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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14248.1877
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   94.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.554
   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 
   ------------------------------------------------------------------------
   217/02:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.3  
   000/00:00:00.000           0.0               0.0              212.7  
   
 
 
    Coasting Arc #1 (Orbit 1047)
    ---------------------------------------
 
    Vector Time (GMT): 2016/204/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =          65021.58                 A    =         6781780.48  meter
     Y    =       -5758015.45  meter          E    =           .0013903
     Z    =        3570225.54                 I    =           51.31654
     XDOT =       5611.910116                 Wp   =           89.58174
     YDOT =       2810.282986  meter/sec      RA   =          240.88330  deg
     ZDOT =       4415.361501                 TA   =          312.87543
                                              MA   =          312.99209
                                              Ha   =            220.521  n.mi
                                              Hp   =            212.825
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         213325.41                 X    =          112062.07
     Y    =      -18891126.82  feet           Y    =        -5757025.49  meter
     Z    =       11713338.39                 Z    =         3570655.37
     XDOT =      18411.778597                 XDOT =        5558.620254
     YDOT =       9220.088536  feet/sec       YDOT =        2872.740937  meter/sec
     ZDOT =      14486.094162                 ZDOT =        4442.492901
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16457724.26                 X    =        -5016314.36
     Y    =        9273400.38  feet           Y    =         2826532.44  meter
     Z    =       11716220.97                 Z    =         3571104.15
     XDOT =       -431.436121                 XDOT =        -131.501730
     YDOT =     -19277.945340  feet/sec       YDOT =       -5875.917740  meter/sec
     ZDOT =      14603.856530                 ZDOT =        4451.255470
  
  
    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   16204.55673918  .00016717  00000-0  10270-3 0  9004
    2 25544  51.6408 241.5667 0002010  67.6285 292.5081 15.54862507 10487
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16204.55673918   =   yrday.fracday
    Element set:     900
    Inclination:       51.6408  deg
    RA of node:       241.5667  deg
    Eccentricity:     .0002010     
    Arg of perigee:    67.6285  deg
    Mean anomaly:     292.5081  deg
    Mean motion:   15.54862507  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1048
    Checksum:              305
 
 
    Coasting Arc #2 (Orbit 1062)
    ---------------------------------------
 
    Vector Time (GMT): 2016/205/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1475678.75                 A    =         6777559.79  meter
     Y    =        4609794.67  meter          E    =           .0013065
     Z    =       -4756732.95                 I    =           51.31975
     XDOT =      -5603.355053                 Wp   =           71.57772
     YDOT =      -4508.771455  meter/sec      RA   =          235.86570  deg
     ZDOT =      -2633.081474                 TA   =          172.30337
                                              MA   =          172.28330
                                              Ha   =            220.495  n.mi
                                              Hp   =            212.778
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4841465.71                 X    =        -1504011.22
     Y    =       15123998.26  feet           Y    =         4593134.38  meter
     Z    =      -15606079.25                 Z    =        -4763969.97
     XDOT =     -18383.710803                 XDOT =       -5539.730241
     YDOT =     -14792.557266  feet/sec       YDOT =       -4571.076083  meter/sec
     ZDOT =      -8638.718748                 ZDOT =       -2660.146280
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15416845.52                 X    =         4699054.51
     Y    =       -3672255.76  feet           Y    =        -1119303.56  meter
     Z    =      -15638421.75                 Z    =        -4766590.95
     XDOT =      -3588.979079                 XDOT =       -1093.920823
     YDOT =      22193.412421  feet/sec       YDOT =        6764.552106  meter/sec
     ZDOT =      -8755.912163                 ZDOT =       -2668.802027
  
  
    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   16205.52080819  .00016717  00000-0  10270-3 0  9015
    2 25544  51.6415 236.7557 0001884  71.4460 288.6898 15.54868746 10635
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16205.52080819   =   yrday.fracday
    Element set:     901
    Inclination:       51.6415  deg
    RA of node:       236.7557  deg
    Eccentricity:     .0001884     
    Arg of perigee:    71.4460  deg
    Mean anomaly:     288.6898  deg
    Mean motion:   15.54868746  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1063
    Checksum:              334
 
 
    Coasting Arc #3 (Orbit 1078)
    ---------------------------------------
 
    Vector Time (GMT): 2016/206/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2908094.17                 A    =         6775225.51  meter
     Y    =       -3106117.52  meter          E    =           .0004558
     Z    =        5268557.25                 I    =           51.32998
     XDOT =       5142.317159                 Wp   =           96.60319
     YDOT =       5673.254541  meter/sec      RA   =          230.83840  deg
     ZDOT =        505.404686                 TA   =          348.55257
                                              MA   =          348.56293
                                              Ha   =            220.412  n.mi
                                              Hp   =            212.758
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9540991.36                 X    =         2917019.42
     Y    =      -10190674.28  feet           Y    =        -3073547.47  meter
     Z    =       17285292.81                 Z    =         5282705.45
     XDOT =      16871.119287                 XDOT =        5076.040207
     YDOT =      18613.039834  feet/sec       YDOT =        5730.388779  meter/sec
     ZDOT =       1658.151858                 ZDOT =         530.223543
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13627837.71                 X    =        -4153764.93
     Y    =       -2647270.68  feet           Y    =         -806888.10  meter
     Z    =       17347498.47                 Z    =         5287517.53
     XDOT =       6746.462497                 XDOT =        2056.321769
     YDOT =     -23142.441762  feet/sec       YDOT =       -7053.816249  meter/sec
     ZDOT =       1765.373027                 ZDOT =         538.085699
  
  
    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   16206.54914351  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6404 231.6237 0002020  73.7837 286.3538 15.54889183 10799
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16206.54914351   =   yrday.fracday
    Element set:     902
    Inclination:       51.6404  deg
    RA of node:       231.6237  deg
    Eccentricity:     .0002020     
    Arg of perigee:    73.7837  deg
    Mean anomaly:     286.3538  deg
    Mean motion:   15.54889183  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1079
    Checksum:              309
 
 
    Coasting Arc #4 (Orbit 1093)
    ---------------------------------------
 
    Vector Time (GMT): 2016/207/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4255666.59                 A    =         6776111.61  meter
     Y    =        1452375.18  meter          E    =           .0015076
     Z    =       -5082624.54                 I    =           51.35582
     XDOT =      -4145.214448                 Wp   =           99.36042
     YDOT =      -6211.571960  meter/sec      RA   =          225.81039  deg
     ZDOT =       1697.713587                 TA   =          187.11795
                                              MA   =          187.13938
                                              Ha   =            220.481  n.mi
                                              Hp   =            212.685
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13962160.73                 X    =        -4246902.20
     Y    =        4765010.44  feet           Y    =         1404834.57  meter
     Z    =      -16675277.37                 Z    =        -5103275.97
     XDOT =     -13599.784935                 XDOT =       -4083.693674
     YDOT =     -20379.173096  feet/sec       YDOT =       -6257.582563  meter/sec
     ZDOT =       5569.926466                 ZDOT =        1677.726706
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11504847.58                 X    =         3506677.54
     Y    =        9070106.36  feet           Y    =         2764568.42  meter
     Z    =      -16765553.53                 Z    =        -5110140.72
     XDOT =      -9091.883468                 XDOT =       -2771.206081
     YDOT =      21657.492728  feet/sec       YDOT =        6601.203783  meter/sec
     ZDOT =       5483.844424                 ZDOT =        1671.475780
  
  
    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   16207.51320209  .00016717  00000-0  10270-3 0  9038
    2 25544  51.6423 226.8128 0001869  72.5108 287.6249 15.54873917 10941
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16207.51320209   =   yrday.fracday
    Element set:     903
    Inclination:       51.6423  deg
    RA of node:       226.8128  deg
    Eccentricity:     .0001869     
    Arg of perigee:    72.5108  deg
    Mean anomaly:     287.6249  deg
    Mean motion:   15.54873917  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1094
    Checksum:              313
 
 
    Coasting Arc #5 (Orbit 1109)
    ---------------------------------------
 
    Vector Time (GMT): 2016/208/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5333086.24                 A    =         6779489.18  meter
     Y    =         200420.74  meter          E    =           .0012195
     Z    =        4172773.44                 I    =           51.38907
     XDOT =       2660.374353                 Wp   =           74.93222
     YDOT =       6182.631879  meter/sec      RA   =          220.79111  deg
     ZDOT =      -3684.962036                 TA   =           53.04407
                                              MA   =           52.93246
                                              Ha   =            220.353  n.mi
                                              Hp   =            212.666
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17497002.09                 X    =         5310179.34
     Y    =         657548.35  feet           Y    =          259930.68  meter
     Z    =       13690201.56                 Z    =         4198624.40
     XDOT =       8728.262312                 XDOT =        2608.940698
     YDOT =      20284.225324  feet/sec       YDOT =        6212.094476  meter/sec
     ZDOT =     -12089.770460                 ZDOT =       -3672.163464
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9126247.73                 X    =        -2781680.31
     Y    =      -14838844.66  feet           Y    =        -4522879.85  meter
     Z    =       13802875.14                 Z    =         4207116.34
     XDOT =      10887.079581                 XDOT =        3318.381856
     YDOT =     -17927.325571  feet/sec       YDOT =       -5464.248834  meter/sec
     ZDOT =     -12035.008939                 ZDOT =       -3668.270725
  
  
    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   16208.54152585  .00016717  00000-0  10270-3 0  9043
    2 25544  51.6405 221.6809 0002042  75.1654 284.9726 15.54926265 11103
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16208.54152585   =   yrday.fracday
    Element set:     904
    Inclination:       51.6405  deg
    RA of node:       221.6809  deg
    Eccentricity:     .0002042     
    Arg of perigee:    75.1654  deg
    Mean anomaly:     284.9726  deg
    Mean motion:   15.54926265  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1110
    Checksum:              300
 
 
    Coasting Arc #6 (Orbit 1124)
    ---------------------------------------
 
    Vector Time (GMT): 2016/209/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5993584.87                 A    =         6783803.49  meter
     Y    =       -1649700.62  meter          E    =           .0006710
     Z    =       -2716937.59                 I    =           51.42851
     XDOT =       -780.181405                 Wp   =           65.11031
     YDOT =      -5624.136988  meter/sec      RA   =          215.78731  deg
     ZDOT =       5148.787156                 TA   =          264.07730
                                              MA   =          264.15379
                                              Ha   =            220.447  n.mi
                                              Hp   =            212.619
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19663992.36                 X    =        -5961494.42
     Y    =       -5412403.62  feet           Y    =        -1716545.35  meter
     Z    =       -8913837.23                 Z    =        -2745974.87
     XDOT =      -2559.650279                 XDOT =        -742.243332
     YDOT =     -18451.893006  feet/sec       YDOT =       -5632.649592  meter/sec
     ZDOT =      16892.346312                 ZDOT =        5145.089161
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6726073.40                 X    =         2050107.17
     Y    =       19195270.40  feet           Y    =         5850718.42  meter
     Z    =       -9040173.32                 Z    =        -2755444.83
     XDOT =     -12239.764867                 XDOT =       -3730.680331
     YDOT =      12217.823980  feet/sec       YDOT =        3723.992749  meter/sec
     ZDOT =      16877.161791                 ZDOT =        5144.158914
  
  
    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   16209.50557597  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6406 216.8705 0002026  80.3441 279.7941 15.54920077 11251
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16209.50557597   =   yrday.fracday
    Element set:     905
    Inclination:       51.6406  deg
    RA of node:       216.8705  deg
    Eccentricity:     .0002026     
    Arg of perigee:    80.3441  deg
    Mean anomaly:     279.7941  deg
    Mean motion:   15.54920077  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1125
    Checksum:              308
 
 
    Coasting Arc #7 (Orbit 1140)
    ---------------------------------------
 
    Vector Time (GMT): 2016/210/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6094315.88                 A    =         6786690.11  meter
     Y    =        2849057.00  meter          E    =           .0014970
     Z    =         844802.88                 I    =           51.46395
     XDOT =      -1357.997286                 Wp   =          120.25860
     YDOT =       4682.128854  meter/sec      RA   =          210.79597  deg
     ZDOT =      -5922.681179                 TA   =           50.57580
                                              MA   =           50.44338
                                              Ha   =            220.488  n.mi
                                              Hp   =            212.636
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19994474.68                 X    =         6057900.41
     Y    =        9347299.87  feet           Y    =         2917004.05  meter
     Z    =        2771662.98                 Z    =          874319.05
     XDOT =      -4455.371673                 XDOT =       -1381.483477
     YDOT =      15361.315139  feet/sec       YDOT =        4666.811857  meter/sec
     ZDOT =     -19431.368697                 ZDOT =       -5929.334708
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4077665.35                 X    =        -1242872.40
     Y    =      -21674786.05  feet           Y    =        -6606474.79  meter
     Z    =        2899903.99                 Z    =          883890.74
     XDOT =      13416.293477                 XDOT =        4089.286252
     YDOT =      -5157.580608  feet/sec       YDOT =       -1572.030569  meter/sec
     ZDOT =     -19461.162794                 ZDOT =       -5931.762420
  
  
    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   16210.53388975  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6398 211.7377 0002067  80.3383 279.8003 15.54923549 11415
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16210.53388975   =   yrday.fracday
    Element set:     906
    Inclination:       51.6398  deg
    RA of node:       211.7377  deg
    Eccentricity:     .0002067     
    Arg of perigee:    80.3383  deg
    Mean anomaly:     279.8003  deg
    Mean motion:   15.54923549  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1141
    Checksum:              320
 
 
    Coasting Arc #8 (Orbit 1156)
    ---------------------------------------
 
    Vector Time (GMT): 2016/211/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5585353.95                 A    =         6786401.47  meter
     Y    =       -3679833.04  meter          E    =           .0015297
     Z    =        1106817.30                 I    =           51.49058
     XDOT =       3482.243357                 Wp   =           60.86290
     YDOT =      -3503.754922  meter/sec      RA   =          205.81213  deg
     ZDOT =       5869.537871                 TA   =          311.17947
                                              MA   =          311.31131
                                              Ha   =            220.383  n.mi
                                              Hp   =            212.662
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18324652.08                 X    =        -5549166.41
     Y    =      -12072943.06  feet           Y    =        -3742089.94  meter
     Z    =        3631290.36                 Z    =         1079772.95
     XDOT =      11424.682930                 XDOT =        3492.653022
     YDOT =     -11495.258930  feet/sec       YDOT =       -3464.756370  meter/sec
     ZDOT =      19257.014013                 ZDOT =        5886.478603
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1291924.95                 X    =          393778.73
     Y    =       21925286.66  feet           Y    =         6682827.37  meter
     Z    =        3513948.29                 Z    =         1071051.44
     XDOT =     -14370.195392                 XDOT =       -4380.035556
     YDOT =      -2280.861070  feet/sec       YDOT =        -695.206454  meter/sec
     ZDOT =      19331.480447                 ZDOT =        5892.235240
  
  
    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   16211.56219533  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6389 206.6064 0001928  88.5728 271.5646 15.54970062 11570
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16211.56219533   =   yrday.fracday
    Element set:     907
    Inclination:       51.6389  deg
    RA of node:       206.6064  deg
    Eccentricity:     .0001928     
    Arg of perigee:    88.5728  deg
    Mean anomaly:     271.5646  deg
    Mean motion:   15.54970062  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1157
    Checksum:              323
 
 
    Coasting Arc #9 (Orbit 1171)
    ---------------------------------------
 
    Vector Time (GMT): 2016/212/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4440170.65                 A    =         6783392.22  meter
     Y    =        4197649.92  meter          E    =           .0006415
     Z    =       -2949030.76                 I    =           51.50856
     XDOT =      -5385.256222                 Wp   =          106.20064
     YDOT =       2197.762310  meter/sec      RA   =          200.82326  deg
     ZDOT =      -4990.736142                 TA   =          107.53294
                                              MA   =          107.46283
                                              Ha   =            220.502  n.mi
                                              Hp   =            212.725
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14567489.01                 X    =         4407226.39
     Y    =       13771817.33  feet           Y    =         4247118.90  meter
     Z    =       -9675297.77                 Z    =        -2927541.52
     XDOT =     -17668.163459                 XDOT =       -5385.189407
     YDOT =       7210.506266  feet/sec       YDOT =        2137.541529  meter/sec
     ZDOT =     -16373.806241                 ZDOT =       -5016.895679
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1948623.65                 X    =          593940.49
     Y    =      -19996734.16  feet           Y    =        -6095004.57  meter
     Z    =       -9582252.59                 Z    =        -2920670.59
     XDOT =      14985.759127                 XDOT =        4567.659382
     YDOT =       9344.226132  feet/sec       YDOT =        2848.120125  meter/sec
     ZDOT =     -16488.278613                 ZDOT =       -5025.627321
  
  
    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   16212.52623142  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6380 201.7943 0002011  85.7549 274.3834 15.54925293 11720
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16212.52623142   =   yrday.fracday
    Element set:     908
    Inclination:       51.6380  deg
    RA of node:       201.7943  deg
    Eccentricity:     .0002011     
    Arg of perigee:    85.7549  deg
    Mean anomaly:     274.3834  deg
    Mean motion:   15.54925293  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1172
    Checksum:              296
 
 
    Coasting Arc #10 (Orbit 1187)
    ---------------------------------------
 
    Vector Time (GMT): 2016/213/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2789267.68                 A    =         6778937.40  meter
     Y    =       -4382132.95  meter          E    =           .0011392
     Z    =        4347922.00                 I    =           51.52481
     XDOT =       6801.122710                 Wp   =          105.70188
     YDOT =       -910.007968  meter/sec      RA   =          195.82488  deg
     ZDOT =       3435.348609                 TA   =          309.36906
                                              MA   =          309.46993
                                              Ha   =            220.406  n.mi
                                              Hp   =            212.705
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9151140.70                 X    =        -2761178.21
     Y    =      -14377076.62  feet           Y    =        -4413167.65  meter
     Z    =       14264835.97                 Z    =         4334440.60
     XDOT =      22313.394717                 XDOT =        6794.106037
     YDOT =      -2985.590447  feet/sec       YDOT =        -833.992746  meter/sec
     ZDOT =      11270.828770                 ZDOT =        3468.369061
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5443507.28                 X    =        -1659181.02
     Y    =       16200804.09  feet           Y    =         4938005.09  meter
     Z    =       14206738.85                 Z    =         4330214.00
     XDOT =     -15050.041733                 XDOT =       -4587.252720
     YDOT =     -15097.269281  feet/sec       YDOT =       -4601.647677  meter/sec
     ZDOT =      11415.037864                 ZDOT =        3479.303541
  
  
    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   16213.55452702  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6383 196.6623 0001802  89.4110 270.7250 15.54962004 11882
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16213.55452702   =   yrday.fracday
    Element set:     909
    Inclination:       51.6383  deg
    RA of node:       196.6623  deg
    Eccentricity:     .0001802     
    Arg of perigee:    89.4110  deg
    Mean anomaly:     270.7250  deg
    Mean motion:   15.54962004  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1188
    Checksum:              295
 
 
    Coasting Arc #11 (Orbit 1202)
    ---------------------------------------
 
    Vector Time (GMT): 2016/214/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         760988.04                 A    =         6775665.47  meter
     Y    =        4327099.12  meter          E    =           .0015770
     Z    =       -5172164.98                 I    =           51.54519
     XDOT =      -7525.861898                 Wp   =           80.83144
     YDOT =       -322.957123  meter/sec      RA   =          190.81430  deg
     ZDOT =      -1378.619843                 TA   =          175.88453
                                              MA   =          175.87154
                                              Ha   =            220.441  n.mi
                                              Hp   =            212.667
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2496679.92                 X    =          737668.38
     Y    =       14196519.41  feet           Y    =         4335478.90  meter
     Z    =      -16969045.21                 Z    =        -5168524.76
     XDOT =     -24691.147958                 XDOT =       -7514.994578
     YDOT =      -1059.570613  feet/sec       YDOT =        -407.055494  meter/sec
     ZDOT =      -4523.030981                 ZDOT =       -1415.151440
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9261902.77                 X    =         2823027.96
     Y    =      -11068271.52  feet           Y    =        -3373609.16  meter
     Z    =      -16953866.58                 Z    =        -5167538.53
     XDOT =      14121.160405                 XDOT =        4304.129692
     YDOT =      18983.077969  feet/sec       YDOT =        5786.042165  meter/sec
     ZDOT =      -4682.380587                 ZDOT =       -1427.189603
  
  
    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   16214.51854995  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6385 191.8500 0001974  89.1313 271.0066 15.54942016 12035
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16214.51854995   =   yrday.fracday
    Element set:     910
    Inclination:       51.6385  deg
    RA of node:       191.8500  deg
    Eccentricity:     .0001974     
    Arg of perigee:    89.1313  deg
    Mean anomaly:     271.0066  deg
    Mean motion:   15.54942016  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1203
    Checksum:              297
 
 
    Coasting Arc #12 (Orbit 1218)
    ---------------------------------------
 
    Vector Time (GMT): 2016/215/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1390652.45                 A    =         6775171.82  meter
     Y    =       -4045131.89  meter          E    =           .0004937
     Z    =        5250249.32                 I    =           51.57537
     XDOT =       7485.834366                 Wp   =           72.54504
     YDOT =       1449.399040  meter/sec      RA   =          185.80083  deg
     ZDOT =       -863.968398                 TA   =           25.73003
                                              MA   =           25.70547
                                              Ha   =            220.342  n.mi
                                              Hp   =            212.693
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4562508.03                 X    =         1410279.93
     Y    =      -13271430.08  feet           Y    =        -4029471.15  meter
     Z    =       17225227.44                 Z    =         5257052.12
     XDOT =      24559.824037                 XDOT =        7473.267149
     YDOT =       4755.246195  feet/sec       YDOT =        1533.040407  meter/sec
     ZDOT =      -2834.541988                 ZDOT =        -827.635402
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12966643.71                 X    =        -3952233.00
     Y    =        5269465.24  feet           Y    =         1606133.00  meter
     Z    =       17255569.63                 Z    =         5259497.62
     XDOT =     -12022.349974                 XDOT =       -3664.412272
     YDOT =     -20797.179152  feet/sec       YDOT =       -6338.980206  meter/sec
     ZDOT =      -2676.218209                 ZDOT =        -815.711310
  
  
    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   16215.54683522  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6383 186.7180 0001861  92.4598 267.6768 15.54950847 12195
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16215.54683522   =   yrday.fracday
    Element set:     911
    Inclination:       51.6383  deg
    RA of node:       186.7180  deg
    Eccentricity:     .0001861     
    Arg of perigee:    92.4598  deg
    Mean anomaly:     267.6768  deg
    Mean motion:   15.54950847  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1219
    Checksum:              338
 
 
    Coasting Arc #13 (Orbit 1233)
    ---------------------------------------
 
    Vector Time (GMT): 2016/216/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3423043.88                 A    =         6777828.44  meter
     Y    =        3609104.73  meter          E    =           .0012175
     Z    =       -4615803.88                 I    =           51.61752
     XDOT =      -6612.197230                 Wp   =          107.99894
     YDOT =      -2456.595704  meter/sec      RA   =          180.79317  deg
     ZDOT =       2985.545182                 TA   =          191.80434
                                              MA   =          191.83290
                                              Ha   =            220.368  n.mi
                                              Hp   =            212.607
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11230458.93                 X    =        -3440726.34
     Y    =       11840894.79  feet           Y    =         3570727.19  meter
     Z    =      -15143713.50                 Z    =        -4632474.65
     XDOT =     -21693.560466                 XDOT =       -6598.737675
     YDOT =      -8059.697192  feet/sec       YDOT =       -2530.462514  meter/sec
     ZDOT =       9795.095740                 ZDOT =        2953.458186
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16244981.72                 X    =         4951470.43
     Y    =         451513.85  feet           Y    =          137621.42  meter
     Z    =      -15217054.91                 Z    =        -4638158.34
     XDOT =       8468.096957                 XDOT =        2581.075952
     YDOT =      20428.667795  feet/sec       YDOT =        6226.657944  meter/sec
     ZDOT =       9655.443698                 ZDOT =        2942.979239
  
  
    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   16216.51084659  .00016717  00000-0  10270-3 0  9124
    2 25544  51.6393 181.9066 0001840  94.6087 265.5277 15.54951129 12343
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16216.51084659   =   yrday.fracday
    Element set:     912
    Inclination:       51.6393  deg
    RA of node:       181.9066  deg
    Eccentricity:     .0001840     
    Arg of perigee:    94.6087  deg
    Mean anomaly:     265.5277  deg
    Mean motion:   15.54951129  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1234
    Checksum:              321
 
 
    Coasting Arc #14 (Orbit 1243)
    ---------------------------------------
 
    Vector Time (GMT): 2016/217/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3041926.22                 A    =         6777065.68  meter
     Y    =       -3686410.68  meter          E    =           .0009292
     Z    =        4799425.44                 I    =           51.63829
     XDOT =       6854.841810                 Wp   =          117.82220
     YDOT =      -2296.835915  meter/sec      RA   =          177.83376  deg
     ZDOT =       2572.433605                 TA   =          306.82359
                                              MA   =          306.90880
                                              Ha   =            220.342  n.mi
                                              Hp   =            212.666
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9980072.91                 X    =        -3023790.77
     Y    =      -12094523.22  feet           Y    =        -3720326.16  meter
     Z    =       15746146.46                 Z    =         4784692.89
     XDOT =      22489.638483                 XDOT =        6867.520662
     YDOT =      -7535.550902  feet/sec       YDOT =       -2220.109621  meter/sec
     ZDOT =       8439.742797                 ZDOT =        2605.762716
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7465065.18                 X    =        -2275351.87
     Y    =      -13861985.63  feet           Y    =        -4225133.22  meter
     Z    =       15682430.67                 Z    =         4780004.87
     XDOT =      22476.275203                 XDOT =        6850.768682
     YDOT =      -2360.992157  feet/sec       YDOT =        -719.630409  meter/sec
     ZDOT =       8585.589354                 ZDOT =        2616.887635
  
  
    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   16217.15351617  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6430 178.6957 0001842 112.1919 247.9430 15.55005516 12446
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16217.15351617   =   yrday.fracday
    Element set:     913
    Inclination:       51.6430  deg
    RA of node:       178.6957  deg
    Eccentricity:     .0001842     
    Arg of perigee:   112.1919  deg
    Mean anomaly:     247.9430  deg
    Mean motion:   15.55005516  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1244
    Checksum:              297
 
 
    Coasting Arc #15 (Orbit 1258)
    ---------------------------------------
 
    Vector Time (GMT): 2016/218/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         949973.99                 A    =         6774927.18  meter
     Y    =        4114445.05  meter          E    =           .0016428
     Z    =       -5312173.05                 I    =           51.66318
     XDOT =      -7545.130693                 Wp   =           89.87366
     YDOT =       1252.371973  meter/sec      RA   =          172.82907  deg
     ZDOT =       -380.273596                 TA   =          176.50232
                                              MA   =          176.49082
                                              Ha   =            220.273  n.mi
                                              Hp   =            212.723
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3116712.55                 X    =          929698.32
     Y    =       13498835.46  feet           Y    =         4124954.86  meter
     Z    =      -17428389.26                 Z    =        -5307607.70
     XDOT =     -24754.365790                 XDOT =       -7556.727100
     YDOT =       4108.831933  feet/sec       YDOT =        1167.932436  meter/sec
     ZDOT =      -1247.616786                 ZDOT =        -416.953353
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         708854.98                 X    =          216059.00
     Y    =       13860065.46  feet           Y    =         4224547.95  meter
     Z    =      -17409115.95                 Z    =        -5306298.54
     XDOT =     -24069.246717                 XDOT =       -7336.306399
     YDOT =       -533.417279  feet/sec       YDOT =        -162.585587  meter/sec
     ZDOT =      -1407.938148                 ZDOT =        -429.139548
  
  
    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   16218.11751845  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6430 173.8854 0001800 112.5529 247.5814 15.54984580 12598
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16218.11751845   =   yrday.fracday
    Element set:     914
    Inclination:       51.6430  deg
    RA of node:       173.8854  deg
    Eccentricity:     .0001800     
    Arg of perigee:   112.5529  deg
    Mean anomaly:     247.5814  deg
    Mean motion:   15.54984580  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1259
    Checksum:              314
 
 
    Coasting Arc #16 (Orbit 1274)
    ---------------------------------------
 
    Vector Time (GMT): 2016/219/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1211397.60                 A    =         6775837.66  meter
     Y    =       -4343751.06  meter          E    =           .0006526
     Z    =        5052658.40                 I    =           51.69885
     XDOT =       7442.962965                 Wp   =           69.66439
     YDOT =        -98.903956  meter/sec      RA   =          167.82349  deg
     ZDOT =      -1865.343864                 TA   =           38.40294
                                              MA   =           38.35651
                                              Ha   =            220.173  n.mi
                                              Hp   =            212.668
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3974401.58                 X    =         1235337.30
     Y    =      -14251151.79  feet           Y    =        -4330070.43  meter
     Z    =       16576963.24                 Z    =         5058601.20
     XDOT =      24419.169834                 XDOT =        7452.576631
     YDOT =       -324.488046  feet/sec       YDOT =         -15.618061  meter/sec
     ZDOT =      -6119.894568                 ZDOT =       -1829.165127
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6175845.49                 X    =         1882397.70
     Y    =      -13411424.60  feet           Y    =        -4087802.22  meter
     Z    =       16603599.86                 Z    =         5060777.24
     XDOT =      23195.721327                 XDOT =        7070.055861
     YDOT =       3283.549034  feet/sec       YDOT =        1000.825745  meter/sec
     ZDOT =      -5961.928322                 ZDOT =       -1817.195753
  
  
    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   16219.14578055  .00016717  00000-0  10270-3 0  9157
    2 25544  51.6432 168.7530 0001789 116.0015 244.1323 15.55022182 12757
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16219.14578055   =   yrday.fracday
    Element set:     915
    Inclination:       51.6432  deg
    RA of node:       168.7530  deg
    Eccentricity:     .0001789     
    Arg of perigee:   116.0015  deg
    Mean anomaly:     244.1323  deg
    Mean motion:   15.55022182  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1275
    Checksum:              288
 
             

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