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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15282.5994
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   101.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.975
   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 
   ------------------------------------------------------------------------
   124/02:16:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.0  
   000/00:00:00.000           0.0               0.0              213.6  
   
   132/13:26:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.9  
   000/00:00:00.000           0.0               0.0              213.5  
   
   135/07:32:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.0  
   000/00:00:00.000           0.0               0.0              213.2  
   
 
 
    Coasting Arc #1 (Orbit 3739)
    ---------------------------------------
 
    Vector Time (GMT): 2016/120/11:18:49.007
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         469015.10                 A    =         6784183.68  meter
     Y    =       -5942563.91  meter          E    =           .0006240
     Z    =       -3242781.01                 I    =           51.32926
     XDOT =       5636.199934                 Wp   =           77.56290
     YDOT =      -2133.220316  meter/sec      RA   =          300.32133  deg
     ZDOT =       4733.469161                 TA   =          244.69864
                                              MA   =          244.76330
                                              Ha   =            221.198  n.mi
                                              Hp   =            213.712
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1538763.44                 X    =          551183.63
     Y    =      -19496600.75  feet           Y    =        -5936859.67  meter
     Z    =      -10639045.31                 Z    =        -3240303.00
     XDOT =      18491.469599                 XDOT =        5636.641903
     YDOT =      -6998.754319  feet/sec       YDOT =       -2070.190065  meter/sec
     ZDOT =      15529.754464                 ZDOT =        4760.849720
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7325443.05                 X    =        -2232795.04
     Y    =      -18140461.19  feet           Y    =        -5529212.57  meter
     Z    =      -10627138.41                 Z    =        -3239151.79
     XDOT =      11962.775047                 XDOT =        3646.253834
     YDOT =     -13980.985634  feet/sec       YDOT =       -4261.404421  meter/sec
     ZDOT =      15649.061757                 ZDOT =        4769.834023
  
  
    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   16120.47810519  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6400 301.0109 0001680  67.2165 292.9165 15.54367588 37404
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16120.47810519   =   yrday.fracday
    Element set:     900
    Inclination:       51.6400  deg
    RA of node:       301.0109  deg
    Eccentricity:     .0001680     
    Arg of perigee:    67.2165  deg
    Mean anomaly:     292.9165  deg
    Mean motion:   15.54367588  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3740
    Checksum:              290
 
 
    Coasting Arc #2 (Orbit 3755)
    ---------------------------------------
 
    Vector Time (GMT): 2016/121/11:18:49.007
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1571348.66                 A    =         6787342.80  meter
     Y    =        6389335.76  meter          E    =           .0014882
     Z    =        1639609.02                 I    =           51.32497
     XDOT =      -5137.916919                 Wp   =          111.27469
     YDOT =        206.405434  meter/sec      RA   =          295.32220  deg
     ZDOT =      -5691.859800                 TA   =           50.68313
                                              MA   =           50.55129
                                              Ha   =            221.053  n.mi
                                              Hp   =            213.687
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5155343.36                 X    =        -1650643.59
     Y    =       20962387.65  feet           Y    =         6371320.56  meter
     Z    =        5379294.69                 Z    =         1631783.03
     XDOT =     -16856.682805                 XDOT =       -5112.194332
     YDOT =        677.183183  feet/sec       YDOT =         149.093543  meter/sec
     ZDOT =     -18674.080709                 ZDOT =       -5716.756220
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5144827.44                 X    =         1568143.40
     Y    =       20973972.38  feet           Y    =         6392866.78  meter
     Z    =        5344090.73                 Z    =         1628878.86
     XDOT =     -12976.475583                 XDOT =       -3955.229758
     YDOT =       7999.421457  feet/sec       YDOT =        2438.223660  meter/sec
     ZDOT =     -18782.229043                 ZDOT =       -5724.823412
  
  
    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   16121.50677514  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6399 295.8814 0001595  60.7774 299.3538 15.54425857 37569
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16121.50677514   =   yrday.fracday
    Element set:     901
    Inclination:       51.6399  deg
    RA of node:       295.8814  deg
    Eccentricity:     .0001595     
    Arg of perigee:    60.7774  deg
    Mean anomaly:     299.3538  deg
    Mean motion:   15.54425857  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3756
    Checksum:              347
 
 
    Coasting Arc #3 (Orbit 3771)
    ---------------------------------------
 
    Vector Time (GMT): 2016/122/11:18:49.007
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2442025.73                 A    =         6788574.53  meter
     Y    =       -6326441.63  meter          E    =           .0013810
     Z    =         115166.96                 I    =           51.31526
     XDOT =       4433.371861                 Wp   =           49.91274
     YDOT =       1828.771612  meter/sec      RA   =          290.32759  deg
     ZDOT =       5985.360405                 TA   =          311.33371
                                              MA   =          311.45246
                                              Ha   =            221.172  n.mi
                                              Hp   =            213.661
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8011895.43                 X    =         2512028.64
     Y    =      -20756042.08  feet           Y    =        -6298741.86  meter
     Z    =         377844.36                 Z    =          127200.03
     XDOT =      14545.183270                 XDOT =        4383.518048
     YDOT =       5999.906865  feet/sec       YDOT =        1878.069963  meter/sec
     ZDOT =      19637.009204                 ZDOT =        6006.775640
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2931887.17                 X    =         -893639.21
     Y    =      -22053674.12  feet           Y    =        -6721959.87  meter
     Z    =         431292.16                 Z    =          131457.85
     XDOT =      13921.900948                 XDOT =        4243.395409
     YDOT =      -1438.676289  feet/sec       YDOT =        -438.508533  meter/sec
     ZDOT =      19729.655591                 ZDOT =        6013.599024
  
  
    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   16122.53544190  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6393 290.7510 0001636  76.1971 283.9364 15.54386374 37720
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16122.53544190   =   yrday.fracday
    Element set:     902
    Inclination:       51.6393  deg
    RA of node:       290.7510  deg
    Eccentricity:     .0001636     
    Arg of perigee:    76.1971  deg
    Mean anomaly:     283.9364  deg
    Mean motion:   15.54386374  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3772
    Checksum:              316
 
 
    Coasting Arc #4 (Orbit 3786)
    ---------------------------------------
 
    Vector Time (GMT): 2016/123/11:18:49.007
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3143299.46                 A    =         6786890.42  meter
     Y    =        5704947.98  meter          E    =           .0007916
     Z    =       -1900976.73                 I    =           51.30010
     XDOT =      -3589.145674                 Wp   =          128.06674
     YDOT =      -3831.710699  meter/sec      RA   =          285.33209  deg
     ZDOT =      -5585.185512                 TA   =           72.97092
                                              MA   =           72.88420
                                              Ha   =            221.168  n.mi
                                              Hp   =            213.508
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10312662.25                 X    =        -3197625.77
     Y    =       18717020.92  feet           Y    =         5669493.68  meter
     Z    =       -6236800.30                 Z    =        -1916378.44
     XDOT =     -11775.412316                 XDOT =       -3518.901072
     YDOT =     -12571.229329  feet/sec       YDOT =       -3871.454385  meter/sec
     ZDOT =     -18324.099448                 ZDOT =       -5602.450084
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         335031.69                 X    =          102117.66
     Y    =       21347446.57  feet           Y    =         6506701.72  meter
     Z    =       -6304746.75                 Z    =        -1921686.81
     XDOT =     -14794.826901                 XDOT =       -4509.463239
     YDOT =      -5181.723633  feet/sec       YDOT =       -1579.389363  meter/sec
     ZDOT =     -18398.350571                 ZDOT =       -5607.817254
  
  
    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   16123.49980749  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6396 285.9415 0001861  74.3744 285.7614 15.54427235 37877
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16123.49980749   =   yrday.fracday
    Element set:     903
    Inclination:       51.6396  deg
    RA of node:       285.9415  deg
    Eccentricity:     .0001861     
    Arg of perigee:    74.3744  deg
    Mean anomaly:     285.7614  deg
    Mean motion:   15.54427235  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3787
    Checksum:              344
 
 
    Coasting Arc #5 (Orbit 3796)
    ---------------------------------------
 
    Vector Time (GMT): 2016/124/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4149651.46                 A    =         6776500.79  meter
     Y    =         865029.97  meter          E    =           .0004129
     Z    =        5283517.45                 I    =           51.26142
     XDOT =      -1599.043589                 Wp   =           81.48932
     YDOT =       7504.091398  meter/sec      RA   =          282.19622  deg
     ZDOT =         27.876616                 TA   =            8.24719
                                              MA   =            8.24040
                                              Ha   =            221.021  n.mi
                                              Hp   =            213.592
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13614342.05                 X    =         4114004.70
     Y    =        2838024.83  feet           Y    =          911235.06  meter
     Z    =       17334374.85                 Z    =         5303589.04
     XDOT =      -5246.206001                 XDOT =       -1682.972783
     YDOT =      24619.722436  feet/sec       YDOT =        7485.740554  meter/sec
     ZDOT =         91.458713                 ZDOT =          19.904572
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6330029.44                 X    =        -1929392.97
     Y    =       12260172.00  feet           Y    =         3736900.43  meter
     Z    =       17421370.65                 Z    =         5310033.78
     XDOT =     -21442.115633                 XDOT =       -6535.556845
     YDOT =     -11146.829936  feet/sec       YDOT =       -3397.553765  meter/sec
     ZDOT =         55.446227                 ZDOT =          16.900010
  
  
    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   16124.14271543  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6408 282.7390 0001797  69.3939 290.7406 15.54418028 37972
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16124.14271543   =   yrday.fracday
    Element set:     904
    Inclination:       51.6408  deg
    RA of node:       282.7390  deg
    Eccentricity:     .0001797     
    Arg of perigee:    69.3939  deg
    Mean anomaly:     290.7406  deg
    Mean motion:   15.54418028  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3797
    Checksum:              328
 
 
    Coasting Arc #6 (Orbit 3811)
    ---------------------------------------
 
    Vector Time (GMT): 2016/125/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3696714.72                 A    =         6777843.43  meter
     Y    =       -2728492.98  meter          E    =           .0014369
     Z    =       -4995953.26                 I    =           51.25992
     XDOT =       2475.796748                 Wp   =          101.11537
     YDOT =      -6971.499703  meter/sec      RA   =          277.16730  deg
     ZDOT =       1977.610918                 TA   =          188.20774
                                              MA   =          188.23127
                                              Ha   =            221.174  n.mi
                                              Hp   =            213.453
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12128329.12                 X    =        -3641660.69
     Y    =       -8951748.63  feet           Y    =        -2769524.51  meter
     Z    =      -16390922.76                 Z    =        -5013777.42
     XDOT =       8122.692743                 XDOT =        2543.963253
     YDOT =     -22872.374355  feet/sec       YDOT =       -6943.432467  meter/sec
     ZDOT =       6488.224796                 ZDOT =        1989.803794
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11669372.72                 X    =         3556824.81
     Y    =       -9408999.31  feet           Y    =        -2867862.99  meter
     Z    =      -16467816.86                 Z    =        -5019390.58
     XDOT =      19446.717066                 XDOT =        5927.359362
     YDOT =      12679.985695  feet/sec       YDOT =        3864.859640  meter/sec
     ZDOT =       6542.454927                 ZDOT =        1994.140262
  
  
    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   16125.10707196  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6407 277.9293 0001778  74.2200 285.9149 15.54413351 38126
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16125.10707196   =   yrday.fracday
    Element set:     905
    Inclination:       51.6407  deg
    RA of node:       277.9293  deg
    Eccentricity:     .0001778     
    Arg of perigee:    74.2200  deg
    Mean anomaly:     285.9149  deg
    Mean motion:   15.54413351  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3812
    Checksum:              308
 
 
    Coasting Arc #7 (Orbit 3827)
    ---------------------------------------
 
    Vector Time (GMT): 2016/126/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3126458.93                 A    =         6781236.22  meter
     Y    =        4396289.88  meter          E    =           .0012204
     Z    =        4100674.11                 I    =           51.26931
     XDOT =      -3246.519894                 Wp   =           76.07542
     YDOT =       5839.098557  meter/sec      RA   =          272.14571  deg
     ZDOT =      -3772.450634                 TA   =           53.05214
                                              MA   =           52.94045
                                              Ha   =            221.062  n.mi
                                              Hp   =            213.559
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10257411.18                 X    =         3057146.44
     Y    =       14423523.24  feet           Y    =         4430864.62  meter
     Z    =       13453655.21                 Z    =         4115693.47
     XDOT =     -10651.311988                 XDOT =       -3293.247553
     YDOT =      19157.147498  feet/sec       YDOT =        5802.532416  meter/sec
     ZDOT =     -12376.806541                 ZDOT =       -3788.335424
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16395936.73                 X    =        -4997481.52
     Y    =        6533638.61  feet           Y    =         1991453.05  meter
     Z    =       13518068.30                 Z    =         4120307.22
     XDOT =     -15692.710581                 XDOT =       -4783.138185
     YDOT =     -13544.352597  feet/sec       YDOT =       -4128.318671  meter/sec
     ZDOT =     -12446.852123                 ZDOT =       -3793.800527
  
  
    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   16126.13570986  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6417 272.7994 0001736  74.7116 285.4228 15.54432508 38288
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16126.13570986   =   yrday.fracday
    Element set:     906
    Inclination:       51.6417  deg
    RA of node:       272.7994  deg
    Eccentricity:     .0001736     
    Arg of perigee:    74.7116  deg
    Mean anomaly:     285.4228  deg
    Mean motion:   15.54432508  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3828
    Checksum:              330
 
 
    Coasting Arc #8 (Orbit 3842)
    ---------------------------------------
 
    Vector Time (GMT): 2016/127/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2494077.29                 A    =         6785187.75  meter
     Y    =       -5678314.08  meter          E    =           .0006526
     Z    =       -2753212.54                 I    =           51.28214
     XDOT =       3892.138403                 Wp   =           63.55150
     YDOT =      -4181.091046  meter/sec      RA   =          267.13507  deg
     ZDOT =       5109.692901                 TA   =          265.11425
                                              MA   =          265.18876
                                              Ha   =            221.147  n.mi
                                              Hp   =            213.497
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8182668.28                 X    =        -2417021.38
     Y    =      -18629639.38  feet           Y    =        -5705773.70  meter
     Z    =       -9032849.53                 Z    =        -2765141.18
     XDOT =      12769.482948                 XDOT =        3913.781885
     YDOT =     -13717.490307  feet/sec       YDOT =       -4137.445485  meter/sec
     ZDOT =      16764.084320                 ZDOT =        5128.652984
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19945550.46                 X    =         6079403.78
     Y    =       -3908308.52  feet           Y    =        -1191252.44  meter
     Z    =       -9083613.58                 Z    =        -2768685.42
     XDOT =      10372.244866                 XDOT =        3161.460235
     YDOT =      13870.674633  feet/sec       YDOT =        4227.781628  meter/sec
     ZDOT =      16847.177901                 ZDOT =        5135.019824
  
  
    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   16127.10005055  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6415 267.9900 0001818  76.2190 283.9166 15.54433607 38431
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16127.10005055   =   yrday.fracday
    Element set:     907
    Inclination:       51.6415  deg
    RA of node:       267.9900  deg
    Eccentricity:     .0001818     
    Arg of perigee:    76.2190  deg
    Mean anomaly:     283.9166  deg
    Mean motion:   15.54433607  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3843
    Checksum:              302
 
 
    Coasting Arc #9 (Orbit 3858)
    ---------------------------------------
 
    Vector Time (GMT): 2016/128/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1737141.86                 A    =         6787952.77  meter
     Y    =        6471685.73  meter          E    =           .0014966
     Z    =        1042398.38                 I    =           51.29489
     XDOT =      -4449.245471                 Wp   =          118.96775
     YDOT =       2148.470212  meter/sec      RA   =          262.13545  deg
     ZDOT =      -5867.203663                 TA   =           49.67208
                                              MA   =           49.54143
                                              Ha   =            221.141  n.mi
                                              Hp   =            213.509
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5699284.31                 X    =         1659581.10
     Y    =       21232564.73  feet           Y    =         6490677.92  meter
     Z    =        3419942.18                 Z    =         1050648.87
     XDOT =     -14597.262043                 XDOT =       -4444.438531
     YDOT =       7048.786785  feet/sec       YDOT =        2098.742747  meter/sec
     ZDOT =     -19249.355850                 ZDOT =       -5888.805767
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21938209.76                 X    =        -6686766.34
     Y    =        1334303.56  feet           Y    =          406695.72  meter
     Z    =        3454596.59                 Z    =         1052961.04
     XDOT =      -3925.806639                 XDOT =       -1196.585864
     YDOT =     -13986.923267  feet/sec       YDOT =       -4263.214212  meter/sec
     ZDOT =     -19343.554382                 ZDOT =       -5895.915376
  
  
    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   16128.12867404  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6424 262.8603 0001789  80.9589 279.1766 15.54441261 38591
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16128.12867404   =   yrday.fracday
    Element set:     908
    Inclination:       51.6424  deg
    RA of node:       262.8603  deg
    Eccentricity:     .0001789     
    Arg of perigee:    80.9589  deg
    Mean anomaly:     279.1766  deg
    Mean motion:   15.54441261  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3859
    Checksum:              340
 
 
    Coasting Arc #10 (Orbit 3874)
    ---------------------------------------
 
    Vector Time (GMT): 2016/129/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -904366.79                 A    =         6788149.68  meter
     Y    =       -6678306.48  meter          E    =           .0014854
     Z    =         754785.02                 I    =           51.30118
     XDOT =       4872.331815                 Wp   =           56.22358
     YDOT =         18.352381  meter/sec      RA   =          257.14029  deg
     ZDOT =       5924.275973                 TA   =          311.97557
                                              MA   =          312.10201
                                              Ha   =            221.103  n.mi
                                              Hp   =            213.521
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2967082.65                 X    =         -833287.58
     Y    =      -21910454.34  feet           Y    =        -6688022.31  meter
     Z    =        2476328.82                 Z    =          750564.14
     XDOT =      15985.340602                 XDOT =        4842.986316
     YDOT =         60.211225  feet/sec       YDOT =          72.673732  meter/sec
     ZDOT =      19436.600961                 ZDOT =        5947.873738
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       22086880.10                 X    =         6732081.05
     Y    =        1061054.70  feet           Y    =          323409.47  meter
     Z    =        2459203.81                 Z    =          749565.32
     XDOT =      -2874.719469                 XDOT =        -876.214494
     YDOT =      13972.264711  feet/sec       YDOT =        4258.746284  meter/sec
     ZDOT =      19539.080051                 ZDOT =        5955.511600
  
  
    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   16129.15728903  .00016717  00000-0  10270-3 0  9090
    2 25544  51.6427 257.7305 0001738  80.6646 279.4703 15.54453629 38754
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16129.15728903   =   yrday.fracday
    Element set:     909
    Inclination:       51.6427  deg
    RA of node:       257.7305  deg
    Eccentricity:     .0001738     
    Arg of perigee:    80.6646  deg
    Mean anomaly:     279.4703  deg
    Mean motion:   15.54453629  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3875
    Checksum:              338
 
 
    Coasting Arc #11 (Orbit 3889)
    ---------------------------------------
 
    Vector Time (GMT): 2016/130/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -80088.82                 A    =         6785652.60  meter
     Y    =        6304378.04  meter          E    =           .0006610
     Z    =       -2508410.75                 I    =           51.30222
     XDOT =      -5130.232313                 Wp   =          119.51441
     YDOT =      -2156.583891  meter/sec      RA   =          252.14265  deg
     ZDOT =      -5270.035892                 TA   =           88.75767
                                              MA   =           88.68194
                                              Ha   =            221.082  n.mi
                                              Hp   =            213.476
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -262758.58                 X    =         -138395.02
     Y    =       20683654.99  feet           Y    =         6303156.56  meter
     Z    =       -8229694.07                 Z    =        -2508941.09
     XDOT =     -16831.470844                 XDOT =       -5080.135594
     YDOT =      -7075.406466  feet/sec       YDOT =       -2213.673169  meter/sec
     ZDOT =     -17290.144003                 ZDOT =       -5294.836109
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20363502.08                 X    =        -6206795.43
     Y    =       -3626824.94  feet           Y    =        -1105456.24  meter
     Z    =       -8233129.07                 Z    =        -2509457.74
     XDOT =       9479.764451                 XDOT =        2889.432205
     YDOT =     -13834.558053  feet/sec       YDOT =       -4216.773295  meter/sec
     ZDOT =     -17397.471177                 ZDOT =       -5302.749215
  
  
    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   16130.12160514  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6438 252.9215 0001737  83.8053 276.3298 15.54473355 38909
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16130.12160514   =   yrday.fracday
    Element set:     910
    Inclination:       51.6438  deg
    RA of node:       252.9215  deg
    Eccentricity:     .0001737     
    Arg of perigee:    83.8053  deg
    Mean anomaly:     276.3298  deg
    Mean motion:   15.54473355  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3890
    Checksum:              302
 
 
    Coasting Arc #12 (Orbit 3905)
    ---------------------------------------
 
    Vector Time (GMT): 2016/131/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1138668.93                 A    =         6781709.72  meter
     Y    =       -5401827.57  meter          E    =           .0012846
     Z    =        3929299.70                 I    =           51.29895
     XDOT =       5172.415156                 Wp   =           98.07233
     YDOT =       4011.696535  meter/sec      RA   =          247.13569  deg
     ZDOT =       4003.166423                 TA   =          309.91790
                                              MA   =          310.03073
                                              Ha   =            221.065  n.mi
                                              Hp   =            213.431
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3735790.45                 X    =         1179901.82
     Y    =      -17722531.40  feet           Y    =        -5388863.90  meter
     Z    =       12891403.22                 Z    =         3934930.97
     XDOT =      16969.865999                 XDOT =        5107.725058
     YDOT =      13161.734039  feet/sec       YDOT =        4069.175981  meter/sec
     ZDOT =      13133.748106                 ZDOT =        4028.136122
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16983290.33                 X    =         5176506.89
     Y    =        6241472.47  feet           Y    =         1902400.81  meter
     Z    =       12916826.13                 Z    =         3937048.61
     XDOT =     -15067.236762                 XDOT =       -4592.493765
     YDOT =      13506.785662  feet/sec       YDOT =        4116.868270  meter/sec
     ZDOT =      13241.494859                 ZDOT =        4036.007633
  
  
    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   16131.15020148  .00016717  00000-0  10270-3 0  9112
    2 25544  51.6429 247.7918 0001825  85.8193 274.3168 15.54485550 39068
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16131.15020148   =   yrday.fracday
    Element set:     911
    Inclination:       51.6429  deg
    RA of node:       247.7918  deg
    Eccentricity:     .0001825     
    Arg of perigee:    85.8193  deg
    Mean anomaly:     274.3168  deg
    Mean motion:   15.54485550  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3906
    Checksum:              314
 
 
    Coasting Arc #13 (Orbit 3920)
    ---------------------------------------
 
    Vector Time (GMT): 2016/132/02:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2293985.59                 A    =         6777888.29  meter
     Y    =        4081650.45  meter          E    =           .0013820
     Z    =       -4913612.15                 I    =           51.30044
     XDOT =      -4903.437885                 Wp   =           75.28271
     YDOT =      -5442.123004  meter/sec      RA   =          242.11780  deg
     ZDOT =      -2233.277865                 TA   =          172.78558
                                              MA   =          172.76567
                                              Ha   =            220.965  n.mi
                                              Hp   =            213.341
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7526199.45                 X    =        -2315588.74
     Y    =       13391241.63  feet           Y    =         4055877.05  meter
     Z    =      -16120774.78                 Z    =        -4924808.10
     XDOT =     -16087.394636                 XDOT =       -4831.369885
     YDOT =     -17854.734265  feet/sec       YDOT =       -5496.553431  meter/sec
     ZDOT =      -7327.027115                 ZDOT =       -2256.922974
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12299015.46                 X    =        -3748739.91
     Y    =       -9116438.24  feet           Y    =        -2778690.38  meter
     Z    =      -16170132.41                 Z    =        -4928656.36
     XDOT =      19142.493628                 XDOT =        5834.632058
     YDOT =     -12659.178943  feet/sec       YDOT =       -3858.517742  meter/sec
     ZDOT =      -7428.784928                 ZDOT =       -2264.293646
  
  
    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   16132.11450067  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6434 242.9830 0001644  86.8755 273.2586 15.54528648 39213
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16132.11450067   =   yrday.fracday
    Element set:     912
    Inclination:       51.6434  deg
    RA of node:       242.9830  deg
    Eccentricity:     .0001644     
    Arg of perigee:    86.8755  deg
    Mean anomaly:     273.2586  deg
    Mean motion:   15.54528648  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3921
    Checksum:              314
 
 
    Coasting Arc #14 (Orbit 3927)
    ---------------------------------------
 
    Vector Time (GMT): 2016/132/13:26:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4693657.24                 A    =         6785846.96  meter
     Y    =       -4291994.05  meter          E    =           .0006602
     Z    =       -2364249.57                 I    =           51.33348
     XDOT =       1981.951874                 Wp   =           57.48093
     YDOT =      -5110.605957  meter/sec      RA   =          239.74529  deg
     ZDOT =       5357.401595                 TA   =          276.01547
                                              MA   =          276.09071
                                              Ha   =            220.949  n.mi
                                              Hp   =            213.502
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15399137.92                 X    =        -4633829.66
     Y    =      -14081345.31  feet           Y    =        -4344147.02  meter
     Z    =       -7756724.32                 Z    =        -2386905.23
     XDOT =       6502.466778                 XDOT =        2012.928527
     YDOT =     -16767.079913  feet/sec       YDOT =       -5088.269514  meter/sec
     ZDOT =      17576.776888                 ZDOT =        5367.104474
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18412855.90                 X    =        -5612238.48
     Y    =        9739595.62  feet           Y    =         2968628.74  meter
     Z    =       -7854395.03                 Z    =        -2394019.61
     XDOT =     -12943.010903                 XDOT =       -3945.029723
     YDOT =     -10297.374205  feet/sec       YDOT =       -3138.639658  meter/sec
     ZDOT =      17619.827719                 ZDOT =        5370.523489
  
  
    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   16132.56450341  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6430 240.7356 0001516 100.4191 259.7132 15.54488691 39289
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16132.56450341   =   yrday.fracday
    Element set:     913
    Inclination:       51.6430  deg
    RA of node:       240.7356  deg
    Eccentricity:     .0001516     
    Arg of perigee:   100.4191  deg
    Mean anomaly:     259.7132  deg
    Mean motion:   15.54488691  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3928
    Checksum:              295
 
 
    Coasting Arc #15 (Orbit 3943)
    ---------------------------------------
 
    Vector Time (GMT): 2016/133/13:26:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4267648.80                 A    =         6788033.31  meter
     Y    =        5238277.87  meter          E    =           .0014675
     Z    =         577882.04                 I    =           51.35721
     XDOT =      -3400.161543                 Wp   =          126.03058
     YDOT =       3437.805431  meter/sec      RA   =          234.75112  deg
     ZDOT =      -5954.637088                 TA   =           47.70571
                                              MA   =           47.58141
                                              Ha   =            220.980  n.mi
                                              Hp   =            213.416
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14001472.44                 X    =         4205948.77
     Y    =       17185951.01  feet           Y    =         5285656.55  meter
     Z    =        1895938.44                 Z    =          598463.63
     XDOT =     -11155.385639                 XDOT =       -3409.426035
     YDOT =      11278.889210  feet/sec       YDOT =        3399.730971  meter/sec
     ZDOT =     -19536.210918                 ZDOT =       -5971.176683
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20750687.19                 X    =         6324809.46
     Y    =       -7775838.35  feet           Y    =        -2370075.53  meter
     Z    =        1984450.59                 Z    =          604860.54
     XDOT =       6602.570663                 XDOT =        2012.463538
     YDOT =      12537.333941  feet/sec       YDOT =        3821.379385  meter/sec
     ZDOT =     -19608.670036                 ZDOT =       -5976.722627
  
  
    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   16133.59307640  .00016717  00000-0  10270-3 0  9140
    2 25544  51.6422 235.6057 0001705 104.2392 255.8950 15.54521796 39443
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16133.59307640   =   yrday.fracday
    Element set:     914
    Inclination:       51.6422  deg
    RA of node:       235.6057  deg
    Eccentricity:     .0001705     
    Arg of perigee:   104.2392  deg
    Mean anomaly:     255.8950  deg
    Mean motion:   15.54521796  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3944
    Checksum:              307
 
 
    Coasting Arc #16 (Orbit 3959)
    ---------------------------------------
 
    Vector Time (GMT): 2016/134/13:26:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3500049.42                 A    =         6787543.82  meter
     Y    =       -5673298.11  meter          E    =           .0014965
     Z    =        1242929.01                 I    =           51.37458
     XDOT =       4720.165124                 Wp   =           63.29155
     YDOT =      -1625.674576  meter/sec      RA   =          229.76028  deg
     ZDOT =       5823.781476                 TA   =          310.27777
                                              MA   =          310.40851
                                              Ha   =            220.972  n.mi
                                              Hp   =            213.453
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11483101.76                 X    =        -3442386.69
     Y    =      -18613182.78  feet           Y    =        -5712115.61  meter
     Z    =        4077851.08                 Z    =         1226066.50
     XDOT =      15486.106051                 XDOT =        4709.703459
     YDOT =      -5333.578006  feet/sec       YDOT =       -1572.949167  meter/sec
     ZDOT =      19106.894606                 ZDOT =        5846.685518
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21223114.73                 X    =        -6468805.37
     Y    =        5336289.58  feet           Y    =         1626501.06  meter
     Z    =        4005556.59                 Z    =         1220893.65
     XDOT =        -43.152117                 XDOT =         -13.152765
     YDOT =     -14708.334805  feet/sec       YDOT =       -4483.100449  meter/sec
     ZDOT =      19206.697260                 ZDOT =        5854.201325
  
  
    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   16134.62164042  .00016717  00000-0  10270-3 0  9153
    2 25544  51.6419 230.4755 0001681 104.0276 256.1064 15.54526688 39602
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16134.62164042   =   yrday.fracday
    Element set:     915
    Inclination:       51.6419  deg
    RA of node:       230.4755  deg
    Eccentricity:     .0001681     
    Arg of perigee:   104.0276  deg
    Mean anomaly:     256.1064  deg
    Mean motion:   15.54526688  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3960
    Checksum:              299
 
 
    Coasting Arc #17 (Orbit 3970)
    ---------------------------------------
 
    Vector Time (GMT): 2016/135/07:32:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3607157.02                 A    =         6776275.57  meter
     Y    =        2321022.06  meter          E    =           .0016451
     Z    =       -5260265.09                 I    =           51.35113
     XDOT =      -4856.812643                 Wp   =           97.20040
     YDOT =      -5873.247428  meter/sec      RA   =          225.96422  deg
     ZDOT =        738.973550                 TA   =          179.89816
                                              MA   =          179.89782
                                              Ha   =            220.983  n.mi
                                              Hp   =            213.192
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11834504.67                 X    =        -3607290.94
     Y    =        7614901.78  feet           Y    =         2280683.75  meter
     Z    =      -17258087.57                 Z    =        -5277788.15
     XDOT =     -15934.424681                 XDOT =       -4794.365187
     YDOT =     -19269.184476  feet/sec       YDOT =       -5927.210384  meter/sec
     ZDOT =       2424.453903                 ZDOT =         715.531844
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13322012.29                 X    =        -4060549.35
     Y    =        4233010.91  feet           Y    =         1290221.73  meter
     Z    =      -17334630.76                 Z    =        -5283595.46
     XDOT =      -9962.012256                 XDOT =       -3036.421336
     YDOT =     -21836.419789  feet/sec       YDOT =       -6655.740752  meter/sec
     ZDOT =       2323.591921                 ZDOT =         708.230818
  
  
    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   16135.32877328  .00016717  00000-0  10270-3 0  9160
    2 25544  51.6398 226.9463 0001872 107.9203 252.2154 15.54557783 39717
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16135.32877328   =   yrday.fracday
    Element set:     916
    Inclination:       51.6398  deg
    RA of node:       226.9463  deg
    Eccentricity:     .0001872     
    Arg of perigee:   107.9203  deg
    Mean anomaly:     252.2154  deg
    Mean motion:   15.54557783  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3971
    Checksum:              331
 
             

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