4628353.16  meter          E    =           .0010081
     Z    =       -4664387.97                 I    =           51.49892
     XDOT =       7089.724901                 Wp   =           62.36968
     YDOT =       -245.673548  meter/sec      RA   =          339.16157  deg
     ZDOT =       2881.895518                 TA   =          236.32831
                                              MA   =          236.42450
                                              Ha   =            228.372  n.mi
                                              Hp   =            220.144
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5674147.64                 X    =         1803764.12
     Y    =      -15184885.69  feet           Y    =        -4608597.93  meter
     Z    =      -15303110.13                 Z    =        -4655806.05
     XDOT =      23260.252301                 XDOT =        7077.946606
     YDOT =       -806.015578  feet/sec       YDOT =        -166.456865  meter/sec
     ZDOT =       9455.037790                 ZDOT =        2916.305951
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1915156.92                 X    =          583739.83
     Y    =      -16134315.46  feet           Y    =        -4917739.35  meter
     Z    =      -15263614.35                 Z    =        -4652349.66
     XDOT =      21129.038240                 XDOT =        6440.130856
     YDOT =      -6555.710628  feet/sec       YDOT =       -1998.180599  meter/sec
     ZDOT =       9611.580078                 ZDOT =        2929.609608
  
  
    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   19245.10533589  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6443 339.7344 0008163 354.1495   5.9559 15.50418285 27187
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19245.10533589   =   yrday.fracday
    Element set:     914
    Inclination:       51.6443  deg
    RA of node:       339.7344  deg
    Eccentricity:     .0008163     
    Arg of perigee:   354.1495  deg
    Mean anomaly:       5.9559  deg
    Mean motion:   15.50418285  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2718
    Checksum:              328
 
 
    Coasting Arc #16 (Orbit 2733)
    ---------------------------------------
 
    Vector Time (GMT): 2019/246/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1906944.42                 A    =         6791913.66  meter
     Y    =        4811543.94  meter          E    =           .0014221
     Z    =        4397373.58                 I    =           51.47096
     XDOT =      -6877.607035                 Wp   =           36.59389
     YDOT =        357.132809  meter/sec      RA   =          334.19259  deg
     ZDOT =      -3356.470413                 TA   =           87.54557
                                              MA   =           87.38277
                                              Ha   =            228.466  n.mi
                                              Hp   =            219.887
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6256379.32                 X    =        -1981966.73
     Y    =       15785905.31  feet           Y    =         4789799.98  meter
     Z    =       14427078.69                 Z    =         4387927.82
     XDOT =     -22564.327543                 XDOT =       -6864.785599
     YDOT =       1171.695569  feet/sec       YDOT =         280.294013  meter/sec
     ZDOT =     -11012.042038                 ZDOT =       -3389.848072
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2037913.51                 X    =         -621156.04
     Y    =       16894833.90  feet           Y    =         5149545.37  meter
     Z    =       14383642.93                 Z    =         4384134.37
     XDOT =     -20182.833557                 XDOT =       -6151.727668
     YDOT =       7117.094088  feet/sec       YDOT =        2169.290278  meter/sec
     ZDOT =     -11163.883991                 ZDOT =       -3402.751840
  
  
    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   19246.13663859  .00016717  00000-0  10270-3 0  9156
    2 25544  51.6438 334.6225 0008258 357.4503   2.6605 15.50456933 27340
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19246.13663859   =   yrday.fracday
    Element set:     915
    Inclination:       51.6438  deg
    RA of node:       334.6225  deg
    Eccentricity:     .0008258     
    Arg of perigee:   357.4503  deg
    Mean anomaly:       2.6605  deg
    Mean motion:   15.50456933  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2734
    Checksum:              320
 
 
    Coasting Arc #17 (Orbit 2748)
    ---------------------------------------
 
    Vector Time (GMT): 2019/247/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1996845.02                 A    =         6792990.57  meter
     Y    =       -5015887.98  meter          E    =           .0009158
     Z    =       -4124876.54                 I    =           51.44456
     XDOT =       6646.101127                 Wp   =           50.31580
     YDOT =       -452.652863  meter/sec      RA   =          329.22168  deg
     ZDOT =       3779.128588                 TA   =          258.75573
                                              MA   =          258.85867
                                              Ha   =            228.573  n.mi
                                              Hp   =            219.820
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6551328.80                 X    =         2072822.08
     Y    =      -16456325.40  feet           Y    =        -4993133.26  meter
     Z    =      -13533059.52                 Z    =        -4114991.81
     XDOT =      21804.793725                 XDOT =        6632.311957
     YDOT =      -1485.081573  feet/sec       YDOT =        -378.408378  meter/sec
     ZDOT =      12398.715841                 ZDOT =        3811.379397
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1839568.94                 X    =          560700.61
     Y    =      -17651473.47  feet           Y    =        -5380169.11  meter
     Z    =      -13487613.77                 Z    =        -4111024.68
     XDOT =      19179.142428                 XDOT =        5845.802612
     YDOT =      -7558.767035  feet/sec       YDOT =       -2303.912192  meter/sec
     ZDOT =      12545.431242                 ZDOT =        3823.847443
  
  
    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   19247.10348520  .00016717  00000-0  10270-3 0  9160
    2 25544  51.6436 329.8295 0008203    .5066 359.6091 15.50422045 27498
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19247.10348520   =   yrday.fracday
    Element set:     916
    Inclination:       51.6436  deg
    RA of node:       329.8295  deg
    Eccentricity:     .0008203     
    Arg of perigee:      .5066  deg
    Mean anomaly:     359.6091  deg
    Mean motion:   15.50422045  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2749
    Checksum:              302
 
 
    Coasting Arc #18 (Orbit 2764)
    ---------------------------------------
 
    Vector Time (GMT): 2019/248/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933315.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2105122.52                 A    =         6794029.89  meter
     Y    =        5234262.73  meter          E    =           .0015478
     Z    =        3783359.70                 I    =           51.42051
     XDOT =      -6391.879367                 Wp   =           50.89969
     YDOT =        477.417308  meter/sec      RA   =          324.24910  deg
     ZDOT =      -4195.893591                 TA   =           83.66482
                                              MA   =           83.48856
                                              Ha   =            228.699  n.mi
                                              Hp   =            219.540
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6906569.95                 X    =        -2181874.57
     Y    =       17172777.99  feet           Y    =         5210292.76  meter
     Z    =       12412597.43                 Z    =         3772947.19
     XDOT =     -20970.732830                 XDOT =       -6376.361599
     YDOT =       1566.329752  feet/sec       YDOT =         406.025425  meter/sec
     ZDOT =     -13766.055087                 ZDOT =       -4226.905282
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1658495.92                 X    =         -505509.56
     Y    =       18467275.47  feet           Y    =         5628825.56  meter
     Z    =       12364736.76                 Z    =         3768771.77
     XDOT =     -18158.817141                 XDOT =       -5534.807465
     YDOT =       7727.357544  feet/sec       YDOT =        2355.298580  meter/sec
     ZDOT =     -13907.129731                 ZDOT =       -4238.893142
  
  
    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   19248.13478393  .00016717  00000-0  10270-3 0  9177
    2 25544  51.6439 324.7165 0008405   4.1981 355.9238 15.50458189 27659
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19248.13478393   =   yrday.fracday
    Element set:     917
    Inclination:       51.6439  deg
    RA of node:       324.7165  deg
    Eccentricity:     .0008405     
    Arg of perigee:     4.1981  deg
    Mean anomaly:     355.9238  deg
    Mean motion:   15.50458189  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2765
    Checksum:              340
 
             

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