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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  17659.2714
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   75.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.540
   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 
   ------------------------------------------------------------------------
   017/20:15:07.803           0.7               0.8              0.8    
   N/A                        0.4              -0.1              221.6  
   000/00:00:15.606          -0.2              -0.0              214.1  
   
   018/18:52:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.8  
   000/00:00:00.000           0.0               0.0              214.1  
   
   023/19:45:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.8  
   000/00:00:00.000           0.0               0.0              213.7  
   
   029/16:58:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.0  
   000/00:00:00.000           0.0               0.0              213.4  
   
 
 
    Coasting Arc #1 (Orbit 1476)
    ---------------------------------------
 
    Vector Time (GMT): 2018/015/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905837.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3221176.16                 A    =         6776902.37  meter
     Y    =        2709845.36  meter          E    =           .0004408
     Z    =        5307650.59                 I    =           51.94725
     XDOT =      -4317.727617                 Wp   =           57.07822
     YDOT =      -6313.095794  meter/sec      RA   =           59.17900  deg
     ZDOT =        604.752764                 TA   =           27.18838
                                              MA   =           27.16531
                                              Ha   =            221.580  n.mi
                                              Hp   =            213.869
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10568163.27                 X    =        -3277020.40
     Y    =        8890568.75  feet           Y    =         2673511.30  meter
     Z    =       17413551.82                 Z    =         5291868.02
     XDOT =     -14165.773023                 XDOT =       -4249.749509
     YDOT =     -20712.256543  feet/sec       YDOT =       -6360.999538  meter/sec
     ZDOT =       1984.096994                 ZDOT =         583.943638
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12470368.95                 X    =        -3800968.45
     Y    =       -6138186.27  feet           Y    =        -1870919.18  meter
     Z    =       17342797.99                 Z    =         5286084.83
     XDOT =      12699.714597                 XDOT =        3870.873009
     YDOT =     -20472.178555  feet/sec       YDOT =       -6239.920024  meter/sec
     ZDOT =       1892.469620                 ZDOT =         576.824740
  
  
    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   18015.54922922  .00016717  00000-0  10270-3 0  9007
    2 25544  51.6405  59.6508 0003688  17.3608 342.7670 15.54317764 14777
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18015.54922922   =   yrday.fracday
    Element set:     900
    Inclination:       51.6405  deg
    RA of node:        59.6508  deg
    Eccentricity:     .0003688     
    Arg of perigee:    17.3608  deg
    Mean anomaly:     342.7670  deg
    Mean motion:   15.54317764  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1477
    Checksum:              318
 
 
    Coasting Arc #2 (Orbit 1491)
    ---------------------------------------
 
    Vector Time (GMT): 2018/016/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905837.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4220909.98                 A    =         6777541.18  meter
     Y    =       -1107721.15  meter          E    =           .0014873
     Z    =       -5198324.03                 I    =           51.93189
     XDOT =       3469.821414                 Wp   =           86.23077
     YDOT =       6682.165967  meter/sec      RA   =           54.19779  deg
     ZDOT =       1397.884255                 TA   =          197.15071
                                              MA   =          197.20102
                                              Ha   =            221.557  n.mi
                                              Hp   =            213.981
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13848129.84                 X    =         4258233.40
     Y    =       -3634255.73  feet           Y    =        -1060310.99  meter
     Z    =      -17054868.87                 Z    =        -5177730.08
     XDOT =      11383.928524                 XDOT =        3388.051680
     YDOT =      21923.116691  feet/sec       YDOT =        6720.510586  meter/sec
     ZDOT =       4586.234433                 ZDOT =        1414.541033
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9195831.35                 X    =         2802889.40
     Y    =       11114947.20  feet           Y    =         3387835.91  meter
     Z    =      -16962950.84                 Z    =        -5170307.42
     XDOT =     -14259.081653                 XDOT =       -4346.168088
     YDOT =      18885.723399  feet/sec       YDOT =        5756.368492  meter/sec
     ZDOT =       4659.297075                 ZDOT =        1420.153749
  
  
    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   18016.51364683  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6410  54.8419 0003718  19.8304 340.2992 15.54293629 14925
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18016.51364683   =   yrday.fracday
    Element set:     901
    Inclination:       51.6410  deg
    RA of node:        54.8419  deg
    Eccentricity:     .0003718     
    Arg of perigee:    19.8304  deg
    Mean anomaly:     340.2992  deg
    Mean motion:   15.54293629  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1492
    Checksum:              309
 
 
    Coasting Arc #3 (Orbit 1507)
    ---------------------------------------
 
    Vector Time (GMT): 2018/017/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905837.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5057450.97                 A    =         6780292.14  meter
     Y    =        -482993.92  meter          E    =           .0012203
     Z    =        4485181.38                 I    =           51.92102
     XDOT =      -2279.428289                 Wp   =           56.03962
     YDOT =      -6557.383378  meter/sec      RA   =           49.22042  deg
     ZDOT =      -3263.417061                 TA   =           66.73875
                                              MA   =           66.61032
                                              Ha   =            221.688  n.mi
                                              Hp   =            213.671
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16592686.91                 X    =        -5073460.35
     Y    =       -1584625.71  feet           Y    =         -539639.57  meter
     Z    =       14715162.00                 Z    =         4460575.59
     XDOT =      -7478.439267                 XDOT =       -2190.080793
     YDOT =     -21513.724992  feet/sec       YDOT =       -6582.373744  meter/sec
     ZDOT =     -10706.748888                 ZDOT =       -3274.272898
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5890349.67                 X    =        -1795378.58
     Y    =      -15695325.42  feet           Y    =        -4783935.19  meter
     Z    =       14605643.80                 Z    =         4451800.23
     XDOT =      14948.030204                 XDOT =        4556.159606
     YDOT =     -15657.215823  feet/sec       YDOT =       -4772.319383  meter/sec
     ZDOT =     -10753.987723                 ZDOT =       -3277.815458
  
  
    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   18017.54235380  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6405  49.7124 0003846  24.7294 335.4043 15.54343027 15089
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18017.54235380   =   yrday.fracday
    Element set:     902
    Inclination:       51.6405  deg
    RA of node:        49.7124  deg
    Eccentricity:     .0003846     
    Arg of perigee:    24.7294  deg
    Mean anomaly:     335.4043  deg
    Mean motion:   15.54343027  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1508
    Checksum:              289
 
 
    Coasting Arc #4 (Orbit 1512)
    ---------------------------------------
 
    Vector Time (GMT): 2018/017/20:15:15.606
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1187710.84                 A    =         6778725.66  meter
     Y    =       -4471396.53  meter          E    =           .0014639
     Z    =       -4967977.90                 I    =           51.90870
     XDOT =       6087.586055                 Wp   =           61.77886
     YDOT =       4081.605427  meter/sec      RA   =           47.55347  deg
     ZDOT =      -2216.472011                 TA   =          186.63162
                                              MA   =          186.65101
                                              Ha   =            221.591  n.mi
                                              Hp   =            214.140
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3896689.12                 X    =         1261754.27
     Y    =      -14669936.12  feet           Y    =        -4457700.47  meter
     Z    =      -16299140.10                 Z    =        -4962028.93
     XDOT =      19972.395193                 XDOT =        6052.258245
     YDOT =      13391.093920  feet/sec       YDOT =        4149.483571  meter/sec
     ZDOT =      -7271.889799                 ZDOT =       -2186.986795
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10730930.28                 X    =        -3270787.55
     Y    =      -10776188.37  feet           Y    =        -3284582.21  meter
     Z    =      -16271880.02                 Z    =        -4959669.03
     XDOT =      20793.725223                 XDOT =        6337.927448
     YDOT =      -9914.424748  feet/sec       YDOT =       -3021.916663  meter/sec
     ZDOT =      -7141.251045                 ZDOT =       -2176.653319
  
  
    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   18017.86382611  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6421  48.1103 0003580  16.4212 343.7056 15.54198369 15139
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18017.86382611   =   yrday.fracday
    Element set:     903
    Inclination:       51.6421  deg
    RA of node:        48.1103  deg
    Eccentricity:     .0003580     
    Arg of perigee:    16.4212  deg
    Mean anomaly:     343.7056  deg
    Mean motion:   15.54198369  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1513
    Checksum:              285
 
 
    Coasting Arc #5 (Orbit 1527)
    ---------------------------------------
 
    Vector Time (GMT): 2018/018/18:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5116157.39                 A    =         6780942.88  meter
     Y    =          11506.13  meter          E    =           .0011974
     Z    =        4445561.48                 I    =           51.89226
     XDOT =      -2917.524052                 Wp   =           56.44305
     YDOT =      -6264.702556  meter/sec      RA   =           42.83312  deg
     ZDOT =      -3328.514345                 TA   =           67.08880
                                              MA   =           66.96246
                                              Ha   =            221.816  n.mi
                                              Hp   =            214.079
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16785293.27                 X    =        -5137499.56
     Y    =          37749.76  feet           Y    =          -45825.75  meter
     Z    =       14585175.45                 Z    =         4420657.64
     XDOT =      -9571.929306                 XDOT =       -2831.085793
     YDOT =     -20553.486076  feet/sec       YDOT =       -6296.844877  meter/sec
     ZDOT =     -10920.322653                 ZDOT =       -3342.476669
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12857435.96                 X    =        -3918946.48
     Y    =       10938799.34  feet           Y    =         3334146.04  meter
     Z    =       14474247.74                 Z    =         4411750.71
     XDOT =     -19734.901318                 XDOT =       -6015.197922
     YDOT =      -8609.280110  feet/sec       YDOT =       -2624.108577  meter/sec
     ZDOT =     -10981.442042                 ZDOT =       -3347.143535
  
  
    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   18018.82832687  .00016717  00000-0  10270-3 0  9043
    2 25544  51.6402  43.3019 0003592  20.3748 339.7547 15.54171843 15286
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18018.82832687   =   yrday.fracday
    Element set:     904
    Inclination:       51.6402  deg
    RA of node:        43.3019  deg
    Eccentricity:     .0003592     
    Arg of perigee:    20.3748  deg
    Mean anomaly:     339.7547  deg
    Mean motion:   15.54171843  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1528
    Checksum:              313
 
 
    Coasting Arc #6 (Orbit 1542)
    ---------------------------------------
 
    Vector Time (GMT): 2018/019/18:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5805203.18                 A    =         6784688.10  meter
     Y    =        1251634.59  meter          E    =           .0007098
     Z    =       -3281701.74                 I    =           51.88082
     XDOT =       1425.058409                 Wp   =           56.09417
     YDOT =       5837.086174  meter/sec      RA   =           37.86308  deg
     ZDOT =       4758.346610                 TA   =          265.96956
                                              MA   =          266.05070
                                              Ha   =            221.761  n.mi
                                              Hp   =            214.073
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19045942.20                 X    =         5806716.06
     Y    =        4106412.69  feet           Y    =         1316560.87  meter
     Z    =      -10766737.99                 Z    =        -3253498.96
     XDOT =       4675.388480                 XDOT =        1336.567565
     YDOT =      19150.545190  feet/sec       YDOT =        5852.527272  meter/sec
     ZDOT =      15611.373392                 ZDOT =        4765.054103
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17080534.39                 X    =         5206146.88
     Y    =       -9515801.56  feet           Y    =        -2900416.32  meter
     Z    =      -10641336.94                 Z    =        -3243479.50
     XDOT =      15370.261008                 XDOT =        4684.855555
     YDOT =      10140.550589  feet/sec       YDOT =        3090.839819  meter/sec
     ZDOT =      15640.248199                 ZDOT =        4767.147651
  
  
    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   18019.79282473  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6408  38.4930 0003543  22.5574 337.5734 15.54189589 15433
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18019.79282473   =   yrday.fracday
    Element set:     905
    Inclination:       51.6408  deg
    RA of node:        38.4930  deg
    Eccentricity:     .0003543     
    Arg of perigee:    22.5574  deg
    Mean anomaly:     337.5734  deg
    Mean motion:   15.54189589  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1543
    Checksum:              330
 
 
    Coasting Arc #7 (Orbit 1558)
    ---------------------------------------
 
    Vector Time (GMT): 2018/020/18:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6125218.79                 A    =         6787983.88  meter
     Y    =       -2343567.83  meter          E    =           .0014434
     Z    =        1731825.24                 I    =           51.86585
     XDOT =        334.442053                 Wp   =          101.19164
     YDOT =      -5115.978739  meter/sec      RA   =           32.90211  deg
     ZDOT =      -5702.785058                 TA   =           59.86727
                                              MA   =           59.72430
                                              Ha   =            221.797  n.mi
                                              Hp   =            213.983
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20095862.19                 X    =        -6106969.28
     Y    =       -7688870.85  feet           Y    =        -2411962.20  meter
     Z    =        5681841.35                 Z    =         1702115.95
     XDOT =       1097.250831                 XDOT =         419.326034
     YDOT =     -16784.707148  feet/sec       YDOT =       -5111.764133  meter/sec
     ZDOT =     -18709.924732                 ZDOT =       -5700.954349
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20074974.78                 X    =        -6118852.31
     Y    =        7838332.57  feet           Y    =         2389123.77  meter
     Z    =        5549924.61                 Z    =         1691617.02
     XDOT =      -9806.710875                 XDOT =       -2989.085475
     YDOT =     -11785.990054  feet/sec       YDOT =       -3592.369768  meter/sec
     ZDOT =     -18700.892539                 ZDOT =       -5700.032046
  
  
    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   18020.82161970  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6415  33.3640 0003537  26.7645 333.3689 15.54174788 15596
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18020.82161970   =   yrday.fracday
    Element set:     906
    Inclination:       51.6415  deg
    RA of node:        33.3640  deg
    Eccentricity:     .0003537     
    Arg of perigee:    26.7645  deg
    Mean anomaly:     333.3689  deg
    Mean motion:   15.54174788  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1559
    Checksum:              318
 
 
    Coasting Arc #8 (Orbit 1574)
    ---------------------------------------
 
    Vector Time (GMT): 2018/021/18:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6004346.74                 A    =         6789162.94  meter
     Y    =        3151365.23  meter          E    =           .0015684
     Z    =         -38055.85                 I    =           51.84222
     XDOT =      -2179.744423                 Wp   =           41.28151
     YDOT =       4208.744431  meter/sec      RA   =           27.94526  deg
     ZDOT =       6031.940422                 TA   =          318.30956
                                              MA   =          318.42899
                                              Ha   =            221.858  n.mi
                                              Hp   =            213.828
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19699300.32                 X    =         5968845.92
     Y    =       10339124.78  feet           Y    =         3218311.46  meter
     Z    =        -124855.15                 Z    =           -8975.56
     XDOT =      -7151.392463                 XDOT =       -2255.945220
     YDOT =      13808.216637  feet/sec       YDOT =        4183.943009  meter/sec
     ZDOT =      19789.830782                 ZDOT =        6021.167059
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21436525.63                 X    =         6533853.01
     Y    =       -5954063.75  feet           Y    =        -1814798.63  meter
     Z    =           4112.42                 Z    =            1253.47
     XDOT =       3715.145559                 XDOT =        1132.376366
     YDOT =      13487.328233  feet/sec       YDOT =        4110.937646  meter/sec
     ZDOT =      19741.127180                 ZDOT =        6017.095564
  
  
    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   18021.85041131  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6418  28.2348 0003689  29.1006 331.0352 15.54187078 15759
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18021.85041131   =   yrday.fracday
    Element set:     907
    Inclination:       51.6418  deg
    RA of node:        28.2348  deg
    Eccentricity:     .0003689     
    Arg of perigee:    29.1006  deg
    Mean anomaly:     331.0352  deg
    Mean motion:   15.54187078  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1575
    Checksum:              292
 
 
    Coasting Arc #9 (Orbit 1589)
    ---------------------------------------
 
    Vector Time (GMT): 2018/022/18:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5399372.21                 A    =         6787927.93  meter
     Y    =       -3744483.61  meter          E    =           .0007201
     Z    =       -1701433.72                 I    =           51.80888
     XDOT =       3999.608773                 Wp   =          114.36234
     YDOT =      -3182.660449  meter/sec      RA   =           22.98791  deg
     ZDOT =      -5710.021603                 TA   =           84.23667
                                              MA   =           84.15457
                                              Ha   =            221.821  n.mi
                                              Hp   =            213.840
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17714475.75                 X    =        -5348834.54
     Y    =      -12285051.21  feet           Y    =        -3804580.54  meter
     Z    =       -5582131.62                 Z    =        -1727538.84
     XDOT =      13122.076027                 XDOT =        4062.636769
     YDOT =     -10441.799372  feet/sec       YDOT =       -3137.581741  meter/sec
     ZDOT =     -18733.666677                 ZDOT =       -5690.440043
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21238049.58                 X    =        -6473357.51
     Y    =        3516584.23  feet           Y    =         1071854.87  meter
     Z    =       -5697737.56                 Z    =        -1736670.41
     XDOT =       2471.197828                 XDOT =         753.221098
     YDOT =     -15172.389019  feet/sec       YDOT =       -4624.544173  meter/sec
     ZDOT =     -18645.916970                 ZDOT =       -5683.275492
  
  
    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   18022.81490208  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6421  23.4273 0003461  32.6404 327.4962 15.54168932 15907
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18022.81490208   =   yrday.fracday
    Element set:     908
    Inclination:       51.6421  deg
    RA of node:        23.4273  deg
    Eccentricity:     .0003461     
    Arg of perigee:    32.6404  deg
    Mean anomaly:     327.4962  deg
    Mean motion:   15.54168932  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1590
    Checksum:              291
 
 
    Coasting Arc #10 (Orbit 1605)
    ---------------------------------------
 
    Vector Time (GMT): 2018/023/18:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4346104.44                 A    =         6784674.71  meter
     Y    =        4081889.04  meter          E    =           .0015273
     Z    =        3220455.01                 I    =           51.76817
     XDOT =      -5589.486747                 Wp   =           75.73995
     YDOT =       2155.141294  meter/sec      RA   =           18.02061  deg
     ZDOT =       4796.232398                 TA   =          321.48879
                                              MA   =          321.59767
                                              Ha   =            221.851  n.mi
                                              Hp   =            213.707
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14258872.83                 X    =         4284493.54
     Y    =       13392024.41  feet           Y    =         4130145.71  meter
     Z    =       10565797.28                 Z    =         3241416.96
     XDOT =     -18338.211111                 XDOT =       -5636.468013
     YDOT =       7070.673537  feet/sec       YDOT =        2092.373186  meter/sec
     ZDOT =      15735.670597                 ZDOT =        4768.966774
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19501371.19                 X    =         5944017.94
     Y    =        -626242.87  feet           Y    =         -190878.83  meter
     Z    =       10658432.62                 Z    =         3248690.26
     XDOT =      -8026.492413                 XDOT =       -2446.474888
     YDOT =      16644.721549  feet/sec       YDOT =        5073.311128  meter/sec
     ZDOT =      15613.887144                 ZDOT =        4759.112802
  
  
    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   18023.84368914  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6427  18.2979 0003695  35.1135 325.0260 15.54189193 16061
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18023.84368914   =   yrday.fracday
    Element set:     909
    Inclination:       51.6427  deg
    RA of node:        18.2979  deg
    Eccentricity:     .0003695     
    Arg of perigee:    35.1135  deg
    Mean anomaly:     325.0260  deg
    Mean motion:   15.54189193  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1606
    Checksum:              318
 
 
    Coasting Arc #11 (Orbit 1605)
    ---------------------------------------
 
    Vector Time (GMT): 2018/023/19:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1742865.00                 A    =         6779424.77  meter
     Y    =       -4508641.92  meter          E    =           .0014263
     Z    =       -4767212.96                 I    =           51.74937
     XDOT =       7167.595106                 Wp   =           61.86395
     YDOT =         76.334519  meter/sec      RA   =           17.83341  deg
     ZDOT =      -2692.207318                 TA   =          181.53587
                                              MA   =          181.54025
                                              Ha   =            221.821  n.mi
                                              Hp   =            213.689
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5718061.02                 X    =        -1669162.26
     Y    =      -14792132.29  feet           Y    =        -4527719.79  meter
     Z    =      -15640462.45                 Z    =        -4775500.04
     XDOT =      23515.731975                 XDOT =        7179.285988
     YDOT =        250.441336  feet/sec       YDOT =         156.552819  meter/sec
     ZDOT =      -8832.701175                 ZDOT =       -2657.361609
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15545810.70                 X    =        -4738363.10
     Y    =       -2949567.06  feet           Y    =         -899028.04  meter
     Z    =      -15676584.10                 Z    =        -4778222.83
     XDOT =      12324.525073                 XDOT =        3756.515242
     YDOT =     -18829.528927  feet/sec       YDOT =       -5739.240417  meter/sec
     ZDOT =      -8677.550797                 ZDOT =       -2644.917483
  
  
    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   18023.84368770  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6424  18.2983 0003630  33.0826 327.0553 15.54214783 16067
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18023.84368770   =   yrday.fracday
    Element set:     910
    Inclination:       51.6424  deg
    RA of node:        18.2983  deg
    Eccentricity:     .0003630     
    Arg of perigee:    33.0826  deg
    Mean anomaly:     327.0553  deg
    Mean motion:   15.54214783  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1606
    Checksum:              296
 
 
    Coasting Arc #12 (Orbit 1621)
    ---------------------------------------
 
    Vector Time (GMT): 2018/024/19:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -32302.53                 A    =         6777310.33  meter
     Y    =        4258145.10  meter          E    =           .0005240
     Z    =        5267963.34                 I    =           51.71044
     XDOT =      -7555.277024                 Wp   =           74.20832
     YDOT =      -1063.257278  meter/sec      RA   =           12.84116  deg
     ZDOT =        813.834754                 TA   =            8.02954
                                              MA   =            8.02116
                                              Ha   =            221.937  n.mi
                                              Hp   =            213.648
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -105979.44                 X    =         -105504.63
     Y    =       13970292.31  feet           Y    =         4257374.58  meter
     Z    =       17283344.28                 Z    =         5267628.62
     XDOT =     -24787.654279                 XDOT =       -7546.779020
     YDOT =      -3488.376895  feet/sec       YDOT =       -1147.698047  meter/sec
     ZDOT =       2670.061528                 ZDOT =         777.154790
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11921509.85                 X    =         3633676.20
     Y    =        7289372.54  feet           Y    =         2221800.75  meter
     Z    =       17281115.10                 Z    =         5267283.88
     XDOT =     -15077.647470                 XDOT =       -4595.666949
     YDOT =      18721.333363  feet/sec       YDOT =        5706.262409  meter/sec
     ZDOT =       2506.926125                 ZDOT =         764.111083
  
  
    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   18024.87247133  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6422  13.1689 0003669  38.4133 321.7280 15.54205752 16226
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18024.87247133   =   yrday.fracday
    Element set:     911
    Inclination:       51.6422  deg
    RA of node:        13.1689  deg
    Eccentricity:     .0003669     
    Arg of perigee:    38.4133  deg
    Mean anomaly:     321.7280  deg
    Mean motion:   15.54205752  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1622
    Checksum:              289
 
 
    Coasting Arc #13 (Orbit 1636)
    ---------------------------------------
 
    Vector Time (GMT): 2018/025/19:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1849950.72                 A    =         6777556.63  meter
     Y    =       -3915816.48  meter          E    =           .0016350
     Z    =       -5227390.99                 I    =           51.67767
     XDOT =       7320.349077                 Wp   =           87.71615
     YDOT =       1926.833972  meter/sec      RA   =            7.84410  deg
     ZDOT =       1151.004654                 TA   =          193.30915
                                              MA   =          193.35233
                                              Ha   =            221.915  n.mi
                                              Hp   =            213.631
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6069392.13                 X    =         1918992.66
     Y    =      -12847166.92  feet           Y    =        -3894742.96  meter
     Z    =      -17150232.92                 Z    =        -5218237.00
     XDOT =      24016.893297                 XDOT =        7292.667707
     YDOT =       6321.633768  feet/sec       YDOT =        2008.540342  meter/sec
     ZDOT =       3776.261987                 ZDOT =        1186.496896
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8127015.42                 X    =        -2477114.30
     Y    =      -11715735.86  feet           Y    =        -3570956.29  meter
     Z    =      -17108794.86                 Z    =        -5214760.67
     XDOT =      16479.459526                 XDOT =        5022.939263
     YDOT =     -17158.378133  feet/sec       YDOT =       -5229.873655  meter/sec
     ZDOT =       3933.948503                 ZDOT =        1199.067504
  
  
    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   18025.83695317  .00016717  00000-0  10270-3 0  9128
    2 25544  51.6408   8.3603 0003660  40.8612 319.2814 15.54223198 16377
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18025.83695317   =   yrday.fracday
    Element set:     912
    Inclination:       51.6408  deg
    RA of node:         8.3603  deg
    Eccentricity:     .0003660     
    Arg of perigee:    40.8612  deg
    Mean anomaly:     319.2814  deg
    Mean motion:   15.54223198  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1637
    Checksum:              299
 
 
    Coasting Arc #14 (Orbit 1652)
    ---------------------------------------
 
    Vector Time (GMT): 2018/026/19:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3569998.14                 A    =         6780067.96  meter
     Y    =        3465727.67  meter          E    =           .0011935
     Z    =        4600105.27                 I    =           51.65436
     XDOT =      -6518.143490                 Wp   =           58.40371
     YDOT =      -2706.488410  meter/sec      RA   =            2.84918  deg
     ZDOT =      -3007.591124                 TA   =           61.64712
                                              MA   =           61.52681
                                              Ha   =            221.940  n.mi
                                              Hp   =            213.555
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11712592.33                 X    =        -3630832.21
     Y    =       11370497.60  feet           Y    =         3425465.22  meter
     Z    =       15092208.90                 Z    =         4582615.96
     XDOT =     -21384.985203                 XDOT =       -6472.785199
     YDOT =      -8879.555150  feet/sec       YDOT =       -2779.125051  meter/sec
     ZDOT =      -9867.424948                 ZDOT =       -3039.143655
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4338058.17                 X    =         1322240.13
     Y    =       15811915.58  feet           Y    =         4819471.87  meter
     Z    =       15013739.75                 Z    =         4576187.87
     XDOT =     -16841.869215                 XDOT =       -5133.401737
     YDOT =      14160.038306  feet/sec       YDOT =        4315.979676  meter/sec
     ZDOT =     -10007.427194                 ZDOT =       -3050.263809
  
  
    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   18026.86572979  .00016717  00000-0  10270-3 0  9131
    2 25544  51.6415   3.2314 0003603  41.3240 318.8185 15.54255194 16533
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18026.86572979   =   yrday.fracday
    Element set:     913
    Inclination:       51.6415  deg
    RA of node:         3.2314  deg
    Eccentricity:     .0003603     
    Arg of perigee:    41.3240  deg
    Mean anomaly:     318.8185  deg
    Mean motion:   15.54255194  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1653
    Checksum:              298
 
 
    Coasting Arc #15 (Orbit 1667)
    ---------------------------------------
 
    Vector Time (GMT): 2018/027/19:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4994528.87                 A    =         6783923.58  meter
     Y    =       -2966043.49  meter          E    =           .0007943
     Z    =       -3508419.73                 I    =           51.63314
     XDOT =       5178.712125                 Wp   =           73.11579
     YDOT =       3386.960325  meter/sec      RA   =          357.85960  deg
     ZDOT =       4519.696211                 TA   =          245.63073
                                              MA   =          245.71366
                                              Ha   =            221.990  n.mi
                                              Hp   =            213.583
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16386249.58                 X    =         5044366.63
     Y    =       -9731113.82  feet           Y    =        -2909912.43  meter
     Z    =      -11510563.42                 Z    =        -3484037.41
     XDOT =      16990.525346                 XDOT =        5118.499282
     YDOT =      11112.074558  feet/sec       YDOT =        3444.535353  meter/sec
     ZDOT =      14828.399643                 ZDOT =        4544.706225
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1002878.90                 X    =         -305677.49
     Y    =      -19097040.26  feet           Y    =        -5820777.87  meter
     Z    =      -11401495.92                 Z    =        -3475175.96
     XDOT =      16279.713287                 XDOT =        4962.056610
     YDOT =      -9752.827728  feet/sec       YDOT =       -2972.661891  meter/sec
     ZDOT =      14939.151138                 ZDOT =        4553.453267
  
  
    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   18027.83020600  .00016717  00000-0  10270-3 0  9149
    2 25544  51.6405 358.4215 0003603  46.5320 313.6132 15.54226306 16687
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18027.83020600   =   yrday.fracday
    Element set:     914
    Inclination:       51.6405  deg
    RA of node:       358.4215  deg
    Eccentricity:     .0003603     
    Arg of perigee:    46.5320  deg
    Mean anomaly:     313.6132  deg
    Mean motion:   15.54226306  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1668
    Checksum:              270
 
 
    Coasting Arc #16 (Orbit 1683)
    ---------------------------------------
 
    Vector Time (GMT): 2018/028/19:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6039099.61                 A    =         6787326.19  meter
     Y    =        2350265.81  meter          E    =           .0015980
     Z    =        1998871.36                 I    =           51.61158
     XDOT =      -3418.219021                 Wp   =           99.76414
     YDOT =      -4018.187384  meter/sec      RA   =          352.88018  deg
     ZDOT =      -5567.449827                 TA   =           58.14707
                                              MA   =           57.99163
                                              Ha   =            221.993  n.mi
                                              Hp   =            213.425
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19813318.92                 X    =        -6074641.38
     Y    =        7710845.85  feet           Y    =         2282533.63  meter
     Z    =        6557976.91                 Z    =         1969449.79
     XDOT =     -11214.629333                 XDOT =       -3345.989222
     YDOT =     -13183.029475  feet/sec       YDOT =       -4056.008088  meter/sec
     ZDOT =     -18265.911506                 ZDOT =       -5583.878869
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1995408.25                 X    =         -608200.44
     Y    =       21207290.17  feet           Y    =         6463982.04  meter
     Z    =        6426585.49                 Z    =         1958823.26
     XDOT =     -15209.952388                 XDOT =       -4635.993488
     YDOT =       4161.880397  feet/sec       YDOT =        1268.541145  meter/sec
     ZDOT =     -18338.350311                 ZDOT =       -5589.529175
  
  
    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   18028.85897607  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6401 353.2925 0003727  49.1963 310.9512 15.54259019 16840
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18028.85897607   =   yrday.fracday
    Element set:     915
    Inclination:       51.6401  deg
    RA of node:       353.2925  deg
    Eccentricity:     .0003727     
    Arg of perigee:    49.1963  deg
    Mean anomaly:     310.9512  deg
    Mean motion:   15.54259019  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1684
    Checksum:              326
 
 
    Coasting Arc #17 (Orbit 1697)
    ---------------------------------------
 
    Vector Time (GMT): 2018/029/16:58:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905759.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3132087.35                 A    =         6778496.98  meter
     Y    =        3383117.26  meter          E    =           .0008256
     Z    =        4962476.72                 I    =           51.55541
     XDOT =      -6699.377950                 Wp   =           98.21959
     YDOT =       3082.327285  meter/sec      RA   =          348.50324  deg
     ZDOT =       2122.815301                 TA   =          331.07452
                                              MA   =          331.12025
                                              Ha   =            221.984  n.mi
                                              Hp   =            213.359
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10275877.12                 X    =         3069919.05
     Y    =       11099466.09  feet           Y    =         3417794.55  meter
     Z    =       16281091.61                 Z    =         4977540.18
     XDOT =     -21979.586449                 XDOT =       -6743.658757
     YDOT =      10112.622325  feet/sec       YDOT =        3007.162552  meter/sec
     ZDOT =       6964.617128                 ZDOT =        2090.165342
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13658704.46                 X    =         4163173.12
     Y    =        6329510.14  feet           Y    =         1929234.69  meter
     Z    =       16347563.61                 Z    =         4982737.39
     XDOT =     -15971.063899                 XDOT =       -4867.980276
     YDOT =      16818.233088  feet/sec       YDOT =        5126.197445  meter/sec
     ZDOT =       6818.729449                 ZDOT =        2078.348736
  
  
    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   18029.75915023  .00016717  00000-0  10270-3 0  9166
    2 25544  51.6422 348.8058 0003708  55.8539 304.2965 15.54223831 16988
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18029.75915023   =   yrday.fracday
    Element set:     916
    Inclination:       51.6422  deg
    RA of node:       348.8058  deg
    Eccentricity:     .0003708     
    Arg of perigee:    55.8539  deg
    Mean anomaly:     304.2965  deg
    Mean motion:   15.54223831  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1698
    Checksum:              328
 
             

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