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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14562.4944
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   69.6
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.788
   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 
   ------------------------------------------------------------------------
   048/17:15:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.1  
   000/00:00:00.000           0.0               0.0              224.3  
   
   049/09:05:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.1  
   000/00:00:00.000           0.0               0.0              224.4  
   
   052/17:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.6  
   000/00:00:00.000           0.0               0.0              224.2  
   
   055/23:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.3  
   000/00:00:00.000           0.0               0.0              223.8  
   
 
 
    Coasting Arc #1 (Orbit 1329)
    ---------------------------------------
 
    Vector Time (GMT): 2020/048/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904514.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -886599.15                 A    =         6793636.95  meter
     Y    =        4626934.70  meter          E    =           .0008038
     Z    =       -4902217.02                 I    =           51.34858
     XDOT =      -6325.843248                 Wp   =           56.21854
     YDOT =      -3646.096029  meter/sec      RA   =          224.52176  deg
     ZDOT =      -2295.622448                 TA   =          191.18728
                                              MA   =          191.20516
                                              Ha   =            227.164  n.mi
                                              Hp   =            224.214
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2908789.86                 X    =         -914461.27
     Y    =       15180231.96  feet           Y    =         4616864.35  meter
     Z    =      -16083389.16                 Z    =        -4906591.34
     XDOT =     -20754.078899                 XDOT =       -6273.450768
     YDOT =     -11962.257313  feet/sec       YDOT =       -3716.543144  meter/sec
     ZDOT =      -7531.569712                 ZDOT =       -2326.223118
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10801207.14                 X    =        -3292207.94
     Y    =       11026512.23  feet           Y    =         3360880.93  meter
     Z    =      -16103597.73                 Z    =        -4908376.59
     XDOT =      -9685.200011                 XDOT =       -2952.048963
     YDOT =     -20699.000130  feet/sec       YDOT =       -6309.055240  meter/sec
     ZDOT =      -7671.484893                 ZDOT =       -2338.268595
  
  
    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   20048.52024880  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6378 225.5202 0004926 282.0303  78.0295 15.49172297 13304
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20048.52024880   =   yrday.fracday
    Element set:     900
    Inclination:       51.6378  deg
    RA of node:       225.5202  deg
    Eccentricity:     .0004926     
    Arg of perigee:   282.0303  deg
    Mean anomaly:      78.0295  deg
    Mean motion:   15.49172297  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1330
    Checksum:              288
 
 
    Coasting Arc #2 (Orbit 1333)
    ---------------------------------------
 
    Vector Time (GMT): 2020/048/17:15:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904514.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2975217.48                 A    =         6801170.53  meter
     Y    =       -5572944.37  meter          E    =           .0009342
     Z    =        2504938.43                 I    =           51.38304
     XDOT =       5525.045495                 Wp   =           62.23376
     YDOT =       -572.955711  meter/sec      RA   =          223.43868  deg
     ZDOT =       5276.745311                 TA   =          325.91420
                                              MA   =          325.97416
                                              Ha   =            227.090  n.mi
                                              Hp   =            224.330
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9761212.20                 X    =        -2924845.38
     Y    =      -18283938.21  feet           Y    =        -5605933.72  meter
     Z    =        8218301.95                 Z    =         2490608.59
     XDOT =      18126.789682                 XDOT =        5505.410904
     YDOT =      -1879.775954  feet/sec       YDOT =        -511.280540  meter/sec
     ZDOT =      17312.156532                 ZDOT =        5303.535616
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19870584.83                 X    =        -6056554.26
     Y    =       -5984452.88  feet           Y    =        -1824061.24  meter
     Z    =        8152933.79                 Z    =         2485014.22
     XDOT =      10967.618638                 XDOT =        3342.930161
     YDOT =     -12615.185477  feet/sec       YDOT =       -3845.108533  meter/sec
     ZDOT =      17434.804917                 ZDOT =        5314.128539
  
  
    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   20048.77828106  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6419 224.2438 0005055 280.2824  79.7756 15.49173451 13346
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20048.77828106   =   yrday.fracday
    Element set:     901
    Inclination:       51.6419  deg
    RA of node:       224.2438  deg
    Eccentricity:     .0005055     
    Arg of perigee:   280.2824  deg
    Mean anomaly:      79.7756  deg
    Mean motion:   15.49173451  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1334
    Checksum:              311
 
 
    Coasting Arc #3 (Orbit 1343)
    ---------------------------------------
 
    Vector Time (GMT): 2020/049/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4342362.80                 A    =         6793111.79  meter
     Y    =       -1553996.81  meter          E    =           .0004903
     Z    =        4989199.69                 I    =           51.37174
     XDOT =       4455.006497                 Wp   =          358.18009
     YDOT =       5886.460022  meter/sec      RA   =          220.12847  deg
     ZDOT =      -2039.208541                 TA   =          111.77339
                                              MA   =          111.72121
                                              Ha   =            227.111  n.mi
                                              Hp   =            224.391
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14246597.10                 X    =         4335183.16
     Y    =       -5098414.73  feet           Y    =        -1505477.61  meter
     Z    =       16368765.39                 Z    =         5010275.28
     XDOT =      14616.163048                 XDOT =        4398.756363
     YDOT =      19312.532879  feet/sec       YDOT =        5935.964564  meter/sec
     ZDOT =      -6690.316736                 ZDOT =       -2017.704911
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8181213.52                 X    =         2493633.88
     Y    =       12603864.29  feet           Y    =         3841657.83  meter
     Z    =       16465302.68                 Z    =         5018624.26
     XDOT =     -14548.852707                 XDOT =       -4434.490305
     YDOT =      18075.678889  feet/sec       YDOT =        5509.466925  meter/sec
     ZDOT =      -6592.109258                 ZDOT =       -2009.274902
  
  
    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   20049.42336171  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6407 221.0552 0005383 287.7767  72.2795 15.49188840 13447
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20049.42336171   =   yrday.fracday
    Element set:     902
    Inclination:       51.6407  deg
    RA of node:       221.0552  deg
    Eccentricity:     .0005383     
    Arg of perigee:   287.7767  deg
    Mean anomaly:      72.2795  deg
    Mean motion:   15.49188840  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1344
    Checksum:              312
 
 
    Coasting Arc #4 (Orbit 1358)
    ---------------------------------------
 
    Vector Time (GMT): 2020/050/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4242753.96                 A    =         6793210.41  meter
     Y    =        1867245.61  meter          E    =           .0007284
     Z    =       -4972576.95                 I    =           51.39763
     XDOT =      -4888.387155                 Wp   =          101.38562
     YDOT =      -5500.731071  meter/sec      RA   =          215.16220  deg
     ZDOT =       2106.571705                 TA   =          189.22672
                                              MA   =          189.24011
                                              Ha   =            227.310  n.mi
                                              Hp   =            224.189
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13919796.46                 X    =        -4239165.40
     Y    =        6126133.90  feet           Y    =         1819820.20  meter
     Z    =      -16314228.83                 Z    =        -4993177.34
     XDOT =     -16038.015601                 XDOT =       -4836.745312
     YDOT =     -18047.017949  feet/sec       YDOT =       -5555.107742  meter/sec
     ZDOT =       6911.324490                 ZDOT =        2082.951847
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9313619.35                 X    =        -2838791.18
     Y    =      -11893621.11  feet           Y    =        -3625175.71  meter
     Z    =      -16408613.09                 Z    =        -5001345.27
     XDOT =      12702.225134                 XDOT =        3871.638221
     YDOT =     -19327.368790  feet/sec       YDOT =       -5890.982007  meter/sec
     ZDOT =       6803.388913                 ZDOT =        2073.672941
  
  
    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   20050.39098321  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6399 216.2661 0005368 291.1883  68.8693 15.49184283 13596
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20050.39098321   =   yrday.fracday
    Element set:     903
    Inclination:       51.6399  deg
    RA of node:       216.2661  deg
    Eccentricity:     .0005368     
    Arg of perigee:   291.1883  deg
    Mean anomaly:      68.8693  deg
    Mean motion:   15.49184283  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1359
    Checksum:              332
 
 
    Coasting Arc #5 (Orbit 1374)
    ---------------------------------------
 
    Vector Time (GMT): 2020/051/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4128717.69                 A    =         6793328.38  meter
     Y    =       -2160151.06  meter          E    =           .0005690
     Z    =        4944888.31                 I    =           51.42623
     XDOT =       5287.059550                 Wp   =            4.60162
     YDOT =       5092.429016  meter/sec      RA   =          210.19898  deg
     ZDOT =      -2184.076730                 TA   =          106.82268
                                              MA   =          106.76027
                                              Ha   =            227.438  n.mi
                                              Hp   =            224.299
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13545661.71                 X    =         4128547.52
     Y    =       -7087109.76  feet           Y    =        -2113981.71  meter
     Z    =       16223386.84                 Z    =         4964943.04
     XDOT =      17345.995898                 XDOT =        5240.330264
     YDOT =      16707.444279  feet/sec       YDOT =        5151.291368  meter/sec
     ZDOT =      -7165.606068                 ZDOT =       -2158.508536
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10347024.72                 X    =         3153773.14
     Y    =       11120281.48  feet           Y    =         3389461.80  meter
     Z    =       16315292.69                 Z    =         4972901.21
     XDOT =     -10777.505455                 XDOT =       -3284.983663
     YDOT =      20397.141649  feet/sec       YDOT =        6217.048775  meter/sec
     ZDOT =      -7048.708329                 ZDOT =       -2148.446299
  
  
    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   20051.42310957  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6400 211.1589 0005385 295.4007  64.6585 15.49180764 13758
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20051.42310957   =   yrday.fracday
    Element set:     904
    Inclination:       51.6400  deg
    RA of node:       211.1589  deg
    Eccentricity:     .0005385     
    Arg of perigee:   295.4007  deg
    Mean anomaly:      64.6585  deg
    Mean motion:   15.49180764  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1375
    Checksum:              302
 
 
    Coasting Arc #6 (Orbit 1389)
    ---------------------------------------
 
    Vector Time (GMT): 2020/052/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3984966.59                 A    =         6793415.38  meter
     Y    =        2461527.93  meter          E    =           .0007270
     Z    =       -4927105.95                 I    =           51.45420
     XDOT =      -5651.082274                 Wp   =           97.48696
     YDOT =      -4646.485989  meter/sec      RA   =          205.23716  deg
     ZDOT =       2251.109557                 TA   =          194.58981
                                              MA   =          194.61081
                                              Ha   =            227.619  n.mi
                                              Hp   =            224.032
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13074037.37                 X    =        -3988263.61
     Y    =        8075879.03  feet           Y    =         2416946.63  meter
     Z    =      -16165045.77                 Z    =        -4946470.85
     XDOT =     -18540.296176                 XDOT =       -5609.638178
     YDOT =     -15244.376604  feet/sec       YDOT =       -4709.448612  meter/sec
     ZDOT =       7385.530043                 ZDOT =        2223.760426
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11355917.38                 X    =        -3461283.62
     Y    =      -10213508.40  feet           Y    =        -3113077.36  meter
     Z    =      -16253810.83                 Z    =        -4954161.54
     XDOT =       8740.595847                 XDOT =        2664.133614
     YDOT =     -21262.485369  feet/sec       YDOT =       -6480.805540  meter/sec
     ZDOT =       7260.434952                 ZDOT =        2212.980574
  
  
    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   20052.39072781  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6381 206.3703 0005243 298.9001  61.1612 15.49181742 13902
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20052.39072781   =   yrday.fracday
    Element set:     905
    Inclination:       51.6381  deg
    RA of node:       206.3703  deg
    Eccentricity:     .0005243     
    Arg of perigee:   298.9001  deg
    Mean anomaly:      61.1612  deg
    Mean motion:   15.49181742  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1390
    Checksum:              284
 
 
    Coasting Arc #7 (Orbit 1394)
    ---------------------------------------
 
    Vector Time (GMT): 2020/052/17:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6317705.16                 A    =         6801263.41  meter
     Y    =        -658560.14  meter          E    =           .0006068
     Z    =       -2420308.73                 I    =           51.49303
     XDOT =      -1492.140276                 Wp   =          354.52918
     YDOT =      -5286.758337  meter/sec      RA   =          203.59881  deg
     ZDOT =       5338.233334                 TA   =          338.40503
                                              MA   =          338.43061
                                              Ha   =            227.561  n.mi
                                              Hp   =            224.184
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20727379.15                 X    =        -6298115.29
     Y    =       -2160630.40  feet           Y    =         -729099.76  meter
     Z    =       -7940645.43                 Z    =        -2450949.13
     XDOT =      -4895.473348                 XDOT =       -1458.840585
     YDOT =     -17345.007667  feet/sec       YDOT =       -5303.258137  meter/sec
     ZDOT =      17513.888892                 ZDOT =        5331.066378
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16102834.33                 X    =        -4908143.90
     Y    =       13143187.15  feet           Y    =         4006043.44  meter
     Z    =       -8080951.55                 Z    =        -2463074.03
     XDOT =     -14879.934987                 XDOT =       -4535.404184
     YDOT =      -7492.033737  feet/sec       YDOT =       -2283.571883  meter/sec
     ZDOT =      17481.236492                 ZDOT =        5328.280883
  
  
    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   20052.71326757  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6410 204.7750 0005267 297.5615  62.5000 15.49155925 13956
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20052.71326757   =   yrday.fracday
    Element set:     906
    Inclination:       51.6410  deg
    RA of node:       204.7750  deg
    Eccentricity:     .0005267     
    Arg of perigee:   297.5615  deg
    Mean anomaly:      62.5000  deg
    Mean motion:   15.49155925  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1395
    Checksum:              300
 
 
    Coasting Arc #8 (Orbit 1410)
    ---------------------------------------
 
    Vector Time (GMT): 2020/053/17:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6375950.25                 A    =         6801290.34  meter
     Y    =         179090.94  meter          E    =           .0008846
     Z    =        2351008.90                 I    =           51.52509
     XDOT =       1844.700397                 Wp   =           97.52401
     YDOT =       5132.589477  meter/sec      RA   =          198.64194  deg
     ZDOT =      -5377.537127                 TA   =           56.26011
                                              MA   =           56.17585
                                              Ha   =            227.756  n.mi
                                              Hp   =            224.022
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20918471.95                 X    =         6362054.22
     Y    =         587568.71  feet           Y    =          250313.78  meter
     Z    =        7713283.79                 Z    =         2381946.07
     XDOT =       6052.166656                 XDOT =        1813.289377
     YDOT =      16839.204321  feet/sec       YDOT =        5153.042303  meter/sec
     ZDOT =     -17642.838343                 ZDOT =       -5368.653137
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14872853.50                 X    =         4533245.75
     Y    =      -14646498.59  feet           Y    =        -4464252.77  meter
     Z    =        7854983.14                 Z    =         2394198.86
     XDOT =      15353.677197                 XDOT =        4679.800810
     YDOT =       6122.634347  feet/sec       YDOT =        1866.178949  meter/sec
     ZDOT =     -17602.302256                 ZDOT =       -5365.181728
  
  
    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   20053.74539176  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6413 199.6684 0005204 302.1317  57.9328 15.49196341 14117
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20053.74539176   =   yrday.fracday
    Element set:     907
    Inclination:       51.6413  deg
    RA of node:       199.6684  deg
    Eccentricity:     .0005204     
    Arg of perigee:   302.1317  deg
    Mean anomaly:      57.9328  deg
    Mean motion:   15.49196341  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1411
    Checksum:              307
 
 
    Coasting Arc #9 (Orbit 1425)
    ---------------------------------------
 
    Vector Time (GMT): 2020/054/17:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6388386.38                 A    =         6801461.90  meter
     Y    =         322330.66  meter          E    =           .0007144
     Z    =       -2298780.65                 I    =           51.55794
     XDOT =      -2195.281349                 Wp   =          358.96747
     YDOT =      -4956.525036  meter/sec      RA   =          193.68660  deg
     ZDOT =       5412.482975                 TA   =          335.45058
                                              MA   =          335.48458
                                              Ha   =            227.869  n.mi
                                              Hp   =            223.979
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20959272.89                 X    =        -6380350.14
     Y    =        1057515.29  feet           Y    =          250935.95  meter
     Z    =       -7541931.26                 Z    =        -2329792.54
     XDOT =      -7202.366630                 XDOT =       -2165.982862
     YDOT =     -16261.565080  feet/sec       YDOT =       -4980.910017  meter/sec
     ZDOT =      17757.490074                 ZDOT =        5401.890986
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13440961.15                 X    =        -4096804.96
     Y    =       16049511.60  feet           Y    =         4891891.14  meter
     Z    =       -7684004.59                 Z    =        -2342084.60
     XDOT =     -15731.938390                 XDOT =       -4795.094821
     YDOT =      -4706.793466  feet/sec       YDOT =       -1434.630648  meter/sec
     ZDOT =      17709.111229                 ZDOT =        5397.737102
  
  
    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   20054.71300608  .00016717  00000-0  10270-3 0  9081
    2 25544  51.6417 194.8805 0005290 306.1352  53.9308 15.49171769 14268
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20054.71300608   =   yrday.fracday
    Element set:     908
    Inclination:       51.6417  deg
    RA of node:       194.8805  deg
    Eccentricity:     .0005290     
    Arg of perigee:   306.1352  deg
    Mean anomaly:      53.9308  deg
    Mean motion:   15.49171769  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1426
    Checksum:              303
 
 
    Coasting Arc #10 (Orbit 1441)
    ---------------------------------------
 
    Vector Time (GMT): 2020/055/17:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6372802.56                 A    =         6801476.50  meter
     Y    =        -806439.17  meter          E    =           .0009213
     Z    =        2225971.27                 I    =           51.59171
     XDOT =       2512.445583                 Wp   =           94.91918
     YDOT =       4757.978653  meter/sec      RA   =          188.73425  deg
     ZDOT =      -5450.480935                 TA   =           60.38204
                                              MA   =           60.29029
                                              Ha   =            228.106  n.mi
                                              Hp   =            223.748
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20908144.89                 X    =         6370534.55
     Y    =       -2645797.81  feet           Y    =         -735186.46  meter
     Z    =        7303055.35                 Z    =         2256921.61
     XDOT =       8242.931703                 XDOT =        2485.528372
     YDOT =      15610.166185  feet/sec       YDOT =        4785.923626  meter/sec
     ZDOT =     -17882.155299                 ZDOT =       -5438.342565
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11946826.21                 X    =         3641392.63
     Y    =      -17301230.01  feet           Y    =        -5273414.91  meter
     Z    =        7444875.43                 Z    =         2269198.03
     XDOT =      15945.637937                 XDOT =        4860.230443
     YDOT =       3313.851032  feet/sec       YDOT =        1010.061794  meter/sec
     ZDOT =     -17826.674302                 ZDOT =       -5433.570327
  
  
    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   20055.74512562  .00016717  00000-0  10270-3 0  9090
    2 25544  51.6421 189.7739 0005318 312.2000  47.8698 15.49216688 14423
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20055.74512562   =   yrday.fracday
    Element set:     909
    Inclination:       51.6421  deg
    RA of node:       189.7739  deg
    Eccentricity:     .0005318     
    Arg of perigee:   312.2000  deg
    Mean anomaly:      47.8698  deg
    Mean motion:   15.49216688  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1442
    Checksum:              317
 
 
    Coasting Arc #11 (Orbit 1445)
    ---------------------------------------
 
    Vector Time (GMT): 2020/055/23:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5740167.38                 A    =         6801280.40  meter
     Y    =        2706353.71  meter          E    =           .0000287
     Z    =       -2446384.54                 I    =           51.59760
     XDOT =      -4031.727232                 Wp   =           89.17863
     YDOT =       3733.664895  meter/sec      RA   =          187.45081  deg
     ZDOT =      -5330.106834                 TA   =          118.14285
                                              MA   =          118.13995
                                              Ha   =            228.282  n.mi
                                              Hp   =            223.808
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18832570.13                 X    =         5721360.36
     Y    =        8879113.22  feet           Y    =         2770438.96  meter
     Z    =       -8026196.00                 Z    =        -2418547.68
     XDOT =     -13227.451550                 XDOT =       -4047.288562
     YDOT =      12249.556743  feet/sec       YDOT =        3688.491770  meter/sec
     ZDOT =     -17487.227147                 ZDOT =       -5349.729026
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10270628.87                 X    =        -3130487.68
     Y    =      -18167233.79  feet           Y    =        -5537372.86  meter
     Z    =       -7898732.23                 Z    =        -2407533.58
     XDOT =      16453.222762                 XDOT =        5014.942298
     YDOT =      -1660.204343  feet/sec       YDOT =        -506.030284  meter/sec
     ZDOT =     -17577.229487                 ZDOT =       -5357.539548
  
  
    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   20056.00315697  .00016717  00000-0  10270-3 0  9102
    2 25544  51.6403 188.4976 0005357 315.3855  44.6863 15.49189603 14466
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20056.00315697   =   yrday.fracday
    Element set:     910
    Inclination:       51.6403  deg
    RA of node:       188.4976  deg
    Eccentricity:     .0005357     
    Arg of perigee:   315.3855  deg
    Mean anomaly:      44.6863  deg
    Mean motion:   15.49189603  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1446
    Checksum:              322
 
 
    Coasting Arc #12 (Orbit 1461)
    ---------------------------------------
 
    Vector Time (GMT): 2020/056/23:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5905190.12                 A    =         6801119.66  meter
     Y    =       -2240791.72  meter          E    =           .0012192
     Z    =        2502041.73                 I    =           51.63065
     XDOT =       3783.440049                 Wp   =           52.52423
     YDOT =      -4037.345512  meter/sec      RA   =          182.50156  deg
     ZDOT =       5303.180928                 TA   =          335.49378
                                              MA   =          335.55169
                                              Ha   =            228.398  n.mi
                                              Hp   =            223.670
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19373983.32                 X    =        -5891847.28
     Y    =       -7351678.88  feet           Y    =        -2306752.91  meter
     Z    =        8208798.33                 Z    =         2473389.86
     XDOT =      12412.861054                 XDOT =        3802.546363
     YDOT =     -13245.884225  feet/sec       YDOT =       -3994.929055  meter/sec
     ZDOT =      17398.887558                 ZDOT =        5321.605804
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11891551.29                 X    =         3624544.83
     Y    =       17033103.56  feet           Y    =         5191689.96  meter
     Z    =        8077572.24                 Z    =         2462044.02
     XDOT =     -16382.119072                 XDOT =       -4993.269893
     YDOT =       3129.325102  feet/sec       YDOT =         953.818291  meter/sec
     ZDOT =      17483.418254                 ZDOT =        5328.945884
  
  
    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   20057.03527538  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6404 183.3914 0005309 317.5200  42.5538 15.49207131 14629
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20057.03527538   =   yrday.fracday
    Element set:     911
    Inclination:       51.6404  deg
    RA of node:       183.3914  deg
    Eccentricity:     .0005309     
    Arg of perigee:   317.5200  deg
    Mean anomaly:      42.5538  deg
    Mean motion:   15.49207131  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1462
    Checksum:              279
 
 
    Coasting Arc #13 (Orbit 1476)
    ---------------------------------------
 
    Vector Time (GMT): 2020/057/23:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6039473.43                 A    =         6800986.92  meter
     Y    =        1779032.19  meter          E    =           .0001176
     Z    =       -2573720.74                 I    =           51.66474
     XDOT =      -3511.673584                 Wp   =           35.35417
     YDOT =       4312.831672  meter/sec      RA   =          177.55388  deg
     ZDOT =      -5259.578968                 TA   =          173.48786
                                              MA   =          173.48634
                                              Ha   =            228.522  n.mi
                                              Hp   =            223.593
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19814545.37                 X    =         6031632.36
     Y    =        5836719.79  feet           Y    =         1846525.78  meter
     Z    =       -8443965.69                 Z    =        -2544403.06
     XDOT =     -11521.238792                 XDOT =       -3534.092345
     YDOT =      14149.710211  feet/sec       YDOT =        4273.435780  meter/sec
     ZDOT =     -17255.836510                 ZDOT =       -5276.691885
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13385322.74                 X    =        -4079846.37
     Y    =      -15804009.48  feet           Y    =        -4817062.09  meter
     Z    =       -8309661.98                 Z    =        -2532784.97
     XDOT =      16153.726526                 XDOT =        4923.655845
     YDOT =      -4567.674188  feet/sec       YDOT =       -1392.227092  meter/sec
     ZDOT =     -17334.369741                 ZDOT =       -5283.515897
  
  
    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   20058.00288582  .00016717  00000-0  10270-3 0  9128
    2 25544  51.6414 178.6038 0005473 322.2384  37.8382 15.49200984 14771
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20058.00288582   =   yrday.fracday
    Element set:     912
    Inclination:       51.6414  deg
    RA of node:       178.6038  deg
    Eccentricity:     .0005473     
    Arg of perigee:   322.2384  deg
    Mean anomaly:      37.8382  deg
    Mean motion:   15.49200984  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1477
    Checksum:              313
 
 
    Coasting Arc #14 (Orbit 1492)
    ---------------------------------------
 
    Vector Time (GMT): 2020/058/23:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6126883.77                 A    =         6800870.13  meter
     Y    =       -1299729.03  meter          E    =           .0012722
     Z    =        2629885.61                 I    =           51.69777
     XDOT =       3221.810556                 Wp   =           53.48313
     YDOT =      -4583.615080  meter/sec      RA   =          172.60868  deg
     ZDOT =       5230.407096                 TA   =          336.07714
                                              MA   =          336.13620
                                              Ha   =            228.739  n.mi
                                              Hp   =            223.409
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20101324.69                 X    =        -6124668.77
     Y    =       -4264202.86  feet           Y    =        -1368231.57  meter
     Z    =        8628233.63                 Z    =         2600129.49
     XDOT =      10570.244607                 XDOT =        3247.420439
     YDOT =     -15038.107219  feet/sec       YDOT =       -4547.442830  meter/sec
     ZDOT =      17160.128267                 ZDOT =        5246.119810
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14740643.84                 X    =         4492948.24
     Y    =       14397716.98  feet           Y    =         4388424.14  meter
     Z    =        8491893.84                 Z    =         2588329.24
     XDOT =     -15831.638828                 XDOT =       -4825.483515
     YDOT =       6024.930258  feet/sec       YDOT =        1836.398743  meter/sec
     ZDOT =      17232.260330                 ZDOT =        5252.392949
  
  
    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   20059.03499978  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6414 173.4971 0005455 326.0545  34.0255 15.49200365 14930
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20059.03499978   =   yrday.fracday
    Element set:     913
    Inclination:       51.6414  deg
    RA of node:       173.4971  deg
    Eccentricity:     .0005455     
    Arg of perigee:   326.0545  deg
    Mean anomaly:      34.0255  deg
    Mean motion:   15.49200365  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1493
    Checksum:              310
 
 
    Coasting Arc #15 (Orbit 1507)
    ---------------------------------------
 
    Vector Time (GMT): 2020/059/23:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6186871.12                 A    =         6800692.42  meter
     Y    =         829829.83  meter          E    =           .0002393
     Z    =       -2702872.45                 I    =           51.73021
     XDOT =      -2910.819741                 Wp   =           34.16846
     YDOT =       4821.781259  meter/sec      RA   =          167.66569  deg
     ZDOT =      -5182.792431                 TA   =          176.23638
                                              MA   =          176.23458
                                              Ha   =            228.831  n.mi
                                              Hp   =            223.288
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20298133.60                 X    =         6190260.78
     Y    =        2722538.80  feet           Y    =          899034.55  meter
     Z    =       -8867691.75                 Z    =        -2672811.18
     XDOT =      -9549.933533                 XDOT =       -2939.347185
     YDOT =      15819.492318  feet/sec       YDOT =        4789.070475  meter/sec
     ZDOT =     -17003.912176                 ZDOT =       -5197.001594
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15958678.18                 X    =        -4864205.11
     Y    =      -12929477.35  feet           Y    =        -3940904.70  meter
     Z    =       -8729926.04                 Z    =        -2660881.46
     XDOT =      15351.187164                 XDOT =        4679.041848
     YDOT =      -7423.414878  feet/sec       YDOT =       -2262.656855  meter/sec
     ZDOT =     -17069.169566                 ZDOT =       -5202.682884
  
  
    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   20060.00260535  .00016717  00000-0  10270-3 0  9141
    2 25544  51.6412 168.7097 0005583 331.0536  29.0303 15.49206070 15086
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20060.00260535   =   yrday.fracday
    Element set:     914
    Inclination:       51.6412  deg
    RA of node:       168.7097  deg
    Eccentricity:     .0005583     
    Arg of perigee:   331.0536  deg
    Mean anomaly:      29.0303  deg
    Mean motion:   15.49206070  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1508
    Checksum:              271
 
 
    Coasting Arc #16 (Orbit 1523)
    ---------------------------------------
 
    Vector Time (GMT): 2020/060/23:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6197437.49                 A    =         6800598.14  meter
     Y    =        -348729.97  meter          E    =           .0013173
     Z    =        2758069.58                 I    =           51.76188
     XDOT =       2581.673663                 Wp   =           55.04811
     YDOT =      -5054.357749  meter/sec      RA   =          162.72519  deg
     ZDOT =       5151.929786                 TA   =          336.08114
                                              MA   =          336.14229
                                              Ha   =            229.030  n.mi
                                              Hp   =            223.137
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20332800.18                 X    =        -6206474.31
     Y    =       -1144127.19  feet           Y    =         -418084.46  meter
     Z    =        9048784.70                 Z    =         2727943.17
     XDOT =       8470.057950                 XDOT =        2612.976177
     YDOT =     -16582.538546  feet/sec       YDOT =       -5025.312274  meter/sec
     ZDOT =      16902.656777                 ZDOT =        5164.546807
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17008706.10                 X    =         5184253.62
     Y    =       11309986.51  feet           Y    =         3447283.89  meter
     Z    =        8910691.13                 Z    =         2715978.66
     XDOT =     -14774.754777                 XDOT =       -4503.345256
     YDOT =       8830.207647  feet/sec       YDOT =        2691.447291  meter/sec
     ZDOT =      16960.634101                 ZDOT =        5169.601274
  
  
    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   20061.03471664  .00016717  00000-0  10270-3 0  9153
    2 25544  51.6408 163.6032 0005542 333.8090  26.2779 15.49195567 15246
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20061.03471664   =   yrday.fracday
    Element set:     915
    Inclination:       51.6408  deg
    RA of node:       163.6032  deg
    Eccentricity:     .0005542     
    Arg of perigee:   333.8090  deg
    Mean anomaly:      26.2779  deg
    Mean motion:   15.49195567  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1524
    Checksum:              303
 
 
    Coasting Arc #17 (Orbit 1538)
    ---------------------------------------
 
    Vector Time (GMT): 2020/061/23:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6184074.70                 A    =         6800379.20  meter
     Y    =        -117721.02  meter          E    =           .0003392
     Z    =       -2831935.21                 I    =           51.79412
     XDOT =      -2235.765460                 Wp   =           34.72145
     YDOT =       5249.623610  meter/sec      RA   =          157.78627  deg
     ZDOT =      -5100.742836                 TA   =          177.26907
                                              MA   =          177.26722
                                              Ha   =            229.041  n.mi
                                              Hp   =            223.048
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20288959.00                 X    =         6198687.30
     Y    =        -386223.80  feet           Y    =          -48484.74  meter
     Z    =       -9291126.02                 Z    =        -2801860.14
     XDOT =      -7335.188517                 XDOT =       -2269.525837
     YDOT =      17223.174573  feet/sec       YDOT =        5224.432673  meter/sec
     ZDOT =     -16734.720589                 ZDOT =       -5111.685479
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17915870.03                 X    =        -5460757.18
     Y    =       -9662086.03  feet           Y    =        -2945003.82  meter
     Z    =       -9153236.80                 Z    =        -2789906.58
     XDOT =      14046.700763                 XDOT =        4281.434393
     YDOT =     -10145.891611  feet/sec       YDOT =       -3092.467763  meter/sec
     ZDOT =     -16785.040073                 ZDOT =       -5116.080214
  
  
    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   20062.00231791  .00016717  00000-0  10270-3 0  9167
    2 25544  51.6419 158.8155 0005647 337.4815  22.6087 15.49212135 15390
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20062.00231791   =   yrday.fracday
    Element set:     916
    Inclination:       51.6419  deg
    RA of node:       158.8155  deg
    Eccentricity:     .0005647     
    Arg of perigee:   337.4815  deg
    Mean anomaly:      22.6087  deg
    Mean motion:   15.49212135  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1539
    Checksum:              301
 
 
    Coasting Arc #18 (Orbit 1554)
    ---------------------------------------
 
    Vector Time (GMT): 2020/062/23:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919228.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6119331.76                 A    =         6800277.04  meter
     Y    =         586801.44  meter          E    =           .0013658
     Z    =        2887539.69                 I    =           51.82415
     XDOT =       1874.175419                 Wp   =           56.77492
     YDOT =      -5438.325590  meter/sec      RA   =          152.84939  deg
     ZDOT =       5066.940555                 TA   =          335.96484
                                              MA   =          336.02853
                                              Ha   =            229.315  n.mi
                                              Hp   =            222.819
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20076547.76                 X    =        -6139464.63
     Y    =        1925201.56  feet           Y    =          518258.25  meter
     Z    =        9473555.42                 Z    =         2857765.74
     XDOT =       6148.869486                 XDOT =        1910.237023
     YDOT =     -17842.275557  feet/sec       YDOT =       -5417.165423  meter/sec
     ZDOT =      16623.820718                 ZDOT =        5076.132249
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18626691.93                 X    =         5677415.70
     Y    =        7898667.55  feet           Y    =         2407513.87  meter
     Z    =        9337013.56                 Z    =         2845921.73
     XDOT =     -13228.509031                 XDOT =       -4032.049553
     YDOT =      11455.111134  feet/sec       YDOT =        3491.517874  meter/sec
     ZDOT =      16666.130471                 ZDOT =        5079.836568
  
  
    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   20063.03442327  .00016717  00000-0  10270-3 0  9171
    2 25544  51.6418 153.7084 0005672 342.0220  18.0729 15.49200917 15559
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20063.03442327   =   yrday.fracday
    Element set:     917
    Inclination:       51.6418  deg
    RA of node:       153.7084  deg
    Eccentricity:     .0005672     
    Arg of perigee:   342.0220  deg
    Mean anomaly:      18.0729  deg
    Mean motion:   15.49200917  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1555
    Checksum:              284
 
             

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