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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  17659.2707
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   96.4
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.743
   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 
   ------------------------------------------------------------------------
   183/05:31:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.1  
   000/00:00:00.000           0.0               0.0              213.6  
   
   183/06:09:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.2  
   000/00:00:00.000           0.0               0.0              213.6  
   
   185/03:48:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.1  
   000/00:00:00.000           0.0               0.0              213.6  
   
   187/04:14:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.2  
   000/00:00:00.000           0.0               0.0              213.5  
   
   189/01:37:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.3  
   000/00:00:00.000           0.0               0.0              213.4  
   
 
 
    Coasting Arc #1 (Orbit 581)
    ---------------------------------------
 
    Vector Time (GMT): 2016/174/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1702754.95                 A    =         6779971.85  meter
     Y    =        4947681.05  meter          E    =           .0009143
     Z    =        4305072.06                 I    =           51.82772
     XDOT =      -6758.387943                 Wp   =          102.66842
     YDOT =       -769.230144  meter/sec      RA   =           30.70803  deg
     ZDOT =       3548.853247                 TA   =          311.24967
                                              MA   =          311.32841
                                              Ha   =            220.094  n.mi
                                              Hp   =            214.008
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5586466.36                 X    =         1626390.14
     Y    =       16232549.38  feet           Y    =         4966294.81  meter
     Z    =       14124252.15                 Z    =         4313158.77
     XDOT =     -22173.188790                 XDOT =       -6766.522605
     YDOT =      -2523.720945  feet/sec       YDOT =        -844.852916  meter/sec
     ZDOT =      11643.219314                 ZDOT =        3516.003037
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13724223.98                 X    =         4183143.47
     Y    =      -10265601.56  feet           Y    =        -3128955.36  meter
     Z    =       14158455.61                 Z    =         4315497.27
     XDOT =       3763.562179                 XDOT =        1147.133752
     YDOT =      20930.240699  feet/sec       YDOT =        6379.537365  meter/sec
     ZDOT =      11500.202631                 ZDOT =        3505.261762
  
  
    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   16174.60402830  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6414  31.0142 0000986 338.6514  21.4598 15.54626203  5825
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16174.60402830   =   yrday.fracday
    Element set:     900
    Inclination:       51.6414  deg
    RA of node:        31.0142  deg
    Eccentricity:     .0000986     
    Arg of perigee:   338.6514  deg
    Mean anomaly:      21.4598  deg
    Mean motion:   15.54626203  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             582
    Checksum:              278
 
 
    Coasting Arc #2 (Orbit 596)
    ---------------------------------------
 
    Vector Time (GMT): 2016/175/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         113617.49                 A    =         6776638.40  meter
     Y    =       -4433468.66  meter          E    =           .0013642
     Z    =       -5136112.21                 I    =           51.78740
     XDOT =       7198.828054                 Wp   =           74.03198
     YDOT =       2055.974923  meter/sec      RA   =           25.71939  deg
     ZDOT =      -1615.365065                 TA   =          180.39655
                                              MA   =          180.39763
                                              Ha   =            220.133  n.mi
                                              Hp   =            213.897
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         372760.80                 X    =          188134.00
     Y    =      -14545500.85  feet           Y    =        -4431780.82  meter
     Z    =      -16850761.83                 Z    =        -5135379.85
     XDOT =      23618.202276                 XDOT =        7183.149272
     YDOT =       6745.324551  feet/sec       YDOT =        2136.389551  meter/sec
     ZDOT =      -5299.754150                 ZDOT =       -1580.433090
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13905253.75                 X    =        -4238321.34
     Y    =        4300413.62  feet           Y    =         1310766.07  meter
     Z    =      -16846634.11                 Z    =        -5134854.08
     XDOT =      -1043.876971                 XDOT =        -318.173701
     YDOT =     -23543.339427  feet/sec       YDOT =       -7176.009857  meter/sec
     ZDOT =      -5147.938384                 ZDOT =       -1569.091619
  
  
    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   16175.56823380  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6402  26.2030 0000870 349.1227  10.9907 15.54655578  5974
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16175.56823380   =   yrday.fracday
    Element set:     901
    Inclination:       51.6402  deg
    RA of node:        26.2030  deg
    Eccentricity:     .0000870     
    Arg of perigee:   349.1227  deg
    Mean anomaly:      10.9907  deg
    Mean motion:   15.54655578  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             597
    Checksum:              301
 
 
    Coasting Arc #3 (Orbit 612)
    ---------------------------------------
 
    Vector Time (GMT): 2016/176/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2020584.94                 A    =         6775989.65  meter
     Y    =        3702714.14  meter          E    =           .0003127
     Z    =        5300970.09                 I    =           51.75534
     XDOT =      -7005.570518                 Wp   =           51.59061
     YDOT =      -3083.797539  meter/sec      RA   =           20.72353  deg
     ZDOT =       -514.204310                 TA   =           43.31754
                                              MA   =           43.29295
                                              Ha   =            220.257  n.mi
                                              Hp   =            213.927
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6629215.69                 X    =        -2087589.02
     Y    =       12148012.27  feet           Y    =         3679743.39  meter
     Z    =       17391634.16                 Z    =         5290992.35
     XDOT =     -22984.155244                 XDOT =       -6968.068294
     YDOT =     -10117.445995  feet/sec       YDOT =       -3161.928752  meter/sec
     ZDOT =      -1687.022013                 ZDOT =        -548.144539
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13725088.93                 X    =         4183407.11
     Y    =        2163438.54  feet           Y    =          659416.07  meter
     Z    =       17347366.05                 Z    =         5287477.17
     XDOT =      -1463.598606                 XDOT =        -446.104855
     YDOT =      24048.835559  feet/sec       YDOT =        7330.085078  meter/sec
     ZDOT =      -1834.293571                 ZDOT =        -559.092680
  
  
    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   16176.59671687  .00016717  00000-0  10270-3 0  9029
    2 25544  51.6400  21.0721 0000825 350.0305  10.0832 15.54629943  6134
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16176.59671687   =   yrday.fracday
    Element set:     902
    Inclination:       51.6400  deg
    RA of node:        21.0721  deg
    Eccentricity:     .0000825     
    Arg of perigee:   350.0305  deg
    Mean anomaly:      10.0832  deg
    Mean motion:   15.54629943  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             613
    Checksum:              277
 
 
    Coasting Arc #4 (Orbit 627)
    ---------------------------------------
 
    Vector Time (GMT): 2016/177/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3824867.05                 A    =         6778038.50  meter
     Y    =       -2868789.89  meter          E    =           .0011060
     Z    =       -4814778.64                 I    =           51.73204
     XDOT =       6112.793916                 Wp   =          104.46041
     YDOT =       3831.721163  meter/sec      RA   =           15.72647  deg
     ZDOT =       2575.213779                 TA   =          190.87998
                                              MA   =          190.90393
                                              Ha   =            220.152  n.mi
                                              Hp   =            213.934
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12548776.41                 X    =         3880050.22
     Y    =       -9412040.33  feet           Y    =        -2825708.69  meter
     Z    =      -15796517.85                 Z    =        -4796064.79
     XDOT =      20055.098149                 XDOT =        6056.983166
     YDOT =      12571.263658  feet/sec       YDOT =        3899.766203  meter/sec
     ZDOT =       8448.864105                 ZDOT =        2604.772741
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13329400.75                 X    =        -4062801.35
     Y    =       -8424630.41  feet           Y    =        -2567827.35  meter
     Z    =      -15714354.81                 Z    =        -4789735.35
     XDOT =       3934.327661                 XDOT =        1199.183071
     YDOT =     -22209.329036  feet/sec       YDOT =       -6769.403490  meter/sec
     ZDOT =       8576.877058                 ZDOT =        2614.232127
  
  
    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   16177.56091427  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6400  16.2606 0000736 355.0962   5.0183 15.54670599  6289
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16177.56091427   =   yrday.fracday
    Element set:     903
    Inclination:       51.6400  deg
    RA of node:        16.2606  deg
    Eccentricity:     .0000736     
    Arg of perigee:   355.0962  deg
    Mean anomaly:       5.0183  deg
    Mean motion:   15.54670599  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             628
    Checksum:              299
 
 
    Coasting Arc #5 (Orbit 643)
    ---------------------------------------
 
    Vector Time (GMT): 2016/178/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5333672.07                 A    =         6782049.07  meter
     Y    =        1957298.28  meter          E    =           .0011791
     Z    =        3695247.06                 I    =           51.71479
     XDOT =      -4604.183624                 Wp   =           80.99415
     YDOT =      -4350.134868  meter/sec      RA   =           10.73795  deg
     ZDOT =      -4327.857797                 TA   =           55.00955
                                              MA   =           54.89891
                                              Ha   =            220.199  n.mi
                                              Hp   =            213.883
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17498924.10                 X    =        -5373112.46
     Y    =        6421582.29  feet           Y    =         1897432.79  meter
     Z    =       12123513.98                 Z    =         3669241.94
     XDOT =     -15105.589317                 XDOT =       -4534.174396
     YDOT =     -14272.096024  feet/sec       YDOT =       -4401.230127  meter/sec
     ZDOT =     -14199.008520                 ZDOT =       -4350.053936
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12548472.93                 X    =         3824774.55
     Y    =       13882716.55  feet           Y    =         4231452.01  meter
     Z    =       12009773.66                 Z    =         3660579.01
     XDOT =      -6584.954314                 XDOT =       -2007.094075
     YDOT =      18357.278849  feet/sec       YDOT =        5595.298593  meter/sec
     ZDOT =     -14294.818479                 ZDOT =       -4357.060672
  
  
    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   16178.58938568  .00016717  00000-0  10270-3 0  9046
    2 25544  51.6405  11.1293 0000824 349.8597  10.2539 15.54676338  6441
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16178.58938568   =   yrday.fracday
    Element set:     904
    Inclination:       51.6405  deg
    RA of node:        11.1293  deg
    Eccentricity:     .0000824     
    Arg of perigee:   349.8597  deg
    Mean anomaly:      10.2539  deg
    Mean motion:   15.54676338  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             644
    Checksum:              331
 
 
    Coasting Arc #6 (Orbit 658)
    ---------------------------------------
 
    Vector Time (GMT): 2016/179/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6353077.71                 A    =         6785862.40  meter
     Y    =       -1052216.14  meter          E    =           .0007092
     Z    =       -2132609.35                 I    =           51.69557
     XDOT =       2614.508259                 Wp   =           37.92860
     YDOT =       4641.165848  meter/sec      RA   =            5.75992  deg
     ZDOT =       5513.941213                 TA   =          298.45439
                                              MA   =          298.52583
                                              Ha   =            220.246  n.mi
                                              Hp   =            213.781
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20843430.81                 X    =         6374730.95
     Y    =       -3452152.69  feet           Y    =         -981050.56  meter
     Z    =       -6996749.83                 Z    =        -2101695.25
     XDOT =       8577.783001                 XDOT =        2535.630986
     YDOT =      15226.922074  feet/sec       YDOT =        4669.961576  meter/sec
     ZDOT =      18090.358309                 ZDOT =        5526.450574
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11347142.47                 X    =        -3458609.02
     Y    =      -17873956.09  feet           Y    =        -5447981.81  meter
     Z    =       -6861816.51                 Z    =        -2091481.67
     XDOT =       9403.175494                 XDOT =        2866.087891
     YDOT =     -12915.454450  feet/sec       YDOT =       -3936.630516  meter/sec
     ZDOT =      18143.889215                 ZDOT =        5530.257433
  
  
    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   16179.55357519  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6402   6.3190 0000707  12.4741 347.6430 15.54681302  6594
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16179.55357519   =   yrday.fracday
    Element set:     905
    Inclination:       51.6402  deg
    RA of node:         6.3190  deg
    Eccentricity:     .0000707     
    Arg of perigee:    12.4741  deg
    Mean anomaly:     347.6430  deg
    Mean motion:   15.54681302  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             659
    Checksum:              294
 
 
    Coasting Arc #7 (Orbit 674)
    ---------------------------------------
 
    Vector Time (GMT): 2016/180/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6776093.48                 A    =         6787559.80  meter
     Y    =         115145.02  meter          E    =           .0011948
     Z    =         263692.04                 I    =           51.66964
     XDOT =       -321.509480                 Wp   =          128.47706
     YDOT =      -4755.274369  meter/sec      RA   =             .78930  deg
     ZDOT =      -6008.493450                 TA   =           48.68199
                                              MA   =           48.57922
                                              Ha   =            220.089  n.mi
                                              Hp   =            213.721
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22231277.81                 X    =        -6778158.35
     Y    =         377772.39  feet           Y    =           39358.66  meter
     Z    =         865131.37                 Z    =          230770.45
     XDOT =      -1054.821129                 XDOT =        -239.124225
     YDOT =     -15601.293862  feet/sec       YDOT =       -4758.408568  meter/sec
     ZDOT =     -19712.905020                 ZDOT =       -6009.855549
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9392568.61                 X    =         2862854.91
     Y    =       20158862.64  feet           Y    =         6144421.33  meter
     Z    =         721657.28                 Z    =          219961.14
     XDOT =     -12405.791408                 XDOT =       -3781.285221
     YDOT =       6510.972354  feet/sec       YDOT =        1984.544373  meter/sec
     ZDOT =     -19717.835201                 ZDOT =       -6009.996169
  
  
    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   16180.58203705  .00016717  00000-0  10270-3 0  9069
    2 25544  51.6401   1.1881 0000930   3.0991 357.0168 15.54730342  6754
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16180.58203705   =   yrday.fracday
    Element set:     906
    Inclination:       51.6401  deg
    RA of node:         1.1881  deg
    Eccentricity:     .0000930     
    Arg of perigee:     3.0991  deg
    Mean anomaly:     357.0168  deg
    Mean motion:   15.54730342  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             675
    Checksum:              277
 
 
    Coasting Arc #8 (Orbit 690)
    ---------------------------------------
 
    Vector Time (GMT): 2016/181/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6538428.79                 A    =         6786482.04  meter
     Y    =         795676.55  meter          E    =           .0014430
     Z    =        1604974.05                 I    =           51.63492
     XDOT =      -1986.510055                 Wp   =           61.20718
     YDOT =       4695.429421  meter/sec      RA   =          355.81691  deg
     ZDOT =       5732.726474                 TA   =          316.36702
                                              MA   =          316.48104
                                              Ha   =            220.142  n.mi
                                              Hp   =            213.629
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21451538.04                 X    =         6521249.10
     Y    =        2610487.36  feet           Y    =          868697.40  meter
     Z    =        5265662.91                 Z    =         1636694.54
     XDOT =      -6517.421439                 XDOT =       -2066.715073
     YDOT =      15404.952169  feet/sec       YDOT =        4672.765935  meter/sec
     ZDOT =      18808.157724                 ZDOT =        5722.882123
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6682840.15                 X    =        -2036929.68
     Y    =      -20514628.39  feet           Y    =        -6252858.73  meter
     Z    =        5403702.79                 Z    =         1647048.61
     XDOT =      15272.930341                 XDOT =        4655.189168
     YDOT =         -5.515255  feet/sec       YDOT =          -1.681050  meter/sec
     ZDOT =      18764.271496                 ZDOT =        5719.349952
  
  
    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   16181.61049562  .00016717  00000-0  10270-3 0  9074
    2 25544  51.6413 356.0568 0000696  18.0547 342.0631 15.54713658  6911
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16181.61049562   =   yrday.fracday
    Element set:     907
    Inclination:       51.6413  deg
    RA of node:       356.0568  deg
    Eccentricity:     .0000696     
    Arg of perigee:    18.0547  deg
    Mean anomaly:     342.0631  deg
    Mean motion:   15.54713658  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             691
    Checksum:              309
 
 
    Coasting Arc #9 (Orbit 705)
    ---------------------------------------
 
    Vector Time (GMT): 2016/182/13:11:11.324
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5667364.29                 A    =         6782899.93  meter
     Y    =       -1737491.29  meter          E    =           .0005089
     Z    =       -3301907.11                 I    =           51.59066
     XDOT =       4101.562533                 Wp   =           83.99617
     YDOT =      -4442.614497  meter/sec      RA   =          350.83566  deg
     ZDOT =      -4707.872970                 TA   =          134.39441
                                              MA   =          134.35273
                                              Ha   =            220.199  n.mi
                                              Hp   =            213.533
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18593714.87                 X    =        -5631474.73
     Y    =       -5700430.74  feet           Y    =        -1800666.48  meter
     Z    =      -10833028.58                 Z    =        -3329350.86
     XDOT =      13456.569989                 XDOT =        4173.805010
     YDOT =     -14575.506880  feet/sec       YDOT =       -4396.343616  meter/sec
     ZDOT =     -15445.777461                 ZDOT =       -4687.773589
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2988968.04                 X    =          911037.46
     Y    =       19149161.66  feet           Y    =         5836664.47  meter
     Z    =      -10952229.41                 Z    =        -3338239.53
     XDOT =     -17645.795001                 XDOT =       -5378.438316
     YDOT =      -6018.539430  feet/sec       YDOT =       -1834.450818  meter/sec
     ZDOT =     -15357.265286                 ZDOT =       -4680.894459
  
  
    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   16182.57467022  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6409 351.2468 0000847  23.9139 336.2053 15.54714414  7063
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16182.57467022   =   yrday.fracday
    Element set:     908
    Inclination:       51.6409  deg
    RA of node:       351.2468  deg
    Eccentricity:     .0000847     
    Arg of perigee:    23.9139  deg
    Mean anomaly:     336.2053  deg
    Mean motion:   15.54714414  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             706
    Checksum:              303
 
 
    Coasting Arc #10 (Orbit 716)
    ---------------------------------------
 
    Vector Time (GMT): 2016/183/05:31:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3211773.78                 A    =         6777074.23  meter
     Y    =        3316522.86  meter          E    =           .0005868
     Z    =        4957243.83                 I    =           51.55211
     XDOT =      -6629.052578                 Wp   =          111.77352
     YDOT =       3217.056171  meter/sec      RA   =          347.43474  deg
     ZDOT =       2138.471631                 TA   =          317.35601
                                              MA   =          317.40155
                                              Ha   =            220.126  n.mi
                                              Hp   =            213.617
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10537315.55                 X    =         3150368.68
     Y    =       10880980.51  feet           Y    =         3352095.08  meter
     Z    =       16263923.31                 Z    =         4972697.13
     XDOT =     -21748.860164                 XDOT =       -6674.921615
     YDOT =      10554.646231  feet/sec       YDOT =        3142.668946  meter/sec
     ZDOT =       7015.983040                 ZDOT =        2106.158289
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10732562.47                 X    =         3271285.04
     Y    =       10586373.37  feet           Y    =         3226726.60  meter
     Z    =       16330546.80                 Z    =         4977550.66
     XDOT =     -20717.841811                 XDOT =       -6314.798184
     YDOT =      10378.303625  feet/sec       YDOT =        3163.306945  meter/sec
     ZDOT =       6874.518254                 ZDOT =        2095.353164
  
  
    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   16183.28172888  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6433 347.7240 0001171  14.4948 345.6239 15.54721448  7179
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16183.28172888   =   yrday.fracday
    Element set:     909
    Inclination:       51.6433  deg
    RA of node:       347.7240  deg
    Eccentricity:     .0001171     
    Arg of perigee:    14.4948  deg
    Mean anomaly:     345.6239  deg
    Mean motion:   15.54721448  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             717
    Checksum:              322
 
 
    Coasting Arc #11 (Orbit 716)
    ---------------------------------------
 
    Vector Time (GMT): 2016/183/06:09:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5843170.69                 A    =         6783225.76  meter
     Y    =       -1287091.55  meter          E    =           .0004689
     Z    =       -3200397.36                 I    =           51.57219
     XDOT =       3663.559749                 Wp   =           83.62152
     YDOT =      -4723.961143  meter/sec      RA   =          347.31129  deg
     ZDOT =      -4794.515912                 TA   =          133.39695
                                              MA   =          133.35790
                                              Ha   =            220.169  n.mi
                                              Hp   =            213.637
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19170507.50                 X    =        -5812797.65
     Y    =       -4222741.31  feet           Y    =        -1352263.54  meter
     Z    =      -10499991.34                 Z    =        -3228708.47
     XDOT =      12019.552981                 XDOT =        3739.401717
     YDOT =     -15498.560182  feet/sec       YDOT =       -4682.568105  meter/sec
     ZDOT =     -15730.039081                 ZDOT =       -4776.535615
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19558407.33                 X    =        -5961402.56
     Y    =        -457095.15  feet           Y    =         -139322.60  meter
     Z    =      -10623063.91                 Z    =        -3237909.88
     XDOT =       8867.638938                 XDOT =        2702.856348
     YDOT =     -16121.924586  feet/sec       YDOT =       -4913.962614  meter/sec
     ZDOT =     -15650.700787                 ZDOT =       -4770.333600
  
  
    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   16183.28172880  .00016717  00000-0  10270-3 0  9103
    2 25544  51.6438 347.7246 0001159   5.8217 354.2950 15.54698485  7179
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16183.28172880   =   yrday.fracday
    Element set:     910
    Inclination:       51.6438  deg
    RA of node:       347.7246  deg
    Eccentricity:     .0001159     
    Arg of perigee:     5.8217  deg
    Mean anomaly:     354.2950  deg
    Mean motion:   15.54698485  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             717
    Checksum:              326
 
 
    Coasting Arc #12 (Orbit 732)
    ---------------------------------------
 
    Vector Time (GMT): 2016/184/06:09:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 891816.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4539276.97                 A    =         6779010.76  meter
     Y    =        2288072.40  meter          E    =           .0008812
     Z    =        4478649.99                 I    =           51.52748
     XDOT =      -5398.811569                 Wp   =          103.51829
     YDOT =       4403.144699  meter/sec      RA   =          342.31383  deg
     ZDOT =       3215.054679                 TA   =          314.08716
                                              MA   =          314.15966
                                              Ha   =            220.139  n.mi
                                              Hp   =            213.621
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14892640.97                 X    =         4491598.48
     Y    =        7506799.22  feet           Y    =         2338566.40  meter
     Z    =       14693733.57                 Z    =         4500585.15
     XDOT =     -17712.636382                 XDOT =       -5463.264714
     YDOT =      14446.012792  feet/sec       YDOT =        4342.410757  meter/sec
     ZDOT =      10548.079654                 ZDOT =        3188.672713
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16043728.08                 X    =         4890128.32
     Y    =        4235371.14  feet           Y    =         1290941.12  meter
     Z    =       14788813.90                 Z    =         4507630.48
     XDOT =     -14043.448109                 XDOT =       -4280.442984
     YDOT =      16686.931635  feet/sec       YDOT =        5086.176762  meter/sec
     ZDOT =      10432.207110                 ZDOT =        3179.736727
  
  
    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   16184.31017392  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6443 342.5930 0001276  14.2556 345.8633 15.54707937  7333
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16184.31017392   =   yrday.fracday
    Element set:     911
    Inclination:       51.6443  deg
    RA of node:       342.5930  deg
    Eccentricity:     .0001276     
    Arg of perigee:    14.2556  deg
    Mean anomaly:     345.8633  deg
    Mean motion:   15.54707937  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             733
    Checksum:              302
 
 
    Coasting Arc #13 (Orbit 746)
    ---------------------------------------
 
    Vector Time (GMT): 2016/185/03:48:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 877382.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3463122.20                 A    =         6776627.94  meter
     Y    =        2916563.44  meter          E    =           .0005192
     Z    =        5038463.35                 I    =           51.49111
     XDOT =      -6192.636600                 Wp   =          110.98677
     YDOT =       4128.903118  meter/sec      RA   =          337.79504  deg
     ZDOT =       1862.997631                 TA   =          320.91707
                                              MA   =          320.95456
                                              Ha   =            220.083  n.mi
                                              Hp   =            213.552
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11361949.49                 X    =         3405776.53
     Y    =        9568777.68  feet           Y    =         2954968.99  meter
     Z    =       16530391.58                 Z    =         5055147.39
     XDOT =     -20317.049211                 XDOT =       -6247.396371
     YDOT =      13546.270072  feet/sec       YDOT =        4059.346475  meter/sec
     ZDOT =       6112.196951                 ZDOT =        1832.783118
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6822808.20                 X    =         2079591.94
     Y    =       13104075.48  feet           Y    =         3994122.21  meter
     Z    =       16602461.94                 Z    =         5060430.40
     XDOT =     -23003.322727                 XDOT =       -7011.412767
     YDOT =       4386.932640  feet/sec       YDOT =        1337.137069  meter/sec
     ZDOT =       5979.687329                 ZDOT =        1822.608698
  
  
    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   16185.21005718  .00016717  00000-0  10270-3 0  9125
    2 25544  51.6430 338.1025 0001251  15.4861 344.6330 15.54752969  7471
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16185.21005718   =   yrday.fracday
    Element set:     912
    Inclination:       51.6430  deg
    RA of node:       338.1025  deg
    Eccentricity:     .0001251     
    Arg of perigee:    15.4861  deg
    Mean anomaly:     344.6330  deg
    Mean motion:   15.54752969  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             747
    Checksum:              290
 
 
    Coasting Arc #14 (Orbit 761)
    ---------------------------------------
 
    Vector Time (GMT): 2016/186/03:48:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 877382.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1651200.83                 A    =         6775603.66  meter
     Y    =       -3900282.31  meter          E    =           .0015343
     Z    =       -5301930.94                 I    =           51.45854
     XDOT =       6904.545440                 Wp   =           87.16071
     YDOT =      -3301.276071  meter/sec      RA   =          332.77795  deg
     ZDOT =        279.668158                 TA   =          185.50691
                                              MA   =          185.52381
                                              Ha   =            220.272  n.mi
                                              Hp   =            213.427
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5417325.55                 X    =        -1581709.94
     Y    =      -12796201.81  feet           Y    =        -3918357.82  meter
     Z    =      -17394786.56                 Z    =        -5309783.77
     XDOT =      22652.708136                 XDOT =        6939.589487
     YDOT =     -10830.958238  feet/sec       YDOT =       -3223.868941  meter/sec
     ZDOT =        917.546451                 ZDOT =         313.293007
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -333631.89                 X    =         -101691.00
     Y    =      -13849769.68  feet           Y    =        -4221409.80  meter
     Z    =      -17428177.36                 Z    =        -5312108.46
     XDOT =      24018.281038                 XDOT =        7320.772060
     YDOT =      -1912.463619  feet/sec       YDOT =        -582.918911  meter/sec
     ZDOT =       1064.736002                 ZDOT =         324.531534
  
  
    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   16186.17421620  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6435 333.2921 0001396  21.6890 338.4322 15.54742676  7621
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16186.17421620   =   yrday.fracday
    Element set:     913
    Inclination:       51.6435  deg
    RA of node:       333.2921  deg
    Eccentricity:     .0001396     
    Arg of perigee:    21.6890  deg
    Mean anomaly:     338.4322  deg
    Mean motion:   15.54742676  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             762
    Checksum:              301
 
 
    Coasting Arc #15 (Orbit 777)
    ---------------------------------------
 
    Vector Time (GMT): 2016/187/03:48:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 877382.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -222655.10                 A    =         6777464.38  meter
     Y    =        4718127.29  meter          E    =           .0008095
     Z    =        4856694.26                 I    =           51.43672
     XDOT =      -6968.301154                 Wp   =           52.66947
     YDOT =       2140.687864  meter/sec      RA   =          327.76090  deg
     ZDOT =      -2391.509472                 TA   =           60.86548
                                              MA   =           60.78448
                                              Ha   =            220.218  n.mi
                                              Hp   =            213.496
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -730495.75                 X    =         -298989.23
     Y    =       15479420.25  feet           Y    =         4715209.94  meter
     Z    =       15934036.29                 Z    =         4855427.91
     XDOT =     -22861.880428                 XDOT =       -6980.104213
     YDOT =       7023.254148  feet/sec       YDOT =        2062.698008  meter/sec
     ZDOT =      -7846.159684                 ZDOT =       -2425.387633
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6115016.60                 X    =        -1863857.06
     Y    =       14246399.44  feet           Y    =         4342302.55  meter
     Z    =       15927531.59                 Z    =         4854711.63
     XDOT =     -22794.864475                 XDOT =       -6947.874692
     YDOT =       -818.985898  feet/sec       YDOT =        -249.626902  meter/sec
     ZDOT =      -7994.205370                 ZDOT =       -2436.633797
  
  
    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   16187.20264652  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6435 328.1617 0001390  18.2593 341.8610 15.54764797  7785
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16187.20264652   =   yrday.fracday
    Element set:     914
    Inclination:       51.6435  deg
    RA of node:       328.1617  deg
    Eccentricity:     .0001390     
    Arg of perigee:    18.2593  deg
    Mean anomaly:     341.8610  deg
    Mean motion:   15.54764797  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             778
    Checksum:              321
 
 
    Coasting Arc #16 (Orbit 777)
    ---------------------------------------
 
    Vector Time (GMT): 2016/187/04:14:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 877382.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6046601.57                 A    =         6783998.98  meter
     Y    =        1117090.21  meter          E    =           .0004559
     Z    =       -2868838.34                 I    =           51.45885
     XDOT =       1353.602012                 Wp   =           98.99483
     YDOT =      -5608.557031  meter/sec      RA   =          327.71444  deg
     ZDOT =      -5044.434006                 TA   =          113.72700
                                              MA   =          113.67916
                                              Ha   =            220.204  n.mi
                                              Hp   =            213.513
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19837931.65                 X    =        -6044708.38
     Y    =        3664994.14  feet           Y    =         1049484.06  meter
     Z    =       -9412199.27                 Z    =        -2898206.05
     XDOT =       4440.951483                 XDOT =        1440.721037
     YDOT =     -18400.777660  feet/sec       YDOT =       -5592.932354  meter/sec
     ZDOT =     -16549.980336                 ZDOT =       -5037.647804
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20080777.23                 X    =        -6120620.90
     Y    =       -1144004.23  feet           Y    =         -348692.49  meter
     Z    =       -9540379.95                 Z    =        -2907907.81
     XDOT =       8709.932429                 XDOT =        2654.787404
     YDOT =     -15328.664779  feet/sec       YDOT =       -4672.177025  meter/sec
     ZDOT =     -16519.240832                 ZDOT =       -5035.064606
  
  
    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   16187.20264675  .00016717  00000-0  10270-3 0  9158
    2 25544  51.6444 328.1617 0001246  15.8757 344.2435 15.54727783  7786
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16187.20264675   =   yrday.fracday
    Element set:     915
    Inclination:       51.6444  deg
    RA of node:       328.1617  deg
    Eccentricity:     .0001246     
    Arg of perigee:    15.8757  deg
    Mean anomaly:     344.2435  deg
    Mean motion:   15.54727783  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             778
    Checksum:              328
 
 
    Coasting Arc #17 (Orbit 793)
    ---------------------------------------
 
    Vector Time (GMT): 2016/188/04:14:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 877382.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5267762.58                 A    =         6779740.07  meter
     Y    =         253048.13  meter          E    =           .0010130
     Z    =        4252754.07                 I    =           51.41855
     XDOT =      -3178.627860                 Wp   =           98.65274
     YDOT =       6001.537552  meter/sec      RA   =          322.71165  deg
     ZDOT =       3571.383685                 TA   =          314.76468
                                              MA   =          314.84705
                                              Ha   =            220.178  n.mi
                                              Hp   =            213.457
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17282685.64                 X    =         5243883.73
     Y    =         830210.41  feet           Y    =          311821.75  meter
     Z    =       13952605.23                 Z    =         4278285.15
     XDOT =     -10428.569096                 XDOT =       -3262.850271
     YDOT =      19690.083832  feet/sec       YDOT =        5965.520676  meter/sec
     ZDOT =      11717.138075                 ZDOT =        3555.739116
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16583117.18                 X    =         5054534.12
     Y    =        4611494.04  feet           Y    =         1405583.38  meter
     Z    =       14063783.71                 Z    =         4286641.28
     XDOT =     -14260.777818                 XDOT =       -4346.685079
     YDOT =      15672.745513  feet/sec       YDOT =        4777.052832  meter/sec
     ZDOT =      11647.733898                 ZDOT =        3550.229292
  
  
    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   16188.23107130  .00016717  00000-0  10270-3 0  9165
    2 25544  51.6449 323.0301 0001456  24.3756 335.7466 15.54741369  7945
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16188.23107130   =   yrday.fracday
    Element set:     916
    Inclination:       51.6449  deg
    RA of node:       323.0301  deg
    Eccentricity:     .0001456     
    Arg of perigee:    24.3756  deg
    Mean anomaly:     335.7466  deg
    Mean motion:   15.54741369  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             794
    Checksum:              304
 
 
    Coasting Arc #18 (Orbit 807)
    ---------------------------------------
 
    Vector Time (GMT): 2016/189/01:37:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 877382.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5222998.24                 A    =         6787474.17  meter
     Y    =       -4310984.22  meter          E    =           .0014177
     Z    =         330872.85                 I    =           51.41938
     XDOT =       2817.689919                 Wp   =           46.28096
     YDOT =       3884.719337  meter/sec      RA   =          318.23060  deg
     ZDOT =       5984.822656                 TA   =          317.29797
                                              MA   =          317.40806
                                              Ha   =            220.326  n.mi
                                              Hp   =            213.407
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17135821.01                 X    =         5269209.36
     Y    =      -14143649.03  feet           Y    =        -4252318.83  meter
     Z    =        1085540.86                 Z    =          356356.24
     XDOT =       9244.389499                 XDOT =        2744.969418
     YDOT =      12745.142182  feet/sec       YDOT =        3915.821418  meter/sec
     ZDOT =      19635.244933                 ZDOT =        5998.333814
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21759790.30                 X    =         6632384.08
     Y    =        4464886.18  feet           Y    =         1360897.31  meter
     Z    =        1197449.69                 Z    =          364982.67
     XDOT =      -3880.623913                 XDOT =       -1182.814169
     YDOT =      13510.324914  feet/sec       YDOT =        4117.947034  meter/sec
     ZDOT =      19693.308506                 ZDOT =        6002.520433
  
  
    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   16189.13093784  .00016717  00000-0  10270-3 0  9175
    2 25544  51.6423 318.5400 0001526  26.5089 333.6142 15.54748627  8085
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16189.13093784   =   yrday.fracday
    Element set:     917
    Inclination:       51.6423  deg
    RA of node:       318.5400  deg
    Eccentricity:     .0001526     
    Arg of perigee:    26.5089  deg
    Mean anomaly:     333.6142  deg
    Mean motion:   15.54748627  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             808
    Checksum:              314
 
             

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