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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14248.1882
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   75.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.596
   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 
   ------------------------------------------------------------------------
   270/16:51:47.699          -0.9               1.4              1.4    
   N/A                       -0.9               0.0              220.7  
   000/00:03:35.398          -0.6               0.0              215.8  
   
   274/01:42:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.9  
   000/00:00:00.000           0.0               0.0              215.6  
   
   277/10:56:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.4  
   000/00:00:00.000           0.0               0.0              215.1  
   
 
 
    Coasting Arc #1 (Orbit 3687)
    ---------------------------------------
 
    Vector Time (GMT): 2017/265/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4249537.99                 A    =         6777125.31  meter
     Y    =          -9962.41  meter          E    =           .0012067
     Z    =       -5289518.02                 I    =           51.24311
     XDOT =        200.378677                 Wp   =           76.03375
     YDOT =      -7656.130859  meter/sec      RA   =          272.36394  deg
     ZDOT =       -143.978680                 TA   =          192.57004
                                              MA   =          192.60016
                                              Ha   =            220.109  n.mi
                                              Hp   =            215.498
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13942053.78                 X    =        -4223416.61
     Y    =         -32685.07  feet           Y    =          -57338.29  meter
     Z    =      -17354061.75                 Z    =        -5310097.71
     XDOT =        657.410357                 XDOT =         286.676062
     YDOT =     -25118.539563  feet/sec       YDOT =       -7653.407589  meter/sec
     ZDOT =       -472.370998                 ZDOT =        -142.794671
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13827390.67                 X    =         4214588.68
     Y    =        -128516.84  feet           Y    =          -39171.93  meter
     Z    =      -17445117.99                 Z    =        -5317271.96
     XDOT =       -374.403124                 XDOT =        -114.118072
     YDOT =      24116.299335  feet/sec       YDOT =        7350.648037  meter/sec
     ZDOT =       -465.991402                 ZDOT =        -142.034179
  
  
    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   17265.51632839  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6384 273.1329 0004097 309.7753  50.3038 15.54210030 36885
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17265.51632839   =   yrday.fracday
    Element set:     900
    Inclination:       51.6384  deg
    RA of node:       273.1329  deg
    Eccentricity:     .0004097     
    Arg of perigee:   309.7753  deg
    Mean anomaly:      50.3038  deg
    Mean motion:   15.54210030  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3688
    Checksum:              304
 
 
    Coasting Arc #2 (Orbit 3703)
    ---------------------------------------
 
    Vector Time (GMT): 2017/266/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4134177.77                 A    =         6778142.39  meter
     Y    =        1867549.42  meter          E    =           .0006171
     Z    =        5036586.77                 I    =           51.24591
     XDOT =      -1113.061802                 Wp   =           14.44401
     YDOT =       7367.559447  meter/sec      RA   =          267.33521  deg
     ZDOT =      -1811.873425                 TA   =           93.22839
                                              MA   =           93.15778
                                              Ha   =            220.112  n.mi
                                              Hp   =            215.548
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13563575.37                 X    =         4088521.51
     Y    =        6127130.65  feet           Y    =         1913525.94  meter
     Z    =       16524234.80                 Z    =         5056558.45
     XDOT =      -3651.777565                 XDOT =       -1186.563786
     YDOT =      24171.782963  feet/sec       YDOT =        7354.701240  meter/sec
     ZDOT =      -5944.466619                 ZDOT =       -1817.459805
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13626750.16                 X    =        -4153433.45
     Y    =       -5736278.45  feet           Y    =        -1748417.67  meter
     Z    =       16612327.72                 Z    =         5063437.49
     XDOT =       2492.919993                 XDOT =         759.842014
     YDOT =     -23272.098919  feet/sec       YDOT =       -7093.335750  meter/sec
     ZDOT =      -5970.270599                 ZDOT =       -1819.738479
  
  
    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   17266.54509468  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6379 268.0029 0004135 314.2890  45.7923 15.54234212 37043
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17266.54509468   =   yrday.fracday
    Element set:     901
    Inclination:       51.6379  deg
    RA of node:       268.0029  deg
    Eccentricity:     .0004135     
    Arg of perigee:   314.2890  deg
    Mean anomaly:      45.7923  deg
    Mean motion:   15.54234212  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3704
    Checksum:              308
 
 
    Coasting Arc #3 (Orbit 3718)
    ---------------------------------------
 
    Vector Time (GMT): 2017/267/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3919878.01                 A    =         6781329.16  meter
     Y    =       -3548538.49  meter          E    =           .0005133
     Z    =       -4250283.94                 I    =           51.25940
     XDOT =       2009.224992                 Wp   =           86.36522
     YDOT =      -6481.268820  meter/sec      RA   =          262.31402  deg
     ZDOT =       3562.195976                 TA   =          220.19414
                                              MA   =          220.23211
                                              Ha   =            220.348  n.mi
                                              Hp   =            215.348
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12860492.15                 X    =        -3859259.90
     Y    =      -11642186.66  feet           Y    =        -3592034.75  meter
     Z    =      -13944501.12                 Z    =        -4269178.14
     XDOT =       6591.945512                 XDOT =        2064.247302
     YDOT =     -21264.005316  feet/sec       YDOT =       -6458.492277  meter/sec
     ZDOT =      11686.994673                 ZDOT =        3572.090614
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13292490.27                 X    =         4051551.04
     Y    =       11041666.86  feet           Y    =         3365500.06  meter
     Z    =      -14027586.22                 Z    =        -4275608.28
     XDOT =      -4721.774774                 XDOT =       -1439.196951
     YDOT =      20571.752000  feet/sec       YDOT =        6270.270010  meter/sec
     ZDOT =      11731.722013                 ZDOT =        3575.828870
  
  
    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   17267.50955981  .00016717  00000-0  10270-3 0  9024
    2 25544  51.6384 263.1947 0004179 320.1639  39.9206 15.54214939 37198
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17267.50955981   =   yrday.fracday
    Element set:     902
    Inclination:       51.6384  deg
    RA of node:       263.1947  deg
    Eccentricity:     .0004179     
    Arg of perigee:   320.1639  deg
    Mean anomaly:      39.9206  deg
    Mean motion:   15.54214939  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3719
    Checksum:              336
 
 
    Coasting Arc #4 (Orbit 3734)
    ---------------------------------------
 
    Vector Time (GMT): 2017/268/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3562656.27                 A    =         6785116.22  meter
     Y    =        4942358.76  meter          E    =           .0010609
     Z    =        2979720.00                 I    =           51.27668
     XDOT =      -2913.901198                 Wp   =           79.61883
     YDOT =       5089.148820  meter/sec      RA   =          257.30268  deg
     ZDOT =      -4940.312250                 TA   =           66.10827
                                              MA   =           65.99715
                                              Ha   =            220.426  n.mi
                                              Hp   =            215.301
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11688504.82                 X    =         3492650.50
     Y    =       16215087.80  feet           Y    =         4981807.66  meter
     Z    =        9775984.26                 Z    =         2996856.02
     XDOT =      -9560.043300                 XDOT =       -2946.594915
     YDOT =      16696.682481  feet/sec       YDOT =        5056.380340  meter/sec
     ZDOT =     -16208.373525                 ZDOT =       -4954.547134
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12627685.08                 X    =        -3848918.41
     Y    =      -15447250.26  feet           Y    =        -4708321.88  meter
     Z    =        9851097.13                 Z    =         3002614.41
     XDOT =       7250.894257                 XDOT =        2210.072569
     YDOT =     -16339.657461  feet/sec       YDOT =       -4980.327594  meter/sec
     ZDOT =     -16272.097487                 ZDOT =       -4959.735314
  
  
    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   17268.53831863  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6372 258.0650 0004374 323.4266  36.6588 15.54263356 37350
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17268.53831863   =   yrday.fracday
    Element set:     903
    Inclination:       51.6372  deg
    RA of node:       258.0650  deg
    Eccentricity:     .0004374     
    Arg of perigee:   323.4266  deg
    Mean anomaly:      36.6588  deg
    Mean motion:   15.54263356  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3735
    Checksum:              325
 
 
    Coasting Arc #5 (Orbit 3749)
    ---------------------------------------
 
    Vector Time (GMT): 2017/269/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3060762.03                 A    =         6788082.86  meter
     Y    =       -5886423.10  meter          E    =           .0010638
     Z    =       -1405878.38                 I    =           51.29473
     XDOT =       3787.555272                 Wp   =           16.37376
     YDOT =      -3342.830189  meter/sec      RA   =          252.30290  deg
     ZDOT =       5771.213425                 TA   =          328.22133
                                              MA   =          328.28548
                                              Ha   =            220.484  n.mi
                                              Hp   =            215.170
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10041870.17                 X    =        -2987881.84
     Y    =      -19312411.73  feet           Y    =        -5920243.24  meter
     Z    =       -4612461.87                 Z    =        -1420569.30
     XDOT =      12426.362442                 XDOT =        3796.620122
     YDOT =     -10967.290646  feet/sec       YDOT =       -3300.424014  meter/sec
     ZDOT =      18934.427247                 ZDOT =        5789.634702
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11533272.68                 X    =         3515341.51
     Y    =       18444401.39  feet           Y    =         5621853.54  meter
     Z    =       -4676631.97                 Z    =        -1425437.42
     XDOT =     -10034.465858                 XDOT =       -3058.505194
     YDOT =      11079.222923  feet/sec       YDOT =        3376.947147  meter/sec
     ZDOT =      19016.423317                 ZDOT =        5796.205827
  
  
    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   17269.50277888  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6372 253.2571 0004120 327.4101  32.6797 15.54260194 37502
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17269.50277888   =   yrday.fracday
    Element set:     904
    Inclination:       51.6372  deg
    RA of node:       253.2571  deg
    Eccentricity:     .0004120     
    Arg of perigee:   327.4101  deg
    Mean anomaly:      32.6797  deg
    Mean motion:   15.54260194  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3750
    Checksum:              307
 
 
    Coasting Arc #6 (Orbit 3765)
    ---------------------------------------
 
    Vector Time (GMT): 2017/270/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2352884.40                 A    =         6788887.87  meter
     Y    =        6355429.48  meter          E    =           .0007272
     Z    =        -350889.56                 I    =           51.30922
     XDOT =      -4605.617673                 Wp   =          128.64745
     YDOT =       1380.326800  meter/sec      RA   =          247.30804  deg
     ZDOT =      -5970.387429                 TA   =           55.15097
                                              MA   =           55.08261
                                              Ha   =            220.698  n.mi
                                              Hp   =            215.077
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7719437.00                 X    =         2283345.89
     Y    =       20851146.60  feet           Y    =         6381352.20  meter
     Z    =       -1151212.45                 Z    =         -339629.22
     XDOT =     -15110.294203                 XDOT =       -4591.709033
     YDOT =       4528.631233  feet/sec       YDOT =        1328.900971  meter/sec
     ZDOT =     -19587.885265                 ZDOT =       -5992.726645
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9725323.39                 X    =        -2964278.57
     Y    =      -19997209.41  feet           Y    =        -6095149.43  meter
     Z    =       -1102276.24                 Z    =         -335973.80
     XDOT =      13009.815441                 XDOT =        3965.391746
     YDOT =      -5258.644693  feet/sec       YDOT =       -1602.834903  meter/sec
     ZDOT =     -19686.943693                 ZDOT =       -6000.580438
  
  
    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   17270.53153100  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6381 248.1269 0004368 332.1021  27.9897 15.54262658 37669
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17270.53153100   =   yrday.fracday
    Element set:     905
    Inclination:       51.6381  deg
    RA of node:       248.1269  deg
    Eccentricity:     .0004368     
    Arg of perigee:   332.1021  deg
    Mean anomaly:      27.9897  deg
    Mean motion:   15.54262658  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3766
    Checksum:              310
 
 
    Coasting Arc #7 (Orbit 3768)
    ---------------------------------------
 
    Vector Time (GMT): 2017/270/16:53:35.398
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2388501.75                 A    =         6779821.85  meter
     Y    =        4150588.55  meter          E    =           .0010499
     Z    =       -4808989.24                 I    =           51.28227
     XDOT =      -4631.308698                 Wp   =           49.04985
     YDOT =      -5565.465384  meter/sec      RA   =          246.30425  deg
     ZDOT =      -2500.072476                 TA   =          196.20505
                                              MA   =          196.23865
                                              Ha   =            220.682  n.mi
                                              Hp   =            215.816
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7836291.82                 X    =        -2411377.26
     Y    =       13617416.51  feet           Y    =         4123750.44  meter
     Z    =      -15777523.75                 Z    =        -4820647.82
     XDOT =     -15194.582341                 XDOT =       -4556.585723
     YDOT =     -18259.400867  feet/sec       YDOT =       -5616.838217  meter/sec
     ZDOT =      -8202.337519                 ZDOT =       -2522.388268
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11926045.17                 X    =        -3635058.57
     Y    =      -10147001.94  feet           Y    =        -3092806.19  meter
     Z    =      -15829704.85                 Z    =        -4824894.04
     XDOT =      20033.683496                 XDOT =        6106.266730
     YDOT =     -10581.151026  feet/sec       YDOT =       -3225.134833  meter/sec
     ZDOT =      -8300.315447                 ZDOT =       -2529.936148
  
  
    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   17270.72442365  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6414 247.1666 0004539 317.4594  42.6207 15.54010516 37693
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17270.72442365   =   yrday.fracday
    Element set:     906
    Inclination:       51.6414  deg
    RA of node:       247.1666  deg
    Eccentricity:     .0004539     
    Arg of perigee:   317.4594  deg
    Mean anomaly:      42.6207  deg
    Mean motion:   15.54010516  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3769
    Checksum:              310
 
 
    Coasting Arc #8 (Orbit 3784)
    ---------------------------------------
 
    Vector Time (GMT): 2017/271/16:53:35.398
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3319683.37                 A    =         6777834.89  meter
     Y    =       -2704501.41  meter          E    =           .0002072
     Z    =        5253936.44                 I    =           51.28909
     XDOT =       4143.264488                 Wp   =          355.12874
     YDOT =       6416.498221  meter/sec      RA   =          241.28325  deg
     ZDOT =        687.078799                 TA   =           88.28996
                                              MA   =           88.26623
                                              Ha   =            220.617  n.mi
                                              Hp   =            215.843
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10891349.63                 X    =         3324157.84
     Y    =       -8873036.14  feet           Y    =        -2667353.06  meter
     Z    =       17237324.29                 Z    =         5270073.63
     XDOT =      13593.387429                 XDOT =        4067.868042
     YDOT =      21051.503349  feet/sec       YDOT =        6462.409512  meter/sec
     ZDOT =       2254.195535                 ZDOT =         707.022072
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6904657.91                 X    =         2104539.73
     Y    =       12132500.13  feet           Y    =         3697986.04  meter
     Z    =       17309123.47                 Z    =         5275820.83
     XDOT =     -22173.346127                 XDOT =       -6758.435899
     YDOT =       9287.836525  feet/sec       YDOT =        2830.932573  meter/sec
     ZDOT =       2341.573009                 ZDOT =         713.711453
  
  
    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   17271.75334753  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6406 242.0386 0004534 320.0628  40.0191 15.54018602 37856
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17271.75334753   =   yrday.fracday
    Element set:     907
    Inclination:       51.6406  deg
    RA of node:       242.0386  deg
    Eccentricity:     .0004534     
    Arg of perigee:   320.0628  deg
    Mean anomaly:      40.0191  deg
    Mean motion:   15.54018602  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3785
    Checksum:              289
 
 
    Coasting Arc #9 (Orbit 3799)
    ---------------------------------------
 
    Vector Time (GMT): 2017/272/16:53:35.398
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4206611.31                 A    =         6778137.19  meter
     Y    =        1186502.85  meter          E    =           .0011319
     Z    =       -5190207.56                 I    =           51.30684
     XDOT =      -3375.706478                 Wp   =           82.64689
     YDOT =      -6772.449118  meter/sec      RA   =          236.26140  deg
     ZDOT =       1191.428380                 TA   =          198.82648
                                              MA   =          198.86837
                                              Ha   =            220.814  n.mi
                                              Hp   =            215.607
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13801218.20                 X    =        -4194354.82
     Y    =        3892725.88  feet           Y    =         1139529.79  meter
     Z    =      -17028240.01                 Z    =        -5210612.41
     XDOT =     -11075.152486                 XDOT =       -3305.511669
     YDOT =     -22219.321254  feet/sec       YDOT =       -6809.805998  meter/sec
     ZDOT =       3908.885762                 ZDOT =        1175.201151
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1744247.92                 X    =         -531646.77
     Y    =      -14124263.76  feet           Y    =        -4305075.60  meter
     Z    =      -17118722.76                 Z    =        -5217786.70
     XDOT =      22629.472372                 XDOT =        6897.463179
     YDOT =      -7431.767120  feet/sec       YDOT =       -2265.202618  meter/sec
     ZDOT =       3837.985199                 ZDOT =        1169.817889
  
  
    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   17272.71796173  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6408 237.2314 0004630 323.2098  36.8736 15.54014536 38006
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17272.71796173   =   yrday.fracday
    Element set:     908
    Inclination:       51.6408  deg
    RA of node:       237.2314  deg
    Eccentricity:     .0004630     
    Arg of perigee:   323.2098  deg
    Mean anomaly:      36.8736  deg
    Mean motion:   15.54014536  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3800
    Checksum:              305
 
 
    Coasting Arc #10 (Orbit 3815)
    ---------------------------------------
 
    Vector Time (GMT): 2017/273/16:53:35.398
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4974587.02                 A    =         6780472.47  meter
     Y    =         322937.04  meter          E    =           .0009001
     Z    =        4595468.55                 I    =           51.33455
     XDOT =       2317.168381                 Wp   =           33.64330
     YDOT =       6679.674627  meter/sec      RA   =          231.24401  deg
     ZDOT =      -2967.572786                 TA   =           86.12202
                                              MA   =           86.01912
                                              Ha   =            220.847  n.mi
                                              Hp   =            215.599
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16320823.57                 X    =         4948283.50
     Y    =        1059504.72  feet           Y    =          378419.59  meter
     Z    =       15076996.56                 Z    =         4619569.74
     XDOT =       7602.258469                 XDOT =        2256.717342
     YDOT =      21914.943003  feet/sec       YDOT =        6705.248525  meter/sec
     ZDOT =      -9736.131189                 ZDOT =       -2956.464059
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3264355.61                 X    =         -994975.59
     Y    =       15925092.90  feet           Y    =         4853968.32  meter
     Z    =       15183644.36                 Z    =         4627974.80
     XDOT =     -21593.952260                 XDOT =       -6581.836649
     YDOT =       4841.988267  feet/sec       YDOT =        1475.838024  meter/sec
     ZDOT =      -9687.856241                 ZDOT =       -2952.858582
  
  
    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   17273.74687711  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6413 232.1031 0004781 327.1683  32.9172 15.54050724 38169
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17273.74687711   =   yrday.fracday
    Element set:     909
    Inclination:       51.6413  deg
    RA of node:       232.1031  deg
    Eccentricity:     .0004781     
    Arg of perigee:   327.1683  deg
    Mean anomaly:      32.9172  deg
    Mean motion:   15.54050724  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3816
    Checksum:              300
 
 
    Coasting Arc #11 (Orbit 3821)
    ---------------------------------------
 
    Vector Time (GMT): 2017/274/01:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3509539.28                 A    =         6789017.29  meter
     Y    =       -5660820.06  meter          E    =           .0014234
     Z    =        1270133.37                 I    =           51.36945
     XDOT =       4731.437873                 Wp   =           41.92183
     YDOT =      -1621.921828  meter/sec      RA   =          229.43638  deg
     ZDOT =       5817.489274                 TA   =          331.95238
                                              MA   =          332.02900
                                              Ha   =            220.909  n.mi
                                              Hp   =            215.618
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11514236.47                 X    =        -3452147.35
     Y    =      -18572244.30  feet           Y    =        -5699745.11  meter
     Z    =        4167104.25                 Z    =         1253224.97
     XDOT =      15523.090136                 XDOT =        4720.964356
     YDOT =      -5321.265840  feet/sec       YDOT =       -1569.069683  meter/sec
     ZDOT =      19086.250900                 ZDOT =        5840.447936
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20049283.23                 X    =        -6111021.53
     Y    =       -8726062.13  feet           Y    =        -2659703.74  meter
     Z    =        4093011.05                 Z    =         1247549.77
     XDOT =       9012.323321                 XDOT =        2746.956148
     YDOT =     -11663.819237  feet/sec       YDOT =       -3555.132103  meter/sec
     ZDOT =      19188.105352                 ZDOT =        5848.534511
  
  
    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   17274.13272084  .00016717  00000-0  10270-3 0  9106
    2 25544  51.6406 230.1749 0004189 326.9696  33.1194 15.54010534 38227
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17274.13272084   =   yrday.fracday
    Element set:     910
    Inclination:       51.6406  deg
    RA of node:       230.1749  deg
    Eccentricity:     .0004189     
    Arg of perigee:   326.9696  deg
    Mean anomaly:      33.1194  deg
    Mean motion:   15.54010534  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3822
    Checksum:              297
 
 
    Coasting Arc #12 (Orbit 3836)
    ---------------------------------------
 
    Vector Time (GMT): 2017/275/01:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2523614.97                 A    =         6786322.76  meter
     Y    =        5633535.94  meter          E    =           .0002315
     Z    =       -2822773.03                 I    =           51.38204
     XDOT =      -5746.227051                 Wp   =           57.76591
     YDOT =         35.303492  meter/sec      RA   =          224.44475  deg
     ZDOT =      -5068.628015                 TA   =          154.39198
                                              MA   =          154.38052
                                              Ha   =            220.984  n.mi
                                              Hp   =            215.554
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8279576.68                 X    =         2474143.42
     Y    =       18482729.46  feet           Y    =         5661479.80  meter
     Z    =       -9261066.38                 Z    =        -2810634.82
     XDOT =     -18852.450956                 XDOT =       -5721.573739
     YDOT =        115.825105  feet/sec       YDOT =         -28.817455  meter/sec
     ZDOT =     -16629.357005                 ZDOT =       -5096.481642
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17541406.00                 X    =         5346620.55
     Y    =       10170572.14  feet           Y    =         3099990.39  meter
     Z    =       -9208070.73                 Z    =        -2806619.96
     XDOT =     -14430.296000                 XDOT =       -4398.354221
     YDOT =       9726.479031  feet/sec       YDOT =        2964.630809  meter/sec
     ZDOT =     -16752.679094                 ZDOT =       -5106.216588
  
  
    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   17275.09732455  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6402 225.3678 0004171 329.2212  30.8696 15.54014026 38378
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17275.09732455   =   yrday.fracday
    Element set:     911
    Inclination:       51.6402  deg
    RA of node:       225.3678  deg
    Eccentricity:     .0004171     
    Arg of perigee:   329.2212  deg
    Mean anomaly:      30.8696  deg
    Mean motion:   15.54014026  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3837
    Checksum:              298
 
 
    Coasting Arc #13 (Orbit 3852)
    ---------------------------------------
 
    Vector Time (GMT): 2017/276/01:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1275351.38                 A    =         6782519.92  meter
     Y    =       -5263026.05  meter          E    =           .0008560
     Z    =        4075411.70                 I    =           51.39451
     XDOT =       6501.641182                 Wp   =           81.11883
     YDOT =       1392.233192  meter/sec      RA   =          219.44521  deg
     ZDOT =       3826.964393                 TA   =          329.18765
                                              MA   =          329.23787
                                              Ha   =            220.996  n.mi
                                              Hp   =            215.395
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4184223.68                 X    =        -1236200.50
     Y    =      -17267145.82  feet           Y    =        -5277068.47  meter
     Z    =       13370773.31                 Z    =         4069312.17
     XDOT =      21330.843772                 XDOT =        6467.000017
     YDOT =       4567.694199  feet/sec       YDOT =        1464.745775  meter/sec
     ZDOT =      12555.657456                 ZDOT =        3858.463214
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13722502.88                 X    =        -4182618.88
     Y    =      -11316278.27  feet           Y    =        -3449201.62  meter
     Z    =       13344451.73                 Z    =         4067388.89
     XDOT =      18958.239440                 XDOT =        5778.471381
     YDOT =      -7997.525041  feet/sec       YDOT =       -2437.645632  meter/sec
     ZDOT =      12694.943645                 ZDOT =        3869.418823
  
  
    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   17276.12622944  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6410 220.2395 0004170 332.3569  27.7361 15.54054963 38532
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17276.12622944   =   yrday.fracday
    Element set:     912
    Inclination:       51.6410  deg
    RA of node:       220.2395  deg
    Eccentricity:     .0004170     
    Arg of perigee:   332.3569  deg
    Mean anomaly:      27.7361  deg
    Mean motion:   15.54054963  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3853
    Checksum:              299
 
 
    Coasting Arc #14 (Orbit 3867)
    ---------------------------------------
 
    Vector Time (GMT): 2017/277/01:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -181264.15                 A    =         6779338.13  meter
     Y    =        4653509.58  meter          E    =           .0012442
     Z    =       -4937828.10                 I    =           51.40979
     XDOT =      -6866.736949                 Wp   =           53.95419
     YDOT =      -2591.982789  meter/sec      RA   =          214.43805  deg
     ZDOT =      -2187.359637                 TA   =          194.59565
                                              MA   =          194.63160
                                              Ha   =            221.179  n.mi
                                              Hp   =            215.334
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -594698.66                 X    =         -209301.70
     Y    =       15267419.87  feet           Y    =         4651325.12  meter
     Z    =      -16200223.43                 Z    =        -4938777.37
     XDOT =     -22528.664532                 XDOT =       -6826.617138
     YDOT =      -8503.880542  feet/sec       YDOT =       -2668.547305  meter/sec
     ZDOT =      -7176.376761                 ZDOT =       -2220.618612
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8922858.47                 X    =         2719687.26
     Y    =       12396562.68  feet           Y    =         3778472.30  meter
     Z    =      -16205025.33                 Z    =        -4939291.72
     XDOT =     -22099.191263                 XDOT =       -6735.833497
     YDOT =       6319.315857  feet/sec       YDOT =        1926.127473  meter/sec
     ZDOT =      -7323.315895                 ZDOT =       -2232.146685
  
  
    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   17277.09082495  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6414 215.4324 0004323 335.8218  24.2731 15.54015785 38681
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17277.09082495   =   yrday.fracday
    Element set:     913
    Inclination:       51.6414  deg
    RA of node:       215.4324  deg
    Eccentricity:     .0004323     
    Arg of perigee:   335.8218  deg
    Mean anomaly:      24.2731  deg
    Mean motion:   15.54015785  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3868
    Checksum:              307
 
 
    Coasting Arc #15 (Orbit 3873)
    ---------------------------------------
 
    Vector Time (GMT): 2017/277/10:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         643250.70                 A    =         6780267.84  meter
     Y    =        4855820.87  meter          E    =           .0011846
     Z    =       -4699430.68                 I    =           51.42139
     XDOT =      -6911.616044                 Wp   =           47.57498
     YDOT =      -1777.391908  meter/sec      RA   =          212.52008  deg
     ZDOT =      -2779.251942                 TA   =          194.74892
                                              MA   =          194.78351
                                              Ha   =            221.391  n.mi
                                              Hp   =            215.147
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2110402.56                 X    =          611731.58
     Y    =       15931170.83  feet           Y    =         4862837.26  meter
     Z    =      -15418079.65                 Z    =        -4696383.16
     XDOT =     -22675.905657                 XDOT =       -6877.726699
     YDOT =      -5831.338281  feet/sec       YDOT =       -1854.493214  meter/sec
     ZDOT =      -9118.280649                 ZDOT =       -2812.744222
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1222957.49                 X    =         -372757.44
     Y    =      -16036120.67  feet           Y    =        -4887809.58  meter
     Z    =      -15405206.65                 Z    =        -4695506.99
     XDOT =      21042.645295                 XDOT =        6413.798286
     YDOT =       7307.561195  feet/sec       YDOT =        2227.344652  meter/sec
     ZDOT =      -9266.362898                 ZDOT =       -2824.387411
  
  
    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   17277.47666212  .00016717  00000-0  10270-3 0  9140
    2 25544  51.6393 213.5108 0004718 342.4226  17.6763 15.54037684 38747
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17277.47666212   =   yrday.fracday
    Element set:     914
    Inclination:       51.6393  deg
    RA of node:       213.5108  deg
    Eccentricity:     .0004718     
    Arg of perigee:   342.4226  deg
    Mean anomaly:      17.6763  deg
    Mean motion:   15.54037684  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3874
    Checksum:              321
 
 
    Coasting Arc #16 (Orbit 3889)
    ---------------------------------------
 
    Vector Time (GMT): 2017/278/10:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         947907.15                 A    =         6777865.10  meter
     Y    =       -4205214.89  meter          E    =           .0003205
     Z    =        5228444.59                 I    =           51.44190
     XDOT =       7071.863300                 Wp   =           34.65777
     YDOT =       2805.429841  meter/sec      RA   =          207.51091  deg
     ZDOT =        976.570030                 TA   =           45.98519
                                              MA   =           45.95879
                                              Ha   =            221.351  n.mi
                                              Hp   =            215.043
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3109931.59                 X    =          969462.92
     Y    =      -13796636.78  feet           Y    =        -4194493.51  meter
     Z    =       17153689.61                 Z    =         5233102.23
     XDOT =      23201.651248                 XDOT =        7035.222868
     YDOT =       9204.166146  feet/sec       YDOT =        2884.307508  meter/sec
     ZDOT =       3203.969915                 ZDOT =        1010.834090
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3609796.37                 X    =        -1100265.93
     Y    =       13647776.93  feet           Y    =         4159842.41  meter
     Z    =       17174850.31                 Z    =         5234894.37
     XDOT =     -21751.205839                 XDOT =       -6629.767540
     YDOT =      -9966.179038  feet/sec       YDOT =       -3037.691371  meter/sec
     ZDOT =       3355.352725                 ZDOT =        1022.711511
  
  
    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   17278.50555487  .00016717  00000-0  10270-3 0  9157
    2 25544  51.6393 208.3835 0004782 344.6696  15.4311 15.54068629 38908
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17278.50555487   =   yrday.fracday
    Element set:     915
    Inclination:       51.6393  deg
    RA of node:       208.3835  deg
    Eccentricity:     .0004782     
    Arg of perigee:   344.6696  deg
    Mean anomaly:      15.4311  deg
    Mean motion:   15.54068629  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3890
    Checksum:              339
 
 
    Coasting Arc #17 (Orbit 3904)
    ---------------------------------------
 
    Vector Time (GMT): 2017/279/10:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2562384.07                 A    =         6777848.23  meter
     Y    =        3459924.16  meter          E    =           .0013759
     Z    =       -5246005.77                 I    =           51.47153
     XDOT =      -6709.717501                 Wp   =           78.05329
     YDOT =      -3575.492556  meter/sec      RA   =          202.49914  deg
     ZDOT =        924.009086                 TA   =          200.79022
                                              MA   =          200.84623
                                              Ha   =            221.527  n.mi
                                              Hp   =            214.834
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8406771.89                 X    =        -2575400.40
     Y    =       11351457.21  feet           Y    =         3431196.39  meter
     Z    =      -17211305.02                 Z    =        -5258485.33
     XDOT =     -22013.508860                 XDOT =       -6673.725179
     YDOT =     -11730.618622  feet/sec       YDOT =       -3650.323837  meter/sec
     ZDOT =       3031.525873                 ZDOT =         891.502590
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8601806.41                 X    =         2621830.59
     Y    =      -11118344.98  feet           Y    =        -3388871.55  meter
     Z    =      -17267013.24                 Z    =        -5262985.64
     XDOT =      20892.202306                 XDOT =        6367.943263
     YDOT =      11702.906511  feet/sec       YDOT =        3567.045905  meter/sec
     ZDOT =       2888.010297                 ZDOT =         880.265538
  
  
    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   17279.47013848  .00016717  00000-0  10270-3 0  9165
    2 25544  51.6397 203.5755 0004752 348.6992  11.4053 15.54046953 39052
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17279.47013848   =   yrday.fracday
    Element set:     916
    Inclination:       51.6397  deg
    RA of node:       203.5755  deg
    Eccentricity:     .0004752     
    Arg of perigee:   348.6992  deg
    Mean anomaly:      11.4053  deg
    Mean motion:   15.54046953  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3905
    Checksum:              331
 
 
    Coasting Arc #18 (Orbit 3920)
    ---------------------------------------
 
    Vector Time (GMT): 2017/280/10:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4095658.41                 A    =         6780002.29  meter
     Y    =       -2638682.40  meter          E    =           .0010391
     Z    =        4713288.79                 I    =           51.51004
     XDOT =       5843.175699                 Wp   =           37.09002
     YDOT =       4135.214718  meter/sec      RA   =          197.49312  deg
     ZDOT =      -2751.137030                 TA   =           80.24791
                                              MA   =           80.13057
                                              Ha   =            221.544  n.mi
                                              Hp   =            214.788
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13437199.51                 X    =         4101965.09
     Y    =       -8657094.49  feet           Y    =        -2592846.18  meter
     Z    =       15463545.91                 Z    =         4733200.29
     XDOT =      19170.523946                 XDOT =        5809.864329
     YDOT =      13566.977421  feet/sec       YDOT =        4200.370544  meter/sec
     ZDOT =      -9026.040126                 ZDOT =       -2722.833403
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13423260.05                 X    =        -4091409.66
     Y    =        8519035.38  feet           Y    =         2596601.98  meter
     Z    =       15552073.61                 Z    =         4740272.04
     XDOT =     -18468.410717                 XDOT =       -5629.171586
     YDOT =     -12783.283785  feet/sec       YDOT =       -3896.344898  meter/sec
     ZDOT =      -8901.196887                 ZDOT =       -2713.084811
  
  
    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   17280.49901953  .00016717  00000-0  10270-3 0  9173
    2 25544  51.6402 198.4477 0004807 352.5868   7.5213 15.54057700 39213
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17280.49901953   =   yrday.fracday
    Element set:     917
    Inclination:       51.6402  deg
    RA of node:       198.4477  deg
    Eccentricity:     .0004807     
    Arg of perigee:   352.5868  deg
    Mean anomaly:       7.5213  deg
    Mean motion:   15.54057700  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3921
    Checksum:              320
 
             

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