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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15282.6
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   79.0
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.582
   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 
   ------------------------------------------------------------------------
   120/03:18:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.1  
   000/00:00:00.000           0.0               0.0              213.0  
   
   124/09:52:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.1  
   000/00:00:00.000           0.0               0.0              213.0  
   
   131/03:18:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.5  
   000/00:00:00.000           0.0               0.0              213.6  
   
 
 
    Coasting Arc #1 (Orbit 1401)
    ---------------------------------------
 
    Vector Time (GMT): 2017/118/12:07:28.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3400675.74                 A    =         6778991.37  meter
     Y    =       -2986300.23  meter          E    =           .0018998
     Z    =       -5064247.23                 I    =           51.26297
     XDOT =       3268.821602                 Wp   =          103.62664
     YDOT =      -6694.472073  meter/sec      RA   =          285.14019  deg
     ZDOT =       1753.756341                 TA   =          183.45018
                                              MA   =          183.46330
                                              Ha   =            223.394  n.mi
                                              Hp   =            212.784
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11157072.64                 X    =        -3342429.25
     Y    =       -9797572.92  feet           Y    =        -3024003.18  meter
     Z    =      -16614984.34                 Z    =        -5080625.56
     XDOT =      10724.480322                 XDOT =        3334.918919
     YDOT =     -21963.491054  feet/sec       YDOT =       -6657.548337  meter/sec
     ZDOT =       5753.793771                 ZDOT =        1769.796106
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14733514.70                 X    =        -4490775.28
     Y    =       -1006893.09  feet           Y    =         -306901.01  meter
     Z    =      -16686525.11                 Z    =        -5086052.85
     XDOT =      -5032.355356                 XDOT =       -1533.861913
     YDOT =     -22841.882788  feet/sec       YDOT =       -6962.205874  meter/sec
     ZDOT =       5825.521433                 ZDOT =        1775.618933
  
  
    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   17118.51821628  .00016717  00000-0  10270-3 0  9008
    2 25544  51.6390 285.8707 0005770 104.7738 255.4055 15.53927297 14025
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17118.51821628   =   yrday.fracday
    Element set:     900
    Inclination:       51.6390  deg
    RA of node:       285.8707  deg
    Eccentricity:     .0005770     
    Arg of perigee:   104.7738  deg
    Mean anomaly:     255.4055  deg
    Mean motion:   15.53927297  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1402
    Checksum:              317
 
 
    Coasting Arc #2 (Orbit 1417)
    ---------------------------------------
 
    Vector Time (GMT): 2017/119/12:07:28.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2730477.24                 A    =         6781974.31  meter
     Y    =        4442761.54  meter          E    =           .0014649
     Z    =        4324111.88                 I    =           51.26402
     XDOT =      -3818.258234                 Wp   =           85.31336
     YDOT =       5702.385889  meter/sec      RA   =          280.12135  deg
     ZDOT =      -3436.544831                 TA   =           39.77122
                                              MA   =           39.66393
                                              Ha   =            223.335  n.mi
                                              Hp   =            212.979
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8958258.67                 X    =         2659589.41
     Y    =       14575989.31  feet           Y    =         4472899.12  meter
     Z    =       14186718.77                 Z    =         4337203.86
     XDOT =     -12527.093942                 XDOT =       -3865.046679
     YDOT =      18708.615121  feet/sec       YDOT =        5659.426015  meter/sec
     ZDOT =     -11274.753382                 ZDOT =       -3455.206577
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16027781.17                 X    =         4885267.70
     Y    =        5848433.88  feet           Y    =         1782602.65  meter
     Z    =       14243556.58                 Z    =         4341436.05
     XDOT =       2383.336030                 XDOT =         726.440822
     YDOT =      21219.414569  feet/sec       YDOT =        6467.677560  meter/sec
     ZDOT =     -11357.841701                 ZDOT =       -3461.870150
  
  
    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   17119.54718229  .00016717  00000-0  10270-3 0  9015
    2 25544  51.6378 280.7424 0005784 109.0002 251.1778 15.53903632 14187
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17119.54718229   =   yrday.fracday
    Element set:     901
    Inclination:       51.6378  deg
    RA of node:       280.7424  deg
    Eccentricity:     .0005784     
    Arg of perigee:   109.0002  deg
    Mean anomaly:     251.1778  deg
    Mean motion:   15.53903632  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1418
    Checksum:              306
 
 
    Coasting Arc #3 (Orbit 1427)
    ---------------------------------------
 
    Vector Time (GMT): 2017/120/03:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4188030.90                 A    =         6779715.81  meter
     Y    =       -2208095.15  meter          E    =           .0012228
     Z    =        4845072.61                 I    =           51.25638
     XDOT =       1039.363873                 Wp   =          114.99395
     YDOT =       7220.298542  meter/sec      RA   =          277.00041  deg
     ZDOT =       2382.347421                 TA   =          311.49826
                                              MA   =          311.60315
                                              Ha   =            223.073  n.mi
                                              Hp   =            212.998
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13740258.86                 X    =         4188875.80
     Y    =       -7244406.66  feet           Y    =        -2161257.18  meter
     Z    =       15895907.51                 Z    =         4865419.05
     XDOT =       3409.986459                 XDOT =         946.974917
     YDOT =      23688.643509  feet/sec       YDOT =        7231.404762  meter/sec
     ZDOT =       7816.100464                 ZDOT =        2387.172217
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6526283.23                 X    =         1989211.13
     Y    =       13993483.31  feet           Y    =         4265213.71  meter
     Z    =       15985808.35                 Z    =         4872474.39
     XDOT =     -22811.196510                 XDOT =       -6952.852696
     YDOT =       1650.337314  feet/sec       YDOT =         503.022813  meter/sec
     ZDOT =       7836.094292                 ZDOT =        2388.441540
  
  
    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   17120.19028201  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6404 277.5427 0005428 107.9665 252.2080 15.53964919 14285
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17120.19028201   =   yrday.fracday
    Element set:     902
    Inclination:       51.6404  deg
    RA of node:       277.5427  deg
    Eccentricity:     .0005428     
    Arg of perigee:   107.9665  deg
    Mean anomaly:     252.2080  deg
    Mean motion:   15.53964919  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1428
    Checksum:              302
 
 
    Coasting Arc #4 (Orbit 1442)
    ---------------------------------------
 
    Vector Time (GMT): 2017/121/03:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4251510.49                 A    =         6777980.22  meter
     Y    =         498676.88  meter          E    =           .0019818
     Z    =       -5272352.42                 I    =           51.24822
     XDOT =       -193.191440                 Wp   =           92.05935
     YDOT =      -7630.012131  meter/sec      RA   =          271.97667  deg
     ZDOT =       -568.445340                 TA   =          172.49059
                                              MA   =          172.46086
                                              Ha   =            223.217  n.mi
                                              Hp   =            212.858
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13948525.24                 X    =        -4231160.08
     Y    =        1636078.99  feet           Y    =          451247.55  meter
     Z    =      -17297744.17                 Z    =        -5292955.71
     XDOT =       -633.830184                 XDOT =        -105.095036
     YDOT =     -25032.848200  feet/sec       YDOT =       -7631.679935  meter/sec
     ZDOT =      -1864.978149                 ZDOT =        -569.170062
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1154041.29                 X    =         -351751.79
     Y    =      -13883758.72  feet           Y    =        -4231769.66  meter
     Z    =      -17388487.48                 Z    =        -5300010.98
     XDOT =      24027.098244                 XDOT =        7323.459545
     YDOT =        330.507778  feet/sec       YDOT =         100.738771  meter/sec
     ZDOT =      -1866.875881                 ZDOT =        -569.023769
  
  
    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   17121.15493125  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6412 272.7350 0005466 109.8512 250.3230 15.53952526 14434
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17121.15493125   =   yrday.fracday
    Element set:     903
    Inclination:       51.6412  deg
    RA of node:       272.7350  deg
    Eccentricity:     .0005466     
    Arg of perigee:   109.8512  deg
    Mean anomaly:     250.3230  deg
    Mean motion:   15.53952526  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1443
    Checksum:              280
 
 
    Coasting Arc #5 (Orbit 1458)
    ---------------------------------------
 
    Vector Time (GMT): 2017/122/03:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4210887.77                 A    =         6778320.07  meter
     Y    =        1244089.34  meter          E    =           .0008413
     Z    =        5156703.52                 I    =           51.24935
     XDOT =       -639.095531                 Wp   =           87.63801
     YDOT =       7537.695365  meter/sec      RA   =          266.95234  deg
     ZDOT =      -1294.469854                 TA   =           14.86463
                                              MA   =           14.83991
                                              Ha   =            222.958  n.mi
                                              Hp   =            213.058
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13815248.60                 X    =         4171614.17
     Y    =        4081657.95  feet           Y    =         1290958.65  meter
     Z    =       16918318.65                 Z    =         5177063.49
     XDOT =      -2096.770115                 XDOT =        -717.048568
     YDOT =      24729.971670  feet/sec       YDOT =        7530.112729  meter/sec
     ZDOT =      -4246.948341                 ZDOT =       -1297.763597
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4321856.96                 X    =        -1317302.00
     Y    =       13631216.73  feet           Y    =         4154794.86  meter
     Z    =       17007704.56                 Z    =         5183948.35
     XDOT =     -23695.690312                 XDOT =       -7222.446407
     YDOT =      -2185.421131  feet/sec       YDOT =        -666.116361  meter/sec
     ZDOT =      -4262.701941                 ZDOT =       -1299.271552
  
  
    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   17122.18388167  .00016717  00000-0  10270-3 0  9046
    2 25544  51.6410 267.6080 0005331 112.9094 247.2622 15.53984366 14590
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17122.18388167   =   yrday.fracday
    Element set:     904
    Inclination:       51.6410  deg
    RA of node:       267.6080  deg
    Eccentricity:     .0005331     
    Arg of perigee:   112.9094  deg
    Mean anomaly:     247.2622  deg
    Mean motion:   15.53984366  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1459
    Checksum:              310
 
 
    Coasting Arc #6 (Orbit 1473)
    ---------------------------------------
 
    Vector Time (GMT): 2017/123/03:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4110706.98                 A    =         6780886.97  meter
     Y    =       -2892458.15  meter          E    =           .0015498
     Z    =       -4566984.94                 I    =           51.26059
     XDOT =       1477.708611                 Wp   =          112.19616
     YDOT =      -6874.596140  meter/sec      RA   =          261.93095  deg
     ZDOT =       3026.422665                 TA   =          188.24500
                                              MA   =          188.27050
                                              Ha   =            223.144  n.mi
                                              Hp   =            212.958
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13486571.45                 X    =        -4055872.94
     Y    =       -9489692.10  feet           Y    =        -2938120.24  meter
     Z    =      -14983546.39                 Z    =        -4586820.42
     XDOT =       4848.125364                 XDOT =        1539.771358
     YDOT =     -22554.449278  feet/sec       YDOT =       -6857.724400  meter/sec
     ZDOT =       9929.208217                 ZDOT =        3033.751668
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9494522.37                 X    =         2893930.42
     Y    =      -13386067.67  feet           Y    =        -4080073.43  meter
     Z    =      -15070360.49                 Z    =        -4593445.88
     XDOT =      21576.194216                 XDOT =        6576.423997
     YDOT =       4096.821902  feet/sec       YDOT =        1248.711316  meter/sec
     ZDOT =       9962.594158                 ZDOT =        3036.598699
  
  
    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   17123.14851995  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6411 262.8003 0005424 115.9805 244.1907 15.53965227 14743
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17123.14851995   =   yrday.fracday
    Element set:     905
    Inclination:       51.6411  deg
    RA of node:       262.8003  deg
    Eccentricity:     .0005424     
    Arg of perigee:   115.9805  deg
    Mean anomaly:     244.1907  deg
    Mean motion:   15.53965227  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1474
    Checksum:              305
 
 
    Coasting Arc #7 (Orbit 1489)
    ---------------------------------------
 
    Vector Time (GMT): 2017/124/03:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3880123.56                 A    =         6784572.38  meter
     Y    =        4317486.47  meter          E    =           .0016999
     Z    =        3495086.22                 I    =           51.27795
     XDOT =      -2355.222090                 Wp   =           97.95143
     YDOT =       5763.106379  meter/sec      RA   =          256.91937  deg
     ZDOT =      -4488.031153                 TA   =           40.66139
                                              MA   =           40.53459
                                              Ha   =            223.036  n.mi
                                              Hp   =            213.150
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12730064.16                 X    =         3814578.40
     Y    =       14164981.85  feet           Y    =         4360510.19  meter
     Z    =       11466818.30                 Z    =         3513775.52
     XDOT =      -7727.106596                 XDOT =       -2397.690826
     YDOT =      18907.829327  feet/sec       YDOT =        5736.531183  meter/sec
     ZDOT =     -14724.511658                 ZDOT =       -4499.575374
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13949594.64                 X    =        -4251836.45
     Y    =       12893144.70  feet           Y    =         3929830.50  meter
     Z    =       11548367.65                 Z    =         3519942.46
     XDOT =     -18092.901882                 XDOT =       -5514.716494
     YDOT =      -6292.323620  feet/sec       YDOT =       -1917.900239  meter/sec
     ZDOT =     -14776.253787                 ZDOT =       -4503.802154
  
  
    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   17124.17746217  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6407 257.6731 0005420 120.5660 239.6028 15.53955752 14908
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17124.17746217   =   yrday.fracday
    Element set:     906
    Inclination:       51.6407  deg
    RA of node:       257.6731  deg
    Eccentricity:     .0005420     
    Arg of perigee:   120.5660  deg
    Mean anomaly:     239.6028  deg
    Mean motion:   15.53955752  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1490
    Checksum:              305
 
 
    Coasting Arc #8 (Orbit 1493)
    ---------------------------------------
 
    Vector Time (GMT): 2017/124/09:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1952886.90                 A    =         6783060.03  meter
     Y    =        5157253.76  meter          E    =           .0011231
     Z    =       -3958420.97                 I    =           51.27289
     XDOT =      -4509.376532                 Wp   =           95.53822
     YDOT =      -4748.961179  meter/sec      RA   =          255.59645  deg
     ZDOT =      -3973.340170                 TA   =          132.83375
                                              MA   =          132.73932
                                              Ha   =            223.093  n.mi
                                              Hp   =            213.038
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6407109.26                 X    =        -1991183.33
     Y    =       16920123.89  feet           Y    =         5135201.07  meter
     Z    =      -12986945.46                 Z    =        -3968000.65
     XDOT =     -14794.542427                 XDOT =       -4436.636602
     YDOT =     -15580.581296  feet/sec       YDOT =       -4798.981426  meter/sec
     ZDOT =     -13035.892946                 ZDOT =       -3995.068713
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3407549.83                 X    =        -1038621.19
     Y    =       17737295.25  feet           Y    =         5406327.59  meter
     Z    =      -13029940.73                 Z    =        -3971525.93
     XDOT =     -15811.695773                 XDOT =       -4819.404871
     YDOT =     -12657.552468  feet/sec       YDOT =       -3858.021992  meter/sec
     ZDOT =     -13130.751858                 ZDOT =       -4002.253166
  
  
    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   17124.43469530  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6384 256.3861 0005602 123.1667 237.0024 15.53987384 14948
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17124.43469530   =   yrday.fracday
    Element set:     907
    Inclination:       51.6384  deg
    RA of node:       256.3861  deg
    Eccentricity:     .0005602     
    Arg of perigee:   123.1667  deg
    Mean anomaly:     237.0024  deg
    Mean motion:   15.53987384  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1494
    Checksum:              315
 
 
    Coasting Arc #9 (Orbit 1509)
    ---------------------------------------
 
    Vector Time (GMT): 2017/125/09:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2749891.22                 A    =         6779703.95  meter
     Y    =       -3866288.16  meter          E    =           .0012516
     Z    =        4836576.93                 I    =           51.27039
     XDOT =       4156.847774                 Wp   =          123.76427
     YDOT =       5982.902653  meter/sec      RA   =          250.58020  deg
     ZDOT =       2407.877240                 TA   =          302.45471
                                              MA   =          302.57567
                                              Ha   =            222.962  n.mi
                                              Hp   =            213.168
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9021952.82                 X    =         2769426.77
     Y    =      -12684672.45  feet           Y    =        -3835427.66  meter
     Z    =       15868034.56                 Z    =         4849982.72
     XDOT =      13637.952016                 XDOT =        4077.940059
     YDOT =      19628.945711  feet/sec       YDOT =        6028.946200  meter/sec
     ZDOT =       7899.859710                 ZDOT =        2427.878284
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6432832.12                 X    =         1960727.23
     Y    =      -14107429.66  feet           Y    =        -4299944.56  meter
     Z    =       15927654.19                 Z    =         4854749.00
     XDOT =      15936.616533                 XDOT =        4857.480719
     YDOT =      16326.235714  feet/sec       YDOT =        4976.236646  meter/sec
     ZDOT =       7986.932762                 ZDOT =        2434.417106
  
  
    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   17125.46362797  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6380 251.2570 0005542 127.9027 232.2628 15.53995540 15109
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17125.46362797   =   yrday.fracday
    Element set:     908
    Inclination:       51.6380  deg
    RA of node:       251.2570  deg
    Eccentricity:     .0005542     
    Arg of perigee:   127.9027  deg
    Mean anomaly:     232.2628  deg
    Mean motion:   15.53995540  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1510
    Checksum:              308
 
 
    Coasting Arc #10 (Orbit 1524)
    ---------------------------------------
 
    Vector Time (GMT): 2017/126/09:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3578944.02                 A    =         6777855.85  meter
     Y    =        2344222.97  meter          E    =           .0019126
     Z    =       -5273168.80                 I    =           51.27648
     XDOT =      -3573.558559                 Wp   =           97.71239
     YDOT =      -6744.421585  meter/sec      RA   =          245.55925  deg
     ZDOT =       -577.197936                 TA   =          166.76622
                                              MA   =          166.71598
                                              Ha   =            223.041  n.mi
                                              Hp   =            213.030
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11741942.31                 X    =        -3579276.96
     Y    =        7691020.25  feet           Y    =         2304198.78  meter
     Z    =      -17300422.59                 Z    =        -5290555.29
     XDOT =     -11724.273487                 XDOT =       -3495.071300
     YDOT =     -22127.367406  feet/sec       YDOT =       -6783.944705  meter/sec
     ZDOT =      -1893.694017                 ZDOT =        -594.366551
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9847525.10                 X    =        -3001525.65
     Y    =        9868367.97  feet           Y    =         3007878.56  meter
     Z    =      -17377318.16                 Z    =        -5296606.58
     XDOT =     -15197.538865                 XDOT =       -4632.209846
     YDOT =     -18606.387624  feet/sec       YDOT =       -5671.226948  meter/sec
     ZDOT =      -1968.195141                 ZDOT =        -599.905879
  
  
    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   17126.42824766  .00016717  00000-0  10270-3 0  9092
    2 25544  51.6385 246.4506 0005685 130.5596 229.6052 15.53999155 15251
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17126.42824766   =   yrday.fracday
    Element set:     909
    Inclination:       51.6385  deg
    RA of node:       246.4506  deg
    Eccentricity:     .0005685     
    Arg of perigee:   130.5596  deg
    Mean anomaly:     229.6052  deg
    Mean motion:   15.53999155  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1525
    Checksum:              337
 
 
    Coasting Arc #11 (Orbit 1540)
    ---------------------------------------
 
    Vector Time (GMT): 2017/127/09:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4323345.29                 A    =         6778365.05  meter
     Y    =        -752742.32  meter          E    =           .0007688
     Z    =        5159232.76                 I    =           51.29260
     XDOT =       2777.229533                 Wp   =          101.97296
     YDOT =       7034.932956  meter/sec      RA   =          240.53512  deg
     ZDOT =      -1300.780911                 TA   =             .57254
                                              MA   =             .57166
                                              Ha   =            222.914  n.mi
                                              Hp   =            213.311
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14184203.70                 X    =         4306379.92
     Y    =       -2469627.02  feet           Y    =         -704490.47  meter
     Z    =       16926616.66                 Z    =         5180193.36
     XDOT =       9111.645449                 XDOT =        2704.675315
     YDOT =      23080.488702  feet/sec       YDOT =        7065.584110  meter/sec
     ZDOT =      -4267.653906                 ZDOT =       -1287.466188
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13198846.21                 X    =         4023008.33
     Y    =       -5472229.06  feet           Y    =        -1667935.42  meter
     Z    =       17018995.61                 Z    =         5187389.86
     XDOT =      13544.795645                 XDOT =        4128.453713
     YDOT =      19575.002430  feet/sec       YDOT =        5966.460741  meter/sec
     ZDOT =      -4210.147549                 ZDOT =       -1283.252973
  
  
    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   17127.45717002  .00016717  00000-0  10270-3 0  9102
    2 25544  51.6389 241.3213 0005666 134.3475 225.8142 15.53964113 15413
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17127.45717002   =   yrday.fracday
    Element set:     910
    Inclination:       51.6389  deg
    RA of node:       241.3213  deg
    Eccentricity:     .0005666     
    Arg of perigee:   134.3475  deg
    Mean anomaly:     225.8142  deg
    Mean motion:   15.53964113  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1541
    Checksum:              289
 
 
    Coasting Arc #12 (Orbit 1555)
    ---------------------------------------
 
    Vector Time (GMT): 2017/128/09:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4971177.65                 A    =         6780777.62  meter
     Y    =        -791830.15  meter          E    =           .0015187
     Z    =       -4558409.58                 I    =           51.31931
     XDOT =      -1713.109410                 Wp   =          120.13102
     YDOT =      -6808.912702  meter/sec      RA   =          235.51773  deg
     ZDOT =       3051.164830                 TA   =          180.56908
                                              MA   =          180.57081
                                              Ha   =            222.895  n.mi
                                              Hp   =            213.211
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16309637.95                 X    =        -4939810.80
     Y    =       -2597867.96  feet           Y    =         -847245.91  meter
     Z    =      -14955412.00                 Z    =        -4582482.26
     XDOT =      -5620.437696                 XDOT =       -1651.664377
     YDOT =     -22338.952436  feet/sec       YDOT =       -6827.726247  meter/sec
     ZDOT =      10010.383299                 ZDOT =        3042.992266
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16369305.58                 X    =        -4989364.34
     Y    =        1273574.34  feet           Y    =          388185.46  meter
     Z    =      -15061254.90                 Z    =        -4590670.49
     XDOT =     -10670.787988                 XDOT =       -3252.456179
     YDOT =     -19189.158486  feet/sec       YDOT =       -5848.855506  meter/sec
     ZDOT =       9975.465150                 ZDOT =        3040.521778
  
  
    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   17128.42177559  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6402 236.5142 0005527 137.9161 222.2417 15.54006534 15560
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17128.42177559   =   yrday.fracday
    Element set:     911
    Inclination:       51.6402  deg
    RA of node:       236.5142  deg
    Eccentricity:     .0005527     
    Arg of perigee:   137.9161  deg
    Mean anomaly:     222.2417  deg
    Mean motion:   15.54006534  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1556
    Checksum:              292
 
 
    Coasting Arc #13 (Orbit 1571)
    ---------------------------------------
 
    Vector Time (GMT): 2017/129/09:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5394384.36                 A    =         6784486.45  meter
     Y    =        2181001.12  meter          E    =           .0016208
     Z    =        3471301.03                 I    =           51.35050
     XDOT =        415.561285                 Wp   =          104.64742
     YDOT =       6188.831560  meter/sec      RA   =          230.50968  deg
     ZDOT =      -4520.507714                 TA   =           34.35560
                                              MA   =           34.25089
                                              Ha   =            222.771  n.mi
                                              Hp   =            213.411
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17698111.41                 X    =         5352732.69
     Y    =        7155515.48  feet           Y    =         2241091.88  meter
     Z    =       11388782.92                 Z    =         3497404.65
     XDOT =       1363.390044                 XDOT =         368.284124
     YDOT =      20304.565484  feet/sec       YDOT =        6193.214311  meter/sec
     ZDOT =     -14831.062053                 ZDOT =       -4518.603828
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18855828.47                 X    =         5747256.52
     Y    =        2501870.19  feet           Y    =          762570.03  meter
     Z    =       11503360.54                 Z    =         3506224.29
     XDOT =       6694.040152                 XDOT =        2040.343438
     YDOT =      17911.107298  feet/sec       YDOT =        5459.305504  meter/sec
     ZDOT =     -14823.635435                 ZDOT =       -4518.244081
  
  
    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   17129.45068402  .00016717  00000-0  10270-3 0  9129
    2 25544  51.6399 231.3858 0005617 141.5349 218.6205 15.53998918 15728
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17129.45068402   =   yrday.fracday
    Element set:     912
    Inclination:       51.6399  deg
    RA of node:       231.3858  deg
    Eccentricity:     .0005617     
    Arg of perigee:   141.5349  deg
    Mean anomaly:     218.6205  deg
    Mean motion:   15.53998918  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1572
    Checksum:              331
 
 
    Coasting Arc #14 (Orbit 1586)
    ---------------------------------------
 
    Vector Time (GMT): 2017/130/09:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5559830.56                 A    =         6787757.71  meter
     Y    =       -3302628.58  meter          E    =           .0007402
     Z    =       -2068461.87                 I    =           51.38374
     XDOT =       1052.218134                 Wp   =           87.64692
     YDOT =      -5213.792829  meter/sec      RA   =          225.51360  deg
     ZDOT =       5513.814414                 TA   =          249.40407
                                              MA   =          249.48348
                                              Ha   =            222.745  n.mi
                                              Hp   =            213.465
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18240913.90                 X    =        -5512438.69
     Y    =      -10835395.59  feet           Y    =        -3364537.34  meter
     Z    =       -6786292.21                 Z    =        -2095355.34
     XDOT =       3452.159231                 XDOT =        1083.657942
     YDOT =     -17105.619517  feet/sec       YDOT =       -5201.850532  meter/sec
     ZDOT =      18089.942303                 ZDOT =        5519.002135
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20433044.56                 X    =        -6227991.98
     Y    =       -5568967.31  feet           Y    =        -1697421.24  meter
     Z    =       -6904186.58                 Z    =        -2104396.07
     XDOT =      -1772.798786                 XDOT =        -540.349070
     YDOT =     -15882.272479  feet/sec       YDOT =       -4840.916652  meter/sec
     ZDOT =      18113.582376                 ZDOT =        5521.019908
  
  
    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   17130.41527930  .00016717  00000-0  10270-3 0  9134
    2 25544  51.6406 226.5788 0005479 144.9036 215.2478 15.54021358 15878
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17130.41527930   =   yrday.fracday
    Element set:     913
    Inclination:       51.6406  deg
    RA of node:       226.5788  deg
    Eccentricity:     .0005479     
    Arg of perigee:   144.9036  deg
    Mean anomaly:     215.2478  deg
    Mean motion:   15.54021358  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1587
    Checksum:              316
 
 
    Coasting Arc #15 (Orbit 1598)
    ---------------------------------------
 
    Vector Time (GMT): 2017/131/03:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2424728.46                 A    =         6777713.35  meter
     Y    =       -3489540.20  meter          E    =           .0007396
     Z    =        5275949.67                 I    =           51.36799
     XDOT =       5939.990443                 Wp   =          133.46421
     YDOT =       4834.432143  meter/sec      RA   =          221.90599  deg
     ZDOT =        462.204017                 TA   =          312.08154
                                              MA   =          312.14442
                                              Ha   =            222.489  n.mi
                                              Hp   =            213.648
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7955145.85                 X    =         2437940.66
     Y    =      -11448622.71  feet           Y    =        -3462351.55  meter
     Z    =       17309546.16                 Z    =         5287760.48
     XDOT =      19488.157623                 XDOT =        5883.243875
     YDOT =      15860.997845  feet/sec       YDOT =        4900.539833  meter/sec
     ZDOT =       1516.417378                 ZDOT =         490.921605
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12413042.66                 X    =         3783495.40
     Y    =        6200818.42  feet           Y    =         1890009.45  meter
     Z    =       17362082.79                 Z    =         5291962.83
     XDOT =     -12592.604592                 XDOT =       -3838.225880
     YDOT =      20560.994030  feet/sec       YDOT =        6266.990980  meter/sec
     ZDOT =       1642.118671                 ZDOT =         500.517771
  
  
    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   17131.18695091  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6416 222.7377 0004943 145.2733 214.8743 15.54030212 15996
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17131.18695091   =   yrday.fracday
    Element set:     914
    Inclination:       51.6416  deg
    RA of node:       222.7377  deg
    Eccentricity:     .0004943     
    Arg of perigee:   145.2733  deg
    Mean anomaly:     214.8743  deg
    Mean motion:   15.54030212  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1599
    Checksum:              304
 
 
    Coasting Arc #16 (Orbit 1613)
    ---------------------------------------
 
    Vector Time (GMT): 2017/132/03:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3773941.33                 A    =         6778224.23  meter
     Y    =        2309488.47  meter          E    =           .0017490
     Z    =       -5150416.14                 I    =           51.39361
     XDOT =      -5255.219753                 Wp   =          112.97992
     YDOT =      -5377.978443  meter/sec      RA   =          216.88771  deg
     ZDOT =       1436.418794                 TA   =          170.92920
                                              MA   =          170.89756
                                              Ha   =            222.440  n.mi
                                              Hp   =            213.566
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12381697.28                 X    =        -3774467.43
     Y    =        7577061.91  feet           Y    =         2267283.02  meter
     Z    =      -16897690.75                 Z    =        -5168750.32
     XDOT =     -17241.534624                 XDOT =       -5201.668774
     YDOT =     -17644.286230  feet/sec       YDOT =       -5436.446517  meter/sec
     ZDOT =       4712.660084                 ZDOT =        1411.019836
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9374321.73                 X    =        -2857293.26
     Y    =      -10958717.32  feet           Y    =        -3340217.04  meter
     Z    =      -16978776.59                 Z    =        -5175131.10
     XDOT =      13975.551172                 XDOT =        4259.747997
     YDOT =     -19098.589183  feet/sec       YDOT =       -5821.249983  meter/sec
     ZDOT =       4601.638172                 ZDOT =        1402.579315
  
  
    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   17132.15153604  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6404 217.9285 0004867 148.5925 211.5519 15.54056156 16149
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17132.15153604   =   yrday.fracday
    Element set:     915
    Inclination:       51.6404  deg
    RA of node:       217.9285  deg
    Eccentricity:     .0004867     
    Arg of perigee:   148.5925  deg
    Mean anomaly:     211.5519  deg
    Mean motion:   15.54056156  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1614
    Checksum:              305
 
 
    Coasting Arc #17 (Orbit 1629)
    ---------------------------------------
 
    Vector Time (GMT): 2017/133/03:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916036.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4954561.16                 A    =         6780813.21  meter
     Y    =       -1126620.36  meter          E    =           .0010420
     Z    =        4480755.11                 I    =           51.42861
     XDOT =       4168.245439                 Wp   =           95.16284
     YDOT =       5594.524816  meter/sec      RA   =          211.87824  deg
     ZDOT =      -3196.849570                 TA   =           27.06025
                                              MA   =           27.00596
                                              Ha   =            222.172  n.mi
                                              Hp   =            213.790
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16255121.93                 X    =         4945025.37
     Y    =       -3696261.03  feet           Y    =        -1071268.70  meter
     Z    =       14700640.13                 Z    =         4504800.06
     XDOT =      13675.345928                 XDOT =        4120.905225
     YDOT =      18354.740210  feet/sec       YDOT =        5640.872462  meter/sec
     ZDOT =     -10488.351607                 ZDOT =       -3176.715776
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6402395.23                 X    =         1951450.07
     Y    =       15289570.63  feet           Y    =         4660261.13  meter
     Z    =       14806705.24                 Z    =         4513083.76
     XDOT =     -14619.834341                 XDOT =       -4456.125507
     YDOT =      16211.352060  feet/sec       YDOT =        4941.220108  meter/sec
     ZDOT =     -10400.533419                 ZDOT =       -3170.082586
  
  
    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   17133.18042242  .00016717  00000-0  10270-3 0  9162
    2 25544  51.6398 212.8011 0004763 152.9358 207.2043 15.54080280 16303
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17133.18042242   =   yrday.fracday
    Element set:     916
    Inclination:       51.6398  deg
    RA of node:       212.8011  deg
    Eccentricity:     .0004763     
    Arg of perigee:   152.9358  deg
    Mean anomaly:     207.2043  deg
    Mean motion:   15.54080280  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1630
    Checksum:              279
 
             

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