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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15282.5994
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   91.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.315
   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 
   ------------------------------------------------------------------------
   239/10:10:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.6  
   000/00:00:00.000           0.0               0.0              215.6  
   
   246/19:55:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.6  
   000/00:00:00.000           0.0               0.0              215.4  
   
   250/21:05:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.9  
   000/00:00:00.000           0.0               0.0              215.1  
   
   250/21:52:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.7  
   000/00:00:00.000           0.0               0.0              215.2  
   
 
 
    Coasting Arc #1 (Orbit 1561)
    ---------------------------------------
 
    Vector Time (GMT): 2016/237/12:45:53.942
    Vector Time (MET): N/A
    Weight (LBS)     : 929160.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -769899.78                 A    =         6785368.39  meter
     Y    =        6117341.29  meter          E    =           .0010259
     Z    =        2823074.31                 I    =           52.00926
     XDOT =      -4857.194880                 Wp   =           84.90770
     YDOT =      -2985.452329  meter/sec      RA   =           76.21964  deg
     ZDOT =       5129.473259                 TA   =          306.97883
                                              MA   =          307.07270
                                              Ha   =            219.723  n.mi
                                              Hp   =            215.441
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2525917.90                 X    =         -851961.45
     Y    =       20070017.34  feet           Y    =         6108273.04  meter
     Z    =        9262054.82                 Z    =         2819134.75
     XDOT =     -15935.678740                 XDOT =       -4848.366483
     YDOT =      -9794.791105  feet/sec       YDOT =       -3039.719141  meter/sec
     ZDOT =      16828.980507                 ZDOT =        5105.899882
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8066866.05                 X    =         2458780.77
     Y    =      -18559382.85  feet           Y    =        -5656899.89  meter
     Z    =        9243727.46                 Z    =         2817488.13
     XDOT =      11333.310884                 XDOT =        3454.393157
     YDOT =      13281.567314  feet/sec       YDOT =        4048.221717  meter/sec
     ZDOT =      16726.468990                 ZDOT =        5098.227748
  
  
    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   16237.59045550  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6394  76.6927 0003283 245.1282 114.9529 15.54333632 15627
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16237.59045550   =   yrday.fracday
    Element set:     900
    Inclination:       51.6394  deg
    RA of node:        76.6927  deg
    Eccentricity:     .0003283     
    Arg of perigee:   245.1282  deg
    Mean anomaly:     114.9529  deg
    Mean motion:   15.54333632  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1562
    Checksum:              310
 
 
    Coasting Arc #2 (Orbit 1576)
    ---------------------------------------
 
    Vector Time (GMT): 2016/238/12:45:53.942
    Vector Time (MET): N/A
    Weight (LBS)     : 929160.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1717400.95                 A    =         6781441.82  meter
     Y    =       -5072165.81  meter          E    =           .0004626
     Z    =       -4165513.13                 I    =           51.98730
     XDOT =       4719.657512                 Wp   =           71.61083
     YDOT =       4704.308941  meter/sec      RA   =           71.25957  deg
     ZDOT =      -3784.379628                 TA   =          159.58515
                                              MA   =          159.56665
                                              Ha   =            219.741  n.mi
                                              Hp   =            215.450
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5634517.54                 X    =         1794225.71
     Y    =      -16640963.95  feet           Y    =        -5052531.26  meter
     Z    =      -13666381.66                 Z    =        -4156983.72
     XDOT =      15484.440656                 XDOT =        4685.084753
     YDOT =      15434.084452  feet/sec       YDOT =        4756.893888  meter/sec
     ZDOT =     -12415.943663                 ZDOT =       -3761.536948
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9877222.49                 X    =        -3010577.42
     Y    =       14565472.54  feet           Y    =         4439556.03  meter
     Z    =      -13628167.24                 Z    =        -4153865.37
     XDOT =      -9922.805864                 XDOT =       -3024.471227
     YDOT =     -18247.043675  feet/sec       YDOT =       -5561.698912  meter/sec
     ZDOT =     -12316.945010                 ZDOT =       -3754.204839
  
  
    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   16238.55487386  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6392  71.8837 0003054 248.8520 111.2307 15.54326230 15779
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16238.55487386   =   yrday.fracday
    Element set:     901
    Inclination:       51.6392  deg
    RA of node:        71.8837  deg
    Eccentricity:     .0003054     
    Arg of perigee:   248.8520  deg
    Mean anomaly:     111.2307  deg
    Mean motion:   15.54326230  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1577
    Checksum:              307
 
 
    Coasting Arc #3 (Orbit 1590)
    ---------------------------------------
 
    Vector Time (GMT): 2016/239/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2378347.01                 A    =         6788779.15  meter
     Y    =       -6339796.24  meter          E    =           .0010157
     Z    =        -396250.67                 I    =           52.00553
     XDOT =       4550.371934                 Wp   =          154.11653
     YDOT =      -1334.499105  meter/sec      RA   =           66.81665  deg
     ZDOT =      -6027.530892                 TA   =           30.13472
                                              MA   =           30.07632
                                              Ha   =            219.639  n.mi
                                              Hp   =            215.571
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7802975.75                 X    =        -2305352.24
     Y    =      -20799856.43  feet           Y    =        -6365984.38  meter
     Z    =       -1300035.02                 Z    =         -407626.55
     XDOT =      14929.041779                 XDOT =        4594.235362
     YDOT =      -4378.277902  feet/sec       YDOT =       -1283.368686  meter/sec
     ZDOT =     -19775.363820                 ZDOT =       -6005.319934
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12006208.66                 X    =        -3659492.40
     Y    =       18688038.66  feet           Y    =         5696114.18  meter
     Z    =       -1348596.93                 Z    =         -411052.34
     XDOT =     -11153.627385                 XDOT =       -3399.625627
     YDOT =      -8570.467428  feet/sec       YDOT =       -2612.278472  meter/sec
     ZDOT =     -19678.018449                 ZDOT =       -5997.860023
  
  
    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   16239.45499254  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6432  67.3988 0003247 255.4663 104.6130 15.54293111 15914
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16239.45499254   =   yrday.fracday
    Element set:     902
    Inclination:       51.6432  deg
    RA of node:        67.3988  deg
    Eccentricity:     .0003247     
    Arg of perigee:   255.4663  deg
    Mean anomaly:     104.6130  deg
    Mean motion:   15.54293111  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1591
    Checksum:              310
 
 
    Coasting Arc #4 (Orbit 1606)
    ---------------------------------------
 
    Vector Time (GMT): 2016/240/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1474212.07                 A    =         6786762.03  meter
     Y    =        6270803.78  meter          E    =           .0010744
     Z    =        2119372.96                 I    =           51.98449
     XDOT =      -5259.543331                 Wp   =           66.61523
     YDOT =       -643.695781  meter/sec      RA   =           61.86706  deg
     ZDOT =       5544.997959                 TA   =          316.75582
                                              MA   =          316.84012
                                              Ha   =            219.497  n.mi
                                              Hp   =            215.484
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4836653.78                 X    =         1393685.91
     Y    =       20573503.23  feet           Y    =         6286839.21  meter
     Z    =        6953323.36                 Z    =         2126338.49
     XDOT =     -17255.719589                 XDOT =       -5278.889356
     YDOT =      -2111.862800  feet/sec       YDOT =        -702.619547  meter/sec
     ZDOT =      18192.250522                 ZDOT =        5519.401744
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13341643.04                 X    =         4066532.80
     Y    =      -16378482.90  feet           Y    =        -4992161.59  meter
     Z    =        6982608.37                 Z    =         2128299.03
     XDOT =       7766.396090                 XDOT =        2367.197528
     YDOT =      14059.732023  feet/sec       YDOT =        4285.406321  meter/sec
     ZDOT =      18080.469732                 ZDOT =        5510.927174
  
  
    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   16240.48369323  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6419  62.2683 0003240 261.0262  99.0524 15.54351666 16078
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16240.48369323   =   yrday.fracday
    Element set:     903
    Inclination:       51.6419  deg
    RA of node:        62.2683  deg
    Eccentricity:     .0003240     
    Arg of perigee:   261.0262  deg
    Mean anomaly:      99.0524  deg
    Mean motion:   15.54351666  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1607
    Checksum:              293
 
 
    Coasting Arc #5 (Orbit 1621)
    ---------------------------------------
 
    Vector Time (GMT): 2016/241/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -342515.97                 A    =         6783159.71  meter
     Y    =       -5723620.72  meter          E    =           .0002225
     Z    =       -3626460.91                 I    =           51.95493
     XDOT =       5746.215178                 Wp   =           76.03653
     YDOT =       2463.797424  meter/sec      RA   =           56.90978  deg
     ZDOT =      -4433.072406                 TA   =          146.70895
                                              MA   =          146.69495
                                              Ha   =            219.506  n.mi
                                              Hp   =            215.539
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1123740.06                 X    =         -260872.02
     Y    =      -18778283.21  feet           Y    =        -5726994.59  meter
     Z    =      -11897837.63                 Z    =        -3627926.24
     XDOT =      18852.412002                 XDOT =        5739.770933
     YDOT =       8083.324881  feet/sec       YDOT =        2528.019261  meter/sec
     ZDOT =     -14544.200808                 ZDOT =       -4405.174892
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13999345.76                 X    =        -4267000.59
     Y    =       12560973.67  feet           Y    =         3828584.78  meter
     Z    =      -11903172.32                 Z    =        -3628086.92
     XDOT =      -4625.859498                 XDOT =       -1409.961975
     YDOT =     -18817.531640  feet/sec       YDOT =       -5735.583644  meter/sec
     ZDOT =     -14422.699566                 ZDOT =       -4396.038828
  
  
    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   16241.44809921  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6405  57.4598 0003236 265.0647  95.0137 15.54331070 16220
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16241.44809921   =   yrday.fracday
    Element set:     904
    Inclination:       51.6405  deg
    RA of node:        57.4598  deg
    Eccentricity:     .0003236     
    Arg of perigee:   265.0647  deg
    Mean anomaly:      95.0137  deg
    Mean motion:   15.54331070  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1622
    Checksum:              296
 
 
    Coasting Arc #6 (Orbit 1637)
    ---------------------------------------
 
    Vector Time (GMT): 2016/242/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -941113.27                 A    =         6779418.24  meter
     Y    =        4782978.09  meter          E    =           .0005253
     Z    =        4709746.07                 I    =           51.92416
     XDOT =      -5922.996006                 Wp   =          132.35157
     YDOT =      -3962.160959  meter/sec      RA   =           51.93882  deg
     ZDOT =       2834.760433                 TA   =          289.61481
                                              MA   =          289.67150
                                              Ha   =            219.583  n.mi
                                              Hp   =            215.561
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3087641.96                 X    =        -1017405.32
     Y    =       15692185.33  feet           Y    =         4772027.59  meter
     Z    =       15451922.82                 Z    =         4704988.92
     XDOT =     -19432.401593                 XDOT =       -5892.019719
     YDOT =     -12999.215746  feet/sec       YDOT =       -4028.222524  meter/sec
     ZDOT =       9300.395120                 ZDOT =        2806.063932
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14111311.53                 X    =         4301127.75
     Y    =       -7570940.49  feet           Y    =        -2307622.66  meter
     Z    =       15430226.15                 Z    =         4703132.93
     XDOT =       1896.041717                 XDOT =         577.913515
     YDOT =      22271.387804  feet/sec       YDOT =        6788.319003  meter/sec
     ZDOT =       9175.685326                 ZDOT =        2796.748887
  
  
    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   16242.47679482  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6409  52.3292 0003209 270.3205  89.7580 15.54308455 16388
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16242.47679482   =   yrday.fracday
    Element set:     905
    Inclination:       51.6409  deg
    RA of node:        52.3292  deg
    Eccentricity:     .0003209     
    Arg of perigee:   270.3205  deg
    Mean anomaly:      89.7580  deg
    Mean motion:   15.54308455  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1638
    Checksum:              316
 
 
    Coasting Arc #7 (Orbit 1652)
    ---------------------------------------
 
    Vector Time (GMT): 2016/243/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2327530.99                 A    =         6776956.30  meter
     Y    =       -3572062.75  meter          E    =           .0011421
     Z    =       -5277789.27                 I    =           51.89434
     XDOT =       5689.342799                 Wp   =           80.41923
     YDOT =       5048.768390  meter/sec      RA   =           46.95703  deg
     ZDOT =       -907.850618                 TA   =          180.91745
                                              MA   =          180.91954
                                              Ha   =            219.507  n.mi
                                              Hp   =            215.532
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7636256.54                 X    =         2392938.50
     Y    =      -11719365.98  feet           Y    =        -3545669.39  meter
     Z    =      -17315581.61                 Z    =        -5266323.80
     XDOT =      18665.822832                 XDOT =        5636.873219
     YDOT =      16564.200754  feet/sec       YDOT =        5112.096993  meter/sec
     ZDOT =      -2978.512525                 ZDOT =        -880.341489
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13939124.08                 X    =        -4248645.02
     Y    =        1764472.28  feet           Y    =          537811.15  meter
     Z    =      -17264784.29                 Z    =        -5262306.25
     XDOT =        510.378394                 XDOT =         155.563334
     YDOT =     -23950.250361  feet/sec       YDOT =       -7300.036310  meter/sec
     ZDOT =      -2859.203869                 ZDOT =        -871.485339
  
  
    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   16243.44118971  .00016717  00000-0  10270-3 0  9064
    2 25544  51.6396  47.5191 0003115 272.6745  87.4051 15.54351949 16538
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16243.44118971   =   yrday.fracday
    Element set:     906
    Inclination:       51.6396  deg
    RA of node:        47.5191  deg
    Eccentricity:     .0003115     
    Arg of perigee:   272.6745  deg
    Mean anomaly:      87.4051  deg
    Mean motion:   15.54351949  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1653
    Checksum:              316
 
 
    Coasting Arc #8 (Orbit 1668)
    ---------------------------------------
 
    Vector Time (GMT): 2016/244/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3685666.84                 A    =         6777212.28  meter
     Y    =        2215112.72  meter          E    =           .0002465
     Z    =        5238614.59                 I    =           51.87208
     XDOT =      -5015.238442                 Wp   =            2.20731
     YDOT =      -5692.605768  meter/sec      RA   =           41.97175  deg
     ZDOT =      -1119.009738                 TA   =           98.49668
                                              MA   =           98.46874
                                              Ha   =            219.664  n.mi
                                              Hp   =            215.512
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12092082.81                 X    =        -3735609.39
     Y    =        7267430.17  feet           Y    =         2173618.33  meter
     Z    =       17187055.73                 Z    =         5220589.34
     XDOT =     -16454.194362                 XDOT =       -4945.773960
     YDOT =     -18676.528110  feet/sec       YDOT =       -5748.301221  meter/sec
     ZDOT =      -3671.291790                 ZDOT =       -1143.202892
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13542586.38                 X    =         4127780.33
     Y    =        4283582.72  feet           Y    =         1305636.01  meter
     Z    =       17107839.31                 Z    =         5214469.42
     XDOT =      -2717.076504                 XDOT =        -828.164918
     YDOT =      23702.458992  feet/sec       YDOT =        7224.509501  meter/sec
     ZDOT =      -3775.975379                 ZDOT =       -1150.917296
  
  
    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   16244.46987552  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6395  42.3895 0003168 275.3568  84.7224 15.54326081 16690
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16244.46987552   =   yrday.fracday
    Element set:     907
    Inclination:       51.6395  deg
    RA of node:        42.3895  deg
    Eccentricity:     .0003168     
    Arg of perigee:   275.3568  deg
    Mean anomaly:      84.7224  deg
    Mean motion:   15.54326081  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1669
    Checksum:              341
 
 
    Coasting Arc #9 (Orbit 1683)
    ---------------------------------------
 
    Vector Time (GMT): 2016/245/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4894913.27                 A    =         6779727.40  meter
     Y    =        -854801.14  meter          E    =           .0007085
     Z    =       -4619389.26                 I    =           51.85621
     XDOT =       3873.258753                 Wp   =          115.14609
     YDOT =       5882.999631  meter/sec      RA   =           36.98753  deg
     ZDOT =       3016.331722                 TA   =          184.88660
                                              MA   =          184.89352
                                              Ha   =            219.529  n.mi
                                              Hp   =            215.553
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16059426.75                 X    =         4926546.77
     Y    =       -2804465.68  feet           Y    =         -799886.55  meter
     Z    =      -15155476.58                 Z    =        -4595534.41
     XDOT =      12707.541842                 XDOT =        3792.533856
     YDOT =      19301.179891  feet/sec       YDOT =        5925.861957  meter/sec
     ZDOT =       9896.101450                 ZDOT =        3034.950099
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13010811.94                 X    =        -3965695.48
     Y    =       -9982168.33  feet           Y    =        -3042564.91  meter
     Z    =      -15051038.95                 Z    =        -4587556.67
     XDOT =       4901.961787                 XDOT =        1494.117953
     YDOT =     -21428.156288  feet/sec       YDOT =       -6531.302037  meter/sec
     ZDOT =       9976.371315                 ZDOT =        3040.797977
  
  
    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   16245.43426353  .00016717  00000-0  10270-3 0  9083
    2 25544  51.6395  37.5792 0003109 277.6832  82.3967 15.54364460 16844
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16245.43426353   =   yrday.fracday
    Element set:     908
    Inclination:       51.6395  deg
    RA of node:        37.5792  deg
    Eccentricity:     .0003109     
    Arg of perigee:   277.6832  deg
    Mean anomaly:      82.3967  deg
    Mean motion:   15.54364460  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1684
    Checksum:              331
 
 
    Coasting Arc #10 (Orbit 1699)
    ---------------------------------------
 
    Vector Time (GMT): 2016/246/10:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5814947.32                 A    =         6783649.22  meter
     Y    =        -429463.61  meter          E    =           .0009243
     Z    =        3459853.97                 I    =           51.84371
     XDOT =      -2314.349246                 Wp   =           84.88525
     YDOT =      -5695.626852  meter/sec      RA   =           32.01242  deg
     ZDOT =      -4585.367521                 TA   =           54.65094
                                              MA   =           54.56459
                                              Ha   =            219.569  n.mi
                                              Hp   =            215.481
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19077911.15                 X    =        -5826519.07
     Y    =       -1409001.33  feet           Y    =         -494554.54  meter
     Z    =       11351226.93                 Z    =         3431578.66
     XDOT =      -7593.009337                 XDOT =       -2228.213793
     YDOT =     -18686.439803  feet/sec       YDOT =       -5721.026371  meter/sec
     ZDOT =     -15043.856695                 ZDOT =       -4596.400061
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12197017.81                 X    =         3717651.03
     Y    =       14831500.86  feet           Y    =         4520641.46  meter
     Z    =       11227718.83                 Z    =         3422208.70
     XDOT =      -7270.457882                 XDOT =       -2216.035562
     YDOT =      17431.621501  feet/sec       YDOT =        5313.158234  meter/sec
     ZDOT =     -15090.996021                 ZDOT =       -4599.735587
  
  
    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   16246.46293813  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6402  32.4493 0003263 282.7938  77.2850 15.54373554 17007
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16246.46293813   =   yrday.fracday
    Element set:     909
    Inclination:       51.6402  deg
    RA of node:        32.4493  deg
    Eccentricity:     .0003263     
    Arg of perigee:   282.7938  deg
    Mean anomaly:      77.2850  deg
    Mean motion:   15.54373554  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1700
    Checksum:              312
 
 
    Coasting Arc #11 (Orbit 1705)
    ---------------------------------------
 
    Vector Time (GMT): 2016/246/19:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         425244.16                 A    =         6777498.81  meter
     Y    =       -4416962.88  meter          E    =           .0011001
     Z    =       -5132734.19                 I    =           51.81595
     XDOT =       7026.364300                 Wp   =           70.16741
     YDOT =       2577.053386  meter/sec      RA   =           30.03341  deg
     ZDOT =      -1634.754630                 TA   =          184.07507
                                              MA   =          184.08403
                                              Ha   =            219.605  n.mi
                                              Hp   =            215.369
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1395158.01                 X    =          499536.54
     Y    =      -14491348.04  feet           Y    =        -4411792.73  meter
     Z    =      -16839679.12                 Z    =        -5130487.52
     XDOT =      23052.376312                 XDOT =        7004.965682
     YDOT =       8454.899559  feet/sec       YDOT =        2655.507058  meter/sec
     ZDOT =      -5363.368210                 ZDOT =       -1600.674914
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14528443.18                 X    =         4428269.48
     Y    =       -1108562.33  feet           Y    =         -337889.80  meter
     Z    =      -16829018.24                 Z    =        -5129484.76
     XDOT =      -4276.067876                 XDOT =       -1303.345489
     YDOT =      23165.926343  feet/sec       YDOT =        7060.974349  meter/sec
     ZDOT =      -5214.902977                 ZDOT =       -1589.502428
  
  
    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   16246.84869088  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6440  30.5288 0003011 286.0928  73.9893 15.54366304 17068
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16246.84869088   =   yrday.fracday
    Element set:     910
    Inclination:       51.6440  deg
    RA of node:        30.5288  deg
    Eccentricity:     .0003011     
    Arg of perigee:   286.0928  deg
    Mean anomaly:      73.9893  deg
    Mean motion:   15.54366304  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1706
    Checksum:              320
 
 
    Coasting Arc #12 (Orbit 1721)
    ---------------------------------------
 
    Vector Time (GMT): 2016/247/19:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2168082.10                 A    =         6776666.07  meter
     Y    =        3604793.06  meter          E    =           .0001948
     Z    =        5313259.16                 I    =           51.78317
     XDOT =      -6804.224267                 Wp   =          355.23449
     YDOT =      -3516.775532  meter/sec      RA   =           25.04260  deg
     ZDOT =       -388.623310                 TA   =           98.47450
                                              MA   =           98.45242
                                              Ha   =            219.769  n.mi
                                              Hp   =            215.245
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7113130.24                 X    =        -2234040.05
     Y    =       11826748.89  feet           Y    =         3580179.96  meter
     Z    =       17431952.64                 Z    =         5302566.59
     XDOT =     -22323.570429                 XDOT =       -6762.505332
     YDOT =     -11537.977466  feet/sec       YDOT =       -3592.631708  meter/sec
     ZDOT =      -1275.010861                 ZDOT =        -421.574581
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13012671.42                 X    =        -3966262.25
     Y    =       -4773887.41  feet           Y    =        -1455080.88  meter
     Z    =       17384532.36                 Z    =         5298805.46
     XDOT =       6604.818890                 XDOT =        2013.148798
     YDOT =     -23191.054021  feet/sec       YDOT =       -7068.633266  meter/sec
     ZDOT =      -1418.351067                 ZDOT =        -432.313405
  
  
    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   16247.87735989  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6423  25.3995 0002884 292.1040  67.9806 15.54383644 17227
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16247.87735989   =   yrday.fracday
    Element set:     911
    Inclination:       51.6423  deg
    RA of node:        25.3995  deg
    Eccentricity:     .0002884     
    Arg of perigee:   292.1040  deg
    Mean anomaly:      67.9806  deg
    Mean motion:   15.54383644  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1722
    Checksum:              336
 
 
    Coasting Arc #13 (Orbit 1736)
    ---------------------------------------
 
    Vector Time (GMT): 2016/248/19:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3828568.42                 A    =         6778563.71  meter
     Y    =       -2713097.62  meter          E    =           .0008784
     Z    =       -4899979.17                 I    =           51.76081
     XDOT =       5978.561512                 Wp   =          103.87740
     YDOT =       4166.696535  meter/sec      RA   =           20.05171  deg
     ZDOT =       2365.731286                 TA   =          189.26367
                                              MA   =          189.27988
                                              Ha   =            219.715  n.mi
                                              Hp   =            215.432
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12560920.00                 X    =         3882424.35
     Y    =       -8901238.91  feet           Y    =        -2669983.45  meter
     Z    =      -16076047.16                 Z    =        -4881249.87
     XDOT =      19614.703125                 XDOT =        5920.032439
     YDOT =      13670.264222  feet/sec       YDOT =        4233.225837  meter/sec
     ZDOT =       7761.585583                 ZDOT =        2394.630917
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11388839.59                 X    =         3471318.31
     Y    =       10485450.13  feet           Y    =         3195965.20  meter
     Z    =      -15993677.69                 Z    =        -4874872.96
     XDOT =      -8440.374891                 XDOT =       -2572.626267
     YDOT =      21190.346085  feet/sec       YDOT =        6458.817487  meter/sec
     ZDOT =       7887.080797                 ZDOT =        2403.982227
  
  
    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   16248.84173150  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6434  20.5912 0003140 295.7000  64.3829 15.54369249 17373
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16248.84173150   =   yrday.fracday
    Element set:     912
    Inclination:       51.6434  deg
    RA of node:        20.5912  deg
    Eccentricity:     .0003140     
    Arg of perigee:   295.7000  deg
    Mean anomaly:      64.3829  deg
    Mean motion:   15.54369249  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1737
    Checksum:              297
 
 
    Coasting Arc #14 (Orbit 1752)
    ---------------------------------------
 
    Vector Time (GMT): 2016/249/19:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5246245.96                 A    =         6782096.17  meter
     Y    =        1779206.45  meter          E    =           .0009163
     Z    =        3907978.21                 I    =           51.74166
     XDOT =      -4603.335575                 Wp   =           67.90584
     YDOT =      -4575.585529  meter/sec      RA   =           15.06611  deg
     ZDOT =      -4085.541950                 TA   =           64.86191
                                              MA   =           64.76689
                                              Ha   =            219.819  n.mi
                                              Hp   =            215.179
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17212093.04                 X    =        -5284734.86
     Y    =        5837291.50  feet           Y    =         1720324.64  meter
     Z    =       12821450.82                 Z    =         3882399.58
     XDOT =     -15102.807005                 XDOT =       -4531.982281
     YDOT =     -15011.763545  feet/sec       YDOT =       -4626.664599  meter/sec
     ZDOT =     -13404.009023                 ZDOT =       -4107.729990
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9645609.72                 X    =        -2939981.84
     Y    =      -15496926.22  feet           Y    =        -4723463.11  meter
     Z    =       12709335.57                 Z    =         3873805.48
     XDOT =      10043.173361                 XDOT =        3061.159240
     YDOT =     -17352.710304  feet/sec       YDOT =       -5289.106101  meter/sec
     ZDOT =     -13500.084457                 ZDOT =       -4114.825743
  
  
    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   16249.87038792  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6425  15.4614 0003119 302.9833  57.1020 15.54426654 17531
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16249.87038792   =   yrday.fracday
    Element set:     913
    Inclination:       51.6425  deg
    RA of node:        15.4614  deg
    Eccentricity:     .0003119     
    Arg of perigee:   302.9833  deg
    Mean anomaly:      57.1020  deg
    Mean motion:   15.54426654  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1753
    Checksum:              302
 
 
    Coasting Arc #15 (Orbit 1767)
    ---------------------------------------
 
    Vector Time (GMT): 2016/250/19:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6250178.28                 A    =         6785953.62  meter
     Y    =        -879206.96  meter          E    =           .0005707
     Z    =       -2484667.16                 I    =           51.72233
     XDOT =       2783.475662                 Wp   =           16.10781
     YDOT =       4763.163679  meter/sec      RA   =           10.09088  deg
     ZDOT =       5324.653610                 TA   =          316.07756
                                              MA   =          316.12291
                                              Ha   =            219.902  n.mi
                                              Hp   =            215.147
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20505834.25                 X    =         6271614.73
     Y    =       -2884537.28  feet           Y    =         -809193.67  meter
     Z    =       -8151795.15                 Z    =        -2454253.16
     XDOT =       9132.137999                 XDOT =        2704.140964
     YDOT =      15627.177423  feet/sec       YDOT =        4793.847313  meter/sec
     ZDOT =      17469.335992                 ZDOT =        5337.981888
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7850450.73                 X    =         2392817.38
     Y    =       19218009.98  feet           Y    =         5857649.44  meter
     Z    =       -8018732.67                 Z    =        -2444109.72
     XDOT =     -11530.646351                 XDOT =       -3514.541008
     YDOT =      12011.691012  feet/sec       YDOT =        3661.163420  meter/sec
     ZDOT =      17526.652729                 ZDOT =        5342.123752
  
  
    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   16250.83474979  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6417  10.6535 0003017 306.7399  53.3477 15.54416941 17685
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16250.83474979   =   yrday.fracday
    Element set:     914
    Inclination:       51.6417  deg
    RA of node:        10.6535  deg
    Eccentricity:     .0003017     
    Arg of perigee:   306.7399  deg
    Mean anomaly:      53.3477  deg
    Mean motion:   15.54416941  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1768
    Checksum:              326
 
 
    Coasting Arc #16 (Orbit 1768)
    ---------------------------------------
 
    Vector Time (GMT): 2016/250/21:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909722.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2231785.18                 A    =         6778724.97  meter
     Y    =       -4240792.71  meter          E    =           .0010053
     Z    =       -4803902.21                 I    =           51.69534
     XDOT =       7160.692118                 Wp   =           56.53101
     YDOT =       -830.233047  meter/sec      RA   =            9.88842  deg
     ZDOT =      -2592.283512                 TA   =          187.91585
                                              MA   =          187.93173
                                              Ha   =            219.855  n.mi
                                              Hp   =            215.097
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7322129.85                 X    =        -2160862.36
     Y    =      -13913361.91  feet           Y    =        -4265353.95  meter
     Z    =      -15760834.02                 Z    =        -4814571.00
     XDOT =      23493.084378                 XDOT =        7182.036016
     YDOT =      -2723.861703  feet/sec       YDOT =        -750.038307  meter/sec
     ZDOT =      -8504.867166                 ZDOT =       -2557.446684
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8026446.24                 X    =         2446460.81
     Y    =      -13465722.80  feet           Y    =        -4104352.31  meter
     Z    =      -15806631.03                 Z    =        -4817861.14
     XDOT =      13735.294208                 XDOT =        4186.517675
     YDOT =      17997.389401  feet/sec       YDOT =        5485.604290  meter/sec
     ZDOT =      -8352.489231                 ZDOT =       -2545.838718
  
  
    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   16250.89904110  .00016717  00000-0  10270-3 0  9159
    2 25544  51.6404  10.3319 0003150 307.2860  52.8005 15.54395823 17692
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16250.89904110   =   yrday.fracday
    Element set:     915
    Inclination:       51.6404  deg
    RA of node:        10.3319  deg
    Eccentricity:     .0003150     
    Arg of perigee:   307.2860  deg
    Mean anomaly:      52.8005  deg
    Mean motion:   15.54395823  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1769
    Checksum:              285
 
 
    Coasting Arc #17 (Orbit 1769)
    ---------------------------------------
 
    Vector Time (GMT): 2016/250/21:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 894613.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1935081.29                 A    =         6778228.10  meter
     Y    =        4260384.02  meter          E    =           .0003311
     Z    =        4901980.93                 I    =           51.69314
     XDOT =      -7280.706669                 Wp   =          117.22075
     YDOT =        621.012227  meter/sec      RA   =            9.72466  deg
     ZDOT =       2331.674344                 TA   =          309.97189
                                              MA   =          310.00096
                                              Ha   =            219.733  n.mi
                                              Hp   =            215.188
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6348691.91                 X    =         1863485.02
     Y    =       13977637.85  feet           Y    =         4281623.56  meter
     Z    =       16082614.59                 Z    =         4911206.76
     XDOT =     -23886.832904                 XDOT =       -7298.436158
     YDOT =       2037.441688  feet/sec       YDOT =         539.495586  meter/sec
     ZDOT =       7649.850210                 ZDOT =        2296.263313
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5826588.80                 X    =        -1775944.27
     Y    =       14158368.80  feet           Y    =         4315470.81  meter
     Z    =       16122102.75                 Z    =         4914016.92
     XDOT =     -16939.192794                 XDOT =       -5163.065964
     YDOT =     -15515.549031  feet/sec       YDOT =       -4729.139345  meter/sec
     ZDOT =       7495.004100                 ZDOT =        2284.477250
  
  
    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   16250.96333132  .00016717  00000-0  10270-3 0  9168
    2 25544  51.6407  10.0117 0003319 305.9294  54.1551 15.54419779 17701
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16250.96333132   =   yrday.fracday
    Element set:     916
    Inclination:       51.6407  deg
    RA of node:        10.0117  deg
    Eccentricity:     .0003319     
    Arg of perigee:   305.9294  deg
    Mean anomaly:      54.1551  deg
    Mean motion:   15.54419779  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1770
    Checksum:              293
 
 
    Coasting Arc #18 (Orbit 1784)
    ---------------------------------------
 
    Vector Time (GMT): 2016/251/21:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 894613.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -34050.97                 A    =         6776568.60  meter
     Y    =       -4219808.70  meter          E    =           .0012632
     Z    =       -5313039.15                 I    =           51.65570
     XDOT =       7643.807501                 Wp   =           77.14331
     YDOT =        364.716405  meter/sec      RA   =            4.72557  deg
     ZDOT =       -336.589501                 TA   =          189.63278
                                              MA   =          189.65702
                                              Ha   =            219.887  n.mi
                                              Hp   =            215.117
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -111715.78                 X    =           38947.05
     Y    =      -13844516.73  feet           Y    =        -4219781.79  meter
     Z    =      -17431230.79                 Z    =        -5313026.88
     XDOT =      25078.108599                 XDOT =        7640.796055
     YDOT =       1196.576132  feet/sec       YDOT =         450.177713  meter/sec
     ZDOT =      -1104.296264                 ZDOT =        -299.465065
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9868579.03                 X    =         3007942.89
     Y    =       -9712088.01  feet           Y    =        -2960244.43  meter
     Z    =      -17430359.30                 Z    =        -5312773.51
     XDOT =      16035.662457                 XDOT =        4887.669917
     YDOT =      17997.145993  feet/sec       YDOT =        5485.530099  meter/sec
     ZDOT =       -942.164619                 ZDOT =        -287.171776
  
  
    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   16251.92768699  .00016717  00000-0  10270-3 0  9176
    2 25544  51.6410   5.2022 0003275 310.6319  49.4548 15.54408271 17852
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16251.92768699   =   yrday.fracday
    Element set:     917
    Inclination:       51.6410  deg
    RA of node:         5.2022  deg
    Eccentricity:     .0003275     
    Arg of perigee:   310.6319  deg
    Mean anomaly:      49.4548  deg
    Mean motion:   15.54408271  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1785
    Checksum:              312
 
             

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