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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15403.1558
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   75.0
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.482
   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 
   ------------------------------------------------------------------------
   057/06:58:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.8  
   000/00:00:00.000           0.0               0.0              213.9  
   
   058/23:08:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.7  
   000/00:00:00.000           0.0               0.0              213.9  
   
   060/14:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.7  
   000/00:00:00.000           0.0               0.0              214.1  
   
   063/17:18:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.6  
   000/00:00:00.000           0.0               0.0              214.0  
   
 
 
    Coasting Arc #1 (Orbit 2020)
    ---------------------------------------
 
    Vector Time (GMT): 2018/050/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1760482.69                 A    =         6788457.90  meter
     Y    =        6387814.33  meter          E    =           .0010993
     Z    =       -1459685.07                 I    =           51.31116
     XDOT =      -5065.768289                 Wp   =          134.88037
     YDOT =         89.080807  meter/sec      RA   =          244.43041  deg
     ZDOT =      -5754.125273                 TA   =           61.11883
                                              MA   =           61.00857
                                              Ha   =            222.011  n.mi
                                              Hp   =            213.687
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5775861.86                 X    =         1696011.86
     Y    =       20957396.09  feet           Y    =         6407140.62  meter
     Z    =       -4788993.02                 Z    =        -1451290.64
     XDOT =     -16619.974701                 XDOT =       -5038.437819
     YDOT =        292.259867  feet/sec       YDOT =          32.584121  meter/sec
     ZDOT =     -18878.363756                 ZDOT =       -5778.666284
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5992718.98                 X    =        -1826580.74
     Y    =       20904760.61  feet           Y    =         6371771.03  meter
     Z    =       -4752450.77                 Z    =        -1448546.99
     XDOT =     -12694.173053                 XDOT =       -3869.183947
     YDOT =      -7929.851799  feet/sec       YDOT =       -2417.018828  meter/sec
     ZDOT =     -18987.618442                 ZDOT =       -5787.426101
  
  
    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   18050.52937749  .00016717  00000-0  10270-3 0  9007
    2 25544  51.6373 245.2698 0002861 111.4643 248.6815 15.54120953 20214
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18050.52937749   =   yrday.fracday
    Element set:     900
    Inclination:       51.6373  deg
    RA of node:       245.2698  deg
    Eccentricity:     .0002861     
    Arg of perigee:   111.4643  deg
    Mean anomaly:     248.6815  deg
    Mean motion:   15.54120953  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2021
    Checksum:              305
 
 
    Coasting Arc #2 (Orbit 2036)
    ---------------------------------------
 
    Vector Time (GMT): 2018/051/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -789483.10                 A    =         6785514.52  meter
     Y    =       -6035674.02  meter          E    =           .0015615
     Z    =        2984617.73                 I    =           51.31582
     XDOT =       5610.602081                 Wp   =           89.31643
     YDOT =       1720.270386  meter/sec      RA   =          239.43163  deg
     ZDOT =       4940.672070                 TA   =          305.01524
                                              MA   =          305.16169
                                              Ha   =            221.949  n.mi
                                              Hp   =            213.690
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2590167.64                 X    =         -736429.42
     Y    =      -19802080.13  feet           Y    =        -6044205.63  meter
     Z    =        9792052.93                 Z    =         2980912.20
     XDOT =      18407.487141                 XDOT =        5566.949645
     YDOT =       5643.931712  feet/sec       YDOT =        1782.768405  meter/sec
     ZDOT =      16209.554034                 ZDOT =        4967.819931
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7762121.24                 X    =         2365894.55
     Y    =      -18408926.72  feet           Y    =        -5611040.86  meter
     Z    =        9776325.37                 Z    =         2979823.97
     XDOT =      11560.699253                 XDOT =        3523.701132
     YDOT =      13585.802397  feet/sec       YDOT =        4140.952571  meter/sec
     ZDOT =      16330.188587                 ZDOT =        4977.441481
  
  
    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   18051.55821540  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6365 240.1401 0002908 119.1781 240.9663 15.54146361 20375
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18051.55821540   =   yrday.fracday
    Element set:     901
    Inclination:       51.6365  deg
    RA of node:       240.1401  deg
    Eccentricity:     .0002908     
    Arg of perigee:   119.1781  deg
    Mean anomaly:     240.9663  deg
    Mean motion:   15.54146361  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2037
    Checksum:              282
 
 
    Coasting Arc #3 (Orbit 2051)
    ---------------------------------------
 
    Vector Time (GMT): 2018/052/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -391329.24                 A    =         6781682.18  meter
     Y    =        5286661.86  meter          E    =           .0010403
     Z    =       -4239352.95                 I    =           51.32020
     XDOT =      -5901.254178                 Wp   =           83.19053
     YDOT =      -3310.374821  meter/sec      RA   =          234.42488  deg
     ZDOT =      -3589.843159                 TA   =          149.94391
                                              MA   =          149.88416
                                              Ha   =            222.014  n.mi
                                              Hp   =            213.617
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1283888.57                 X    =         -429824.67
     Y    =       17344691.14  feet           Y    =         5282070.14  meter
     Z    =      -13908638.28                 Z    =        -4241347.83
     XDOT =     -19361.070137                 XDOT =       -5846.360661
     YDOT =     -10860.809781  feet/sec       YDOT =       -3376.060082  meter/sec
     ZDOT =     -11777.700653                 ZDOT =       -3618.375544
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9581251.86                 X    =        -2920365.57
     Y    =       14505883.73  feet           Y    =         4421393.36  meter
     Z    =      -13918184.12                 Z    =        -4242262.52
     XDOT =     -10372.332283                 XDOT =       -3161.486880
     YDOT =     -18252.901023  feet/sec       YDOT =       -5563.484232  meter/sec
     ZDOT =     -11904.309804                 ZDOT =       -3628.433628
  
  
    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   18052.52275003  .00016717  00000-0  10270-3 0  9029
    2 25544  51.6361 235.3316 0003086 119.2616 240.8846 15.54138186 20523
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18052.52275003   =   yrday.fracday
    Element set:     902
    Inclination:       51.6361  deg
    RA of node:       235.3316  deg
    Eccentricity:     .0003086     
    Arg of perigee:   119.2616  deg
    Mean anomaly:     240.8846  deg
    Mean motion:   15.54138186  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2052
    Checksum:              286
 
 
    Coasting Arc #4 (Orbit 2067)
    ---------------------------------------
 
    Vector Time (GMT): 2018/053/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1659530.29                 A    =         6778637.29  meter
     Y    =       -4236994.14  meter          E    =           .0008684
     Z    =        5019467.48                 I    =           51.33015
     XDOT =       5884.360651                 Wp   =          124.02173
     YDOT =       4547.696598  meter/sec      RA   =          229.40921  deg
     ZDOT =       1886.163474                 TA   =          307.58577
                                              MA   =          307.66460
                                              Ha   =            221.948  n.mi
                                              Hp   =            213.765
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5444653.17                 X    =         1682404.43
     Y    =      -13900899.42  feet           Y    =        -4218307.89  meter
     Z    =       16468069.14                 Z    =         5027584.69
     XDOT =      19305.645182                 XDOT =        5823.907824
     YDOT =      14920.264430  feet/sec       YDOT =        4613.161680  meter/sec
     ZDOT =       6188.200375                 ZDOT =        1914.600284
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11326211.76                 X    =         3452229.35
     Y    =       -9663702.24  feet           Y    =        -2945496.44  meter
     Z    =       16504736.90                 Z    =         5030643.81
     XDOT =       9094.931567                 XDOT =        2772.135142
     YDOT =      21483.579974  feet/sec       YDOT =        6548.195176  meter/sec
     ZDOT =       6314.245316                 ZDOT =        1924.581972
  
  
    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   18053.55158171  .00016717  00000-0  10270-3 0  9030
    2 25544  51.6365 230.2021 0002963 123.2363 236.9074 15.54107784 20687
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18053.55158171   =   yrday.fracday
    Element set:     903
    Inclination:       51.6365  deg
    RA of node:       230.2021  deg
    Eccentricity:     .0002963     
    Arg of perigee:   123.2363  deg
    Mean anomaly:     236.9074  deg
    Mean motion:   15.54107784  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2068
    Checksum:              291
 
 
    Coasting Arc #5 (Orbit 2082)
    ---------------------------------------
 
    Vector Time (GMT): 2018/054/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2994976.61                 A    =         6777309.84  meter
     Y    =        3001950.20  meter          E    =           .0017563
     Z    =       -5301969.10                 I    =           51.34873
     XDOT =      -5451.473933                 Wp   =           96.54110
     YDOT =      -5374.869210  meter/sec      RA   =          224.38905  deg
     ZDOT =         34.339938                 TA   =          173.79888
                                              MA   =          173.77711
                                              Ha   =            222.001  n.mi
                                              Hp   =            213.534
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9826038.75                 X    =        -3002568.70
     Y    =        9848917.98  feet           Y    =         2968415.59  meter
     Z    =      -17394911.76                 Z    =        -5316536.13
     XDOT =     -17885.413165                 XDOT =       -5391.132330
     YDOT =     -17634.085336  feet/sec       YDOT =       -5435.493943  meter/sec
     ZDOT =        112.663837                 ZDOT =           8.005654
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13163998.20                 X    =        -4012386.65
     Y    =        4241183.09  feet           Y    =         1292712.61  meter
     Z    =      -17460145.91                 Z    =        -5321852.47
     XDOT =      -7395.626292                 XDOT =       -2254.186894
     YDOT =     -22946.052590  feet/sec       YDOT =       -6993.956829  meter/sec
     ZDOT =         -3.936064                 ZDOT =          -1.199712
  
  
    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   18054.51610522  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6370 225.3938 0003210 126.3264 233.8185 15.54146022 20839
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18054.51610522   =   yrday.fracday
    Element set:     904
    Inclination:       51.6370  deg
    RA of node:       225.3938  deg
    Eccentricity:     .0003210     
    Arg of perigee:   126.3264  deg
    Mean anomaly:     233.8185  deg
    Mean motion:   15.54146022  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2083
    Checksum:              274
 
 
    Coasting Arc #6 (Orbit 2098)
    ---------------------------------------
 
    Vector Time (GMT): 2018/055/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4241794.40                 A    =         6778614.78  meter
     Y    =       -1691024.47  meter          E    =           .0007242
     Z    =        5003812.13                 I    =           51.37571
     XDOT =       4620.374788                 Wp   =           81.65096
     YDOT =       5807.340125  meter/sec      RA   =          219.37031  deg
     ZDOT =      -1950.720281                 TA   =           27.35819
                                              MA   =           27.32007
                                              Ha   =            221.887  n.mi
                                              Hp   =            213.764
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13916648.30                 X    =         4236083.05
     Y    =       -5547980.54  feet           Y    =        -1643621.54  meter
     Z    =       16416706.45                 Z    =         5024403.23
     XDOT =      15158.709935                 XDOT =        4564.567599
     YDOT =      19052.953166  feet/sec       YDOT =        5858.696213  meter/sec
     ZDOT =      -6400.000923                 ZDOT =       -1928.412156
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14831007.01                 X    =         4520490.94
     Y    =        1211766.17  feet           Y    =          369346.33  meter
     Z    =       16508612.67                 Z    =         5031825.14
     XDOT =       5167.354260                 XDOT =        1575.009578
     YDOT =      22756.672946  feet/sec       YDOT =        6936.233914  meter/sec
     ZDOT =      -6301.362253                 ZDOT =       -1920.655215
  
  
    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   18055.54492760  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6356 220.2645 0003214 130.9822 229.1609 15.54112285 20997
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18055.54492760   =   yrday.fracday
    Element set:     905
    Inclination:       51.6356  deg
    RA of node:       220.2645  deg
    Eccentricity:     .0003214     
    Arg of perigee:   130.9822  deg
    Mean anomaly:     229.1609  deg
    Mean motion:   15.54112285  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2099
    Checksum:              299
 
 
    Coasting Arc #7 (Orbit 2113)
    ---------------------------------------
 
    Vector Time (GMT): 2018/056/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5314248.38                 A    =         6781648.93  meter
     Y    =         429082.10  meter          E    =           .0011047
     Z    =       -4203027.78                 I    =           51.41424
     XDOT =      -3360.063301                 Wp   =          117.34010
     YDOT =      -5830.531642  meter/sec      RA   =          214.35999  deg
     ZDOT =       3655.626902                 TA   =          190.28650
                                              MA   =          190.30912
                                              Ha   =            221.893  n.mi
                                              Hp   =            213.628
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17435198.10                 X    =        -5298235.77
     Y    =        1407749.68  feet           Y    =          369743.91  meter
     Z    =      -13789461.22                 Z    =        -4228803.25
     XDOT =     -11023.829728                 XDOT =       -3312.371809
     YDOT =     -19129.040821  feet/sec       YDOT =       -5867.839385  meter/sec
     ZDOT =      11993.526582                 ZDOT =        3639.421193
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16252211.29                 X    =        -4953674.00
     Y    =       -6217132.21  feet           Y    =        -1894981.90  meter
     Z    =      -13904316.87                 Z    =        -4238035.78
     XDOT =      -2212.491197                 XDOT =        -674.367317
     YDOT =     -20861.636640  feet/sec       YDOT =       -6358.626848  meter/sec
     ZDOT =      11922.048729                 ZDOT =        3633.840453
  
  
    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   18056.50944246  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6374 215.4561 0003164 134.9202 225.2208 15.54156151 21140
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18056.50944246   =   yrday.fracday
    Element set:     906
    Inclination:       51.6374  deg
    RA of node:       215.4561  deg
    Eccentricity:     .0003164     
    Arg of perigee:   134.9202  deg
    Mean anomaly:     225.2208  deg
    Mean motion:   15.54156151  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2114
    Checksum:              281
 
 
    Coasting Arc #8 (Orbit 2126)
    ---------------------------------------
 
    Vector Time (GMT): 2018/057/06:58:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1694926.81                 A    =         6781511.41  meter
     Y    =       -4964820.79  meter          E    =           .0012311
     Z    =        4290335.02                 I    =           51.43786
     XDOT =       6778.775823                 Wp   =          112.28948
     YDOT =        735.053417  meter/sec      RA   =          210.46118  deg
     ZDOT =       3515.938372                 TA   =          301.76865
                                              MA   =          301.88854
                                              Ha   =            221.806  n.mi
                                              Hp   =            213.902
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5560783.51                 X    =        -1660122.64
     Y    =      -16288782.13  feet           Y    =        -4983579.85  meter
     Z    =       14075902.31                 Z    =         4282186.56
     XDOT =      22240.078160                 XDOT =        6752.974212
     YDOT =       2411.592574  feet/sec       YDOT =         810.714222  meter/sec
     ZDOT =      11535.230880                 ZDOT =        3548.803963
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17029830.09                 X    =         5190692.21
     Y    =       -2689893.43  feet           Y    =         -819879.52  meter
     Z    =       14040196.68                 Z    =         4279451.95
     XDOT =      -6482.802118                 XDOT =       -1975.958085
     YDOT =      20147.834707  feet/sec       YDOT =        6141.060019  meter/sec
     ZDOT =      11681.543180                 ZDOT =        3560.534361
  
  
    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   18057.34535155  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6401 211.2936 0002603 130.7675 229.3704 15.54143713 21276
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18057.34535155   =   yrday.fracday
    Element set:     907
    Inclination:       51.6401  deg
    RA of node:       211.2936  deg
    Eccentricity:     .0002603     
    Arg of perigee:   130.7675  deg
    Mean anomaly:     229.3704  deg
    Mean motion:   15.54143713  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2127
    Checksum:              286
 
 
    Coasting Arc #9 (Orbit 2141)
    ---------------------------------------
 
    Vector Time (GMT): 2018/058/06:58:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =          60149.90                 A    =         6778284.11  meter
     Y    =        4507005.73  meter          E    =           .0014667
     Z    =       -5075438.06                 I    =           51.45488
     XDOT =      -7211.632915                 Wp   =           85.45586
     YDOT =      -1880.606517  meter/sec      RA   =          205.45244  deg
     ZDOT =      -1758.710495                 TA   =          167.48558
                                              MA   =          167.44912
                                              Ha   =            221.657  n.mi
                                              Hp   =            213.881
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         197342.20                 X    =           34400.10
     Y    =       14786764.20  feet           Y    =         4507534.10  meter
     Z    =      -16651699.69                 Z    =        -5075208.68
     XDOT =     -23660.212976                 XDOT =       -7181.524796
     YDOT =      -6169.968887  feet/sec       YDOT =       -1961.083705  meter/sec
     ZDOT =      -5770.047556                 ZDOT =       -1793.668053
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14645058.83                 X    =        -4463813.93
     Y    =       -2055724.68  feet           Y    =         -626584.88  meter
     Z    =      -16651206.87                 Z    =        -5075287.85
     XDOT =       9710.309902                 XDOT =        2959.702458
     YDOT =     -21266.600107  feet/sec       YDOT =       -6482.059713  meter/sec
     ZDOT =      -5925.567529                 ZDOT =       -1806.112983
  
  
    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   18058.30985719  .00016717  00000-0  10270-3 0  9089
    2 25544  51.6387 206.4842 0002553 135.3188 224.8170 15.54180714 21421
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18058.30985719   =   yrday.fracday
    Element set:     908
    Inclination:       51.6387  deg
    RA of node:       206.4842  deg
    Eccentricity:     .0002553     
    Arg of perigee:   135.3188  deg
    Mean anomaly:     224.8170  deg
    Mean motion:   15.54180714  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2142
    Checksum:              314
 
 
    Coasting Arc #10 (Orbit 2152)
    ---------------------------------------
 
    Vector Time (GMT): 2018/058/23:08:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1305431.53                 A    =         6779511.36  meter
     Y    =       -4630033.25  meter          E    =           .0010127
     Z    =        4772193.25                 I    =           51.47704
     XDOT =       7182.818758                 Wp   =          124.19475
     YDOT =        673.889329  meter/sec      RA   =          202.09274  deg
     ZDOT =       2609.122351                 TA   =          299.98824
                                              MA   =          300.08871
                                              Ha   =            221.689  n.mi
                                              Hp   =            213.897
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4282911.84                 X    =        -1276740.45
     Y    =      -15190397.80  feet           Y    =        -4644470.72  meter
     Z    =       15656802.01                 Z    =         4765922.09
     XDOT =      23565.678341                 XDOT =        7162.075881
     YDOT =       2210.922996  feet/sec       YDOT =         754.096750  meter/sec
     ZDOT =       8560.112700                 ZDOT =        2643.962697
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5383870.70                 X    =        -1641003.79
     Y    =       14864817.94  feet           Y    =         4530796.51  meter
     Z    =       15629398.33                 Z    =         4763840.61
     XDOT =     -16630.417726                 XDOT =       -5068.951323
     YDOT =     -15219.892501  feet/sec       YDOT =       -4639.023234  meter/sec
     ZDOT =       8715.267001                 ZDOT =        2656.413382
  
  
    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   18059.01716070  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6365 202.9580 0002698 139.6292 220.5062 15.54190440 21532
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18059.01716070   =   yrday.fracday
    Element set:     909
    Inclination:       51.6365  deg
    RA of node:       202.9580  deg
    Eccentricity:     .0002698     
    Arg of perigee:   139.6292  deg
    Mean anomaly:     220.5062  deg
    Mean motion:   15.54190440  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2153
    Checksum:              297
 
 
    Coasting Arc #11 (Orbit 2167)
    ---------------------------------------
 
    Vector Time (GMT): 2018/059/23:08:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -449372.27                 A    =         6777432.09  meter
     Y    =        4250285.30  meter          E    =           .0016233
     Z    =       -5273891.68                 I    =           51.50187
     XDOT =      -7434.458863                 Wp   =           92.53167
     YDOT =      -1681.866161  meter/sec      RA   =          197.08356  deg
     ZDOT =       -724.600226                 TA   =          170.53839
                                              MA   =          170.50777
                                              Ha   =            221.681  n.mi
                                              Hp   =            213.893
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1474318.47                 X    =         -471249.56
     Y    =       13944505.58  feet           Y    =         4245137.27  meter
     Z    =      -17302794.22                 Z    =        -5276128.07
     XDOT =     -24391.269234                 XDOT =       -7411.579602
     YDOT =      -5517.933600  feet/sec       YDOT =       -1764.875534  meter/sec
     ZDOT =      -2377.297330                 ZDOT =        -760.657614
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9117381.91                 X    =         2778978.01
     Y    =      -10636465.95  feet           Y    =        -3241994.82  meter
     Z    =      -17313245.73                 Z    =        -5277077.30
     XDOT =      16016.091510                 XDOT =        4881.704692
     YDOT =      17845.448066  feet/sec       YDOT =        5439.292571  meter/sec
     ZDOT =      -2537.779906                 ZDOT =        -773.515315
  
  
    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   18059.98166162  .00016717  00000-0  10270-3 0  9100
    2 25544  51.6375 198.1487 0002728 140.5071 219.6281 15.54171330 21680
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18059.98166162   =   yrday.fracday
    Element set:     910
    Inclination:       51.6375  deg
    RA of node:       198.1487  deg
    Eccentricity:     .0002728     
    Arg of perigee:   140.5071  deg
    Mean anomaly:     219.6281  deg
    Mean motion:   15.54171330  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2168
    Checksum:              314
 
 
    Coasting Arc #12 (Orbit 2177)
    ---------------------------------------
 
    Vector Time (GMT): 2018/060/14:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3795379.92                 A    =         6782960.82  meter
     Y    =        4096001.71  meter          E    =           .0007532
     Z    =       -3856039.41                 I    =           51.54391
     XDOT =      -6183.024881                 Wp   =           98.54693
     YDOT =       1847.518203  meter/sec      RA   =          193.92319  deg
     ZDOT =      -4131.279628                 TA   =          127.97392
                                              MA   =          127.90586
                                              Ha   =            221.666  n.mi
                                              Hp   =            214.061
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12452033.87                 X    =         3768025.41
     Y    =       13438325.82  feet           Y    =         4138290.87  meter
     Z    =      -12651047.92                 Z    =        -3837670.11
     XDOT =     -20285.514703                 XDOT =       -6183.157694
     YDOT =       6061.411426  feet/sec       YDOT =        1778.374156  meter/sec
     ZDOT =     -13554.067021                 ZDOT =       -4161.314437
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15538388.02                 X    =         4736100.67
     Y    =        9810868.03  feet           Y    =         2990352.58  meter
     Z    =      -12569651.07                 Z    =        -3831229.65
     XDOT =     -17277.253414                 XDOT =       -5266.106841
     YDOT =       9860.308885  feet/sec       YDOT =        3005.422148  meter/sec
     ZDOT =     -13688.123409                 ZDOT =       -4172.140015
  
  
    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   18060.62465832  .00016717  00000-0  10270-3 0  9110
    2 25544  51.6410 194.9410 0002975 150.6464 209.4857 15.54179389 21781
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18060.62465832   =   yrday.fracday
    Element set:     911
    Inclination:       51.6410  deg
    RA of node:       194.9410  deg
    Eccentricity:     .0002975     
    Arg of perigee:   150.6464  deg
    Mean anomaly:     209.4857  deg
    Mean motion:   15.54179389  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2178
    Checksum:              325
 
 
    Coasting Arc #13 (Orbit 2193)
    ---------------------------------------
 
    Vector Time (GMT): 2018/061/14:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2219387.74                 A    =         6779252.87  meter
     Y    =       -4218032.92  meter          E    =           .0009867
     Z    =        4816731.80                 I    =           51.56458
     XDOT =       7190.134779                 Wp   =          129.11318
     YDOT =       -894.820365  meter/sec      RA   =          188.92698  deg
     ZDOT =       2519.810970                 TA   =          296.04301
                                              MA   =          296.14456
                                              Ha   =            221.571  n.mi
                                              Hp   =            213.992
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7281455.84                 X    =        -2195452.28
     Y    =      -13838690.67  feet           Y    =        -4242717.16  meter
     Z    =       15802925.86                 Z    =         4806009.71
     XDOT =      23589.681034                 XDOT =        7187.366853
     YDOT =      -2935.762353  feet/sec       YDOT =        -814.430473  meter/sec
     ZDOT =       8267.096359                 ZDOT =        2554.730843
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10855790.38                 X    =        -3308844.91
     Y    =      -11321393.08  feet           Y    =        -3450760.61  meter
     Z    =       15755611.65                 Z    =         4802310.43
     XDOT =      21035.690129                 XDOT =        6411.678351
     YDOT =      -8405.009371  feet/sec       YDOT =       -2561.846856  meter/sec
     ZDOT =       8422.829144                 ZDOT =        2567.278323
  
  
    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   18061.65344832  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6414 189.8125 0002897 153.5615 206.5686 15.54225877 21944
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18061.65344832   =   yrday.fracday
    Element set:     912
    Inclination:       51.6414  deg
    RA of node:       189.8125  deg
    Eccentricity:     .0002897     
    Arg of perigee:   153.5615  deg
    Mean anomaly:     206.5686  deg
    Mean motion:   15.54225877  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2194
    Checksum:              329
 
 
    Coasting Arc #14 (Orbit 2208)
    ---------------------------------------
 
    Vector Time (GMT): 2018/062/14:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         407547.73                 A    =         6777333.32  meter
     Y    =        4232737.22  meter          E    =           .0015719
     Z    =       -5290738.79                 I    =           51.58986
     XDOT =      -7632.197082                 Wp   =           95.15847
     YDOT =        -33.048610  meter/sec      RA   =          183.92498  deg
     ZDOT =       -617.314420                 TA   =          168.95349
                                              MA   =          168.91894
                                              Ha   =            221.493  n.mi
                                              Hp   =            214.124
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1337098.86                 X    =          385885.05
     Y    =       13886933.12  feet           Y    =         4237172.80  meter
     Z    =      -17358066.89                 Z    =        -5288812.32
     XDOT =     -25040.016673                 XDOT =       -7628.261745
     YDOT =       -108.427198  feet/sec       YDOT =        -118.375171  meter/sec
     ZDOT =      -2025.309776                 ZDOT =        -654.378843
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5378835.72                 X    =         1639469.13
     Y    =       12883499.36  feet           Y    =         3926890.60  meter
     Z    =      -17349951.06                 Z    =        -5288265.08
     XDOT =     -23063.245862                 XDOT =       -7029.677339
     YDOT =       6692.040263  feet/sec       YDOT =        2039.733872  meter/sec
     ZDOT =      -2190.512115                 ZDOT =        -667.668093
  
  
    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   18062.61793673  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6408 185.0049 0002816 157.5013 202.6263 15.54187366 22092
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18062.61793673   =   yrday.fracday
    Element set:     913
    Inclination:       51.6408  deg
    RA of node:       185.0049  deg
    Eccentricity:     .0002816     
    Arg of perigee:   157.5013  deg
    Mean anomaly:     202.6263  deg
    Mean motion:   15.54187366  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2209
    Checksum:              306
 
 
    Coasting Arc #15 (Orbit 2224)
    ---------------------------------------
 
    Vector Time (GMT): 2018/063/14:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1439102.49                 A    =         6777545.54  meter
     Y    =       -4126799.83  meter          E    =           .0004360
     Z    =        5176317.65                 I    =           51.62516
     XDOT =       7496.359244                 Wp   =           92.38386
     YDOT =        924.941287  meter/sec      RA   =          178.92216  deg
     ZDOT =      -1345.905473                 TA   =           10.55116
                                              MA   =           10.54202
                                              Ha   =            221.288  n.mi
                                              Hp   =            214.107
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4721464.86                 X    =         1459998.98
     Y    =      -13539369.51  feet           Y    =        -4110589.21  meter
     Z    =       16982669.45                 Z    =         5183359.58
     XDOT =      24594.354474                 XDOT =        7491.996785
     YDOT =       3034.584274  feet/sec       YDOT =        1008.746145  meter/sec
     ZDOT =      -4415.700372                 ZDOT =       -1309.501898
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         280586.15                 X    =           85522.66
     Y    =      -14298435.45  feet           Y    =        -4358163.13  meter
     Z    =       17014518.32                 Z    =         5186025.19
     XDOT =      23338.970598                 XDOT =        7113.718238
     YDOT =      -4606.641763  feet/sec       YDOT =       -1404.104409  meter/sec
     ZDOT =      -4253.527349                 ZDOT =       -1296.475136
  
  
    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   18063.64671548  .00016717  00000-0  10270-3 0  9141
    2 25544  51.6417 179.8758 0002696 161.3082 198.8170 15.54250255 22254
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18063.64671548   =   yrday.fracday
    Element set:     914
    Inclination:       51.6417  deg
    RA of node:       179.8758  deg
    Eccentricity:     .0002696     
    Arg of perigee:   161.3082  deg
    Mean anomaly:     198.8170  deg
    Mean motion:   15.54250255  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2225
    Checksum:              329
 
 
    Coasting Arc #16 (Orbit 2226)
    ---------------------------------------
 
    Vector Time (GMT): 2018/063/17:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3748675.55                 A    =         6780642.74  meter
     Y    =       -3438476.21  meter          E    =           .0011367
     Z    =        4478132.90                 I    =           51.63748
     XDOT =       6392.700565                 Wp   =          120.29198
     YDOT =      -2743.503203  meter/sec      RA   =          178.35678  deg
     ZDOT =       3233.072397                 TA   =          297.13592
                                              MA   =          297.25179
                                              Ha   =            221.583  n.mi
                                              Hp   =            214.013
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12298804.29                 X    =        -3731699.15
     Y    =      -11281089.93  feet           Y    =        -3480300.92  meter
     Z    =       14692037.08                 Z    =         4459965.06
     XDOT =      20973.427051                 XDOT =        6407.199650
     YDOT =      -9000.994760  feet/sec       YDOT =       -2671.934099  meter/sec
     ZDOT =      10607.192903                 ZDOT =        3264.161191
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15858952.71                 X    =        -4833808.79
     Y    =        5420260.35  feet           Y    =         1652095.35  meter
     Z    =       14611431.38                 Z    =         4453564.29
     XDOT =       2589.639363                 XDOT =         789.322078
     YDOT =     -21495.731148  feet/sec       YDOT =       -6551.898854  meter/sec
     ZDOT =      10746.083092                 ZDOT =        3275.406126
  
  
    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   18063.77531416  .00016717  00000-0  10270-3 0  9155
    2 25544  51.6403 179.2357 0002720 151.3417 208.7885 15.54220336 22270
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18063.77531416   =   yrday.fracday
    Element set:     915
    Inclination:       51.6403  deg
    RA of node:       179.2357  deg
    Eccentricity:     .0002720     
    Arg of perigee:   151.3417  deg
    Mean anomaly:     208.7885  deg
    Mean motion:   15.54220336  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2227
    Checksum:              299
 
 
    Coasting Arc #17 (Orbit 2241)
    ---------------------------------------
 
    Vector Time (GMT): 2018/064/17:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2050476.35                 A    =         6777804.06  meter
     Y    =        3882417.06  meter          E    =           .0014587
     Z    =       -5176062.51                 I    =           51.66174
     XDOT =      -7266.196116                 Wp   =           89.58740
     YDOT =       1965.990994  meter/sec      RA   =          173.36180  deg
     ZDOT =      -1407.169624                 TA   =          166.88282
                                              MA   =          166.84485
                                              Ha   =            221.424  n.mi
                                              Hp   =            214.149
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6727284.62                 X    =         2032052.11
     Y    =       12737588.79  feet           Y    =         3905243.21  meter
     Z    =      -16981832.38                 Z    =        -5166147.33
     XDOT =     -23839.226102                 XDOT =       -7280.805087
     YDOT =       6450.101685  feet/sec       YDOT =        1884.653526  meter/sec
     ZDOT =      -4616.698242                 ZDOT =       -1442.501753
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14456052.13                 X    =         4406204.69
     Y    =         -99035.71  feet           Y    =          -30186.09  meter
     Z    =      -16938060.88                 Z    =        -5162720.96
     XDOT =      -5423.703877                 XDOT =       -1653.144942
     YDOT =      23010.197509  feet/sec       YDOT =        7013.508201  meter/sec
     ZDOT =      -4774.434181                 ZDOT =       -1455.247538
  
  
    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   18064.73978877  .00016717  00000-0  10270-3 0  9169
    2 25544  51.6412 174.4277 0002640 156.3134 203.8141 15.54215141 22426
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18064.73978877   =   yrday.fracday
    Element set:     916
    Inclination:       51.6412  deg
    RA of node:       174.4277  deg
    Eccentricity:     .0002640     
    Arg of perigee:   156.3134  deg
    Mean anomaly:     203.8141  deg
    Mean motion:   15.54215141  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2242
    Checksum:              299
 
             

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