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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  21963.7584
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   88.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.118
   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 
   ------------------------------------------------------------------------
   344/13:26:46.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.0  
   000/00:00:00.000           0.0               0.0              216.7  
   
   345/20:56:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.9  
   000/00:00:00.000           0.0               0.0              216.4  
   
   348/10:55:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.5  
   000/00:00:00.000           0.0               0.0              216.1  
   
   349/01:45:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.5  
   000/00:00:00.000           0.0               0.0              215.9  
   
   352/04:52:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.9  
   000/00:00:00.000           0.0               0.0              215.4  
   
 
 
    Coasting Arc #1 (Orbit 3193)
    ---------------------------------------
 
    Vector Time (GMT): 2016/342/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2857619.28                 A    =         6783813.00  meter
     Y    =        4783847.88  meter          E    =           .0007942
     Z    =        3868253.12                 I    =           51.26908
     XDOT =      -3557.178328                 Wp   =           47.33685
     YDOT =       5430.289596  meter/sec      RA   =          272.98037  deg
     ZDOT =      -4077.147510                 TA   =           85.69236
                                              MA   =           85.60161
                                              Ha   =            220.705  n.mi
                                              Hp   =            217.031
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9375391.34                 X    =         2785122.29
     Y    =       15695038.98  feet           Y    =         4815398.22  meter
     Z    =       12691119.16                 Z    =         3881958.85
     XDOT =     -11670.532572                 XDOT =       -3597.831733
     YDOT =      17815.910749  feet/sec       YDOT =        5390.283664  meter/sec
     ZDOT =     -13376.468209                 ZDOT =       -4094.526031
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17493351.62                 X    =        -5331973.57
     Y    =        5168262.66  feet           Y    =         1575286.46  meter
     Z    =       12750232.43                 Z    =         3886270.84
     XDOT =     -14060.642714                 XDOT =       -4285.683899
     YDOT =     -14315.967472  feet/sec       YDOT =       -4363.506886  meter/sec
     ZDOT =     -13453.545734                 ZDOT =       -4100.640740
  
  
    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   16342.54056526  .00016717  00000-0  10270-3 0  9006
    2 25544  51.6415 273.6416 0006404 304.9852  55.0698 15.53825053 31945
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16342.54056526   =   yrday.fracday
    Element set:     900
    Inclination:       51.6415  deg
    RA of node:       273.6416  deg
    Eccentricity:     .0006404     
    Arg of perigee:   304.9852  deg
    Mean anomaly:      55.0698  deg
    Mean motion:   15.53825053  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3194
    Checksum:              305
 
 
    Coasting Arc #2 (Orbit 3208)
    ---------------------------------------
 
    Vector Time (GMT): 2016/343/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2300840.02                 A    =         6787300.24  meter
     Y    =       -5821801.22  meter          E    =           .0007081
     Z    =       -2611473.79                 I    =           51.27928
     XDOT =       4036.453657                 Wp   =          352.57100
     YDOT =      -3927.438873  meter/sec      RA   =          267.97548  deg
     ZDOT =       5204.496197                 TA   =          337.85975
                                              MA   =          337.89031
                                              Ha   =            220.824  n.mi
                                              Hp   =            216.868
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7548687.72                 X    =        -2222882.63
     Y    =      -19100397.70  feet           Y    =        -5847094.80  meter
     Z    =       -8567827.41                 Z    =        -2622461.59
     XDOT =      13242.958191                 XDOT =        4054.789908
     YDOT =     -12885.298140  feet/sec       YDOT =       -3882.198155  meter/sec
     ZDOT =      17075.118756                 ZDOT =        5224.148847
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20306638.22                 X    =         6189463.33
     Y    =       -2939406.40  feet           Y    =         -895931.07  meter
     Z    =       -8614863.88                 Z    =        -2625810.51
     XDOT =       9335.100972                 XDOT =        2845.338776
     YDOT =      14243.239755  feet/sec       YDOT =        4341.339477  meter/sec
     ZDOT =      17161.867859                 ZDOT =        5230.937324
  
  
    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   16343.50528600  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6409 268.8348 0006376 309.0707  50.9878 15.53820028 32099
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16343.50528600   =   yrday.fracday
    Element set:     901
    Inclination:       51.6409  deg
    RA of node:       268.8348  deg
    Eccentricity:     .0006376     
    Arg of perigee:   309.0707  deg
    Mean anomaly:      50.9878  deg
    Mean motion:   15.53820028  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3209
    Checksum:              314
 
 
    Coasting Arc #3 (Orbit 3224)
    ---------------------------------------
 
    Vector Time (GMT): 2016/344/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1680715.68                 A    =         6789671.29  meter
     Y    =        6483818.65  meter          E    =           .0007427
     Z    =        1092510.92                 I    =           51.29032
     XDOT =      -4461.080207                 Wp   =          115.21322
     YDOT =       2147.215591  meter/sec      RA   =          262.97895  deg
     ZDOT =      -5852.164634                 TA   =           52.88125
                                              MA   =           52.81340
                                              Ha   =            221.009  n.mi
                                              Hp   =            216.722
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5514159.06                 X    =         1602780.04
     Y    =       21272370.89  feet           Y    =         6502177.74  meter
     Z    =        3584353.42                 Z    =         1100486.41
     XDOT =     -14636.089917                 XDOT =       -4456.331778
     YDOT =       7044.670573  feet/sec       YDOT =        2097.355529  meter/sec
     ZDOT =     -19200.015204                 ZDOT =       -5873.824068
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21952571.16                 X    =        -6691143.69
     Y    =         872534.84  feet           Y    =          265948.62  meter
     Z    =        3618094.16                 Z    =         1102795.10
     XDOT =      -3754.488688                 XDOT =       -1144.368152
     YDOT =     -14070.806344  feet/sec       YDOT =       -4288.781774  meter/sec
     ZDOT =     -19295.223146                 ZDOT =       -5881.184015
  
  
    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   16344.53431473  .00016717  00000-0  10270-3 0  9027
    2 25544  51.6418 263.7077 0006360 312.2749  47.7864 15.53833091 32258
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16344.53431473   =   yrday.fracday
    Element set:     902
    Inclination:       51.6418  deg
    RA of node:       263.7077  deg
    Eccentricity:     .0006360     
    Arg of perigee:   312.2749  deg
    Mean anomaly:      47.7864  deg
    Mean motion:   15.53833091  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3225
    Checksum:              309
 
 
    Coasting Arc #4 (Orbit 3225)
    ---------------------------------------
 
    Vector Time (GMT): 2016/344/13:26:46.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3103628.28                 A    =         6786330.90  meter
     Y    =        5230635.11  meter          E    =           .0008798
     Z    =        3006491.35                 I    =           51.27977
     XDOT =      -3355.486837                 Wp   =           72.01406
     YDOT =       4827.199697  meter/sec      RA   =          262.66464  deg
     ZDOT =      -4919.788351                 TA   =           73.37735
                                              MA   =           73.28076
                                              Ha   =            220.996  n.mi
                                              Hp   =            216.707
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10182507.48                 X    =         3030302.91
     Y    =       17160876.34  feet           Y    =         5264931.88  meter
     Z    =        9863816.76                 Z    =         3021390.23
     XDOT =     -11008.815081                 XDOT =       -3385.317973
     YDOT =      15837.269348  feet/sec       YDOT =        4789.509751  meter/sec
     ZDOT =     -16141.037898                 ZDOT =       -4936.160940
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15244302.85                 X    =        -4646463.51
     Y    =       12826464.86  feet           Y    =         3909506.49  meter
     Z    =        9928093.78                 Z    =         3026082.99
     XDOT =     -16490.623216                 XDOT =       -5026.341956
     YDOT =      -7012.548731  feet/sec       YDOT =       -2137.424853  meter/sec
     ZDOT =     -16213.586353                 ZDOT =       -4941.901120
  
  
    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   16344.59862909  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6422 263.3883 0006279 312.2878  47.7742 15.53825752 32267
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16344.59862909   =   yrday.fracday
    Element set:     903
    Inclination:       51.6422  deg
    RA of node:       263.3883  deg
    Eccentricity:     .0006279     
    Arg of perigee:   312.2878  deg
    Mean anomaly:      47.7742  deg
    Mean motion:   15.53825752  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3226
    Checksum:              337
 
 
    Coasting Arc #5 (Orbit 3240)
    ---------------------------------------
 
    Vector Time (GMT): 2016/345/13:26:46.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2605010.94                 A    =         6789037.44  meter
     Y    =       -6064513.88  meter          E    =           .0010989
     Z    =       -1559187.26                 I    =           51.29567
     XDOT =       3995.964336                 Wp   =            2.19317
     YDOT =      -3184.169638  meter/sec      RA   =          257.66507  deg
     ZDOT =       5720.807291                 TA   =          340.67328
                                              MA   =          340.71492
                                              Ha   =            221.038  n.mi
                                              Hp   =            216.558
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8546623.81                 X    =        -2529428.42
     Y    =      -19896699.09  feet           Y    =        -6093222.19  meter
     Z    =       -5115443.75                 Z    =        -1571658.61
     XDOT =      13110.119212                 XDOT =        4003.483972
     YDOT =     -10446.750782  feet/sec       YDOT =       -3139.442301  meter/sec
     ZDOT =      18769.052792                 ZDOT =        5740.237055
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18004240.58                 X    =         5487692.53
     Y    =      -12009180.67  feet           Y    =        -3660398.27  meter
     Z    =       -5168953.36                 Z    =        -1575496.99
     XDOT =      11768.816553                 XDOT =        3587.135285
     YDOT =       9545.450565  feet/sec       YDOT =        2909.453332  meter/sec
     ZDOT =      18854.687053                 ZDOT =        5746.908614
  
  
    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   16345.56333404  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6436 258.5807 0006462 315.5601  44.5032 15.53866596 32413
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16345.56333404   =   yrday.fracday
    Element set:     904
    Inclination:       51.6436  deg
    RA of node:       258.5807  deg
    Eccentricity:     .0006462     
    Arg of perigee:   315.5601  deg
    Mean anomaly:      44.5032  deg
    Mean motion:   15.53866596  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3241
    Checksum:              305
 
 
    Coasting Arc #6 (Orbit 3245)
    ---------------------------------------
 
    Vector Time (GMT): 2016/345/20:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4427635.00                 A    =         6779389.07  meter
     Y    =       -1196231.54  meter          E    =           .0008245
     Z    =       -4999341.80                 I    =           51.26330
     XDOT =       -211.061588                 Wp   =           83.30529
     YDOT =      -7403.649164  meter/sec      RA   =          256.09687  deg
     ZDOT =       1962.193767                 TA   =          205.84012
                                              MA   =          205.88132
                                              Ha   =            220.900  n.mi
                                              Hp   =            216.386
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14526361.55                 X    =        -4389644.39
     Y    =       -3924644.16  feet           Y    =        -1245531.65  meter
     Z    =      -16402040.02                 Z    =        -5020758.22
     XDOT =       -692.459278                 XDOT =        -137.788016
     YDOT =     -24290.187547  feet/sec       YDOT =       -7405.599803  meter/sec
     ZDOT =       6437.643593                 ZDOT =        1961.346053
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14219224.30                 X    =        -4334019.57
     Y    =        4599368.47  feet           Y    =         1401887.51  meter
     Z    =      -16495587.24                 Z    =        -5027854.99
     XDOT =     -13563.625561                 XDOT =       -4134.193071
     YDOT =     -18896.525283  feet/sec       YDOT =       -5759.660906  meter/sec
     ZDOT =       6435.259403                 ZDOT =        1961.467066
  
  
    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   16345.88490142  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6414 256.9739 0006007 314.6128  45.4533 15.53865205 32461
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16345.88490142   =   yrday.fracday
    Element set:     905
    Inclination:       51.6414  deg
    RA of node:       256.9739  deg
    Eccentricity:     .0006007     
    Arg of perigee:   314.6128  deg
    Mean anomaly:      45.4533  deg
    Mean motion:   15.53865205  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3246
    Checksum:              312
 
 
    Coasting Arc #7 (Orbit 3261)
    ---------------------------------------
 
    Vector Time (GMT): 2016/346/20:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4529224.60                 A    =         6782490.75  meter
     Y    =        2756064.74  meter          E    =           .0009185
     Z    =        4229756.89                 I    =           51.28182
     XDOT =       -734.317749                 Wp   =           37.94806
     YDOT =       6733.752493  meter/sec      RA   =          251.08008  deg
     ZDOT =      -3590.045200                 TA   =           88.98862
                                              MA   =           88.88339
                                              Ha   =            221.114  n.mi
                                              Hp   =            216.386
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14859660.75                 X    =         4477522.34
     Y    =        9042207.14  feet           Y    =         2806424.16  meter
     Z    =       13877155.16                 Z    =         4251633.66
     XDOT =      -2409.178967                 XDOT =        -792.122596
     YDOT =      22092.363822  feet/sec       YDOT =        6725.217925  meter/sec
     ZDOT =     -11778.363517                 ZDOT =       -3593.752271
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17299437.26                 X    =         5272868.48
     Y    =        -804130.11  feet           Y    =         -245098.86  meter
     Z    =       13972448.19                 Z    =         4258802.21
     XDOT =      10409.075921                 XDOT =        3172.686341
     YDOT =      18331.685779  feet/sec       YDOT =        5587.497825  meter/sec
     ZDOT =     -11795.794356                 ZDOT =       -3595.358120
  
  
    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   16346.91391300  .00016717  00000-0  10270-3 0  9069
    2 25544  51.6411 251.8461 0005919 318.5190  41.5512 15.53837187 32627
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16346.91391300   =   yrday.fracday
    Element set:     906
    Inclination:       51.6411  deg
    RA of node:       251.8461  deg
    Eccentricity:     .0005919     
    Arg of perigee:   318.5190  deg
    Mean anomaly:      41.5512  deg
    Mean motion:   15.53837187  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3262
    Checksum:              300
 
 
    Coasting Arc #8 (Orbit 3276)
    ---------------------------------------
 
    Vector Time (GMT): 2016/347/20:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4491328.35                 A    =         6786023.70  meter
     Y    =       -4045883.29  meter          E    =           .0006017
     Z    =       -3076898.09                 I    =           51.30568
     XDOT =       1760.273279                 Wp   =            5.79878
     YDOT =      -5653.610483  meter/sec      RA   =          246.07405  deg
     ZDOT =       4871.315115                 TA   =          318.66625
                                              MA   =          318.71177
                                              Ha   =            221.192  n.mi
                                              Hp   =            216.218
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14735329.23                 X    =        -4430806.03
     Y    =      -13273895.32  feet           Y    =        -4095769.64  meter
     Z    =      -10094810.00                 Z    =        -3098569.47
     XDOT =       5775.174801                 XDOT =        1799.699574
     YDOT =     -18548.590824  feet/sec       YDOT =       -5633.705962  meter/sec
     ZDOT =      15982.004972                 ZDOT =        4879.961377
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19636093.57                 X    =        -5985081.32
     Y    =       -2416562.81  feet           Y    =         -736568.35  meter
     Z    =      -10188987.52                 Z    =        -3105603.40
     XDOT =      -6209.530717                 XDOT =       -1892.664962
     YDOT =     -17000.647718  feet/sec       YDOT =       -5181.797425  meter/sec
     ZDOT =      16020.866800                 ZDOT =        4883.160201
  
  
    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   16347.87860471  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6415 247.0399 0006113 321.9045  38.1674 15.53857834 32770
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16347.87860471   =   yrday.fracday
    Element set:     907
    Inclination:       51.6415  deg
    RA of node:       247.0399  deg
    Eccentricity:     .0006113     
    Arg of perigee:   321.9045  deg
    Mean anomaly:      38.1674  deg
    Mean motion:   15.53857834  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3277
    Checksum:              330
 
 
    Coasting Arc #9 (Orbit 3285)
    ---------------------------------------
 
    Vector Time (GMT): 2016/348/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3889326.88                 A    =         6789343.29  meter
     Y    =       -5403539.57  meter          E    =           .0012593
     Z    =       -1289559.04                 I    =           51.32503
     XDOT =       3307.867009                 Wp   =            8.53420
     YDOT =      -3762.631496  meter/sec      RA   =          243.17372  deg
     ZDOT =       5809.220036                 TA   =          337.36817
                                              MA   =          337.42365
                                              Ha   =            221.468  n.mi
                                              Hp   =            216.069
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12760258.78                 X    =        -3822349.87
     Y    =      -17728148.20  feet           Y    =        -5446658.01  meter
     Z    =       -4230836.75                 Z    =        -1308290.48
     XDOT =      10852.582052                 XDOT =        3321.476961
     YDOT =     -12344.591522  feet/sec       YDOT =       -3725.565245  meter/sec
     ZDOT =      19059.120852                 ZDOT =        5825.321600
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21415994.62                 X    =         6527595.16
     Y    =       -4215926.14  feet           Y    =        -1285014.29  meter
     Z    =       -4311909.53                 Z    =        -1314270.03
     XDOT =       6462.243366                 XDOT =        1969.691778
     YDOT =      13325.257983  feet/sec       YDOT =        4061.538633  meter/sec
     ZDOT =      19130.295143                 ZDOT =        5830.913960
  
  
    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   16348.45741819  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6419 244.1602 0006537 326.7504  33.3237 15.53871754 32861
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16348.45741819   =   yrday.fracday
    Element set:     908
    Inclination:       51.6419  deg
    RA of node:       244.1602  deg
    Eccentricity:     .0006537     
    Arg of perigee:   326.7504  deg
    Mean anomaly:      33.3237  deg
    Mean motion:   15.53871754  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3286
    Checksum:              321
 
 
    Coasting Arc #10 (Orbit 3295)
    ---------------------------------------
 
    Vector Time (GMT): 2016/349/01:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1453495.73                 A    =         6787783.22  meter
     Y    =        6220260.74  meter          E    =           .0001505
     Z    =       -2298539.15                 I    =           51.32924
     XDOT =      -5395.878731                 Wp   =           37.47300
     YDOT =       -730.767206  meter/sec      RA   =          240.11069  deg
     ZDOT =      -5390.400428                 TA   =          168.22699
                                              MA   =          168.22348
                                              Ha   =            221.546  n.mi
                                              Hp   =            215.909
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4768686.76                 X    =         1394996.51
     Y    =       20407679.61  feet           Y    =         6236187.89  meter
     Z    =       -7541138.93                 Z    =        -2291619.75
     XDOT =     -17703.014208                 XDOT =       -5361.121713
     YDOT =      -2397.530202  feet/sec       YDOT =        -790.912576  meter/sec
     ZDOT =     -17685.040775                 ZDOT =       -5416.528042
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17812173.85                 X    =         5429150.59
     Y    =      -11062545.92  feet           Y    =        -3371864.00  meter
     Z    =       -7511928.99                 Z    =        -2289635.96
     XDOT =       2517.155693                 XDOT =         767.229055
     YDOT =      16137.892332  feet/sec       YDOT =        4918.829583  meter/sec
     ZDOT =     -17799.336491                 ZDOT =       -5425.237763
  
  
    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   16349.10054032  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6419 240.9542 0006281 329.5230  30.5556 15.53895324 32964
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16349.10054032   =   yrday.fracday
    Element set:     909
    Inclination:       51.6419  deg
    RA of node:       240.9542  deg
    Eccentricity:     .0006281     
    Arg of perigee:   329.5230  deg
    Mean anomaly:      30.5556  deg
    Mean motion:   15.53895324  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3296
    Checksum:              302
 
 
    Coasting Arc #11 (Orbit 3311)
    ---------------------------------------
 
    Vector Time (GMT): 2016/350/01:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -429044.77                 A    =         6784416.61  meter
     Y    =       -5703288.36  meter          E    =           .0010278
     Z    =        3636936.06                 I    =           51.33370
     XDOT =       5872.471535                 Wp   =           62.40694
     YDOT =       2335.502763  meter/sec      RA   =          235.11171  deg
     ZDOT =       4350.425577                 TA   =          341.00487
                                              MA   =          341.04318
                                              Ha   =            221.673  n.mi
                                              Hp   =            215.742
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1407627.19                 X    =         -382903.88
     Y    =      -18711575.99  feet           Y    =        -5707828.67  meter
     Z    =       11932204.91                 Z    =         3634963.26
     XDOT =      19266.638895                 XDOT =        5824.786432
     YDOT =       7662.410639  feet/sec       YDOT =        2400.905543  meter/sec
     ZDOT =      14273.049792                 ZDOT =        4378.836989
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17135418.23                 X    =        -5222875.48
     Y    =        7659267.32  feet           Y    =         2334544.68  meter
     Z    =       11924557.46                 Z    =         3634605.11
     XDOT =       1365.894331                 XDOT =         416.324592
     YDOT =     -19383.156386  feet/sec       YDOT =       -5907.986066  meter/sec
     ZDOT =      14397.085890                 ZDOT =        4388.231779
  
  
    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   16350.12953286  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6408 235.8270 0006299 333.9507  26.1328 15.53889687 33120
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16350.12953286   =   yrday.fracday
    Element set:     910
    Inclination:       51.6408  deg
    RA of node:       235.8270  deg
    Eccentricity:     .0006299     
    Arg of perigee:   333.9507  deg
    Mean anomaly:      26.1328  deg
    Mean motion:   15.53889687  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3312
    Checksum:              323
 
 
    Coasting Arc #12 (Orbit 3326)
    ---------------------------------------
 
    Vector Time (GMT): 2016/351/01:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -749398.33                 A    =         6780881.62  meter
     Y    =        4894832.91  meter          E    =           .0011834
     Z    =       -4643262.26                 I    =           51.34136
     XDOT =      -6073.104969                 Wp   =           38.57074
     YDOT =      -3669.120232  meter/sec      RA   =          230.10431  deg
     ZDOT =      -2882.649976                 TA   =          202.58648
                                              MA   =          202.63861
                                              Ha   =            221.797  n.mi
                                              Hp   =            215.560
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2458655.93                 X    =         -781523.10
     Y    =       16059163.10  feet           Y    =         4886273.52  meter
     Z    =      -15233800.06                 Z    =        -4646980.12
     XDOT =     -19924.885068                 XDOT =       -6017.621983
     YDOT =     -12037.796036  feet/sec       YDOT =       -3736.723236  meter/sec
     ZDOT =      -9457.513044                 ZDOT =       -2912.017042
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15865358.04                 X    =         4835761.13
     Y    =       -3421974.34  feet           Y    =        -1043017.78  meter
     Z    =      -15250930.41                 Z    =        -4648483.59
     XDOT =      -4557.099644                 XDOT =       -1389.003971
     YDOT =      21666.679057  feet/sec       YDOT =        6604.003777  meter/sec
     ZDOT =      -9585.527124                 ZDOT =       -2921.668667
  
  
    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   16351.09421020  .00016717  00000-0  10270-3 0  9113
    2 25544  51.6410 231.0202 0006283 336.6930  23.3937 15.53890940 33274
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16351.09421020   =   yrday.fracday
    Element set:     911
    Inclination:       51.6410  deg
    RA of node:       231.0202  deg
    Eccentricity:     .0006283     
    Arg of perigee:   336.6930  deg
    Mean anomaly:      23.3937  deg
    Mean motion:   15.53890940  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3327
    Checksum:              271
 
 
    Coasting Arc #13 (Orbit 3342)
    ---------------------------------------
 
    Vector Time (GMT): 2016/352/01:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2032316.93                 A    =         6778433.40  meter
     Y    =       -3846590.16  meter          E    =           .0004048
     Z    =        5196349.39                 I    =           51.35416
     XDOT =       5962.278085                 Wp   =           18.91404
     YDOT =       4687.809912  meter/sec      RA   =          225.08965  deg
     ZDOT =       1141.779854                 TA   =           60.11815
                                              MA   =           60.07793
                                              Ha   =            221.860  n.mi
                                              Hp   =            215.368
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6667706.47                 X    =         2049938.07
     Y    =      -12620046.46  feet           Y    =        -3823765.36  meter
     Z    =       17048390.40                 Z    =         5206264.24
     XDOT =      19561.279806                 XDOT =        5903.868443
     YDOT =      15379.953780  feet/sec       YDOT =        4754.157423  meter/sec
     ZDOT =       3745.996896                 ZDOT =        1170.601375
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14143988.34                 X    =        -4311087.65
     Y    =       -1471750.68  feet           Y    =         -448589.61  meter
     Z    =       17092484.94                 Z    =         5209789.41
     XDOT =       7035.514959                 XDOT =        2144.424960
     YDOT =     -22784.790397  feet/sec       YDOT =       -6944.804113  meter/sec
     ZDOT =       3871.471541                 ZDOT =        1180.024526
  
  
    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   16352.12319343  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6402 225.8923 0006383 341.8177  18.2747 15.53912515 33431
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16352.12319343   =   yrday.fracday
    Element set:     912
    Inclination:       51.6402  deg
    RA of node:       225.8923  deg
    Eccentricity:     .0006383     
    Arg of perigee:   341.8177  deg
    Mean anomaly:      18.2747  deg
    Mean motion:   15.53912515  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3343
    Checksum:              298
 
 
    Coasting Arc #14 (Orbit 3344)
    ---------------------------------------
 
    Vector Time (GMT): 2016/352/04:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2616893.80                 A    =         6778099.11  meter
     Y    =       -3347324.94  meter          E    =           .0005282
     Z    =        5280338.63                 I    =           51.35368
     XDOT =       5699.248735                 Wp   =            5.36108
     YDOT =       5114.404618  meter/sec      RA   =          224.43441  deg
     ZDOT =        422.763245                 TA   =           80.62145
                                              MA   =           80.56173
                                              Ha   =            221.905  n.mi
                                              Hp   =            215.401
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8585609.57                 X    =         2628480.60
     Y    =      -10982037.21  feet           Y    =        -3317996.75  meter
     Z    =       17323945.65                 Z    =         5293078.58
     XDOT =      18698.322620                 XDOT =        5639.580989
     YDOT =      16779.542709  feet/sec       YDOT =        5177.803788  meter/sec
     ZDOT =       1387.018520                 ZDOT =         450.304009
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11920740.42                 X    =        -3633441.68
     Y    =        7089211.16  feet           Y    =         2160791.56  meter
     Z    =       17380332.52                 Z    =         5297525.35
     XDOT =     -10680.630100                 XDOT =       -3255.456055
     YDOT =     -21612.891737  feet/sec       YDOT =       -6587.609401  meter/sec
     ZDOT =       1506.812534                 ZDOT =         459.276460
  
  
    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   16352.25181662  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6381 225.2516 0006516 341.5576  18.5339 15.53893851 33450
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16352.25181662   =   yrday.fracday
    Element set:     913
    Inclination:       51.6381  deg
    RA of node:       225.2516  deg
    Eccentricity:     .0006516     
    Arg of perigee:   341.5576  deg
    Mean anomaly:      18.5339  deg
    Mean motion:   15.53893851  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3345
    Checksum:              313
 
 
    Coasting Arc #15 (Orbit 3359)
    ---------------------------------------
 
    Vector Time (GMT): 2016/353/04:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3850934.36                 A    =         6778674.43  meter
     Y    =        2162480.76  meter          E    =           .0012588
     Z    =       -5152027.74                 I    =           51.37939
     XDOT =      -5030.891572                 Wp   =           72.46561
     YDOT =      -5599.945052  meter/sec      RA   =          219.41851  deg
     ZDOT =       1416.487187                 TA   =          211.18788
                                              MA   =          211.26264
                                              Ha   =            222.112  n.mi
                                              Hp   =            215.082
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12634299.09                 X    =        -3849803.51
     Y    =        7094753.13  feet           Y    =         2119423.68  meter
     Z    =      -16902978.16                 Z    =        -5170731.53
     XDOT =     -16505.549776                 XDOT =       -4974.778252
     YDOT =     -18372.523138  feet/sec       YDOT =       -5655.890207  meter/sec
     ZDOT =       4647.267673                 ZDOT =        1392.184564
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14219919.57                 X    =         4334231.49
     Y    =       -2228279.30  feet           Y    =         -679179.53  meter
     Z    =      -16985298.50                 Z    =        -5177118.98
     XDOT =       8843.780483                 XDOT =        2695.584291
     YDOT =      21981.315830  feet/sec       YDOT =        6699.905065  meter/sec
     ZDOT =       4541.719633                 ZDOT =        1384.316144
  
  
    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   16353.21648338  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6381 220.4446 0006620 345.4393  14.6567 15.53891886 33608
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16353.21648338   =   yrday.fracday
    Element set:     914
    Inclination:       51.6381  deg
    RA of node:       220.4446  deg
    Eccentricity:     .0006620     
    Arg of perigee:   345.4393  deg
    Mean anomaly:      14.6567  deg
    Mean motion:   15.53891886  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3360
    Checksum:              317
 
 
    Coasting Arc #16 (Orbit 3375)
    ---------------------------------------
 
    Vector Time (GMT): 2016/354/04:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4972354.21                 A    =         6781183.81  meter
     Y    =        -956122.51  meter          E    =           .0011992
     Z    =        4510067.22                 I    =           51.41324
     XDOT =       3969.809138                 Wp   =           34.36036
     YDOT =       5757.957871  meter/sec      RA   =          214.40816  deg
     ZDOT =      -3142.239071                 TA   =           87.32922
                                              MA   =           87.19196
                                              Ha   =            222.138  n.mi
                                              Hp   =            215.010
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16313498.07                 X    =         4960768.52
     Y    =       -3136884.88  feet           Y    =         -900583.30  meter
     Z    =       14796808.45                 Z    =         4534193.25
     XDOT =      13024.308194                 XDOT =        3920.390623
     YDOT =      18890.937896  feet/sec       YDOT =        5802.074780  meter/sec
     ZDOT =     -10309.183304                 ZDOT =       -3123.074674
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16327778.69                 X    =        -4976706.94
     Y    =       -2495820.46  feet           Y    =         -760726.08  meter
     Z    =       14902695.39                 Z    =         4542341.55
     XDOT =      -6164.713902                 XDOT =       -1879.004797
     YDOT =     -20999.722854  feet/sec       YDOT =       -6400.715526  meter/sec
     ZDOT =     -10226.157061                 ZDOT =       -3116.932672
  
  
    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   16354.24545778  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6376 215.3167 0006680 348.3922  11.7075 15.53921814 33765
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16354.24545778   =   yrday.fracday
    Element set:     915
    Inclination:       51.6376  deg
    RA of node:       215.3167  deg
    Eccentricity:     .0006680     
    Arg of perigee:   348.3922  deg
    Mean anomaly:      11.7075  deg
    Mean motion:   15.53921814  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3376
    Checksum:              323
 
 
    Coasting Arc #17 (Orbit 3390)
    ---------------------------------------
 
    Vector Time (GMT): 2016/355/04:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5834521.05                 A    =         6784798.91  meter
     Y    =        -126045.50  meter          E    =           .0007575
     Z    =       -3457880.45                 I    =           51.45320
     XDOT =      -2569.009928                 Wp   =           33.52504
     YDOT =      -5609.773271  meter/sec      RA   =          209.40847  deg
     ZDOT =       4550.165403                 TA   =          285.79904
                                              MA   =          285.88255
                                              Ha   =            222.278  n.mi
                                              Hp   =            214.818
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19142129.45                 X    =        -5815881.18
     Y    =        -413535.12  feet           Y    =         -191186.69  meter
     Z    =      -11344752.13                 Z    =        -3486177.61
     XDOT =      -8428.510261                 XDOT =       -2528.191640
     YDOT =     -18404.767950  feet/sec       YDOT =       -5638.273613  meter/sec
     ZDOT =      14928.364184                 ZDOT =        4537.784818
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17934439.12                 X    =         5466417.04
     Y    =        6489927.82  feet           Y    =         1978130.00  meter
     Z    =      -11468751.55                 Z    =        -3495675.47
     XDOT =       2666.367228                 XDOT =         812.708731
     YDOT =      18855.411926  feet/sec       YDOT =        5747.129555  meter/sec
     ZDOT =      14875.028152                 ZDOT =        4533.908581
  
  
    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   16355.21011732  .00016717  00000-0  10270-3 0  9161
    2 25544  51.6384 210.5096 0006727 352.1881   7.9165 15.53903443 33913
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16355.21011732   =   yrday.fracday
    Element set:     916
    Inclination:       51.6384  deg
    RA of node:       210.5096  deg
    Eccentricity:     .0006727     
    Arg of perigee:   352.1881  deg
    Mean anomaly:       7.9165  deg
    Mean motion:   15.53903443  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3391
    Checksum:              298
 
 
    Coasting Arc #18 (Orbit 3406)
    ---------------------------------------
 
    Vector Time (GMT): 2016/356/04:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6376085.44                 A    =         6788059.58  meter
     Y    =        1114518.85  meter          E    =           .0012674
     Z    =        2037641.50                 I    =           51.49380
     XDOT =        865.069778                 Wp   =           81.82130
     YDOT =       5230.419191  meter/sec      RA   =          204.41973  deg
     ZDOT =      -5536.460044                 TA   =           75.61450
                                              MA   =           75.47386
                                              Ha   =            222.448  n.mi
                                              Hp   =            214.623
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20918915.49                 X    =         6353250.79
     Y    =        3656557.89  feet           Y    =         1185692.77  meter
     Z    =        6685175.52                 Z    =         2068559.35
     XDOT =       2838.155441                 XDOT =         833.411192
     YDOT =      17160.167951  feet/sec       YDOT =        5239.916172  meter/sec
     ZDOT =     -18164.238990                 ZDOT =       -5532.334476
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18781407.40                 X    =        -5724572.98
     Y    =       -9818469.73  feet           Y    =        -2992669.57  meter
     Z    =        6820513.24                 Z    =         2078892.44
     XDOT =       1673.382821                 XDOT =         510.047084
     YDOT =     -15876.973182  feet/sec       YDOT =       -4839.301426  meter/sec
     ZDOT =     -18147.012734                 ZDOT =       -5531.209481
  
  
    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   16356.23908217  .00016717  00000-0  10270-3 0  9178
    2 25544  51.6393 205.3812 0006823 355.9492   4.1604 15.53935836 34073
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16356.23908217   =   yrday.fracday
    Element set:     917
    Inclination:       51.6393  deg
    RA of node:       205.3812  deg
    Eccentricity:     .0006823     
    Arg of perigee:   355.9492  deg
    Mean anomaly:       4.1604  deg
    Mean motion:   15.53935836  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3407
    Checksum:              315
 
 
    Coasting Arc #19 (Orbit 3421)
    ---------------------------------------
 
    Vector Time (GMT): 2016/357/04:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930289.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6489925.94                 A    =         6789775.63  meter
     Y    =       -1909194.64  meter          E    =           .0016727
     Z    =        -452677.20                 I    =           51.52865
     XDOT =        972.305984                 Wp   =           26.25191
     YDOT =      -4700.893064  meter/sec      RA   =          199.44072  deg
     ZDOT =       5985.871327                 TA   =          328.85606
                                              MA   =          328.95509
                                              Ha   =            222.501  n.mi
                                              Hp   =            214.523
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21292407.95                 X    =        -6465895.59
     Y    =       -6263761.93  feet           Y    =        -1981634.97  meter
     Z    =       -1485161.41                 Z    =         -484145.26
     XDOT =       3189.980262                 XDOT =         995.723611
     YDOT =     -15422.877505  feet/sec       YDOT =       -4689.889393  meter/sec
     ZDOT =      19638.685455                 ZDOT =        5990.651219
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18589574.70                 X    =         5666102.37
     Y    =       12107902.27  feet           Y    =         3690488.61  meter
     Z    =       -1622796.84                 Z    =         -494628.48
     XDOT =      -6476.109748                 XDOT =       -1973.918251
     YDOT =      12538.028608  feet/sec       YDOT =        3821.591120  meter/sec
     ZDOT =      19660.406129                 ZDOT =        5992.491788
  
  
    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   16357.20373320  .00016717  00000-0  10270-3 0  9188
    2 25544  51.6386 200.5746 0006795 359.6107    .5039 15.53940235 34228
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16357.20373320   =   yrday.fracday
    Element set:     918
    Inclination:       51.6386  deg
    RA of node:       200.5746  deg
    Eccentricity:     .0006795     
    Arg of perigee:   359.6107  deg
    Mean anomaly:        .5039  deg
    Mean motion:   15.53940235  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3422
    Checksum:              300
 
             

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