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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15846.6289
   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 2082)
    ---------------------------------------
 
    Vector Time (GMT): 2018/054/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920932.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2992333.59                 A    =         6777325.90  meter
     Y    =        3004591.83  meter          E    =           .0017559
     Z    =       -5301984.94                 I    =           51.34856
     XDOT =      -5453.342827                 Wp   =           96.41211
     YDOT =      -5372.980798  meter/sec      RA   =          224.38857  deg
     ZDOT =         31.098959                 TA   =          173.89664
                                              MA   =          173.87522
                                              Ha   =            222.007  n.mi
                                              Hp   =            213.544
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9817367.42                 X    =        -2999955.34
     Y    =        9857584.73  feet           Y    =         2971086.60  meter
     Z    =      -17394963.70                 Z    =        -5316539.19
     XDOT =     -17891.544708                 XDOT =       -5393.006460
     YDOT =     -17627.889757  feet/sec       YDOT =       -5433.626459  meter/sec
     ZDOT =        102.030704                 ZDOT =           4.755584
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13160316.91                 X    =        -4011264.59
     Y    =        4252877.33  feet           Y    =         1296277.01  meter
     Z    =      -17460141.33                 Z    =        -5321851.08
     XDOT =      -7403.012309                 XDOT =       -2256.438152
     YDOT =     -22943.631035  feet/sec       YDOT =       -6993.218739  meter/sec
     ZDOT =        -14.609912                 ZDOT =          -4.453101
  
  
    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   18054.51611082  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6368 225.3935 0003190 125.8429 234.3021 15.54140528 20837
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18054.51611082   =   yrday.fracday
    Element set:     900
    Inclination:       51.6368  deg
    RA of node:       225.3935  deg
    Eccentricity:     .0003190     
    Arg of perigee:   125.8429  deg
    Mean anomaly:     234.3021  deg
    Mean motion:   15.54140528  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2083
    Checksum:              280
 
 
    Coasting Arc #2 (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    =        4237978.99                 A    =         6778629.40  meter
     Y    =       -1695886.57  meter          E    =           .0007237
     Z    =        5005431.23                 I    =           51.37552
     XDOT =       4624.916757                 Wp   =           81.44004
     YDOT =       5805.490615  meter/sec      RA   =          219.36986  deg
     ZDOT =      -1945.382449                 TA   =           27.51536
                                              MA   =           27.47706
                                              Ha   =            221.897  n.mi
                                              Hp   =            213.775
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13904130.53                 X    =         4232314.43
     Y    =       -5563932.32  feet           Y    =        -1648526.05  meter
     Z    =       16422018.46                 Z    =         5026003.91
     XDOT =      15173.611407                 XDOT =        4569.103983
     YDOT =      19046.885219  feet/sec       YDOT =        5856.897464  meter/sec
     ZDOT =      -6382.488350                 ZDOT =       -1923.052274
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14826910.28                 X    =         4519242.25
     Y    =        1191885.80  feet           Y    =          363286.79  meter
     Z    =       16513843.24                 Z    =         5033419.42
     XDOT =       5181.842426                 XDOT =        1579.425571
     YDOT =      22758.155469  feet/sec       YDOT =        6936.685787  meter/sec
     ZDOT =      -6283.751259                 ZDOT =       -1915.287384
  
  
    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   18055.54493747  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6354 220.2641 0003197 130.5210 229.6221 15.54104949 20991
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18055.54493747   =   yrday.fracday
    Element set:     901
    Inclination:       51.6354  deg
    RA of node:       220.2641  deg
    Eccentricity:     .0003197     
    Arg of perigee:   130.5210  deg
    Mean anomaly:     229.6221  deg
    Mean motion:   15.54104949  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2099
    Checksum:              295
 
 
    Coasting Arc #3 (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    =       -5309903.74                 A    =         6781658.97  meter
     Y    =         436701.10  meter          E    =           .0011065
     Z    =       -4207764.99                 I    =           51.41401
     XDOT =      -3368.853792                 Wp   =          117.20227
     YDOT =      -5829.792900  meter/sec      RA   =          214.35957  deg
     ZDOT =       3648.670907                 TA   =          190.34046
                                              MA   =          190.36324
                                              Ha   =            221.907  n.mi
                                              Hp   =            213.641
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17420944.04                 X    =        -5293953.65
     Y    =        1432746.41  feet           Y    =          377411.14  meter
     Z    =      -13805003.23                 Z    =        -4233519.51
     XDOT =     -11052.669921                 XDOT =       -3321.136119
     YDOT =     -19126.617127  feet/sec       YDOT =       -5867.198798  meter/sec
     ZDOT =      11970.705076                 ZDOT =        3632.422561
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16250049.77                 X    =        -4953015.17
     Y    =       -6188388.42  feet           Y    =        -1886220.79  meter
     Z    =      -13919766.49                 Z    =        -4242744.83
     XDOT =      -2237.319508                 XDOT =        -681.934986
     YDOT =     -20871.992440  feet/sec       YDOT =       -6361.783296  meter/sec
     ZDOT =      11899.037229                 ZDOT =        3626.826547
  
  
    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   18056.50945749  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6372 215.4558 0003149 134.4837 225.6573 15.54146916 21143
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18056.50945749   =   yrday.fracday
    Element set:     902
    Inclination:       51.6372  deg
    RA of node:       215.4558  deg
    Eccentricity:     .0003149     
    Arg of perigee:   134.4837  deg
    Mean anomaly:     225.6573  deg
    Mean motion:   15.54146916  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2114
    Checksum:              319
 
 
    Coasting Arc #4 (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    =       -1706669.06                 A    =         6781564.89  meter
     Y    =       -4966088.61  meter          E    =           .0012331
     Z    =        4284256.43                 I    =           51.43777
     XDOT =       6775.028351                 Wp   =          112.04833
     YDOT =        724.012959  meter/sec      RA   =          210.46081  deg
     ZDOT =       3525.430538                 TA   =          301.89774
                                              MA   =          302.01765
                                              Ha   =            221.823  n.mi
                                              Hp   =            213.916
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5599307.93                 X    =        -1671820.31
     Y    =      -16292941.65  feet           Y    =        -4984978.73  meter
     Z    =       14055959.42                 Z    =         4276051.03
     XDOT =      22227.783304                 XDOT =        6749.304369
     YDOT =       2375.370599  feet/sec       YDOT =         799.632292  meter/sec
     ZDOT =      11566.373156                 ZDOT =        3558.278114
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17040702.33                 X    =         5194006.07
     Y    =       -2726948.17  feet           Y    =         -831173.80  meter
     Z    =       14020000.35                 Z    =         4273296.11
     XDOT =      -6447.647002                 XDOT =       -1965.242806
     YDOT =      20141.131060  feet/sec       YDOT =        6139.016747  meter/sec
     ZDOT =      11712.606527                 ZDOT =        3570.002469
  
  
    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   18057.34537198  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6399 211.2932 0002593 130.2258 229.9121 15.54133048 21277
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18057.34537198   =   yrday.fracday
    Element set:     903
    Inclination:       51.6399  deg
    RA of node:       211.2932  deg
    Eccentricity:     .0002593     
    Arg of perigee:   130.2258  deg
    Mean anomaly:     229.9121  deg
    Mean motion:   15.54133048  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2127
    Checksum:              302
 
 
    Coasting Arc #5 (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    =          77335.28                 A    =         6778339.58  meter
     Y    =        4511507.54  meter          E    =           .0014646
     Z    =       -5071260.18                 I    =           51.45477
     XDOT =      -7211.411850                 Wp   =           85.29728
     YDOT =      -1866.909428  meter/sec      RA   =          205.45222  deg
     ZDOT =      -1774.073042                 TA   =          167.49025
                                              MA   =          167.45385
                                              Ha   =            221.679  n.mi
                                              Hp   =            213.898
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         253724.68                 X    =           51513.57
     Y    =       14801533.91  feet           Y    =         4512227.69  meter
     Z    =      -16637992.72                 Z    =        -5070947.49
     XDOT =     -23659.487696                 XDOT =       -7181.382290
     YDOT =      -6125.030932  feet/sec       YDOT =       -1947.384584  meter/sec
     ZDOT =      -5820.449614                 ZDOT =       -1809.029718
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14668621.61                 X    =        -4470995.87
     Y    =       -2002511.64  feet           Y    =         -610365.55  meter
     Z    =      -16637129.30                 Z    =        -5070997.01
     XDOT =       9669.663123                 XDOT =        2947.313320
     YDOT =     -21271.006761  feet/sec       YDOT =       -6483.402861  meter/sec
     ZDOT =      -5975.967266                 ZDOT =       -1821.474823
  
  
    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   18058.30988488  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6385 206.4839 0002544 134.8111 225.3249 15.54168021 21425
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18058.30988488   =   yrday.fracday
    Element set:     904
    Inclination:       51.6385  deg
    RA of node:       206.4839  deg
    Eccentricity:     .0002544     
    Arg of perigee:   134.8111  deg
    Mean anomaly:     225.3249  deg
    Mean motion:   15.54168021  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2142
    Checksum:              310
 
 
    Coasting Arc #6 (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    =       -1326053.98                 A    =         6779581.55  meter
     Y    =       -4631962.12  meter          E    =           .0010168
     Z    =        4764695.59                 I    =           51.47697
     XDOT =       7177.994659                 Wp   =          123.91409
     YDOT =        656.845734  meter/sec      RA   =          202.09257  deg
     ZDOT =       2626.648343                 TA   =          300.08276
                                              MA   =          300.18354
                                              Ha   =            221.713  n.mi
                                              Hp   =            213.915
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4350570.79                 X    =        -1297303.37
     Y    =      -15196726.13  feet           Y    =        -4646629.87  meter
     Z    =       15632203.36                 Z    =         4758324.40
     XDOT =      23549.851245                 XDOT =        7157.357597
     YDOT =       2155.005688  feet/sec       YDOT =         736.999801  meter/sec
     ZDOT =       8617.612674                 ZDOT =        2661.465515
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5333000.01                 X    =        -1625498.40
     Y    =       14909626.87  feet           Y    =         4544454.27  meter
     Z    =       15604354.22                 Z    =         4756207.17
     XDOT =     -16646.919902                 XDOT =       -5073.981186
     YDOT =     -15168.847707  feet/sec       YDOT =       -4623.464781  meter/sec
     ZDOT =       8772.665698                 ZDOT =        2673.908505
  
  
    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   18059.01719440  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6363 202.9577 0002692 139.1990 220.9364 15.54176984 21536
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18059.01719440   =   yrday.fracday
    Element set:     905
    Inclination:       51.6363  deg
    RA of node:       202.9577  deg
    Eccentricity:     .0002692     
    Arg of perigee:   139.1990  deg
    Mean anomaly:     220.9364  deg
    Mean motion:   15.54176984  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2153
    Checksum:              321
 
 
    Coasting Arc #7 (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    =        -421890.36                 A    =         6777490.86  meter
     Y    =        4256512.72  meter          E    =           .0016218
     Z    =       -5271201.08                 I    =           51.50174
     XDOT =      -7436.478877                 Wp   =           92.31590
     YDOT =      -1661.852143  meter/sec      RA   =          197.08358  deg
     ZDOT =       -749.398302                 TA   =          170.51523
                                              MA   =          170.48456
                                              Ha   =            221.708  n.mi
                                              Hp   =            213.915
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1384154.74                 X    =         -443852.41
     Y    =       13964936.75  feet           Y    =         4251671.54  meter
     Z    =      -17293966.78                 Z    =        -5273304.18
     XDOT =     -24397.896578                 XDOT =       -7413.702815
     YDOT =      -5452.270812  feet/sec       YDOT =       -1744.884685  meter/sec
     ZDOT =      -2458.655846                 ZDOT =        -785.465754
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9055330.00                 X    =         2760064.58
     Y    =      -10704917.88  feet           Y    =        -3262858.97  meter
     Z    =      -17303825.06                 Z    =        -5274205.88
     XDOT =      16053.775130                 XDOT =        4893.190660
     YDOT =      17799.706899  feet/sec       YDOT =        5425.350663  meter/sec
     ZDOT =      -2619.185560                 ZDOT =        -798.327759
  
  
    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   18059.98170455  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6373 198.1484 0002724 140.0798 220.0556 15.54155592 21685
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18059.98170455   =   yrday.fracday
    Element set:     906
    Inclination:       51.6373  deg
    RA of node:       198.1484  deg
    Eccentricity:     .0002724     
    Arg of perigee:   140.0798  deg
    Mean anomaly:     220.0556  deg
    Mean motion:   15.54155592  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2168
    Checksum:              324
 
 
    Coasting Arc #8 (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    =        3821789.41                 A    =         6783067.84  meter
     Y    =        4088091.35  meter          E    =           .0007495
     Z    =       -3838384.70                 I    =           51.54393
     XDOT =      -6162.261382                 Wp   =           98.96235
     YDOT =       1869.821920  meter/sec      RA   =          193.92308  deg
     ZDOT =      -4152.237354                 TA   =          127.28217
                                              MA   =          127.21382
                                              Ha   =            221.696  n.mi
                                              Hp   =            214.083
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12538679.17                 X    =         3794435.63
     Y    =       13412373.21  feet           Y    =         4130675.85  meter
     Z    =      -12593125.64                 Z    =        -3819887.11
     XDOT =     -20217.392984                 XDOT =       -6162.543345
     YDOT =       6134.586353  feet/sec       YDOT =        1800.909229  meter/sec
     ZDOT =     -13622.825965                 ZDOT =       -4182.171669
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15615223.84                 X    =         4759520.23
     Y    =        9763851.63  feet           Y    =         2976021.98  meter
     Z    =      -12511156.20                 Z    =        -3813400.41
     XDOT =     -17195.765488                 XDOT =       -5241.269321
     YDOT =       9908.048047  feet/sec       YDOT =        3019.973045  meter/sec
     ZDOT =     -13756.437036                 ZDOT =       -4192.962008
  
  
    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   18060.62470803  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6408 194.9408 0002971 150.2795 209.8527 15.54162446 21788
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18060.62470803   =   yrday.fracday
    Element set:     907
    Inclination:       51.6408  deg
    RA of node:       194.9408  deg
    Eccentricity:     .0002971     
    Arg of perigee:   150.2795  deg
    Mean anomaly:     209.8527  deg
    Mean motion:   15.54162446  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2178
    Checksum:              321
 
 
    Coasting Arc #9 (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    =       -2257299.20                 A    =         6779364.24  meter
     Y    =       -4213268.15  meter          E    =           .0009948
     Z    =        4803378.27                 I    =           51.56460
     XDOT =       7175.026623                 Wp   =          128.70318
     YDOT =       -923.280995  meter/sec      RA   =          188.92717  deg
     ZDOT =       2552.315390                 TA   =          296.11067
                                              MA   =          296.21300
                                              Ha   =            221.606  n.mi
                                              Hp   =            214.017
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7405837.26                 X    =        -2233349.34
     Y    =      -13823058.23  feet           Y    =        -4238376.26  meter
     Z    =       15759115.06                 Z    =         4792472.05
     XDOT =      23540.113594                 XDOT =        7172.420188
     YDOT =      -3029.137124  feet/sec       YDOT =        -843.059146  meter/sec
     ZDOT =       8373.738156                 ZDOT =        2587.162270
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10971015.52                 X    =        -3343965.53
     Y    =      -11272755.08  feet           Y    =        -3435935.75  meter
     Z    =       15710979.70                 Z    =         4788706.61
     XDOT =      20965.568301                 XDOT =        6390.305218
     YDOT =      -8472.878394  feet/sec       YDOT =       -2582.533335  meter/sec
     ZDOT =       8529.148812                 ZDOT =        2599.684558
  
  
    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   18061.65351004  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6412 189.8123 0002896 153.2160 206.9142 15.54206751 21942
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18061.65351004   =   yrday.fracday
    Element set:     908
    Inclination:       51.6412  deg
    RA of node:       189.8123  deg
    Eccentricity:     .0002896     
    Arg of perigee:   153.2160  deg
    Mean anomaly:     206.9142  deg
    Mean motion:   15.54206751  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2194
    Checksum:              291
 
 
    Coasting Arc #10 (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    =         456437.14                 A    =         6777416.04  meter
     Y    =        4232897.97  meter          E    =           .0015689
     Z    =       -5286691.99                 I    =           51.58975
     XDOT =      -7628.635218                 Wp   =           94.85825
     YDOT =          1.434228  meter/sec      RA   =          183.92548  deg
     ZDOT =       -660.475341                 TA   =          168.83932
                                              MA   =          168.80448
                                              Ha   =            221.532  n.mi
                                              Hp   =            214.154
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1497497.17                 X    =          434749.37
     Y    =       13887460.55  feet           Y    =         4237880.14  meter
     Z    =      -17344790.01                 Z    =        -5284528.10
     XDOT =     -25028.330769                 XDOT =       -7624.876093
     YDOT =          4.705471  feet/sec       YDOT =         -83.853494  meter/sec
     ZDOT =      -2166.913849                 ZDOT =        -697.522896
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5532539.57                 X    =         1686318.06
     Y    =       12837960.30  feet           Y    =         3913010.30  meter
     Z    =      -17335615.94                 Z    =        -5283895.74
     XDOT =     -23021.986118                 XDOT =       -7017.101369
     YDOT =       6785.561858  feet/sec       YDOT =        2068.239254  meter/sec
     ZDOT =      -2332.044834                 ZDOT =        -710.807265
  
  
    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   18062.61801113  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6406 185.0049 0002818 157.1904 202.9375 15.54165715 22098
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18062.61801113   =   yrday.fracday
    Element set:     909
    Inclination:       51.6406  deg
    RA of node:       185.0049  deg
    Eccentricity:     .0002818     
    Arg of perigee:   157.1904  deg
    Mean anomaly:     202.9375  deg
    Mean motion:   15.54165715  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2209
    Checksum:              296
 
 
    Coasting Arc #11 (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    =        1381637.13                 A    =         6777572.13  meter
     Y    =       -4133783.86  meter          E    =           .0004297
     Z    =        5186463.83                 I    =           51.62484
     XDOT =       7510.145107                 Wp   =           93.49632
     YDOT =        884.481426  meter/sec      RA   =          178.92285  deg
     ZDOT =      -1295.019308                 TA   =            8.94123
                                              MA   =            8.93358
                                              Ha   =            221.333  n.mi
                                              Hp   =            214.138
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4532930.23                 X    =         1402566.71
     Y    =      -13562282.99  feet           Y    =        -4118215.67  meter
     Z    =       17015957.45                 Z    =         5193226.70
     XDOT =      24639.583684                 XDOT =        7505.986882
     YDOT =       2901.841948  feet/sec       YDOT =         968.441597  meter/sec
     ZDOT =      -4248.751009                 ZDOT =       -1258.548264
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =          93791.70                 X    =           28587.71
     Y    =      -14262947.55  feet           Y    =        -4347346.41  meter
     Z    =       17046563.13                 Z    =         5195792.44
     XDOT =      23343.295791                 XDOT =        7115.036557
     YDOT =      -4732.881769  feet/sec       YDOT =       -1442.582363  meter/sec
     ZDOT =      -4086.272745                 ZDOT =       -1245.495933
  
  
    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   18063.64680488  .00016717  00000-0  10270-3 0  9100
    2 25544  51.6415 179.8758 0002702 161.0108 199.1146 15.54226390 22256
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18063.64680488   =   yrday.fracday
    Element set:     910
    Inclination:       51.6415  deg
    RA of node:       179.8758  deg
    Eccentricity:     .0002702     
    Arg of perigee:   161.0108  deg
    Mean anomaly:     199.1146  deg
    Mean motion:   15.54226390  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2225
    Checksum:              310
 
 
    Coasting Arc #12 (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    =       -3798566.61                 A    =         6780811.06  meter
     Y    =       -3416919.96  meter          E    =           .0011480
     Z    =        4452702.79                 I    =           51.63763
     XDOT =       6354.944743                 Wp   =          119.69180
     YDOT =      -2777.786451  meter/sec      RA   =          178.35726  deg
     ZDOT =       3277.821257                 TA   =          297.22852
                                              MA   =          297.34545
                                              Ha   =            221.628  n.mi
                                              Hp   =            214.045
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12462488.87                 X    =        -3781704.02
     Y    =      -11210367.32  feet           Y    =        -3459303.22  meter
     Z    =       14608604.95                 Z    =         4434292.31
     XDOT =      20849.556244                 XDOT =        6369.612634
     YDOT =      -9113.472607  feet/sec       YDOT =       -2706.638608  meter/sec
     ZDOT =      10754.006749                 ZDOT =        3308.727063
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15875660.02                 X    =        -4838901.17
     Y    =        5597272.06  feet           Y    =         1706048.52  meter
     Z    =       14526915.28                 Z    =         4427803.78
     XDOT =       2443.824193                 XDOT =         744.877614
     YDOT =     -21439.376910  feet/sec       YDOT =       -6534.722082  meter/sec
     ZDOT =      10892.085031                 ZDOT =        3319.907517
  
  
    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   18063.77540554  .00016717  00000-0  10270-3 0  9114
    2 25544  51.6401 179.2357 0002729 151.0185 209.1120 15.54196004 22277
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18063.77540554   =   yrday.fracday
    Element set:     911
    Inclination:       51.6401  deg
    RA of node:       179.2357  deg
    Eccentricity:     .0002729     
    Arg of perigee:   151.0185  deg
    Mean anomaly:     209.1120  deg
    Mean motion:   15.54196004  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2227
    Checksum:              285
 
 
    Coasting Arc #13 (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    =        2117451.01                 A    =         6777941.29  meter
     Y    =        3864126.27  meter          E    =           .0014492
     Z    =       -5162850.67                 I    =           51.66177
     XDOT =      -7241.692576                 Wp   =           89.27073
     YDOT =       2011.433401  meter/sec      RA   =          173.36273  deg
     ZDOT =      -1467.982559                 TA   =          166.60233
                                              MA   =          166.56381
                                              Ha   =            221.473  n.mi
                                              Hp   =            214.187
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6947017.74                 X    =         2099162.15
     Y    =       12677579.63  feet           Y    =         3887702.14  meter
     Z    =      -16938486.47                 Z    =        -5152609.83
     XDOT =     -23758.833910                 XDOT =       -7256.516122
     YDOT =       6599.190947  feet/sec       YDOT =        1930.368741  meter/sec
     ZDOT =      -4816.215744                 ZDOT =       -1503.196186
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14505482.80                 X    =         4421271.16
     Y    =        -321099.21  feet           Y    =          -97871.04  meter
     Z    =      -16893261.04                 Z    =        -5149065.97
     XDOT =      -5269.920099                 XDOT =       -1606.271646
     YDOT =      23003.969054  feet/sec       YDOT =        7011.609768  meter/sec
     ZDOT =      -4973.428436                 ZDOT =       -1515.900987
  
  
    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   18064.73989596  .00016717  00000-0  10270-3 0  9125
    2 25544  51.6410 174.4278 0002652 156.0530 204.0747 15.54188475 22429
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18064.73989596   =   yrday.fracday
    Element set:     912
    Inclination:       51.6410  deg
    RA of node:       174.4278  deg
    Eccentricity:     .0002652     
    Arg of perigee:   156.0530  deg
    Mean anomaly:     204.0747  deg
    Mean motion:   15.54188475  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2242
    Checksum:              318
 
 
    Coasting Arc #14 (Orbit 2257)
    ---------------------------------------
 
    Vector Time (GMT): 2018/065/17:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -308073.88                 A    =         6777173.70  meter
     Y    =       -4210360.45  meter          E    =           .0003923
     Z    =        5298492.47                 I    =           51.69012
     XDOT =       7567.283987                 Wp   =          113.87819
     YDOT =      -1165.176961  meter/sec      RA   =          168.36522  deg
     ZDOT =       -487.166830                 TA   =          340.75617
                                              MA   =          340.77098
                                              Ha   =            221.461  n.mi
                                              Hp   =            214.103
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1010741.08                 X    =         -286706.73
     Y    =      -13813518.55  feet           Y    =        -4213685.48  meter
     Z    =       17383505.47                 Z    =         5297048.33
     XDOT =      24827.047202                 XDOT =        7582.117284
     YDOT =      -3822.759060  feet/sec       YDOT =       -1080.471506  meter/sec
     ZDOT =      -1598.316371                 ZDOT =        -450.371651
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12830762.46                 X    =        -3910816.40
     Y    =       -5235825.41  feet           Y    =        -1595879.58  meter
     Z    =       17377537.84                 Z    =         5296673.53
     XDOT =       7428.238436                 XDOT =        2264.127075
     YDOT =     -22949.443221  feet/sec       YDOT =       -6994.990294  meter/sec
     ZDOT =      -1434.128353                 ZDOT =        -437.122322
  
  
    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   18065.76868104  .00016717  00000-0  10270-3 0  9131
    2 25544  51.6390 169.2989 0002655 156.4112 203.7163 15.54208805 22585
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18065.76868104   =   yrday.fracday
    Element set:     913
    Inclination:       51.6390  deg
    RA of node:       169.2989  deg
    Eccentricity:     .0002655     
    Arg of perigee:   156.4112  deg
    Mean anomaly:     203.7163  deg
    Mean motion:   15.54208805  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2258
    Checksum:              320
 
 
    Coasting Arc #15 (Orbit 2272)
    ---------------------------------------
 
    Vector Time (GMT): 2018/066/17:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1490222.95                 A    =         6778997.25  meter
     Y    =        4469051.27  meter          E    =           .0013522
     Z    =       -4887315.24                 I    =           51.72936
     XDOT =      -7270.225837                 Wp   =          116.18558
     YDOT =        197.749675  meter/sec      RA   =          163.37143  deg
     ZDOT =       2396.962851                 TA   =          177.31463
                                              MA   =          177.30736
                                              Ha   =            221.321  n.mi
                                              Hp   =            214.221
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4889182.89                 X    =        -1516346.47
     Y    =       14662241.70  feet           Y    =         4452240.04  meter
     Z    =      -16034498.84                 Z    =        -4894618.07
     XDOT =     -23852.446973                 XDOT =       -7283.539908
     YDOT =        648.785022  feet/sec       YDOT =         116.374798  meter/sec
     ZDOT =       7864.051349                 ZDOT =        2361.614467
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11104393.61                 X    =         3384619.17
     Y    =       10701229.37  feet           Y    =         3261734.71  meter
     Z    =      -16067567.53                 Z    =        -4897394.58
     XDOT =      -9065.887349                 XDOT =       -2763.282464
     YDOT =      20981.686305  feet/sec       YDOT =        6395.217986  meter/sec
     ZDOT =       7706.403574                 ZDOT =        2348.911809
  
  
    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   18066.73316136  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6403 164.4907 0002462 163.4657 196.6577 15.54193288 22739
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18066.73316136   =   yrday.fracday
    Element set:     914
    Inclination:       51.6403  deg
    RA of node:       164.4907  deg
    Eccentricity:     .0002462     
    Arg of perigee:   163.4657  deg
    Mean anomaly:     196.6577  deg
    Mean motion:   15.54193288  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2273
    Checksum:              326
 
 
    Coasting Arc #16 (Orbit 2288)
    ---------------------------------------
 
    Vector Time (GMT): 2018/067/17:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3113091.62                 A    =         6782362.23  meter
     Y    =       -4561105.03  meter          E    =           .0011558
     Z    =        3927387.83                 I    =           51.77105
     XDOT =       6446.200530                 Wp   =           92.09519
     YDOT =        890.693189  meter/sec      RA   =          158.38698  deg
     ZDOT =      -4065.343969                 TA   =           40.36099
                                              MA   =           40.27527
                                              Ha   =            221.171  n.mi
                                              Hp   =            214.177
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10213555.18                 X    =         3144786.71
     Y    =      -14964255.35  feet           Y    =        -4526114.75  meter
     Z    =       12885130.68                 Z    =         3942587.41
     XDOT =      21148.951870                 XDOT =        6455.508628
     YDOT =       2922.221750  feet/sec       YDOT =         962.830737  meter/sec
     ZDOT =     -13337.742679                 ZDOT =       -4034.008247
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9311759.16                 X    =        -2838224.19
     Y    =      -15484569.25  feet           Y    =        -4719696.71  meter
     Z    =       12953435.70                 Z    =         3948207.20
     XDOT =      10457.385716                 XDOT =        3187.411166
     YDOT =     -17356.367776  feet/sec       YDOT =       -5290.220898  meter/sec
     ZDOT =     -13198.094204                 ZDOT =       -4022.779113
  
  
    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   18067.76193444  .00016717  00000-0  10270-3 0  9153
    2 25544  51.6389 159.3613 0002374 163.1906 196.9326 15.54248027 22899
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18067.76193444   =   yrday.fracday
    Element set:     915
    Inclination:       51.6389  deg
    RA of node:       159.3613  deg
    Eccentricity:     .0002374     
    Arg of perigee:   163.1906  deg
    Mean anomaly:     196.9326  deg
    Mean motion:   15.54248027  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2289
    Checksum:              336
 
 
    Coasting Arc #17 (Orbit 2303)
    ---------------------------------------
 
    Vector Time (GMT): 2018/068/17:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905824.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4416530.49                 A    =         6786146.29  meter
     Y    =        4468496.65  meter          E    =           .0004679
     Z    =       -2567753.11                 I    =           51.81322
     XDOT =      -5154.446820                 Wp   =           81.30648
     YDOT =      -2065.172542  meter/sec      RA   =          153.41618  deg
     ZDOT =       5280.653664                 TA   =          249.92157
                                              MA   =          249.97194
                                              Ha   =            221.203  n.mi
                                              Hp   =            214.203
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14489929.42                 X    =        -4453697.50
     Y    =       14660422.07  feet           Y    =         4418899.95  meter
     Z    =       -8424386.84                 Z    =        -2589297.51
     XDOT =     -16910.914764                 XDOT =       -5156.620825
     YDOT =      -6775.500466  feet/sec       YDOT =       -2122.824853  meter/sec
     ZDOT =      17324.979211                 ZDOT =        5255.610247
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7554828.94                 X    =         2302711.86
     Y    =       19135661.43  feet           Y    =         5832549.61  meter
     Z    =       -8520994.35                 Z    =        -2597199.08
     XDOT =     -11695.453826                 XDOT =       -3564.774326
     YDOT =      12269.622704  feet/sec       YDOT =        3739.781000  meter/sec
     ZDOT =      17213.513963                 ZDOT =        5246.679056
  
  
    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   18068.72640625  .00016717  00000-0  10270-3 0  9169
    2 25544  51.6383 154.5536 0002446 166.0881 194.0339 15.54238504 23048
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18068.72640625   =   yrday.fracday
    Element set:     916
    Inclination:       51.6383  deg
    RA of node:       154.5536  deg
    Eccentricity:     .0002446     
    Arg of perigee:   166.0881  deg
    Mean anomaly:     194.0339  deg
    Mean motion:   15.54238504  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2304
    Checksum:              311
 
             

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