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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  12398.9484
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   73.5
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.468
   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 
   ------------------------------------------------------------------------
   144/03:23:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.4  
   000/00:00:00.000           0.0               0.0              213.5  
   
   144/09:20:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.4  
   000/00:00:00.000           0.0               0.0              213.6  
   
   146/20:57:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.2  
   000/00:00:00.000           0.0               0.0              213.6  
   
   148/06:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.2  
   000/00:00:00.000           0.0               0.0              213.8  
   
   153/12:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.0  
   000/00:00:00.000           0.0               0.0              213.9  
   
   154/09:16:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.9  
   000/00:00:00.000           0.0               0.0              214.0  
   
   156/19:28:00.000           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  
   
 
 
    Coasting Arc #1 (Orbit 3466)
    ---------------------------------------
 
    Vector Time (GMT): 2018/143/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907607.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1863129.55                 A    =         6783487.79  meter
     Y    =        5339941.89  meter          E    =           .0009812
     Z    =       -3756081.17                 I    =           51.87374
     XDOT =      -6295.692261                 Wp   =          105.89459
     YDOT =        812.936128  meter/sec      RA   =          140.64934  deg
     ZDOT =       4285.264331                 TA   =          209.41466
                                              MA   =          209.46991
                                              Ha   =            222.464  n.mi
                                              Hp   =            213.379
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6112629.75                 X    =        -1904458.62
     Y    =       17519494.40  feet           Y    =         5318876.18  meter
     Z    =      -12323100.96                 Z    =        -3765231.79
     XDOT =     -20655.158337                 XDOT =       -6325.130482
     YDOT =       2667.113280  feet/sec       YDOT =         742.368563  meter/sec
     ZDOT =      14059.266177                 ZDOT =        4254.610426
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12199285.91                 X    =         3718342.35
     Y    =       13944464.19  feet           Y    =         4250272.69  meter
     Z    =      -12364670.85                 Z    =        -3768751.68
     XDOT =      -6986.380006                 XDOT =       -2129.448626
     YDOT =      18437.490488  feet/sec       YDOT =        5619.747101  meter/sec
     ZDOT =      13922.087031                 ZDOT =        4243.452127
  
  
    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   18143.50806457  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6376 141.7447 0003897 109.7913 250.3660 15.54069155 34678
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18143.50806457   =   yrday.fracday
    Element set:     900
    Inclination:       51.6376  deg
    RA of node:       141.7447  deg
    Eccentricity:     .0003897     
    Arg of perigee:   109.7913  deg
    Mean anomaly:     250.3660  deg
    Mean motion:   15.54069155  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3467
    Checksum:              321
 
 
    Coasting Arc #2 (Orbit 3476)
    ---------------------------------------
 
    Vector Time (GMT): 2018/144/03:23:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907607.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -423302.92                 A    =         6781095.53  meter
     Y    =        5117897.39  meter          E    =           .0013076
     Z    =       -4441804.04                 I    =           51.88322
     XDOT =      -6466.346780                 Wp   =          113.54267
     YDOT =       2368.317960  meter/sec      RA   =          137.46338  deg
     ZDOT =       3347.759344                 TA   =          190.20426
                                              MA   =          190.23083
                                              Ha   =            222.379  n.mi
                                              Hp   =            213.465
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1388789.11                 X    =         -458925.09
     Y    =       16791001.95  feet           Y    =         5112964.75  meter
     Z    =      -14572847.89                 Z    =        -4443946.61
     XDOT =     -21215.048492                 XDOT =       -6508.611134
     YDOT =       7770.072048  feet/sec       YDOT =        2295.770357  meter/sec
     ZDOT =      10983.462414                 ZDOT =        3316.245292
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16090064.14                 X    =        -4904251.55
     Y    =        4967764.16  feet           Y    =         1514174.52  meter
     Z    =      -14583056.34                 Z    =        -4444915.57
     XDOT =     -14687.338393                 XDOT =       -4476.700742
     YDOT =     -15769.077829  feet/sec       YDOT =       -4806.414922  meter/sec
     ZDOT =      10842.237546                 ZDOT =        3304.714004
  
  
    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   18144.15110373  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6387 138.5356 0003879 119.5056 240.6484 15.54086543 34777
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18144.15110373   =   yrday.fracday
    Element set:     901
    Inclination:       51.6387  deg
    RA of node:       138.5356  deg
    Eccentricity:     .0003879     
    Arg of perigee:   119.5056  deg
    Mean anomaly:     240.6484  deg
    Mean motion:   15.54086543  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3477
    Checksum:              318
 
 
    Coasting Arc #3 (Orbit 3480)
    ---------------------------------------
 
    Vector Time (GMT): 2018/144/09:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4285011.58                 A    =         6778716.79  meter
     Y    =        1410375.85  meter          E    =           .0016108
     Z    =       -5073929.89                 I    =           51.88172
     XDOT =      -4233.004596                 Wp   =           84.94723
     YDOT =       6094.937817  meter/sec      RA   =          136.27331  deg
     ZDOT =      -1884.418849                 TA   =          166.84288
                                              MA   =          166.80081
                                              Ha   =            222.418  n.mi
                                              Hp   =            213.583
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14058436.95                 X    =         4293568.58
     Y    =        4627217.34  feet           Y    =         1458341.86  meter
     Z    =      -16646751.60                 Z    =        -5053093.77
     XDOT =     -13887.810353                 XDOT =       -4291.691664
     YDOT =      19996.515149  feet/sec       YDOT =        6047.273385  meter/sec
     ZDOT =      -6182.476539                 ZDOT =       -1905.123767
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14884274.02                 X    =         4536726.72
     Y    =        -772770.01  feet           Y    =         -235540.30  meter
     Z    =      -16553741.02                 Z    =        -5045580.26
     XDOT =      -5795.165826                 XDOT =       -1766.366544
     YDOT =      22550.081787  feet/sec       YDOT =        6873.264929  meter/sec
     ZDOT =      -6275.821858                 ZDOT =       -1912.870502
  
  
    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   18144.40831837  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6395 137.2561 0003848 115.9255 244.2295 15.54077432 34819
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18144.40831837   =   yrday.fracday
    Element set:     902
    Inclination:       51.6395  deg
    RA of node:       137.2561  deg
    Eccentricity:     .0003848     
    Arg of perigee:   115.9255  deg
    Mean anomaly:     244.2295  deg
    Mean motion:   15.54077432  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3481
    Checksum:              314
 
 
    Coasting Arc #4 (Orbit 3496)
    ---------------------------------------
 
    Vector Time (GMT): 2018/145/09:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3131147.63                 A    =         6777438.89  meter
     Y    =       -2768447.68  meter          E    =           .0006171
     Z    =        5330226.31                 I    =           51.89956
     XDOT =       5071.619746                 Wp   =          107.87904
     YDOT =      -5758.518463  meter/sec      RA   =          131.29186  deg
     ZDOT =        -13.497727                 TA   =          342.23826
                                              MA   =          342.25982
                                              Ha   =            222.520  n.mi
                                              Hp   =            213.418
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10272794.06                 X    =        -3125849.11
     Y    =       -9082833.61  feet           Y    =        -2803432.97  meter
     Z    =       17487619.14                 Z    =         5315028.84
     XDOT =      16639.172395                 XDOT =        5135.701707
     YDOT =     -18892.777110  feet/sec       YDOT =       -5701.445812  meter/sec
     ZDOT =        -44.283882                 ZDOT =          11.294101
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13036917.79                 X    =        -3973652.54
     Y    =       -4519696.14  feet           Y    =        -1377603.38  meter
     Z    =       17419991.64                 Z    =         5309613.45
     XDOT =       8004.249072                 XDOT =        2439.695117
     YDOT =     -22805.253959  feet/sec       YDOT =       -6951.041407  meter/sec
     ZDOT =         67.316840                 ZDOT =          20.518173
  
  
    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   18145.43717720  .00016717  00000-0  10270-3 0  9030
    2 25544  51.6382 132.1274 0003925 117.7767 242.3784 15.54095672 34979
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18145.43717720   =   yrday.fracday
    Element set:     903
    Inclination:       51.6382  deg
    RA of node:       132.1274  deg
    Eccentricity:     .0003925     
    Arg of perigee:   117.7767  deg
    Mean anomaly:     242.3784  deg
    Mean motion:   15.54095672  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3497
    Checksum:              323
 
 
    Coasting Arc #5 (Orbit 3511)
    ---------------------------------------
 
    Vector Time (GMT): 2018/146/09:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1920327.19                 A    =         6778685.28  meter
     Y    =        4090721.48  meter          E    =           .0016606
     Z    =       -5067706.71                 I    =           51.92619
     XDOT =      -5507.861908                 Wp   =          108.06381
     YDOT =       4959.601056  meter/sec      RA   =          126.31178  deg
     ZDOT =       1916.482370                 TA   =          180.47778
                                              MA   =          180.47937
                                              Ha   =            222.323  n.mi
                                              Hp   =            213.622
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6300286.07                 X    =         1899057.51
     Y    =       13421002.22  feet           Y    =         4112077.29  meter
     Z    =      -16626334.33                 Z    =        -5058429.69
     XDOT =     -18070.413084                 XDOT =       -5572.221563
     YDOT =      16271.657008  feet/sec       YDOT =        4897.648374  meter/sec
     ZDOT =       6287.671818                 ZDOT =        1889.570683
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11148358.73                 X    =         3398019.74
     Y    =        9843370.67  feet           Y    =         3000259.38  meter
     Z    =      -16585356.49                 Z    =        -5055216.66
     XDOT =      -9586.394364                 XDOT =       -2921.933002
     YDOT =      21246.909412  feet/sec       YDOT =        6476.057989  meter/sec
     ZDOT =       6166.668923                 ZDOT =        1879.600688
  
  
    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   18146.40172945  .00016717  00000-0  10270-3 0  9043
    2 25544  51.6398 127.3193 0003699 121.0768 239.0747 15.54075188 35129
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18146.40172945   =   yrday.fracday
    Element set:     904
    Inclination:       51.6398  deg
    RA of node:       127.3193  deg
    Eccentricity:     .0003699     
    Arg of perigee:   121.0768  deg
    Mean anomaly:     239.0747  deg
    Mean motion:   15.54075188  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3512
    Checksum:              326
 
 
    Coasting Arc #6 (Orbit 3519)
    ---------------------------------------
 
    Vector Time (GMT): 2018/146/20:57:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1082129.96                 A    =         6780381.11  meter
     Y    =       -4851558.46  meter          E    =           .0010697
     Z    =        4603107.00                 I    =           51.94007
     XDOT =       5676.599664                 Wp   =           81.26346
     YDOT =      -4166.735806  meter/sec      RA   =          123.89979  deg
     ZDOT =      -3049.529526                 TA   =           39.08813
                                              MA   =           39.01089
                                              Ha   =            222.187  n.mi
                                              Hp   =            213.617
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3550295.13                 X    =        -1050157.88
     Y    =      -15917186.56  feet           Y    =        -4863481.14  meter
     Z    =       15102057.10                 Z    =         4597927.62
     XDOT =      18624.014646                 XDOT =        5737.584580
     YDOT =     -13670.393065  feet/sec       YDOT =       -4102.914955  meter/sec
     ZDOT =     -10005.018131                 ZDOT =       -3021.806316
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8359800.73                 X    =         2548067.26
     Y    =       14026963.35  feet           Y    =         4275418.43  meter
     Z    =       15079508.71                 Z    =         4596234.25
     XDOT =     -12567.727309                 XDOT =       -3830.643284
     YDOT =      18138.887636  feet/sec       YDOT =        5528.732951  meter/sec
     ZDOT =      -9880.475937                 ZDOT =       -3011.569066
  
  
    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   18146.91615526  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6382 124.7541 0003369 122.5389 237.6090 15.54118633 35206
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18146.91615526   =   yrday.fracday
    Element set:     905
    Inclination:       51.6382  deg
    RA of node:       124.7541  deg
    Eccentricity:     .0003369     
    Arg of perigee:   122.5389  deg
    Mean anomaly:     237.6090  deg
    Mean motion:   15.54118633  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3520
    Checksum:              307
 
 
    Coasting Arc #7 (Orbit 3534)
    ---------------------------------------
 
    Vector Time (GMT): 2018/147/20:57:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -47148.39                 A    =         6784121.25  meter
     Y    =        5797166.40  meter          E    =           .0008343
     Z    =       -3532885.14                 I    =           51.96829
     XDOT =      -5548.547303                 Wp   =          108.38151
     YDOT =       2712.218918  meter/sec      RA   =          118.93317  deg
     ZDOT =       4530.765528                 TA   =          210.26816
                                              MA   =          210.31638
                                              Ha   =            222.171  n.mi
                                              Hp   =            213.668
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -154686.32                 X    =          -94809.22
     Y    =       19019574.81  feet           Y    =         5796372.99  meter
     Z    =      -11590830.53                 Z    =        -3533229.41
     XDOT =     -18203.895352                 XDOT =       -5600.472121
     YDOT =       8898.356029  feet/sec       YDOT =        2649.880498  meter/sec
     ZDOT =      14864.716300                 ZDOT =        4503.686298
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6075048.63                 X    =        -1851674.82
     Y    =      -18022450.66  feet           Y    =        -5493242.96  meter
     Z    =      -11593125.65                 Z    =        -3533584.70
     XDOT =      13127.448511                 XDOT =        4001.246306
     YDOT =     -13895.688593  feet/sec       YDOT =       -4235.405883  meter/sec
     ZDOT =      14743.223252                 ZDOT =        4493.734447
  
  
    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   18147.88070636  .00016717  00000-0  10270-3 0  9062
    2 25544  51.6366 119.9455 0003522 127.5882 232.5591 15.54100667 35356
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18147.88070636   =   yrday.fracday
    Element set:     906
    Inclination:       51.6366  deg
    RA of node:       119.9455  deg
    Eccentricity:     .0003522     
    Arg of perigee:   127.5882  deg
    Mean anomaly:     232.5591  deg
    Mean motion:   15.54100667  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3535
    Checksum:              322
 
 
    Coasting Arc #8 (Orbit 3540)
    ---------------------------------------
 
    Vector Time (GMT): 2018/148/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3837003.73                 A    =         6777539.81  meter
     Y    =        1680711.98  meter          E    =           .0017691
     Z    =       -5343078.83                 I    =           51.95371
     XDOT =      -3327.520851                 Wp   =           96.46552
     YDOT =       6890.847698  meter/sec      RA   =          117.09148  deg
     ZDOT =       -224.576449                 TA   =          171.41484
                                              MA   =          171.38454
                                              Ha   =            222.233  n.mi
                                              Hp   =            213.824
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12588594.91                 X    =         3843878.65
     Y    =        5514146.93  feet           Y    =         1723658.97  meter
     Z    =      -17529786.19                 Z    =        -5324422.83
     XDOT =     -10917.063159                 XDOT =       -3403.237995
     YDOT =      22607.768037  feet/sec       YDOT =        6853.213729  meter/sec
     ZDOT =       -736.799372                 ZDOT =        -240.923879
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9158751.99                 X    =         2791587.61
     Y    =       10387841.16  feet           Y    =         3166213.99  meter
     Z    =      -17446545.79                 Z    =        -5317707.16
     XDOT =     -18725.448906                 XDOT =       -5707.516826
     YDOT =      15162.288732  feet/sec       YDOT =        4621.465606  meter/sec
     ZDOT =       -810.836707                 ZDOT =        -247.143028
  
  
    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   18148.26652695  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6384 118.0227 0003664 131.3750 228.7718 15.54073731 35413
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18148.26652695   =   yrday.fracday
    Element set:     907
    Inclination:       51.6384  deg
    RA of node:       118.0227  deg
    Eccentricity:     .0003664     
    Arg of perigee:   131.3750  deg
    Mean anomaly:     228.7718  deg
    Mean motion:   15.54073731  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3541
    Checksum:              314
 
 
    Coasting Arc #9 (Orbit 3556)
    ---------------------------------------
 
    Vector Time (GMT): 2018/149/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2994536.52                 A    =         6778268.99  meter
     Y    =       -3269885.07  meter          E    =           .0006748
     Z    =        5121242.95                 I    =           51.97177
     XDOT =       4001.397091                 Wp   =           86.71266
     YDOT =      -6324.037614  meter/sec      RA   =          112.11458  deg
     ZDOT =      -1695.836538                 TA   =           19.59422
                                              MA   =           19.56830
                                              Ha   =            222.212  n.mi
                                              Hp   =            213.680
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9824594.89                 X    =        -2982625.88
     Y    =      -10727969.40  feet           Y    =        -3303306.05  meter
     Z    =       16801978.17                 Z    =         5106724.85
     XDOT =      13127.943211                 XDOT =        4080.054419
     YDOT =     -20748.154903  feet/sec       YDOT =       -6278.851235  meter/sec
     ZDOT =      -5563.768168                 ZDOT =       -1676.208545
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4676201.24                 X    =        -1425306.14
     Y    =      -13853123.05  feet           Y    =        -4222431.91  meter
     Z    =       16737460.57                 Z    =         5101577.98
     XDOT =      19492.109223                 XDOT =        5941.194891
     YDOT =     -13203.875022  feet/sec       YDOT =       -4024.541107  meter/sec
     ZDOT =      -5475.104415                 ZDOT =       -1668.811826
  
  
    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   18149.29537577  .00016717  00000-0  10270-3 0  9083
    2 25544  51.6393 112.8941 0003589 134.6249 225.5197 15.54127428 35579
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18149.29537577   =   yrday.fracday
    Element set:     908
    Inclination:       51.6393  deg
    RA of node:       112.8941  deg
    Eccentricity:     .0003589     
    Arg of perigee:   134.6249  deg
    Mean anomaly:     225.5197  deg
    Mean motion:   15.54127428  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3557
    Checksum:              346
 
 
    Coasting Arc #10 (Orbit 3571)
    ---------------------------------------
 
    Vector Time (GMT): 2018/150/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2144453.21                 A    =         6781241.14  meter
     Y    =        4707306.39  meter          E    =           .0012369
     Z    =       -4397804.74                 I    =           51.99347
     XDOT =      -4421.417589                 Wp   =          117.27147
     YDOT =       5222.868961  meter/sec      RA   =          107.14382  deg
     ZDOT =       3436.363499                 TA   =          187.43747
                                              MA   =          187.45584
                                              Ha   =            222.155  n.mi
                                              Hp   =            213.721
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7035607.64                 X    =         2113017.93
     Y    =       15443918.61  feet           Y    =         4731111.97  meter
     Z    =      -14428493.25                 Z    =        -4387463.32
     XDOT =     -14505.963219                 XDOT =       -4496.184782
     YDOT =      17135.396854  feet/sec       YDOT =        5173.007117  meter/sec
     ZDOT =      11274.158461                 ZDOT =        3414.704608
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         479807.89                 X    =          146245.45
     Y    =       17002907.48  feet           Y    =         5182486.20  meter
     Z    =      -14382862.58                 Z    =        -4383896.51
     XDOT =     -18906.726455                 XDOT =       -5762.770223
     YDOT =       9982.553183  feet/sec       YDOT =        3042.682210  meter/sec
     ZDOT =      11176.533281                 ZDOT =        3406.607344
  
  
    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   18150.25992160  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6397 108.0860 0003685 133.2141 226.9320 15.54114438 35720
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18150.25992160   =   yrday.fracday
    Element set:     909
    Inclination:       51.6397  deg
    RA of node:       108.0860  deg
    Eccentricity:     .0003685     
    Arg of perigee:   133.2141  deg
    Mean anomaly:     226.9320  deg
    Mean motion:   15.54114438  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3572
    Checksum:              299
 
 
    Coasting Arc #11 (Orbit 3587)
    ---------------------------------------
 
    Vector Time (GMT): 2018/151/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1289526.58                 A    =         6785009.37  meter
     Y    =       -5837393.26  meter          E    =           .0015619
     Z    =        3191896.92                 I    =           52.01468
     XDOT =       4667.949657                 Wp   =          103.25119
     YDOT =      -3689.889707  meter/sec      RA   =          102.18393  deg
     ZDOT =      -4845.923112                 TA   =           40.05171
                                              MA   =           39.93664
                                              Ha   =            222.087  n.mi
                                              Hp   =            213.730
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4230730.26                 X    =        -1239660.12
     Y    =      -19151552.69  feet           Y    =        -5851535.27  meter
     Z    =       10472102.74                 Z    =         3185753.07
     XDOT =      15314.795461                 XDOT =        4732.403244
     YDOT =     -12105.937359  feet/sec       YDOT =       -3637.328408  meter/sec
     ZDOT =     -15898.697875                 ZDOT =       -4823.091585
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3249273.29                 X    =          990378.50
     Y    =      -19356689.11  feet           Y    =        -5899918.84  meter
     Z    =       10445419.81                 Z    =         3183763.96
     XDOT =      17438.197127                 XDOT =        5315.162484
     YDOT =      -5625.780693  feet/sec       YDOT =       -1714.737955  meter/sec
     ZDOT =     -15796.016624                 ZDOT =       -4814.625867
  
  
    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   18151.28876711  .00016717  00000-0  10270-3 0  9104
    2 25544  51.6394 102.9579 0003596 138.4425 221.7001 15.54135126 35883
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18151.28876711   =   yrday.fracday
    Element set:     910
    Inclination:       51.6394  deg
    RA of node:       102.9579  deg
    Eccentricity:     .0003596     
    Arg of perigee:   138.4425  deg
    Mean anomaly:     221.7001  deg
    Mean motion:   15.54135126  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3588
    Checksum:              311
 
 
    Coasting Arc #12 (Orbit 3602)
    ---------------------------------------
 
    Vector Time (GMT): 2018/152/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         498111.88                 A    =         6788110.29  meter
     Y    =        6554699.92  meter          E    =           .0007753
     Z    =       -1690809.84                 I    =           52.03190
     XDOT =      -4742.963550                 Wp   =           65.68191
     YDOT =       1833.294118  meter/sec      RA   =           97.23367  deg
     ZDOT =       5733.512879                 TA   =          275.89810
                                              MA   =          275.98647
                                              Ha   =            222.048  n.mi
                                              Hp   =            213.774
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1634225.34                 X    =          432991.53
     Y    =       21504921.00  feet           Y    =         6559906.28  meter
     Z    =       -5547276.39                 Z    =        -1688547.40
     XDOT =     -15560.904034                 XDOT =       -4790.961995
     YDOT =       6014.744483  feet/sec       YDOT =        1779.985833  meter/sec
     ZDOT =      18810.737792                 ZDOT =        5710.356739
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6218088.15                 X    =        -1895273.27
     Y    =       20653563.70  feet           Y    =         6295206.22  meter
     Z    =       -5538075.56                 Z    =        -1688005.43
     XDOT =     -15293.104212                 XDOT =       -4661.338164
     YDOT =        390.939382  feet/sec       YDOT =         119.158324  meter/sec
     ZDOT =      18706.848778                 ZDOT =        5701.847508
  
  
    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   18152.25330920  .00016717  00000-0  10270-3 0  9110
    2 25544  51.6404  98.1500 0003687 141.1852 218.9566 15.54130124 36036
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18152.25330920   =   yrday.fracday
    Element set:     911
    Inclination:       51.6404  deg
    RA of node:        98.1500  deg
    Eccentricity:     .0003687     
    Arg of perigee:   141.1852  deg
    Mean anomaly:     218.9566  deg
    Mean motion:   15.54130124  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3603
    Checksum:              280
 
 
    Coasting Arc #13 (Orbit 3618)
    ---------------------------------------
 
    Vector Time (GMT): 2018/153/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         292609.17                 A    =         6789357.40  meter
     Y    =       -6775271.72  meter          E    =           .0015659
     Z    =         -27739.58                 I    =           52.03978
     XDOT =       4713.430565                 Wp   =          136.74654
     YDOT =        220.050049  meter/sec      RA   =           92.29010  deg
     ZDOT =      -6048.001949                 TA   =           43.55071
                                              MA   =           43.42718
                                              Ha   =            222.035  n.mi
                                              Hp   =            213.828
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         960003.82                 X    =          368485.11
     Y    =      -22228581.77  feet           Y    =        -6771575.31  meter
     Z    =         -91009.11                 Z    =          -26134.83
     XDOT =      15464.011040                 XDOT =        4739.997694
     YDOT =        721.948981  feet/sec       YDOT =         272.908268  meter/sec
     ZDOT =     -19842.526081                 ZDOT =       -6025.041098
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8581519.19                 X    =         2615647.05
     Y    =      -20527795.80  feet           Y    =        -6256872.16  meter
     Z    =         -82857.97                 Z    =          -25255.11
     XDOT =      12888.823834                 XDOT =        3928.513505
     YDOT =       5438.373948  feet/sec       YDOT =        1657.616379  meter/sec
     ZDOT =     -19739.793389                 ZDOT =       -6016.689025
  
  
    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   18153.28214974  .00016717  00000-0  10270-3 0  9125
    2 25544  51.6411  93.0213 0003631 143.7191 216.4208 15.54119546 36190
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18153.28214974   =   yrday.fracday
    Element set:     912
    Inclination:       51.6411  deg
    RA of node:        93.0213  deg
    Eccentricity:     .0003631     
    Arg of perigee:   143.7191  deg
    Mean anomaly:     216.4208  deg
    Mean motion:   15.54119546  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3619
    Checksum:              289
 
 
    Coasting Arc #14 (Orbit 3622)
    ---------------------------------------
 
    Vector Time (GMT): 2018/153/12:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922320.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3569470.38                 A    =         6780880.59  meter
     Y    =       -3628764.45  meter          E    =           .0010843
     Z    =       -4489759.59                 I    =           52.01101
     XDOT =       2454.003748                 Wp   =           86.74317
     YDOT =       6470.083650  meter/sec      RA   =           90.98759  deg
     ZDOT =      -3284.552204                 TA   =          150.32587
                                              MA   =          150.26431
                                              Ha   =            221.960  n.mi
                                              Hp   =            213.948
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11710860.82                 X    =         3631591.87
     Y    =      -11905395.19  feet           Y    =        -3588500.22  meter
     Z    =      -14730182.37                 Z    =        -4472269.90
     XDOT =       8051.193399                 XDOT =        2397.425779
     YDOT =      21227.308563  feet/sec       YDOT =        6497.210116  meter/sec
     ZDOT =     -10776.089907                 ZDOT =       -3272.767996
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8771436.44                 X    =        -2673533.83
     Y    =      -14291950.34  feet           Y    =        -4356186.46  meter
     Z    =      -14651383.09                 Z    =        -4465741.57
     XDOT =      21503.983324                 XDOT =        6554.414117
     YDOT =      -2224.750760  feet/sec       YDOT =        -678.104032  meter/sec
     ZDOT =     -10724.275811                 ZDOT =       -3268.759267
  
  
    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   18153.53936057  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6402  91.7396 0003367 142.3774 217.7615 15.54130692 36231
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18153.53936057   =   yrday.fracday
    Element set:     913
    Inclination:       51.6402  deg
    RA of node:        91.7396  deg
    Eccentricity:     .0003367     
    Arg of perigee:   142.3774  deg
    Mean anomaly:     217.7615  deg
    Mean motion:   15.54130692  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3623
    Checksum:              312
 
 
    Coasting Arc #15 (Orbit 3636)
    ---------------------------------------
 
    Vector Time (GMT): 2018/154/09:16:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907088.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3514112.94                 A    =         6779848.76  meter
     Y    =        3334511.67  meter          E    =           .0010857
     Z    =        4738641.93                 I    =           52.00520
     XDOT =      -2564.899011                 Wp   =          126.64474
     YDOT =      -6672.754479  meter/sec      RA   =           86.67604  deg
     ZDOT =       2782.713445                 TA   =          295.89290
                                              MA   =          296.00479
                                              Ha   =            221.931  n.mi
                                              Hp   =            213.959
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11529241.93                 X    =        -3574157.03
     Y    =       10939998.92  feet           Y    =         3294878.10  meter
     Z    =       15546725.48                 Z    =         4721426.16
     XDOT =      -8415.023001                 XDOT =       -2503.608781
     YDOT =     -21892.239103  feet/sec       YDOT =       -6701.094613  meter/sec
     ZDOT =       9129.637286                 ZDOT =        2770.402038
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4594228.91                 X    =        -1400320.97
     Y    =       15293954.09  feet           Y    =         4661597.21  meter
     Z    =       15469185.44                 Z    =         4715007.72
     XDOT =     -17178.642909                 XDOT =       -5236.050359
     YDOT =     -14375.581700  feet/sec       YDOT =       -4381.677302  meter/sec
     ZDOT =       9075.500297                 ZDOT =        2766.212490
  
  
    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   18154.43959303  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6379  87.2527 0003386 149.6557 210.4792 15.54142777 36378
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18154.43959303   =   yrday.fracday
    Element set:     914
    Inclination:       51.6379  deg
    RA of node:        87.2527  deg
    Eccentricity:     .0003386     
    Arg of perigee:   149.6557  deg
    Mean anomaly:     210.4792  deg
    Mean motion:   15.54142777  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3637
    Checksum:              339
 
 
    Coasting Arc #16 (Orbit 3651)
    ---------------------------------------
 
    Vector Time (GMT): 2018/155/09:16:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907088.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3937236.26                 A    =         6777675.08  meter
     Y    =       -1624440.09  meter          E    =           .0016006
     Z    =       -5285789.76                 I    =           51.99508
     XDOT =       1807.757960                 Wp   =           94.28395
     YDOT =       7382.584824  meter/sec      RA   =           81.70290  deg
     ZDOT =       -925.853745                 TA   =          166.90952
                                              MA   =          166.86793
                                              Ha   =            221.867  n.mi
                                              Hp   =            214.149
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12917441.80                 X    =         3980784.14
     Y    =       -5329527.86  feet           Y    =        -1580167.09  meter
     Z    =      -17341829.92                 Z    =        -5266558.45
     XDOT =       5930.964437                 XDOT =        1729.566827
     YDOT =      24221.078818  feet/sec       YDOT =        7402.363334  meter/sec
     ZDOT =      -3037.577905                 ZDOT =        -917.261325
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8421380.03                 X    =         2566836.63
     Y    =      -11284101.97  feet           Y    =        -3439394.28  meter
     Z    =      -17255510.30                 Z    =        -5259479.54
     XDOT =      16758.343393                 XDOT =        5107.943066
     YDOT =      17076.700997  feet/sec       YDOT =        5204.978464  meter/sec
     ZDOT =      -3000.200451                 ZDOT =        -914.461097
  
  
    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   18155.40412811  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6383  82.4438 0003400 151.4630 208.6709 15.54114515 36524
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18155.40412811   =   yrday.fracday
    Element set:     915
    Inclination:       51.6383  deg
    RA of node:        82.4438  deg
    Eccentricity:     .0003400     
    Arg of perigee:   151.4630  deg
    Mean anomaly:     208.6709  deg
    Mean motion:   15.54114515  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3652
    Checksum:              282
 
 
    Coasting Arc #17 (Orbit 3667)
    ---------------------------------------
 
    Vector Time (GMT): 2018/156/09:16:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907088.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4263863.79                 A    =         6777706.41  meter
     Y    =        -163164.85  meter          E    =           .0004607
     Z    =        5261928.77                 I    =           51.99023
     XDOT =       -964.038683                 Wp   =          102.76980
     YDOT =      -7543.499838  meter/sec      RA   =           76.72763  deg
     ZDOT =      -1015.342274                 TA   =          356.89811
                                              MA   =          356.90097
                                              Ha   =            221.927  n.mi
                                              Hp   =            214.086
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13989054.44                 X    =        -4287282.01
     Y    =        -535317.75  feet           Y    =         -210977.80  meter
     Z    =       17263545.84                 Z    =         5241159.50
     XDOT =      -3162.856571                 XDOT =        -874.681556
     YDOT =     -24749.015215  feet/sec       YDOT =       -7553.780649  meter/sec
     ZDOT =      -3331.175439                 ZDOT =       -1019.808998
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12242540.33                 X    =        -3731526.29
     Y    =        7021455.66  feet           Y    =         2140139.68  meter
     Z    =       17170602.52                 Z    =         5233599.65
     XDOT =     -15267.852837                 XDOT =       -4653.641545
     YDOT =     -18430.488158  feet/sec       YDOT =       -5617.612790  meter/sec
     ZDOT =      -3350.050692                 ZDOT =       -1021.095451
  
  
    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   18156.43296106  .00016717  00000-0  10270-3 0  9166
    2 25544  51.6390  77.3154 0003299 154.8597 205.2716 15.54122422 36689
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18156.43296106   =   yrday.fracday
    Element set:     916
    Inclination:       51.6390  deg
    RA of node:        77.3154  deg
    Eccentricity:     .0003299     
    Arg of perigee:   154.8597  deg
    Mean anomaly:     205.2716  deg
    Mean motion:   15.54122422  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3668
    Checksum:              319
 
 
    Coasting Arc #18 (Orbit 3673)
    ---------------------------------------
 
    Vector Time (GMT): 2018/156/19:28:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907088.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4064196.25                 A    =         6783769.26  meter
     Y    =        4036464.92  meter          E    =           .0007975
     Z    =       -3644099.88                 I    =           52.00645
     XDOT =      -1943.946053                 Wp   =          121.35560
     YDOT =       5945.379414  meter/sec      RA   =           74.60066  deg
     ZDOT =       4420.564132                 TA   =          195.71416
                                              MA   =          195.73893
                                              Ha   =            221.834  n.mi
                                              Hp   =            214.124
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13333977.19                 X    =         4036458.45
     Y    =       13242995.14  feet           Y    =         4081758.83  meter
     Z    =      -11955708.25                 Z    =        -3624424.38
     XDOT =      -6377.775763                 XDOT =       -2031.757211
     YDOT =      19505.837972  feet/sec       YDOT =        5923.149447  meter/sec
     ZDOT =      14503.163162                 ZDOT =        4410.908425
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14578090.25                 X    =        -4443401.91
     Y    =      -11947177.42  feet           Y    =        -3641499.68  meter
     Z    =      -11868237.62                 Z    =        -3617438.83
     XDOT =       3773.859720                 XDOT =        1150.272443
     YDOT =     -18958.301865  feet/sec       YDOT =       -5778.490409  meter/sec
     ZDOT =      14459.056226                 ZDOT =        4407.120338
  
  
    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   18156.81877242  .00016717  00000-0  10270-3 0  9175
    2 25544  51.6382  75.3883 0003699 156.9195 203.2125 15.54134823 36745
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18156.81877242   =   yrday.fracday
    Element set:     917
    Inclination:       51.6382  deg
    RA of node:        75.3883  deg
    Eccentricity:     .0003699     
    Arg of perigee:   156.9195  deg
    Mean anomaly:     203.2125  deg
    Mean motion:   15.54134823  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3674
    Checksum:              334
 
 
    Coasting Arc #19 (Orbit 3689)
    ---------------------------------------
 
    Vector Time (GMT): 2018/157/19:28:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907088.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3755526.22                 A    =         6787309.70  meter
     Y    =       -5199503.82  meter          E    =           .0016298
     Z    =        2192652.42                 I    =           52.00735
     XDOT =       2938.769157                 Wp   =          119.46842
     YDOT =      -4456.737871  meter/sec      RA   =           69.64680  deg
     ZDOT =      -5512.083000                 TA   =           36.29803
                                              MA   =           36.18758
                                              Ha   =            221.767  n.mi
                                              Hp   =            214.185
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12321280.26                 X    =        -3707755.60
     Y    =      -17058739.56  feet           Y    =        -5241233.79  meter
     Z    =        7193741.53                 Z    =         2174524.89
     XDOT =       9641.631092                 XDOT =        3015.162055
     YDOT =     -14621.843410  feet/sec       YDOT =       -4423.446900  meter/sec
     ZDOT =     -18084.261810                 ZDOT =       -5497.622296
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14161139.48                 X    =         4316315.31
     Y    =       15602127.67  feet           Y    =         4755528.51  meter
     Z    =        7113381.80                 Z    =         2168158.77
     XDOT =      -6964.462818                 XDOT =       -2122.768267
     YDOT =      14571.041110  feet/sec       YDOT =        4441.253330  meter/sec
     ZDOT =     -18018.861248                 ZDOT =       -5492.148908
  
  
    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   18157.84760093  .00016717  00000-0  10270-3 0  9185
    2 25544  51.6370  70.2595 0003606 163.0291 197.0983 15.54138578 36901
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18157.84760093   =   yrday.fracday
    Element set:     918
    Inclination:       51.6370  deg
    RA of node:        70.2595  deg
    Eccentricity:     .0003606     
    Arg of perigee:   163.0291  deg
    Mean anomaly:     197.0983  deg
    Mean motion:   15.54138578  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3690
    Checksum:              330
 
             

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