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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  13813.3262
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   72.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.331
   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 
   ------------------------------------------------------------------------
   201/19:34:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.2  
   000/00:00:00.000           0.0               0.0              215.3  
   
   203/18:49:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.4  
   000/00:00:00.000           0.0               0.0              215.1  
   
   206/03:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.5  
   000/00:00:00.000           0.0               0.0              214.8  
   
   207/15:56:37.126          -1.2               1.3              1.3    
   N/A                        0.4              -0.1              221.8  
   000/00:03:14.253          -0.3              -0.0              215.4  
   
   209/20:18:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.0  
   000/00:00:00.000           0.0               0.0              215.3  
   
   212/23:22:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.2  
   000/00:00:00.000           0.0               0.0              214.9  
   
   215/12:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.5  
   000/00:00:00.000           0.0               0.0              214.7  
   
   216/02:50:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.5  
   000/00:00:00.000           0.0               0.0              214.6  
   
 
 
    Coasting Arc #1 (Orbit 368)
    ---------------------------------------
 
    Vector Time (GMT): 2018/201/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944469.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4871209.72                 A    =         6780891.55  meter
     Y    =        1269310.69  meter          E    =           .0007773
     Z    =       -4549777.70                 I    =           51.42537
     XDOT =      -4315.320413                 Wp   =           87.75127
     YDOT =      -5530.342155  meter/sec      RA   =          211.52096  deg
     ZDOT =       3082.182402                 TA   =          213.19122
                                              MA   =          213.24000
                                              Ha   =            221.173  n.mi
                                              Hp   =            215.272
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15981659.18                 X    =        -4862941.22
     Y    =        4164405.15  feet           Y    =         1214883.99  meter
     Z    =      -14927092.21                 Z    =        -4573420.00
     XDOT =     -14157.875370                 XDOT =       -4268.129376
     YDOT =     -18144.167174  feet/sec       YDOT =       -5578.335391  meter/sec
     ZDOT =      10112.146989                 ZDOT =        3061.334491
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10993110.53                 X    =         3350700.09
     Y    =       12195528.36  feet           Y    =         3717197.04  meter
     Z    =      -15033109.83                 Z    =        -4582091.88
     XDOT =      -8693.289894                 XDOT =       -2649.714760
     YDOT =      20167.315928  feet/sec       YDOT =        6146.997895  meter/sec
     ZDOT =      10019.420676                 ZDOT =        3053.919422
  
  
    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   18201.51062806  .00016717  00000-0  10270-3 0  9007
    2 25544  51.6384 212.6239 0004169 336.3803  23.7158 15.53971967  3697
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18201.51062806   =   yrday.fracday
    Element set:     900
    Inclination:       51.6384  deg
    RA of node:       212.6239  deg
    Eccentricity:     .0004169     
    Arg of perigee:   336.3803  deg
    Mean anomaly:      23.7158  deg
    Mean motion:   15.53971967  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             369
    Checksum:              308
 
 
    Coasting Arc #2 (Orbit 373)
    ---------------------------------------
 
    Vector Time (GMT): 2018/201/19:34:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944469.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1690498.22                 A    =         6777766.53  meter
     Y    =        3897769.54  meter          E    =           .0013916
     Z    =       -5292496.72                 I    =           51.42577
     XDOT =      -6786.491616                 Wp   =           69.63737
     YDOT =      -3523.804916  meter/sec      RA   =          209.97251  deg
     ZDOT =       -423.641289                 TA   =          196.28290
                                              MA   =          196.32765
                                              Ha   =            221.205  n.mi
                                              Hp   =            215.260
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5546254.01                 X    =        -1708250.55
     Y    =       12787957.80  feet           Y    =         3878766.33  meter
     Z    =      -17363834.39                 Z    =        -5300751.36
     XDOT =     -22265.392442                 XDOT =       -6744.525265
     YDOT =     -11561.039751  feet/sec       YDOT =       -3599.461474  meter/sec
     ZDOT =      -1389.899243                 ZDOT =        -456.505782
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6552179.51                 X    =        -1997104.31
     Y    =      -12249944.46  feet           Y    =        -3733783.07  meter
     Z    =      -17401245.56                 Z    =        -5303899.65
     XDOT =      22070.384408                 XDOT =        6727.053168
     YDOT =      -9604.167258  feet/sec       YDOT =       -2927.350180  meter/sec
     ZDOT =      -1536.672691                 ZDOT =        -468.377836
  
  
    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   18201.83216750  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6401 211.0223 0004352 336.7904  23.3052 15.54013035  3742
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18201.83216750   =   yrday.fracday
    Element set:     901
    Inclination:       51.6401  deg
    RA of node:       211.0223  deg
    Eccentricity:     .0004352     
    Arg of perigee:   336.7904  deg
    Mean anomaly:      23.3052  deg
    Mean motion:   15.54013035  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             374
    Checksum:              248
 
 
    Coasting Arc #3 (Orbit 389)
    ---------------------------------------
 
    Vector Time (GMT): 2018/202/19:34:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944469.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3230333.18                 A    =         6778277.23  meter
     Y    =       -3013471.91  meter          E    =           .0007104
     Z    =        5140463.76                 I    =           51.45721
     XDOT =       6251.278637                 Wp   =           18.15866
     YDOT =       4194.631344  meter/sec      RA   =          204.96024  deg
     ZDOT =      -1462.217536                 TA   =           85.99157
                                              MA   =           85.91037
                                              Ha   =            221.160  n.mi
                                              Hp   =            215.221
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10598205.97                 X    =         3238821.09
     Y    =       -9886718.85  feet           Y    =        -2977301.06  meter
     Z    =       16865038.59                 Z    =         5156175.85
     XDOT =      20509.444348                 XDOT =        6211.011138
     YDOT =      13761.913858  feet/sec       YDOT =        4264.312431  meter/sec
     ZDOT =      -4797.301626                 ZDOT =       -1431.948661
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1368854.13                 X    =          417226.74
     Y    =       14345914.39  feet           Y    =         4372634.71  meter
     Z    =       16935751.68                 Z    =         5162017.11
     XDOT =     -22425.465975                 XDOT =       -6835.282029
     YDOT =       7671.289536  feet/sec       YDOT =        2338.209051  meter/sec
     ZDOT =      -4662.208532                 ZDOT =       -1421.041161
  
  
    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   18202.86108773  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6403 205.8938 0004449 339.8396  20.2580 15.54040308  3907
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18202.86108773   =   yrday.fracday
    Element set:     902
    Inclination:       51.6403  deg
    RA of node:       205.8938  deg
    Eccentricity:     .0004449     
    Arg of perigee:   339.8396  deg
    Mean anomaly:      20.2580  deg
    Mean motion:   15.54040308  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             390
    Checksum:              303
 
 
    Coasting Arc #4 (Orbit 404)
    ---------------------------------------
 
    Vector Time (GMT): 2018/203/18:49:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944469.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5016972.54                 A    =         6782006.97  meter
     Y    =       -1736040.18  meter          E    =           .0011101
     Z    =        4217631.32                 I    =           51.49773
     XDOT =       4733.815142                 Wp   =           50.51845
     YDOT =       4813.688809  meter/sec      RA   =          200.10963  deg
     ZDOT =      -3636.276485                 TA   =           76.83963
                                              MA   =           76.71578
                                              Ha   =            221.382  n.mi
                                              Hp   =            215.056
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16459883.65                 X    =         5015525.69
     Y    =       -5695669.88  feet           Y    =        -1679945.42  meter
     Z    =       13837373.11                 Z    =         4241998.15
     XDOT =      15530.889572                 XDOT =        4697.298286
     YDOT =      15792.942287  feet/sec       YDOT =        4866.421770  meter/sec
     ZDOT =     -11930.040961                 ZDOT =       -3613.369672
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8394391.42                 X    =        -2558610.50
     Y    =       15161285.36  feet           Y    =         4621159.78  meter
     Z    =       13946717.85                 Z    =         4250959.60
     XDOT =     -21058.020376                 XDOT =       -6418.484611
     YDOT =       -738.922757  feet/sec       YDOT =        -225.223656  meter/sec
     ZDOT =     -11827.974646                 ZDOT =       -3605.166672
  
  
    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   18203.82570242  .00016717  00000-0  10270-3 0  9034
    2 25544  51.6391 201.0865 0004443 346.0748  14.0281 15.54011537  4053
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18203.82570242   =   yrday.fracday
    Element set:     903
    Inclination:       51.6391  deg
    RA of node:       201.0865  deg
    Eccentricity:     .0004443     
    Arg of perigee:   346.0748  deg
    Mean anomaly:      14.0281  deg
    Mean motion:   15.54011537  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             405
    Checksum:              271
 
 
    Coasting Arc #5 (Orbit 419)
    ---------------------------------------
 
    Vector Time (GMT): 2018/204/18:49:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944469.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6010158.78                 A    =         6785690.52  meter
     Y    =         864999.55  meter          E    =           .0006595
     Z    =       -3024921.98                 I    =           51.54182
     XDOT =      -3188.117419                 Wp   =           30.79689
     YDOT =      -4922.996507  meter/sec      RA   =          195.11769  deg
     ZDOT =       4936.956520                 TA   =          294.49240
                                              MA   =          294.56117
                                              Ha   =            221.423  n.mi
                                              Hp   =            214.974
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19718368.69                 X    =        -6004691.44
     Y    =        2837925.02  feet           Y    =          797820.69  meter
     Z    =       -9924284.70                 Z    =        -3054103.57
     XDOT =     -10459.702819                 XDOT =       -3156.811044
     YDOT =     -16151.563343  feet/sec       YDOT =       -4958.473714  meter/sec
     ZDOT =      16197.363910                 ZDOT =        4921.545430
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12483588.28                 X    =         3804997.71
     Y    =      -15440658.84  feet           Y    =        -4706312.82  meter
     Z    =      -10055117.46                 Z    =        -3064799.80
     XDOT =      17602.948246                 XDOT =        5365.378625
     YDOT =       3750.237948  feet/sec       YDOT =        1143.072526  meter/sec
     ZDOT =      16128.873116                 ZDOT =        4916.080526
  
  
    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   18204.79031410  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6395 196.2785 0004464 347.3207  12.7833 15.54008981  4204
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18204.79031410   =   yrday.fracday
    Element set:     904
    Inclination:       51.6395  deg
    RA of node:       196.2785  deg
    Eccentricity:     .0004464     
    Arg of perigee:   347.3207  deg
    Mean anomaly:      12.7833  deg
    Mean motion:   15.54008981  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             420
    Checksum:              299
 
 
    Coasting Arc #6 (Orbit 435)
    ---------------------------------------
 
    Vector Time (GMT): 2018/205/18:49:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944469.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6617302.04                 A    =         6788752.03  meter
     Y    =         -24579.99  meter          E    =           .0011916
     Z    =        1499226.57                 I    =           51.58406
     XDOT =       1331.776821                 Wp   =          100.75339
     YDOT =       4879.664251  meter/sec      RA   =          190.13782  deg
     ZDOT =      -5761.431696                 TA   =           62.86644
                                              MA   =           62.74497
                                              Ha   =            221.645  n.mi
                                              Hp   =            214.902
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21710308.53                 X    =         6609802.74
     Y    =         -80643.01  feet           Y    =           49377.16  meter
     Z    =        4918722.36                 Z    =         1531352.48
     XDOT =       4369.346525                 XDOT =        1305.097706
     YDOT =      16009.397148  feet/sec       YDOT =        4894.408557  meter/sec
     ZDOT =     -18902.334960                 ZDOT =       -5755.026736
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15586104.67                 X    =        -4750644.70
     Y    =       15065872.07  feet           Y    =         4592077.81  meter
     Z    =        5062674.14                 Z    =         1543103.08
     XDOT =     -13227.519038                 XDOT =       -4031.747803
     YDOT =      -7302.477768  feet/sec       YDOT =       -2225.795224  meter/sec
     ZDOT =     -18874.179966                 ZDOT =       -5752.850054
  
  
    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   18205.81923194  .00016717  00000-0  10270-3 0  9055
    2 25544  51.6397 191.1504 0004367 352.4363   7.6723 15.53980215  4367
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18205.81923194   =   yrday.fracday
    Element set:     905
    Inclination:       51.6397  deg
    RA of node:       191.1504  deg
    Eccentricity:     .0004367     
    Arg of perigee:   352.4363  deg
    Mean anomaly:       7.6723  deg
    Mean motion:   15.53980215  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             436
    Checksum:              306
 
 
    Coasting Arc #7 (Orbit 440)
    ---------------------------------------
 
    Vector Time (GMT): 2018/206/03:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944469.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -885536.61                 A    =         6777675.78  meter
     Y    =        4131308.42  meter          E    =           .0014826
     Z    =       -5311886.86                 I    =           51.55756
     XDOT =      -7540.769033                 Wp   =           76.46937
     YDOT =      -1312.366845  meter/sec      RA   =          188.44418  deg
     ZDOT =        240.376326                 TA   =          195.80430
                                              MA   =          195.85062
                                              Ha   =            221.529  n.mi
                                              Hp   =            214.813
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2905303.83                 X    =         -905866.26
     Y    =       13554161.50  feet           Y    =         4121292.65  meter
     Z    =      -17427450.33                 Z    =        -5316237.35
     XDOT =     -24740.055882                 XDOT =       -7526.700948
     YDOT =      -4305.665503  feet/sec       YDOT =       -1396.614298  meter/sec
     ZDOT =        788.636239                 ZDOT =         203.780439
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5788408.66                 X    =        -1764306.96
     Y    =       12567994.87  feet           Y    =         3830724.84  meter
     Z    =      -17447404.95                 Z    =        -5317969.03
     XDOT =     -22208.716984                 XDOT =       -6769.216937
     YDOT =      -9379.244437  feet/sec       YDOT =       -2858.793705  meter/sec
     ZDOT =        624.795434                 ZDOT =         190.437648
  
  
    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   18206.14076715  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6388 189.5430 0003996 353.3535   6.7564 15.54023275  4418
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18206.14076715   =   yrday.fracday
    Element set:     906
    Inclination:       51.6388  deg
    RA of node:       189.5430  deg
    Eccentricity:     .0003996     
    Arg of perigee:   353.3535  deg
    Mean anomaly:       6.7564  deg
    Mean motion:   15.54023275  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             441
    Checksum:              313
 
 
    Coasting Arc #8 (Orbit 456)
    ---------------------------------------
 
    Vector Time (GMT): 2018/207/03:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944469.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2611032.21                 A    =         6779137.16  meter
     Y    =       -3792710.62  meter          E    =           .0008828
     Z    =        4973439.94                 I    =           51.59491
     XDOT =       7070.980309                 Wp   =           34.36905
     YDOT =       2096.553321  meter/sec      RA   =          183.44174  deg
     ZDOT =      -2104.456116                 TA   =           76.17637
                                              MA   =           76.07815
                                              Ha   =            221.598  n.mi
                                              Hp   =            214.779
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8566378.64                 X    =         2629091.37
     Y    =      -12443276.31  feet           Y    =        -3763411.80  meter
     Z    =       16317060.17                 Z    =         4986166.67
     XDOT =      23198.754296                 XDOT =        7057.232704
     YDOT =       6878.455776  feet/sec       YDOT =        2175.549257  meter/sec
     ZDOT =      -6904.383582                 ZDOT =       -2070.141517
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10880394.98                 X    =         3316344.39
     Y    =      -10390216.33  feet           Y    =        -3166937.94  meter
     Z    =       16374517.71                 Z    =         4990953.00
     XDOT =      20525.658971                 XDOT =        6256.220854
     YDOT =      10808.841562  feet/sec       YDOT =        3294.534908  meter/sec
     ZDOT =      -6750.826595                 ZDOT =       -2057.651946
  
  
    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   18207.16968232  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6385 184.4141 0004009 358.1890   1.9247 15.53997775  4577
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18207.16968232   =   yrday.fracday
    Element set:     907
    Inclination:       51.6385  deg
    RA of node:       184.4141  deg
    Eccentricity:     .0004009     
    Arg of perigee:   358.1890  deg
    Mean anomaly:       1.9247  deg
    Mean motion:   15.53997775  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             457
    Checksum:              330
 
 
    Coasting Arc #9 (Orbit 464)
    ---------------------------------------
 
    Vector Time (GMT): 2018/207/15:58:14.253
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1597496.45                 A    =         6779108.80  meter
     Y    =        4110858.68  meter          E    =           .0014249
     Z    =       -5160628.75                 I    =           51.61048
     XDOT =      -7442.580118                 Wp   =           61.50293
     YDOT =       1055.274655  meter/sec      RA   =          180.78011  deg
     ZDOT =      -1459.698742                 TA   =          194.40102
                                              MA   =          194.44167
                                              Ha   =            221.828  n.mi
                                              Hp   =            215.428
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5241130.07                 X    =         1576476.10
     Y    =       13487069.15  feet           Y    =         4128605.97  meter
     Z    =      -16931196.67                 Z    =        -5152919.45
     XDOT =     -24417.913772                 XDOT =       -7446.737035
     YDOT =       3462.187188  feet/sec       YDOT =         972.023486  meter/sec
     ZDOT =      -4789.037866                 ZDOT =       -1495.861521
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6047055.53                 X    =        -1843142.53
     Y    =      -13189282.15  feet           Y    =        -4020093.20  meter
     Z    =      -16897096.06                 Z    =        -5150234.88
     XDOT =      23210.931705                 XDOT =        7074.691984
     YDOT =      -4283.603359  feet/sec       YDOT =       -1305.642304  meter/sec
     ZDOT =      -4951.239970                 ZDOT =       -1509.137943
  
  
    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   18207.68414010  .00016717  00000-0  10270-3 0  9087
    2 25544  51.6386 181.8539 0004289 347.3404  12.7640 15.53787298  4654
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18207.68414010   =   yrday.fracday
    Element set:     908
    Inclination:       51.6386  deg
    RA of node:       181.8539  deg
    Eccentricity:     .0004289     
    Arg of perigee:   347.3404  deg
    Mean anomaly:      12.7640  deg
    Mean motion:   15.53787298  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             465
    Checksum:              325
 
 
    Coasting Arc #10 (Orbit 480)
    ---------------------------------------
 
    Vector Time (GMT): 2018/208/15:58:14.253
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =          78580.55                 A    =         6778293.63  meter
     Y    =       -4216189.23  meter          E    =           .0005062
     Z    =        5305730.18                 I    =           51.64160
     XDOT =       7656.247937                 Wp   =           18.29209
     YDOT =       -293.301413  meter/sec      RA   =          175.78362  deg
     ZDOT =       -341.675216                 TA   =           74.99284
                                              MA   =           74.93682
                                              Ha   =            221.779  n.mi
                                              Hp   =            215.345
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         257810.21                 X    =           99949.41
     Y    =      -13832641.85  feet           Y    =        -4215191.47  meter
     Z    =       17407251.26                 Z    =         5306163.43
     XDOT =      25118.923679                 XDOT =        7660.618334
     YDOT =       -962.274978  feet/sec       YDOT =        -207.659495  meter/sec
     ZDOT =      -1120.981680                 ZDOT =        -304.474014
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         814425.62                 X    =          248236.93
     Y    =       13808021.40  feet           Y    =         4208684.92  meter
     Z    =       17409655.34                 Z    =         5306462.95
     XDOT =     -23992.234831                 XDOT =       -7312.833176
     YDOT =       2637.989426  feet/sec       YDOT =         804.059177  meter/sec
     ZDOT =       -954.183936                 ZDOT =        -290.835264
  
  
    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   18208.71320711  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6390 176.7268 0004330 347.9675  12.1373 15.53813173  4811
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18208.71320711   =   yrday.fracday
    Element set:     909
    Inclination:       51.6390  deg
    RA of node:       176.7268  deg
    Eccentricity:     .0004330     
    Arg of perigee:   347.9675  deg
    Mean anomaly:      12.1373  deg
    Mean motion:   15.53813173  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             481
    Checksum:              302
 
 
    Coasting Arc #11 (Orbit 495)
    ---------------------------------------
 
    Vector Time (GMT): 2018/209/15:58:14.253
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1711843.57                 A    =         6779756.94  meter
     Y    =        4271602.77  meter          E    =           .0011794
     Z    =       -4988619.76                 I    =           51.68040
     XDOT =      -7348.181571                 Wp   =           85.38464
     YDOT =       -493.320326  meter/sec      RA   =          170.78996  deg
     ZDOT =       2104.327326                 TA   =          205.08477
                                              MA   =          205.14211
                                              Ha   =            221.990  n.mi
                                              Hp   =            215.161
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5616284.68                 X    =        -1735251.04
     Y    =       14014444.79  feet           Y    =         4252329.22  meter
     Z    =      -16366862.74                 Z    =        -4996991.67
     XDOT =     -24108.207254                 XDOT =       -7352.340484
     YDOT =      -1618.505007  feet/sec       YDOT =        -575.516170  meter/sec
     ZDOT =       6903.961042                 ZDOT =        2068.623063
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4277724.07                 X    =         1303850.30
     Y    =      -14436172.02  feet           Y    =        -4400145.23  meter
     Z    =      -16404862.89                 Z    =        -5000202.21
     XDOT =      23150.315400                 XDOT =        7056.216134
     YDOT =       -784.322599  feet/sec       YDOT =        -239.061528  meter/sec
     ZDOT =       6743.936524                 ZDOT =        2055.551853
  
  
    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   18209.67795735  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6402 171.9199 0004396 353.6097   6.4999 15.53782501  4965
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18209.67795735   =   yrday.fracday
    Element set:     910
    Inclination:       51.6402  deg
    RA of node:       171.9199  deg
    Eccentricity:     .0004396     
    Arg of perigee:   353.6097  deg
    Mean anomaly:       6.4999  deg
    Mean motion:   15.53782501  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             496
    Checksum:              346
 
 
    Coasting Arc #12 (Orbit 498)
    ---------------------------------------
 
    Vector Time (GMT): 2018/209/20:18:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5575652.86                 A    =         6785415.36  meter
     Y    =        1772967.55  meter          E    =           .0006123
     Z    =       -3444810.52                 I    =           51.70141
     XDOT =      -4242.299907                 Wp   =           45.36894
     YDOT =       4431.774382  meter/sec      RA   =          169.93171  deg
     ZDOT =      -4586.326744                 TA   =          174.90943
                                              MA   =          174.90321
                                              Ha   =            221.988  n.mi
                                              Hp   =            215.336
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18292824.35                 X    =         5572145.36
     Y    =        5816822.67  feet           Y    =         1835298.97  meter
     Z    =      -11301871.80                 Z    =        -3417734.94
     XDOT =     -13918.306782                 XDOT =       -4269.264478
     YDOT =      14539.942199  feet/sec       YDOT =        4384.183593  meter/sec
     ZDOT =     -15047.003753                 ZDOT =       -4606.999102
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11728864.43                 X    =        -3574957.88
     Y    =       15284682.51  feet           Y    =         4658771.23  meter
     Z    =      -11180669.69                 Z    =        -3407868.12
     XDOT =      -7842.909069                 XDOT =       -2390.518684
     YDOT =     -17091.309652  feet/sec       YDOT =       -5209.431182  meter/sec
     ZDOT =     -15140.171456                 ZDOT =       -4614.724260
  
  
    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   18209.87090552  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6367 170.9566 0004395 353.1446   6.9646 15.53783651  4998
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18209.87090552   =   yrday.fracday
    Element set:     911
    Inclination:       51.6367  deg
    RA of node:       170.9566  deg
    Eccentricity:     .0004395     
    Arg of perigee:   353.1446  deg
    Mean anomaly:       6.9646  deg
    Mean motion:   15.53783651  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             499
    Checksum:              337
 
 
    Coasting Arc #13 (Orbit 514)
    ---------------------------------------
 
    Vector Time (GMT): 2018/210/20:18:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4432241.07                 A    =         6781951.06  meter
     Y    =       -2476442.54  meter          E    =           .0008237
     Z    =        4488753.82                 I    =           51.72187
     XDOT =       5590.944348                 Wp   =           82.96849
     YDOT =      -4143.059822  meter/sec      RA   =          164.95252  deg
     ZDOT =       3230.737746                 TA   =          334.57057
                                              MA   =          334.61108
                                              Ha   =            222.186  n.mi
                                              Hp   =            215.208
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14541473.33                 X    =        -4426022.92
     Y    =       -8124811.48  feet           Y    =        -2525972.37  meter
     Z    =       14726882.60                 Z    =         4467238.98
     XDOT =      18342.993269                 XDOT =        5621.164782
     YDOT =     -13592.715952  feet/sec       YDOT =       -4080.369205  meter/sec
     ZDOT =      10599.533286                 ZDOT =        3257.969217
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12436387.14                 X    =         3790610.80
     Y    =      -11208376.38  feet           Y    =        -3416313.12  meter
     Z    =       14630675.07                 Z    =         4459429.76
     XDOT =       6105.846285                 XDOT =        1861.061948
     YDOT =      20788.373761  feet/sec       YDOT =        6336.296322  meter/sec
     ZDOT =      10722.091625                 ZDOT =        3268.093527
  
  
    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   18210.89997094  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6366 165.8290 0004368 355.6469   4.4645 15.53761978  5155
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18210.89997094   =   yrday.fracday
    Element set:     912
    Inclination:       51.6366  deg
    RA of node:       165.8290  deg
    Eccentricity:     .0004368     
    Arg of perigee:   355.6469  deg
    Mean anomaly:       4.4645  deg
    Mean motion:   15.53761978  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             515
    Checksum:              346
 
 
    Coasting Arc #14 (Orbit 529)
    ---------------------------------------
 
    Vector Time (GMT): 2018/211/20:18:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3057103.50                 A    =         6779221.65  meter
     Y    =        3204120.93  meter          E    =           .0015039
     Z    =       -5145930.98                 I    =           51.74466
     XDOT =      -6520.018669                 Wp   =           62.31607
     YDOT =       3694.680271  meter/sec      RA   =          159.96700  deg
     ZDOT =      -1569.624738                 TA   =          192.53220
                                              MA   =          192.56964
                                              Ha   =            222.125  n.mi
                                              Hp   =            215.112
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10029867.12                 X    =         3046042.64
     Y    =       10512207.78  feet           Y    =         3238245.90  meter
     Z    =      -16882975.65                 Z    =        -5131107.69
     XDOT =     -21391.137365                 XDOT =       -6553.224771
     YDOT =      12121.654434  feet/sec       YDOT =        3621.583300  meter/sec
     ZDOT =      -5149.687459                 ZDOT =       -1601.376618
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13125944.21                 X    =        -4000787.80
     Y    =        6406477.97  feet           Y    =         1952694.49  meter
     Z    =      -16816844.00                 Z    =        -5125774.05
     XDOT =      -4478.159550                 XDOT =       -1364.943031
     YDOT =     -23096.279523  feet/sec       YDOT =       -7039.745998  meter/sec
     ZDOT =      -5292.483318                 ZDOT =       -1613.148915
  
  
    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   18211.86471718  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6366 161.0217 0004236    .8198 359.2961 15.53785972  5303
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18211.86471718   =   yrday.fracday
    Element set:     913
    Inclination:       51.6366  deg
    RA of node:       161.0217  deg
    Eccentricity:     .0004236     
    Arg of perigee:      .8198  deg
    Mean anomaly:     359.2961  deg
    Mean motion:   15.53785972  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             530
    Checksum:              313
 
 
    Coasting Arc #15 (Orbit 545)
    ---------------------------------------
 
    Vector Time (GMT): 2018/212/20:18:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1530455.52                 A    =         6778458.83  meter
     Y    =       -3909608.51  meter          E    =           .0005427
     Z    =        5319363.17                 I    =           51.77285
     XDOT =       7023.389333                 Wp   =           31.72049
     YDOT =      -3074.497690  meter/sec      RA   =          154.97894  deg
     ZDOT =       -234.340942                 TA   =           60.53542
                                              MA   =           60.48129
                                              Ha   =            222.314  n.mi
                                              Hp   =            214.963
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5021179.52                 X    =        -1512461.66
     Y    =      -12826799.58  feet           Y    =        -3926622.61  meter
     Z    =       17451978.91                 Z    =         5311972.51
     XDOT =      23042.615923                 XDOT =        7058.385510
     YDOT =     -10086.934679  feet/sec       YDOT =       -2995.761615  meter/sec
     ZDOT =       -768.835110                 ZDOT =        -200.139410
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13766410.65                 X    =         4196001.96
     Y    =       -1168830.34  feet           Y    =         -356259.49  meter
     Z    =       17419252.93                 Z    =         5309388.29
     XDOT =       2833.876958                 XDOT =         863.765697
     YDOT =      23984.133701  feet/sec       YDOT =        7310.363952  meter/sec
     ZDOT =       -615.103682                 ZDOT =        -187.483602
  
  
    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   18212.89377838  .00016717  00000-0  10270-3 0  9149
    2 25544  51.6368 155.8938 0004275   5.3571 354.7627 15.53750617  5468
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18212.89377838   =   yrday.fracday
    Element set:     914
    Inclination:       51.6368  deg
    RA of node:       155.8938  deg
    Eccentricity:     .0004275     
    Arg of perigee:     5.3571  deg
    Mean anomaly:     354.7627  deg
    Mean motion:   15.53750617  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             546
    Checksum:              341
 
 
    Coasting Arc #16 (Orbit 547)
    ---------------------------------------
 
    Vector Time (GMT): 2018/212/23:22:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1879290.39                 A    =         6778323.58  meter
     Y    =       -3748118.44  meter          E    =           .0004728
     Z    =        5323433.54                 I    =           51.77918
     XDOT =       6891.623887                 Wp   =           37.13422
     YDOT =      -3367.563640  meter/sec      RA   =          154.34314  deg
     ZDOT =         65.515452                 TA   =           52.26429
                                              MA   =           52.22145
                                              Ha   =            222.211  n.mi
                                              Hp   =            214.904
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6165650.90                 X    =        -1863096.22
     Y    =      -12296976.52  feet           Y    =        -3769043.51  meter
     Z    =       17465333.13                 Z    =         5314344.02
     XDOT =      22610.314589                 XDOT =        6928.450482
     YDOT =     -11048.437139  feet/sec       YDOT =       -3290.290828  meter/sec
     ZDOT =        214.945709                 ZDOT =          99.081382
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7653229.62                 X    =         2332704.39
     Y    =      -11492051.74  feet           Y    =        -3502777.37  meter
     Z    =       17424969.64                 Z    =         5311130.75
     XDOT =      19855.377360                 XDOT =        6051.919019
     YDOT =      13759.396714  feet/sec       YDOT =        4193.864118  meter/sec
     ZDOT =        365.860091                 ZDOT =         111.514156
  
  
    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   18213.02241056  .00016717  00000-0  10270-3 0  9158
    2 25544  51.6394 155.2515 0004035   6.0275 354.0925 15.53793887  5487
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18213.02241056   =   yrday.fracday
    Element set:     915
    Inclination:       51.6394  deg
    RA of node:       155.2515  deg
    Eccentricity:     .0004035     
    Arg of perigee:     6.0275  deg
    Mean anomaly:     354.0925  deg
    Mean motion:   15.53793887  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             548
    Checksum:              299
 
 
    Coasting Arc #17 (Orbit 562)
    ---------------------------------------
 
    Vector Time (GMT): 2018/213/23:22:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         378739.54                 A    =         6779230.35  meter
     Y    =        4449553.40  meter          E    =           .0013840
     Z    =       -5112287.88                 I    =           51.81127
     XDOT =      -7003.929795                 Wp   =           86.48689
     YDOT =       2572.057710  meter/sec      RA   =          149.35968  deg
     ZDOT =       1724.598014                 TA   =          200.13581
                                              MA   =          200.19045
                                              Ha   =            222.218  n.mi
                                              Hp   =            214.786
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1242583.81                 X    =          353787.72
     Y    =       14598272.32  feet           Y    =         4453649.27  meter
     Z    =      -16772598.02                 Z    =        -5110508.67
     XDOT =     -22978.772293                 XDOT =       -7040.547784
     YDOT =       8438.509546  feet/sec       YDOT =        2493.530161  meter/sec
     ZDOT =       5658.129967                 ZDOT =        1690.486909
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11925463.23                 X    =        -3634881.19
     Y    =        8525747.08  feet           Y    =         2598647.71  meter
     Z    =      -16765099.96                 Z    =        -5110002.47
     XDOT =     -18266.363645                 XDOT =       -5567.587639
     YDOT =     -14756.781153  feet/sec       YDOT =       -4497.866895  meter/sec
     ZDOT =       5504.840046                 ZDOT =        1677.875246
  
  
    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   18213.98715276  .00016717  00000-0  10270-3 0  9164
    2 25544  51.6389 150.4462 0003950  10.5489 349.5746 15.53804058  5631
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18213.98715276   =   yrday.fracday
    Element set:     916
    Inclination:       51.6389  deg
    RA of node:       150.4462  deg
    Eccentricity:     .0003950     
    Arg of perigee:    10.5489  deg
    Mean anomaly:     349.5746  deg
    Mean motion:   15.53804058  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             563
    Checksum:              329
 
 
    Coasting Arc #18 (Orbit 578)
    ---------------------------------------
 
    Vector Time (GMT): 2018/214/23:22:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944334.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1074126.90                 A    =         6782086.42  meter
     Y    =       -5033392.28  meter          E    =           .0011973
     Z    =        4412384.70                 I    =           51.84894
     XDOT =       6710.111206                 Wp   =           54.69009
     YDOT =      -1541.923076  meter/sec      RA   =          144.38079  deg
     ZDOT =      -3379.204178                 TA   =           69.44962
                                              MA   =           69.32119
                                              Ha   =            222.307  n.mi
                                              Hp   =            214.745
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3524038.38                 X    =         1108899.03
     Y    =      -16513754.19  feet           Y    =        -5021186.28  meter
     Z    =       14476327.74                 Z    =         4417686.77
     XDOT =      22014.800545                 XDOT =        6743.268934
     YDOT =      -5058.802742  feet/sec       YDOT =       -1466.700532  meter/sec
     ZDOT =     -11086.627879                 ZDOT =       -3346.528601
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15895315.94                 X    =         4844892.30
     Y    =       -5635305.24  feet           Y    =        -1717641.04  meter
     Z    =       14500663.95                 Z    =         4419802.37
     XDOT =      15372.733826                 XDOT =        4685.609270
     YDOT =      15099.778035  feet/sec       YDOT =        4602.412345  meter/sec
     ZDOT =     -10939.873858                 ZDOT =       -3334.473552
  
  
    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   18215.01620966  .00016717  00000-0  10270-3 0  9172
    2 25544  51.6394 145.3182 0003914  14.7217 345.4049 15.53769920  5790
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18215.01620966   =   yrday.fracday
    Element set:     917
    Inclination:       51.6394  deg
    RA of node:       145.3182  deg
    Eccentricity:     .0003914     
    Arg of perigee:    14.7217  deg
    Mean anomaly:     345.4049  deg
    Mean motion:   15.53769920  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             579
    Checksum:              316
 
 
    Coasting Arc #19 (Orbit 586)
    ---------------------------------------
 
    Vector Time (GMT): 2018/215/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919627.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5661403.05                 A    =         6790062.09  meter
     Y    =       -3660239.29  meter          E    =           .0008513
     Z    =        -795954.59                 I    =           51.88974
     XDOT =       1999.860877                 Wp   =          115.22985
     YDOT =       4378.452546  meter/sec      RA   =          141.80253  deg
     ZDOT =      -5963.386897                 TA   =           73.34026
                                              MA   =           73.24682
                                              Ha   =            222.459  n.mi
                                              Hp   =            214.656
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18574156.98                 X    =         5705778.38
     Y    =      -12008659.07  feet           Y    =        -3596681.43  meter
     Z    =       -2611399.56                 Z    =         -768345.97
     XDOT =       6561.223350                 XDOT =        1979.717921
     YDOT =      14365.001792  feet/sec       YDOT =        4400.703849  meter/sec
     ZDOT =     -19564.917641                 ZDOT =       -5953.721198
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21275194.65                 X    =        -6484679.33
     Y    =       -6099742.08  feet           Y    =        -1859201.39  meter
     Z    =       -2487136.26                 Z    =         -758079.13
     XDOT =       5970.001486                 XDOT =        1819.656453
     YDOT =     -12937.527471  feet/sec       YDOT =       -3943.358373  meter/sec
     ZDOT =     -19522.036054                 ZDOT =       -5950.316589
  
  
    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   18215.53073623  .00016717  00000-0  10270-3 0  9182
    2 25544  51.6395 142.7583 0004525  13.7220 346.4055 15.53790899  5875
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18215.53073623   =   yrday.fracday
    Element set:     918
    Inclination:       51.6395  deg
    RA of node:       142.7583  deg
    Eccentricity:     .0004525     
    Arg of perigee:    13.7220  deg
    Mean anomaly:     346.4055  deg
    Mean motion:   15.53790899  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             587
    Checksum:              321
 
 
    Coasting Arc #20 (Orbit 596)
    ---------------------------------------
 
    Vector Time (GMT): 2018/216/02:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919627.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5461932.25                 A    =         6783722.87  meter
     Y    =         661665.20  meter          E    =           .0012324
     Z    =        3956305.04                 I    =           51.88464
     XDOT =       2191.527135                 Wp   =           80.03772
     YDOT =      -6141.937554  meter/sec      RA   =          138.74979  deg
     ZDOT =       4044.134532                 TA   =          327.86783
                                              MA   =          327.94289
                                              Ha   =            222.511  n.mi
                                              Hp   =            214.610
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17919725.23                 X    =        -5488142.74
     Y    =        2170817.57  feet           Y    =          600439.45  meter
     Z    =       12980003.40                 Z    =         3929709.41
     XDOT =       7190.049654                 XDOT =        2240.400962
     YDOT =     -20150.713759  feet/sec       YDOT =       -6117.157209  meter/sec
     ZDOT =      13268.157913                 ZDOT =        4054.898694
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18132475.50                 X    =        -5526778.53
     Y    =         357224.34  feet           Y    =          108881.98  meter
     Z    =       12860607.00                 Z    =         3919913.01
     XDOT =       9110.594473                 XDOT =        2776.909195
     YDOT =     -18014.695050  feet/sec       YDOT =       -5490.879051  meter/sec
     ZDOT =      13317.133148                 ZDOT =        4059.062183
  
  
    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   18216.17389155  .00016717  00000-0  10270-3 0  9194
    2 25544  51.6396 139.5523 0004219  16.1732 343.9555 15.53813140  5972
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18216.17389155   =   yrday.fracday
    Element set:     919
    Inclination:       51.6396  deg
    RA of node:       139.5523  deg
    Eccentricity:     .0004219     
    Arg of perigee:    16.1732  deg
    Mean anomaly:     343.9555  deg
    Mean motion:   15.53813140  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             597
    Checksum:              320
 
             

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