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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15204.0235
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   68.6
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.562
   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 
   ------------------------------------------------------------------------
   292/20:35:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.8  
   000/00:00:00.000           0.0               0.0              220.1  
   
   297/21:50:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.2  
   000/00:00:00.000           0.0               0.0              220.7  
   
   301/10:55:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.8  
   000/00:00:00.000           0.0               0.0              221.2  
   
 
 
    Coasting Arc #1 (Orbit 3406)
    ---------------------------------------
 
    Vector Time (GMT): 2019/289/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4780322.62                 A    =         6791519.21  meter
     Y    =       -1041962.94  meter          E    =           .0013049
     Z    =       -4720101.08                 I    =           51.96423
     XDOT =      -1282.764517                 Wp   =          102.12473
     YDOT =       6985.914030  meter/sec      RA   =          118.70306  deg
     ZDOT =      -2850.584778                 TA   =          139.70161
                                              MA   =          139.60483
                                              Ha   =            229.084  n.mi
                                              Hp   =            219.631
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15683473.16                 X    =         4814547.11
     Y    =       -3418513.57  feet           Y    =         -988314.85  meter
     Z    =      -15485895.92                 Z    =        -4696796.27
     XDOT =      -4208.545002                 XDOT =       -1346.940766
     YDOT =      22919.665453  feet/sec       YDOT =        6971.210288  meter/sec
     ZDOT =      -9352.312265                 ZDOT =       -2856.972334
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13060857.66                 X    =        -3980949.42
     Y    =        9505460.28  feet           Y    =         2897264.29  meter
     Z    =      -15379556.56                 Z    =        -4687688.84
     XDOT =      -4772.991232                 XDOT =       -1454.807728
     YDOT =     -21688.055578  feet/sec       YDOT =       -6610.519340  meter/sec
     ZDOT =      -9381.852831                 ZDOT =       -2859.588743
  
  
    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   19289.52125135  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6379 119.6194 0006812 156.1555 203.9912 15.50199261 34078
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19289.52125135   =   yrday.fracday
    Element set:     900
    Inclination:       51.6379  deg
    RA of node:       119.6194  deg
    Eccentricity:     .0006812     
    Arg of perigee:   156.1555  deg
    Mean anomaly:     203.9912  deg
    Mean motion:   15.50199261  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3407
    Checksum:              312
 
 
    Coasting Arc #2 (Orbit 3422)
    ---------------------------------------
 
    Vector Time (GMT): 2019/290/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4609615.75                 A    =         6790920.52  meter
     Y    =         992376.04  meter          E    =           .0013010
     Z    =        4883568.65                 I    =           51.97667
     XDOT =       1066.909694                 Wp   =          139.56750
     YDOT =      -7182.116457  meter/sec      RA   =          113.76848  deg
     ZDOT =       2453.223857                 TA   =          286.38653
                                              MA   =          286.52952
                                              Ha   =            229.108  n.mi
                                              Hp   =            219.712
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15123411.26                 X    =        -4644092.48
     Y    =        3255826.89  feet           Y    =          940635.41  meter
     Z    =       16022206.86                 Z    =         4861092.51
     XDOT =       3500.359889                 XDOT =        1135.226194
     YDOT =     -23563.374204  feet/sec       YDOT =       -7169.803477  meter/sec
     ZDOT =       8048.634701                 ZDOT =        2458.572755
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12458604.33                 X    =         3797382.60
     Y    =       -9347587.14  feet           Y    =        -2849144.56  meter
     Z    =       15919638.25                 Z    =         4852305.74
     XDOT =       6078.113964                 XDOT =        1852.609136
     YDOT =      21925.480154  feet/sec       YDOT =        6682.886351  meter/sec
     ZDOT =       8073.472395                 ZDOT =        2460.794386
  
  
    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   19290.55269493  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6376 114.5077 0006762 159.8044 200.3376 15.50168488 34236
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19290.55269493   =   yrday.fracday
    Element set:     901
    Inclination:       51.6376  deg
    RA of node:       114.5077  deg
    Eccentricity:     .0006762     
    Arg of perigee:   159.8044  deg
    Mean anomaly:     200.3376  deg
    Mean motion:   15.50168488  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3423
    Checksum:              322
 
 
    Coasting Arc #3 (Orbit 3437)
    ---------------------------------------
 
    Vector Time (GMT): 2019/291/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4467342.26                 A    =         6790161.20  meter
     Y    =        -867925.30  meter          E    =           .0014735
     Z    =       -5050743.53                 I    =           51.98665
     XDOT =       -840.282843                 Wp   =          103.39714
     YDOT =       7335.095890  meter/sec      RA   =          108.83380  deg
     ZDOT =      -2011.936288                 TA   =          147.15457
                                              MA   =          147.06291
                                              Ha   =            228.979  n.mi
                                              Hp   =            219.839
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14656634.71                 X    =         4501249.93
     Y    =       -2847523.94  feet           Y    =         -817778.77  meter
     Z    =      -16570680.88                 Z    =        -5028959.97
     XDOT =      -2756.833475                 XDOT =        -912.470454
     YDOT =      24065.275230  feet/sec       YDOT =        7325.295615  meter/sec
     ZDOT =      -6600.840839                 ZDOT =       -2016.193550
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12056725.59                 X    =        -3674889.96
     Y    =        8991413.10  feet           Y    =         2740582.71  meter
     Z    =      -16471267.61                 Z    =        -5020442.37
     XDOT =      -7374.939310                 XDOT =       -2247.881502
     YDOT =     -21967.779409  feet/sec       YDOT =       -6695.779164  meter/sec
     ZDOT =      -6620.731402                 ZDOT =       -2017.998931
  
  
    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   19291.51967184  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6374 109.7153 0006960 163.0234 197.1151 15.50200240 34386
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19291.51967184   =   yrday.fracday
    Element set:     902
    Inclination:       51.6374  deg
    RA of node:       109.7153  deg
    Eccentricity:     .0006960     
    Arg of perigee:   163.0234  deg
    Mean anomaly:     197.1151  deg
    Mean motion:   15.50200240  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3438
    Checksum:              292
 
 
    Coasting Arc #4 (Orbit 3453)
    ---------------------------------------
 
    Vector Time (GMT): 2019/292/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4343453.51                 A    =         6789748.40  meter
     Y    =         769443.53  meter          E    =           .0011010
     Z    =        5159125.48                 I    =           51.99535
     XDOT =        572.924284                 Wp   =          149.64759
     YDOT =      -7476.247456  meter/sec      RA   =          103.89982  deg
     ZDOT =       1586.649806                 TA   =          285.05940
                                              MA   =          285.18121
                                              Ha   =            228.980  n.mi
                                              Hp   =            219.947
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14250175.55                 X    =        -4376795.52
     Y    =        2524421.02  feet           Y    =          720685.51  meter
     Z    =       16926264.71                 Z    =         5137945.20
     XDOT =       1879.672847                 XDOT =         648.776047
     YDOT =     -24528.370919  feet/sec       YDOT =       -7469.416508  meter/sec
     ZDOT =       5205.543983                 ZDOT =        1589.617106
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11685156.96                 X    =         3561635.84
     Y    =       -8726989.62  feet           Y    =        -2659986.44  meter
     Z    =       16829598.94                 Z    =         5129661.76
     XDOT =       8769.385863                 XDOT =        2672.908811
     YDOT =      21875.846815  feet/sec       YDOT =        6667.758109  meter/sec
     ZDOT =       5219.580713                 ZDOT =        1590.928201
  
  
    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   19292.55111439  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6381 104.6034 0006846 167.1054 193.0273 15.50168292 34542
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19292.55111439   =   yrday.fracday
    Element set:     903
    Inclination:       51.6381  deg
    RA of node:       104.6034  deg
    Eccentricity:     .0006846     
    Arg of perigee:   167.1054  deg
    Mean anomaly:     193.0273  deg
    Mean motion:   15.50168292  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3454
    Checksum:              298
 
 
    Coasting Arc #5 (Orbit 3458)
    ---------------------------------------
 
    Vector Time (GMT): 2019/292/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4038656.10                 A    =         6788894.78  meter
     Y    =        1120342.80  meter          E    =           .0017709
     Z    =       -5354894.92                 I    =           51.99882
     XDOT =      -1770.005542                 Wp   =          113.81801
     YDOT =       7439.196168  meter/sec      RA   =          102.12418  deg
     ZDOT =        215.099487                 TA   =          158.26454
                                              MA   =          158.18929
                                              Ha   =            228.828  n.mi
                                              Hp   =            220.096
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13250184.05                 X    =         4051839.54
     Y    =        3675665.36  feet           Y    =         1165579.66  meter
     Z    =      -17568552.90                 Z    =        -5335244.24
     XDOT =      -5807.104797                 XDOT =       -1854.106094
     YDOT =      24406.811575  feet/sec       YDOT =        7418.932480  meter/sec
     ZDOT =        705.706978                 ZDOT =         206.297090
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10700345.44                 X    =         3261465.29
     Y    =        8815865.34  feet           Y    =         2687075.76  meter
     Z    =      -17478989.38                 Z    =        -5327595.96
     XDOT =     -14633.606466                 XDOT =       -4460.323251
     YDOT =      19121.982930  feet/sec       YDOT =        5828.380397  meter/sec
     ZDOT =        665.048079                 ZDOT =         202.706655
  
  
    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   19292.87343845  .00016717  00000-0  10270-3 0  9046
    2 25544  51.6415 103.0084 0006854 168.2583 191.8729 15.50180065 34595
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19292.87343845   =   yrday.fracday
    Element set:     904
    Inclination:       51.6415  deg
    RA of node:       103.0084  deg
    Eccentricity:     .0006854     
    Arg of perigee:   168.2583  deg
    Mean anomaly:     191.8729  deg
    Mean motion:   15.50180065  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3459
    Checksum:              325
 
 
    Coasting Arc #6 (Orbit 3474)
    ---------------------------------------
 
    Vector Time (GMT): 2019/293/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4025609.15                 A    =         6788894.15  meter
     Y    =       -1262055.41  meter          E    =           .0006590
     Z    =        5315153.31                 I    =           52.00482
     XDOT =       1472.258770                 Wp   =          145.27096
     YDOT =      -7493.287460  meter/sec      RA   =           97.19151  deg
     ZDOT =       -669.039028                 TA   =          311.05897
                                              MA   =          311.11590
                                              Ha   =            228.808  n.mi
                                              Hp   =            220.014
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13207379.09                 X    =        -4037015.74
     Y    =       -4140601.72  feet           Y    =        -1307136.43  meter
     Z    =       17438167.02                 Z    =         5295570.40
     XDOT =       4830.245309                 XDOT =        1559.191332
     YDOT =     -24584.276444  feet/sec       YDOT =       -7476.337548  meter/sec
     ZDOT =      -2195.009935                 ZDOT =        -661.676152
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10627605.68                 X    =        -3239294.21
     Y    =       -9040915.76  feet           Y    =        -2755671.12  meter
     Z    =       17348917.95                 Z    =         5287950.19
     XDOT =      13453.257078                 XDOT =        4100.552758
     YDOT =     -19930.166770  feet/sec       YDOT =       -6074.714832  meter/sec
     ZDOT =      -2160.894472                 ZDOT =        -658.640635
  
  
    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   19293.90487726  .00016717  00000-0  10270-3 0  9059
    2 25544  51.6412  97.8978 0006790 171.1087 189.0185 15.50218646 34755
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19293.90487726   =   yrday.fracday
    Element set:     905
    Inclination:       51.6412  deg
    RA of node:        97.8978  deg
    Eccentricity:     .0006790     
    Arg of perigee:   171.1087  deg
    Mean anomaly:     189.0185  deg
    Mean motion:   15.50218646  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3475
    Checksum:              348
 
 
    Coasting Arc #7 (Orbit 3489)
    ---------------------------------------
 
    Vector Time (GMT): 2019/294/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4057609.83                 A    =         6789291.71  meter
     Y    =        1438837.16  meter          E    =           .0017084
     Z    =       -5263811.26                 I    =           52.00939
     XDOT =      -1177.489608                 Wp   =          121.26219
     YDOT =       7473.988818  meter/sec      RA   =           92.25811  deg
     ZDOT =       1129.406949                 TA   =          159.56888
                                              MA   =          159.50046
                                              Ha   =            228.619  n.mi
                                              Hp   =            220.377
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13312368.21                 X    =         4066787.73
     Y    =        4720594.37  feet           Y    =         1484263.52  meter
     Z    =      -17269721.97                 Z    =        -5244078.39
     XDOT =      -3863.154883                 XDOT =       -1266.464502
     YDOT =      24520.960688  feet/sec       YDOT =        7460.323811  meter/sec
     ZDOT =       3705.403377                 ZDOT =        1123.470955
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10659121.73                 X    =         3248900.30
     Y    =        9433139.55  feet           Y    =         2875220.93  meter
     Z    =      -17179797.95                 Z    =        -5236402.42
     XDOT =     -12156.281858                 XDOT =       -3705.234710
     YDOT =      20469.678083  feet/sec       YDOT =        6239.157880  meter/sec
     ZDOT =       3677.782443                 ZDOT =        1120.988089
  
  
    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   19294.87185268  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6418  93.1059 0006759 175.0888 185.0330 15.50182878 34909
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19294.87185268   =   yrday.fracday
    Element set:     906
    Inclination:       51.6418  deg
    RA of node:        93.1059  deg
    Eccentricity:     .0006759     
    Arg of perigee:   175.0888  deg
    Mean anomaly:     185.0330  deg
    Mean motion:   15.50182878  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3490
    Checksum:              346
 
 
    Coasting Arc #8 (Orbit 3505)
    ---------------------------------------
 
    Vector Time (GMT): 2019/295/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4110698.27                 A    =         6789555.69  meter
     Y    =       -1579219.40  meter          E    =           .0005797
     Z    =        5163236.20                 I    =           52.00983
     XDOT =        884.863724                 Wp   =          132.89101
     YDOT =      -7449.756051  meter/sec      RA   =           87.32563  deg
     ZDOT =      -1576.809469                 TA   =          332.22211
                                              MA   =          332.25306
                                              Ha   =            228.619  n.mi
                                              Hp   =            220.280
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13486542.89                 X    =        -4117813.85
     Y    =       -5181166.01  feet           Y    =        -1625227.81  meter
     Z    =       16939751.32                 Z    =         5143250.53
     XDOT =       2903.096206                 XDOT =         975.762633
     YDOT =     -24441.456861  feet/sec       YDOT =       -7439.352665  meter/sec
     ZDOT =      -5173.259412                 ZDOT =       -1572.290156
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10813915.59                 X    =        -3296081.47
     Y    =       -9740001.34  feet           Y    =        -2968752.41  meter
     Z    =       16848682.40                 Z    =         5135478.40
     XDOT =      10851.783457                 XDOT =        3307.623598
     YDOT =     -20945.067360  feet/sec       YDOT =       -6384.056531  meter/sec
     ZDOT =      -5152.089984                 ZDOT =       -1570.357027
  
  
    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   19295.90329108  .00016717  00000-0  10270-3 0  9072
    2 25544  51.6407  87.9947 0006741 177.8718 182.2462 15.50222100 35063
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19295.90329108   =   yrday.fracday
    Element set:     907
    Inclination:       51.6407  deg
    RA of node:        87.9947  deg
    Eccentricity:     .0006741     
    Arg of perigee:   177.8718  deg
    Mean anomaly:     182.2462  deg
    Mean motion:   15.50222100  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3506
    Checksum:              319
 
 
    Coasting Arc #9 (Orbit 3520)
    ---------------------------------------
 
    Vector Time (GMT): 2019/296/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4210374.84                 A    =         6790202.58  meter
     Y    =        1738703.38  meter          E    =           .0015549
     Z    =       -5048906.80                 I    =           52.01056
     XDOT =       -608.877205                 Wp   =          129.42669
     YDOT =       7354.073697  meter/sec      RA   =           82.39259  deg
     ZDOT =       2019.342145                 TA   =          160.17039
                                              MA   =          160.10988
                                              Ha   =            228.360  n.mi
                                              Hp   =            220.695
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13813565.74                 X    =         4215144.27
     Y    =        5704407.41  feet           Y    =         1785813.22  meter
     Z    =      -16564654.87                 Z    =        -5028442.66
     XDOT =      -1997.628624                 XDOT =        -700.876282
     YDOT =      24127.538375  feet/sec       YDOT =        7346.750488  meter/sec
     ZDOT =       6625.138272                 ZDOT =        2016.160655
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11103990.87                 X    =         3384496.42
     Y    =       10155615.03  feet           Y    =         3095431.46  meter
     Z    =      -16471415.35                 Z    =        -5020487.40
     XDOT =      -9496.984764                 XDOT =       -2894.680956
     YDOT =      21133.866071  feet/sec       YDOT =        6441.602378  meter/sec
     ZDOT =       6610.067680                 ZDOT =        2014.748629
  
  
    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   19296.87026344  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6424  83.2026 0006614 182.5930 177.5187 15.50189210 35219
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19296.87026344   =   yrday.fracday
    Element set:     908
    Inclination:       51.6424  deg
    RA of node:        83.2026  deg
    Eccentricity:     .0006614     
    Arg of perigee:   182.5930  deg
    Mean anomaly:     177.5187  deg
    Mean motion:   15.50189210  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3521
    Checksum:              309
 
 
    Coasting Arc #10 (Orbit 3536)
    ---------------------------------------
 
    Vector Time (GMT): 2019/297/20:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4325150.65                 A    =         6790705.62  meter
     Y    =       -1857819.27  meter          E    =           .0006251
     Z    =        4888539.45                 I    =           52.00545
     XDOT =        347.250588                 Wp   =          118.55966
     YDOT =      -7255.658160  meter/sec      RA   =           77.45992  deg
     ZDOT =      -2450.714499                 TA   =          355.36900
                                              MA   =          355.37478
                                              Ha   =            228.356  n.mi
                                              Hp   =            220.593
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14190126.81                 X    =        -4327800.64
     Y    =       -6095207.57  feet           Y    =        -1906200.68  meter
     Z    =       16038515.25                 Z    =         4867522.89
     XDOT =       1139.273584                 XDOT =         440.264020
     YDOT =     -23804.652755  feet/sec       YDOT =       -7251.255037  meter/sec
     ZDOT =      -8040.401899                 ZDOT =       -2448.801306
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11500873.36                 X    =        -3505466.20
     Y    =      -10454821.82  feet           Y    =        -3186629.69  meter
     Z    =       15942767.59                 Z    =         4859355.56
     XDOT =       8188.466939                 XDOT =        2495.844723
     YDOT =     -21251.863683  feet/sec       YDOT =       -6477.568051  meter/sec
     ZDOT =      -8031.113255                 ZDOT =       -2447.883320
  
  
    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   19297.90169910  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6407  78.0910 0006556 185.1709 174.9375 15.50228236 35371
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19297.90169910   =   yrday.fracday
    Element set:     909
    Inclination:       51.6407  deg
    RA of node:        78.0910  deg
    Eccentricity:     .0006556     
    Arg of perigee:   185.1709  deg
    Mean anomaly:     174.9375  deg
    Mean motion:   15.50228236  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3537
    Checksum:              334
 
 
    Coasting Arc #11 (Orbit 3537)
    ---------------------------------------
 
    Vector Time (GMT): 2019/297/21:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1800659.81                 A    =         6794768.18  meter
     Y    =        5360458.90  meter          E    =           .0013268
     Z    =        3764661.40                 I    =           52.01685
     XDOT =      -4456.179752                 Wp   =          125.68378
     YDOT =      -4521.215905  meter/sec      RA   =           77.24769  deg
     ZDOT =       4288.179068                 TA   =          278.99158
                                              MA   =          279.14172
                                              Ha   =            228.183  n.mi
                                              Hp   =            220.705
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5907676.54                 X    =        -1878755.06
     Y    =       17586807.42  feet           Y    =         5339886.23  meter
     Z    =       12351251.30                 Z    =         3755724.34
     XDOT =     -14620.012310                 XDOT =       -4426.120876
     YDOT =     -14833.385514  feet/sec       YDOT =       -4570.879719  meter/sec
     ZDOT =      14068.828964                 ZDOT =        4266.605624
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6109152.22                 X    =        -1862069.60
     Y    =       17546808.90  feet           Y    =         5348267.35  meter
     Z    =       12310061.03                 Z    =         3752106.60
     XDOT =     -13334.880114                 XDOT =       -4064.471459
     YDOT =     -14485.796237  feet/sec       YDOT =       -4415.270693  meter/sec
     ZDOT =      13970.746114                 ZDOT =        4258.283416
  
  
    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   19297.96616384  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6389  77.7719 0006571 186.9777 173.1284 15.50223730 35389
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19297.96616384   =   yrday.fracday
    Element set:     910
    Inclination:       51.6389  deg
    RA of node:        77.7719  deg
    Eccentricity:     .0006571     
    Arg of perigee:   186.9777  deg
    Mean anomaly:     173.1284  deg
    Mean motion:   15.50223730  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3538
    Checksum:              352
 
 
    Coasting Arc #12 (Orbit 3552)
    ---------------------------------------
 
    Vector Time (GMT): 2019/298/21:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1675643.52                 A    =         6793876.54  meter
     Y    =       -5184677.78  meter          E    =           .0007082
     Z    =       -4059896.35                 I    =           52.00493
     XDOT =       4693.931081                 Wp   =          126.30134
     YDOT =       4594.215320  meter/sec      RA   =           72.31628  deg
     ZDOT =      -3938.544763                 TA   =          103.00185
                                              MA   =          102.92277
                                              Ha   =            228.167  n.mi
                                              Hp   =            220.875
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5497518.11                 X    =         1753216.63
     Y    =      -17010097.70  feet           Y    =        -5165506.10  meter
     Z    =      -13319869.93                 Z    =        -4051567.78
     XDOT =      15400.036356                 XDOT =        4661.339971
     YDOT =      15072.884908  feet/sec       YDOT =        4646.523666  meter/sec
     ZDOT =     -12921.734786                 ZDOT =       -3915.822487
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5408866.56                 X    =         1648622.53
     Y    =      -17068451.72  feet           Y    =        -5202464.08  meter
     Z    =      -13281460.11                 Z    =        -4048189.04
     XDOT =      14399.171193                 XDOT =        4388.867380
     YDOT =      14514.735810  feet/sec       YDOT =        4424.091475  meter/sec
     ZDOT =     -12818.427413                 ZDOT =       -3907.056676
  
  
    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   19298.93313652  .00016717  00000-0  10270-3 0  9110
    2 25544  51.6387  72.9792 0006511 189.5070 170.5956 15.50193729 35532
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19298.93313652   =   yrday.fracday
    Element set:     911
    Inclination:       51.6387  deg
    RA of node:        72.9792  deg
    Eccentricity:     .0006511     
    Arg of perigee:   189.5070  deg
    Mean anomaly:     170.5956  deg
    Mean motion:   15.50193729  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3553
    Checksum:              336
 
 
    Coasting Arc #13 (Orbit 3568)
    ---------------------------------------
 
    Vector Time (GMT): 2019/299/21:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1549270.39                 A    =         6792910.72  meter
     Y    =        5023223.01  meter          E    =           .0012043
     Z    =        4301556.65                 I    =           51.99165
     XDOT =      -4956.491793                 Wp   =          139.82418
     YDOT =      -4611.486439  meter/sec      RA   =           67.38510  deg
     ZDOT =       3585.457296                 TA   =          273.66555
                                              MA   =          273.80326
                                              Ha   =            227.920  n.mi
                                              Hp   =            221.029
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5082908.10                 X    =        -1626221.44
     Y    =       16480390.45  feet           Y    =         5005468.00  meter
     Z    =       14112718.68                 Z    =         4293843.47
     XDOT =     -16261.456015                 XDOT =       -4921.972996
     YDOT =     -15129.548685  feet/sec       YDOT =       -4666.720187  meter/sec
     ZDOT =      11763.311340                 ZDOT =        3561.464112
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4720027.42                 X    =        -1438664.36
     Y    =       16618186.53  feet           Y    =         5065223.25  meter
     Z    =       14077118.67                 Z    =         4290705.77
     XDOT =     -15540.974964                 XDOT =       -4736.889169
     YDOT =     -14326.759766  feet/sec       YDOT =       -4366.796377  meter/sec
     ZDOT =      11654.221471                 ZDOT =        3552.206704
  
  
    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   19299.96457081  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6396  67.8683 0006558 195.0872 165.0084 15.50233324 35691
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19299.96457081   =   yrday.fracday
    Element set:     912
    Inclination:       51.6396  deg
    RA of node:        67.8683  deg
    Eccentricity:     .0006558     
    Arg of perigee:   195.0872  deg
    Mean anomaly:     165.0084  deg
    Mean motion:   15.50233324  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3569
    Checksum:              345
 
 
    Coasting Arc #14 (Orbit 3583)
    ---------------------------------------
 
    Vector Time (GMT): 2019/300/21:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1491026.57                 A    =         6792092.36  meter
     Y    =       -4826384.54  meter          E    =           .0007699
     Z    =       -4545203.96                 I    =           51.97564
     XDOT =       5217.114520                 Wp   =          110.32032
     YDOT =       4608.726661  meter/sec      RA   =           62.45083  deg
     ZDOT =      -3189.362390                 TA   =          127.79326
                                              MA   =          127.72351
                                              Ha   =            227.866  n.mi
                                              Hp   =            221.206
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4891819.45                 X    =         1566964.47
     Y    =      -15834594.95  feet           Y    =        -4809286.46  meter
     Z    =      -14912086.48                 Z    =        -4537776.23
     XDOT =      17116.517454                 XDOT =        5180.683227
     YDOT =      15120.494295  feet/sec       YDOT =        4666.864263  meter/sec
     ZDOT =     -10463.787368                 ZDOT =       -3164.107625
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4276939.27                 X    =         1303611.09
     Y    =      -16043493.55  feet           Y    =        -4890056.83  meter
     Z    =      -14877792.96                 Z    =        -4534751.29
     XDOT =      16677.783195                 XDOT =        5083.388318
     YDOT =      14021.796978  feet/sec       YDOT =        4273.843719  meter/sec
     ZDOT =     -10348.958096                 ZDOT =       -3154.362428
  
  
    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   19300.93154094  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6405  63.0754 0006367 197.4285 162.6648 15.50203026 35843
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19300.93154094   =   yrday.fracday
    Element set:     913
    Inclination:       51.6405  deg
    RA of node:        63.0754  deg
    Eccentricity:     .0006367     
    Arg of perigee:   197.4285  deg
    Mean anomaly:     162.6648  deg
    Mean motion:   15.50203026  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3584
    Checksum:              306
 
 
    Coasting Arc #15 (Orbit 3592)
    ---------------------------------------
 
    Vector Time (GMT): 2019/301/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         107096.47                 A    =         6795212.65  meter
     Y    =        5764537.34  meter          E    =           .0012063
     Z    =        3594640.77                 I    =           51.97922
     XDOT =      -5610.959912                 Wp   =          126.01605
     YDOT =      -2691.601716  meter/sec      RA   =           59.76102  deg
     ZDOT =       4466.188256                 TA   =          276.17340
                                              MA   =          276.31082
                                              Ha   =            227.829  n.mi
                                              Hp   =            221.185
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         351366.38                 X    =           25166.51
     Y    =       18912524.09  feet           Y    =         5765277.00  meter
     Z    =       11793440.84                 Z    =         3594961.81
     XDOT =     -18408.661128                 XDOT =       -5602.139507
     YDOT =      -8830.714291  feet/sec       YDOT =       -2754.297954  meter/sec
     ZDOT =      14652.848610                 ZDOT =        4438.953052
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6525697.06                 X    =        -1989032.46
     Y    =      -17753856.71  feet           Y    =        -5411375.52  meter
     Z    =       11794410.65                 Z    =         3594936.37
     XDOT =      19093.039240                 XDOT =        5819.558360
     YDOT =       2671.834266  feet/sec       YDOT =         814.375084  meter/sec
     ZDOT =      14528.828907                 ZDOT =        4428.387051
  
  
    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   19301.51172151  .00016717  00000-0  10270-3 0  9149
    2 25544  51.6420  60.1968 0006851 199.4216 160.6674 15.50238629 35933
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19301.51172151   =   yrday.fracday
    Element set:     914
    Inclination:       51.6420  deg
    RA of node:        60.1968  deg
    Eccentricity:     .0006851     
    Arg of perigee:   199.4216  deg
    Mean anomaly:     160.6674  deg
    Mean motion:   15.50238629  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3593
    Checksum:              306
 
 
    Coasting Arc #16 (Orbit 3607)
    ---------------------------------------
 
    Vector Time (GMT): 2019/302/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -182885.01                 A    =         6794324.09  meter
     Y    =       -5559140.62  meter          E    =           .0005787
     Z    =       -3901407.68                 I    =           51.95806
     XDOT =       5857.625057                 Wp   =          141.46981
     YDOT =       2701.019346  meter/sec      RA   =           54.82846  deg
     ZDOT =      -4130.978430                 TA   =           85.34469
                                              MA   =           85.27860
                                              Ha   =            227.780  n.mi
                                              Hp   =            221.381
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -600016.44                 X    =         -101756.07
     Y    =      -18238650.32  feet           Y    =        -5560732.18  meter
     Z    =      -12799893.97                 Z    =        -3902098.99
     XDOT =      19217.929978                 XDOT =        5847.052709
     YDOT =       8861.612026  feet/sec       YDOT =        2766.464296  meter/sec
     ZDOT =     -13553.078840                 ZDOT =       -4102.549150
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6822631.79                 X    =         2079538.17
     Y    =       16923119.38  feet           Y    =         5158166.79  meter
     Z    =      -12802554.30                 Z    =        -3902218.55
     XDOT =     -19950.954455                 XDOT =       -6081.050918
     YDOT =      -2092.734469  feet/sec       YDOT =        -637.865466  meter/sec
     ZDOT =     -13423.623310                 ZDOT =       -4091.520385
  
  
    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   19302.47869126  .00016717  00000-0  10270-3 0  9151
    2 25544  51.6419  55.4057 0006825 202.7986 157.2862 15.50207374 36081
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19302.47869126   =   yrday.fracday
    Element set:     915
    Inclination:       51.6419  deg
    RA of node:        55.4057  deg
    Eccentricity:     .0006825     
    Arg of perigee:   202.7986  deg
    Mean anomaly:     157.2862  deg
    Mean motion:   15.50207374  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3608
    Checksum:              326
 
 
    Coasting Arc #17 (Orbit 3623)
    ---------------------------------------
 
    Vector Time (GMT): 2019/303/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         259941.36                 A    =         6793350.27  meter
     Y    =        5364758.64  meter          E    =           .0011065
     Z    =        4159483.82                 I    =           51.93615
     XDOT =      -6108.692824                 Wp   =          141.05756
     YDOT =      -2650.292746  meter/sec      RA   =           49.89352  deg
     ZDOT =       3786.167453                 TA   =          269.99132
                                              MA   =          270.11812
                                              Ha   =            227.548  n.mi
                                              Hp   =            221.538
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         852825.99                 X    =          179726.74
     Y    =       17600914.17  feet           Y    =         5367216.91  meter
     Z    =       13646600.45                 Z    =         4160551.81
     XDOT =     -20041.643125                 XDOT =       -6096.994069
     YDOT =      -8695.186176  feet/sec       YDOT =       -2718.539113  meter/sec
     ZDOT =      12421.809228                 ZDOT =        3756.521271
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7110938.23                 X    =        -2167413.97
     Y    =      -16119381.35  feet           Y    =        -4913187.44  meter
     Z    =       13650981.58                 Z    =         4160819.18
     XDOT =      20733.525709                 XDOT =        6319.578636
     YDOT =       1297.316885  feet/sec       YDOT =         395.422186  meter/sec
     ZDOT =      12286.806839                 ZDOT =        3745.018725
  
  
    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   19303.51012253  .00016717  00000-0  10270-3 0  9169
    2 25544  51.6431  50.2945 0006847 207.2785 152.8007 15.50242009 36249
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19303.51012253   =   yrday.fracday
    Element set:     916
    Inclination:       51.6431  deg
    RA of node:        50.2945  deg
    Eccentricity:     .0006847     
    Arg of perigee:   207.2785  deg
    Mean anomaly:     152.8007  deg
    Mean motion:   15.50242009  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3624
    Checksum:              282
 
 
    Coasting Arc #18 (Orbit 3638)
    ---------------------------------------
 
    Vector Time (GMT): 2019/304/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 949211.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -265623.85                 A    =         6792509.45  meter
     Y    =       -5156563.57  meter          E    =           .0005701
     Z    =       -4416162.94                 I    =           51.91134
     XDOT =       6357.717246                 Wp   =          117.25379
     YDOT =       2580.588001  meter/sec      RA   =           44.95685  deg
     ZDOT =      -3401.555140                 TA   =          118.41899
                                              MA   =          118.36153
                                              Ha   =            227.477  n.mi
                                              Hp   =            221.727
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -871469.31                 X    =         -186490.14
     Y    =      -16917859.49  feet           Y    =        -5159091.35  meter
     Z    =      -14488723.56                 Z    =        -4417261.24
     XDOT =      20858.652382                 XDOT =        6344.911096
     YDOT =       8466.496066  feet/sec       YDOT =        2651.612992  meter/sec
     ZDOT =     -11159.957810                 ZDOT =       -3370.702020
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7139808.38                 X    =         2176213.59
     Y    =       15357909.74  feet           Y    =         4681090.89  meter
     Z    =      -14493249.58                 Z    =        -4417542.47
     XDOT =     -21460.333567                 XDOT =       -6541.109671
     YDOT =       -403.967681  feet/sec       YDOT =        -123.129349  meter/sec
     ZDOT =     -11019.450468                 ZDOT =       -3358.728503
  
  
    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   19304.47708983  .00016717  00000-0  10270-3 0  9178
    2 25544  51.6438  45.5032 0006744 210.5409 149.5350 15.50210622 36392
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19304.47708983   =   yrday.fracday
    Element set:     917
    Inclination:       51.6438  deg
    RA of node:        45.5032  deg
    Eccentricity:     .0006744     
    Arg of perigee:   210.5409  deg
    Mean anomaly:     149.5350  deg
    Mean motion:   15.50210622  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3639
    Checksum:              304
 
             

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