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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  25295.19
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   124.4
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.3
   ET - UTC  (sec) :   67.18
   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 
   ------------------------------------------------------------------------
   099/21:16:36.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              226.7  
   000/00:00:00.000           0.0               0.0              220.1  
   
   102/15:22:48.548           3.6               5.5              5.6    
   N/A                        4.0              -0.4              226.7  
   000/00:13:37.097          -1.2              -0.0              223.2  
   
   106/11:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              226.8  
   000/00:00:00.000           0.0               0.0              222.8  
   
 
 
    Coasting Arc #1 (Orbit 39)
    ---------------------------------------
 
    Vector Time (GMT): 2014/097/17:01:59.341
    Vector Time (MET): N/A
    Weight (LBS)     : 888709.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3693920.11                 A    =         6789790.79  meter
     Y    =        2975442.53  meter          E    =           .0006081
     Z    =        4853486.36                 I    =           51.99365
     XDOT =      -2214.843543                 Wp   =           98.91659
     YDOT =      -6887.827804  meter/sec      RA   =           88.05407  deg
     ZDOT =       2533.297027                 TA   =          326.26719
                                              MA   =          326.30587
                                              Ha   =            226.859  n.mi
                                              Hp   =            220.294
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12119160.46                 X    =        -3750494.34
     Y    =        9761950.55  feet           Y    =         2933818.81  meter
     Z    =       15923511.68                 Z    =         4835404.14
     XDOT =      -7266.547058                 XDOT =       -2149.963643
     YDOT =     -22597.860249  feet/sec       YDOT =       -6912.232637  meter/sec
     ZDOT =       8311.341951                 ZDOT =        2522.695762
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9883031.22                 X    =         3012347.92
     Y    =       12121907.05  feet           Y    =         3694757.27  meter
     Z    =       15846545.87                 Z    =         4830027.18
     XDOT =     -21640.117816                 XDOT =       -6595.907910
     YDOT =       6819.776895  feet/sec       YDOT =        2078.667998  meter/sec
     ZDOT =       8267.559728                 ZDOT =        2519.952205
  
  
    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   14097.76250877  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6480  88.5903 0002624 354.6196   5.4926 15.50582954   401
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14097.76250877   =   yrday.fracday
    Element set:     900
    Inclination:       51.6480  deg
    RA of node:        88.5903  deg
    Eccentricity:     .0002624     
    Arg of perigee:   354.6196  deg
    Mean anomaly:       5.4926  deg
    Mean motion:   15.50582954  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              40
    Checksum:              315
 
 
    Coasting Arc #2 (Orbit 54)
    ---------------------------------------
 
    Vector Time (GMT): 2014/098/17:01:59.341
    Vector Time (MET): N/A
    Weight (LBS)     : 888709.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3664006.40                 A    =         6788813.54  meter
     Y    =       -2672934.87  meter          E    =           .0013775
     Z    =       -5064060.27                 I    =           51.98958
     XDOT =       2390.419362                 Wp   =           64.48906
     YDOT =       6998.998874  meter/sec      RA   =           83.11619  deg
     ZDOT =      -1963.095481                 TA   =          186.49965
                                              MA   =          186.51754
                                              Ha   =            226.737  n.mi
                                              Hp   =            220.241
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12021018.36                 X    =         3718223.03
     Y    =       -8769471.36  feet           Y    =        -2631658.92  meter
     Z    =      -16614370.97                 Z    =        -5046129.10
     XDOT =       7842.583208                 XDOT =        2321.513408
     YDOT =      22962.594732  feet/sec       YDOT =        7025.344624  meter/sec
     ZDOT =      -6440.601971                 ZDOT =       -1951.651157
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9095485.01                 X    =        -2772303.83
     Y    =      -11883169.46  feet           Y    =        -3621990.05  meter
     Z    =      -16538085.41                 Z    =        -5040808.43
     XDOT =      21873.984544                 XDOT =        6667.190489
     YDOT =      -7837.512099  feet/sec       YDOT =       -2388.873688  meter/sec
     ZDOT =      -6393.278405                 ZDOT =       -1948.671258
  
  
    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   14098.72924083  .00016717  00000-0  10270-3 0  9015
    2 25544  51.6487  83.7969 0002698 359.5081    .6067 15.50632406   552
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14098.72924083   =   yrday.fracday
    Element set:     901
    Inclination:       51.6487  deg
    RA of node:        83.7969  deg
    Eccentricity:     .0002698     
    Arg of perigee:   359.5081  deg
    Mean anomaly:        .6067  deg
    Mean motion:   15.50632406  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              55
    Checksum:              321
 
 
    Coasting Arc #3 (Orbit 70)
    ---------------------------------------
 
    Vector Time (GMT): 2014/099/17:01:59.341
    Vector Time (MET): N/A
    Weight (LBS)     : 888709.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3670633.53                 A    =         6788013.94  meter
     Y    =        2334960.16  meter          E    =           .0003621
     Z    =        5207570.23                 I    =           51.98245
     XDOT =      -2573.959126                 Wp   =           87.90130
     YDOT =      -7090.590709  meter/sec      RA   =           78.17700  deg
     ZDOT =       1364.284211                 TA   =          349.03869
                                              MA   =          349.04658
                                              Ha   =            226.814  n.mi
                                              Hp   =            220.032
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12042760.93                 X    =        -3721767.50
     Y    =        7660630.44  feet           Y    =         2293627.40  meter
     Z    =       17085204.15                 Z    =         5189614.35
     XDOT =      -8444.747789                 XDOT =       -2501.106499
     YDOT =     -23263.092877  feet/sec       YDOT =       -7118.966891  meter/sec
     ZDOT =       4475.998067                 ZDOT =        1351.957941
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8191919.71                 X    =         2496897.13
     Y    =       11798668.60  feet           Y    =         3596234.19  meter
     Z    =       17008863.02                 Z    =         5184301.45
     XDOT =     -22004.833167                 XDOT =       -6707.073149
     YDOT =       8895.889168  feet/sec       YDOT =        2711.467018  meter/sec
     ZDOT =       4424.965993                 ZDOT =        1348.729635
  
  
    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   14099.76039187  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6484  78.6836 0002609   1.1659 358.9497 15.50676759   711
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14099.76039187   =   yrday.fracday
    Element set:     902
    Inclination:       51.6484  deg
    RA of node:        78.6836  deg
    Eccentricity:     .0002609     
    Arg of perigee:     1.1659  deg
    Mean anomaly:     358.9497  deg
    Mean motion:   15.50676759  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              71
    Checksum:              348
 
 
    Coasting Arc #4 (Orbit 72)
    ---------------------------------------
 
    Vector Time (GMT): 2014/099/21:16:36.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904195.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2529385.52                 A    =         6798595.34  meter
     Y    =        6141136.13  meter          E    =           .0010681
     Z    =       -1427721.61                 I    =           52.01382
     XDOT =      -3986.082897                 Wp   =           28.43754
     YDOT =       2989.050158  meter/sec      RA   =           77.27818  deg
     ZDOT =       5822.108749                 TA   =          316.09732
                                              MA   =          316.18214
                                              Ha   =            226.693  n.mi
                                              Hp   =            220.140
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8298508.91                 X    =         2467461.38
     Y    =       20148084.41  feet           Y    =         6169074.95  meter
     Z    =       -4684126.03                 Z    =        -1415585.25
     XDOT =     -13077.699793                 XDOT =       -4047.492848
     YDOT =       9806.595007  feet/sec       YDOT =        2944.132460  meter/sec
     ZDOT =      19101.406656                 ZDOT =        5802.595427
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         449360.22                 X    =          136964.99
     Y    =      -21796285.00  feet           Y    =        -6643507.67  meter
     Z    =       -4633748.76                 Z    =        -1412366.62
     XDOT =      14432.961985                 XDOT =        4399.166813
     YDOT =      -3726.600963  feet/sec       YDOT =       -1135.867973  meter/sec
     ZDOT =      19018.371654                 ZDOT =        5796.799680
  
  
    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   14099.88928247  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6458  78.0423 0002630 357.3834   2.7303 15.50656548   739
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14099.88928247   =   yrday.fracday
    Element set:     903
    Inclination:       51.6458  deg
    RA of node:        78.0423  deg
    Eccentricity:     .0002630     
    Arg of perigee:   357.3834  deg
    Mean anomaly:       2.7303  deg
    Mean motion:   15.50656548  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              73
    Checksum:              314
 
 
    Coasting Arc #5 (Orbit 88)
    ---------------------------------------
 
    Vector Time (GMT): 2014/100/21:16:36.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904195.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2666626.80                 A    =         6798880.91  meter
     Y    =       -6191080.30  meter          E    =           .0011997
     Z    =         849719.14                 I    =           52.00819
     XDOT =       4065.633978                 Wp   =          115.05349
     YDOT =      -2577.627504  meter/sec      RA   =           72.34764  deg
     ZDOT =      -5960.960530                 TA   =           55.81562
                                              MA   =           55.70196
                                              Ha   =            226.597  n.mi
                                              Hp   =            219.935
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8748775.58                 X    =        -2601326.22
     Y    =      -20311943.25  feet           Y    =        -6220535.02  meter
     Z    =        2787792.45                 Z    =          836924.32
     XDOT =      13338.694152                 XDOT =        4123.111944
     YDOT =      -8456.783150  feet/sec       YDOT =       -2531.842275  meter/sec
     ZDOT =     -19556.957121                 ZDOT =       -5941.070293
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         267034.21                 X    =           81392.03
     Y    =       22120992.41  feet           Y    =         6742478.49  meter
     Z    =        2734645.64                 Z    =          833519.99
     XDOT =     -14067.015237                 XDOT =       -4287.626244
     YDOT =       2602.151793  feet/sec       YDOT =         793.135866  meter/sec
     ZDOT =     -19472.389585                 ZDOT =       -5935.184345
  
  
    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   14100.92039954  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6461  72.9287 0002747   1.3394 358.7764 15.50747802   896
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14100.92039954   =   yrday.fracday
    Element set:     904
    Inclination:       51.6461  deg
    RA of node:        72.9287  deg
    Eccentricity:     .0002747     
    Arg of perigee:     1.3394  deg
    Mean anomaly:     358.7764  deg
    Mean motion:   15.50747802  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              89
    Checksum:              318
 
 
    Coasting Arc #6 (Orbit 103)
    ---------------------------------------
 
    Vector Time (GMT): 2014/101/21:16:36.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904195.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2810326.08                 A    =         6799158.02  meter
     Y    =        6176822.52  meter          E    =           .0013587
     Z    =        -284861.68                 I    =           51.99777
     XDOT =      -4197.094140                 Wp   =           36.88896
     YDOT =       2180.401413  meter/sec      RA   =           67.41502  deg
     ZDOT =       6031.385330                 TA   =          320.06005
                                              MA   =          320.15993
                                              Ha   =            226.649  n.mi
                                              Hp   =            219.854
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9220229.92                 X    =         2742430.36
     Y    =       20265165.75  feet           Y    =         6207869.73  meter
     Z    =        -934585.58                 Z    =         -271375.11
     XDOT =     -13769.993898                 XDOT =       -4250.462646
     YDOT =       7153.547943  feet/sec       YDOT =        2133.169144  meter/sec
     ZDOT =      19788.009612                 ZDOT =        6010.866430
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1092075.81                 X    =         -332864.71
     Y    =      -22239572.99  feet           Y    =        -6778621.85  meter
     Z    =        -878519.49                 Z    =         -267772.74
     XDOT =      13931.962212                 XDOT =        4246.462082
     YDOT =      -1440.408561  feet/sec       YDOT =        -439.036529  meter/sec
     ZDOT =      19700.844282                 ZDOT =        6004.817337
  
  
    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   14101.88704635  .00016717  00000-0  10270-3 0  9050
    2 25544  51.6451  68.1333 0002467   6.2464 353.8717 15.50742964  1041
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14101.88704635   =   yrday.fracday
    Element set:     905
    Inclination:       51.6451  deg
    RA of node:        68.1333  deg
    Eccentricity:     .0002467     
    Arg of perigee:     6.2464  deg
    Mean anomaly:     353.8717  deg
    Mean motion:   15.50742964  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             104
    Checksum:              295
 
 
    Coasting Arc #7 (Orbit 115)
    ---------------------------------------
 
    Vector Time (GMT): 2014/102/15:29:37.097
    Vector Time (MET): N/A
    Weight (LBS)     : 903571.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4109081.79                 A    =         6790485.86  meter
     Y    =       -1065324.06  meter          E    =           .0010685
     Z    =       -5309373.51                 I    =           51.95254
     XDOT =       2827.099260                 Wp   =           92.33654
     YDOT =       7070.310185  meter/sec      RA   =           63.66523  deg
     ZDOT =        770.234213                 TA   =          185.00034
                                              MA   =          185.01102
                                              Ha   =            226.694  n.mi
                                              Hp   =            223.166
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13481239.47                 X    =         4146480.54
     Y    =       -3495157.67  feet           Y    =        -1019165.21  meter
     Z    =      -17419204.42                 Z    =        -5289321.03
     XDOT =       9275.260041                 XDOT =        2744.085756
     YDOT =      23196.555724  feet/sec       YDOT =        7101.460564  meter/sec
     ZDOT =       2527.015136                 ZDOT =         783.765465
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         791940.29                 X    =          241383.40
     Y    =      -14010253.91  feet           Y    =        -4270325.39  meter
     Z    =      -17334192.90                 Z    =        -5283462.00
     XDOT =      23891.027700                 XDOT =        7281.985243
     YDOT =      -1841.777197  feet/sec       YDOT =        -561.373690  meter/sec
     ZDOT =       2583.116775                 ZDOT =         787.333993
  
  
    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   14102.66035009  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6485  64.2998 0003913 285.8468  74.2251 15.49698906  1162
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14102.66035009   =   yrday.fracday
    Element set:     906
    Inclination:       51.6485  deg
    RA of node:        64.2998  deg
    Eccentricity:     .0003913     
    Arg of perigee:   285.8468  deg
    Mean anomaly:      74.2251  deg
    Mean motion:   15.49698906  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             116
    Checksum:              326
 
 
    Coasting Arc #8 (Orbit 131)
    ---------------------------------------
 
    Vector Time (GMT): 2014/103/15:29:37.097
    Vector Time (MET): N/A
    Weight (LBS)     : 903571.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4136533.54                 A    =         6790442.68  meter
     Y    =        1131978.56  meter          E    =           .0003403
     Z    =        5265887.64                 I    =           51.93861
     XDOT =      -3216.089636                 Wp   =          348.00259
     YDOT =      -6873.772858  meter/sec      RA   =           58.73274  deg
     ZDOT =      -1045.613430                 TA   =          111.99848
                                              MA   =          111.96232
                                              Ha   =            226.721  n.mi
                                              Hp   =            222.950
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13571304.25                 X    =        -4174464.44
     Y    =        3713840.42  feet           Y    =         1085509.73  meter
     Z    =       17276534.26                 Z    =         5245700.43
     XDOT =     -10551.475184                 XDOT =       -3133.907210
     YDOT =     -22551.748222  feet/sec       YDOT =       -6909.277854  meter/sec
     ZDOT =      -3430.490256                 ZDOT =       -1061.036486
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -366946.68                 X    =         -111845.35
     Y    =       14169981.26  feet           Y    =         4319010.29  meter
     Z    =       17190943.16                 Z    =         5239799.48
     XDOT =     -23592.039179                 XDOT =       -7190.853542
     YDOT =       3641.175390  feet/sec       YDOT =        1109.830259  meter/sec
     ZDOT =      -3494.613619                 ZDOT =       -1065.158231
  
  
    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   14103.69211542  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6485  59.1907 0004055 288.9004  71.1707 15.49770414  1328
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14103.69211542   =   yrday.fracday
    Element set:     907
    Inclination:       51.6485  deg
    RA of node:        59.1907  deg
    Eccentricity:     .0004055     
    Arg of perigee:   288.9004  deg
    Mean anomaly:      71.1707  deg
    Mean motion:   15.49770414  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             132
    Checksum:              295
 
 
    Coasting Arc #9 (Orbit 146)
    ---------------------------------------
 
    Vector Time (GMT): 2014/104/15:29:37.097
    Vector Time (MET): N/A
    Weight (LBS)     : 903571.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4183817.91                 A    =         6790626.24  meter
     Y    =       -1207220.98  meter          E    =           .0010034
     Z    =       -5219452.62                 I    =           51.92341
     XDOT =       3570.174148                 Wp   =           95.24373
     YDOT =       6638.775738  meter/sec      RA   =           53.79864  deg
     ZDOT =       1327.589418                 TA   =          187.47810
                                              MA   =          187.49307
                                              Ha   =            226.680  n.mi
                                              Hp   =            223.003
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13726436.73                 X    =         4222361.21
     Y    =       -3960698.76  feet           Y    =        -1160219.90  meter
     Z    =      -17124188.40                 Z    =        -5199034.16
     XDOT =      11713.169777                 XDOT =        3489.223407
     YDOT =      21780.760296  feet/sec       YDOT =        6678.247240  meter/sec
     ZDOT =       4355.608328                 ZDOT =        1344.735748
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         -72796.13                 X    =          -22188.26
     Y    =      -14389393.67  feet           Y    =        -4385887.19  meter
     Z    =      -17037607.78                 Z    =        -5193062.85
     XDOT =      23080.688327                 XDOT =        7034.993802
     YDOT =      -5353.473961  feet/sec       YDOT =       -1631.738863  meter/sec
     ZDOT =       4427.045430                 ZDOT =        1349.363447
  
  
    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   14104.65937126  .00016717  00000-0  10270-3 0  9084
    2 25544  51.6495  54.4006 0003990 292.4264  67.6464 15.49786420  1472
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14104.65937126   =   yrday.fracday
    Element set:     908
    Inclination:       51.6495  deg
    RA of node:        54.4006  deg
    Eccentricity:     .0003990     
    Arg of perigee:   292.4264  deg
    Mean anomaly:      67.6464  deg
    Mean motion:   15.49786420  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             147
    Checksum:              320
 
 
    Coasting Arc #10 (Orbit 162)
    ---------------------------------------
 
    Vector Time (GMT): 2014/105/15:29:37.097
    Vector Time (MET): N/A
    Weight (LBS)     : 903571.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4247700.18                 A    =         6790715.32  meter
     Y    =        1268111.54  meter          E    =           .0004687
     Z    =        5144981.96                 I    =           51.90565
     XDOT =      -3889.484079                 Wp   =            4.90416
     YDOT =      -6395.469088  meter/sec      RA   =           48.86339  deg
     ZDOT =      -1630.178265                 TA   =          100.80966
                                              MA   =          100.75690
                                              Ha   =            226.712  n.mi
                                              Hp   =            222.771
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13936024.23                 X    =        -4286557.93
     Y    =        4160470.92  feet           Y    =         1220394.23  meter
     Z    =       16879862.07                 Z    =         5124252.35
     XDOT =     -12760.774537                 XDOT =       -3809.760392
     YDOT =     -20982.510132  feet/sec       YDOT =       -6438.518182  meter/sec
     ZDOT =      -5348.353888                 ZDOT =       -1648.878955
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         460692.17                 X    =          140418.97
     Y    =       14637964.90  feet           Y    =         4461651.70  meter
     Z    =       16791955.79                 Z    =         5118188.12
     XDOT =     -22459.179323                 XDOT =       -6845.557858
     YDOT =       6949.350737  feet/sec       YDOT =        2118.162105  meter/sec
     ZDOT =      -5426.391149                 ZDOT =       -1653.964022
  
  
    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   14105.69108058  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6497  49.2914 0004124 295.5585  64.5139 15.49858912  1633
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14105.69108058   =   yrday.fracday
    Element set:     909
    Inclination:       51.6497  deg
    RA of node:        49.2914  deg
    Eccentricity:     .0004124     
    Arg of perigee:   295.5585  deg
    Mean anomaly:      64.5139  deg
    Mean motion:   15.49858912  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             163
    Checksum:              331
 
 
    Coasting Arc #11 (Orbit 174)
    ---------------------------------------
 
    Vector Time (GMT): 2014/106/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925957.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5631122.99                 A    =         6797632.88  meter
     Y    =        2069828.91  meter          E    =           .0003066
     Z    =       -3193297.30                 I    =           51.90873
     XDOT =        567.681024                 Wp   =           16.67602
     YDOT =       5911.340173  meter/sec      RA   =           44.84085  deg
     ZDOT =       4836.676119                 TA   =          306.66902
                                              MA   =          306.69720
                                              Ha   =            226.813  n.mi
                                              Hp   =            222.816
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18474812.96                 X    =         5623071.49
     Y    =        6790777.26  feet           Y    =         2132754.49  meter
     Z    =      -10476697.17                 Z    =        -3165961.27
     XDOT =       1862.470550                 XDOT =         478.041409
     YDOT =      19394.160672  feet/sec       YDOT =        5917.187497  meter/sec
     ZDOT =      15868.359970                 ZDOT =        4839.215721
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19353030.94                 X    =         5898803.83
     Y    =        3911001.34  feet           Y    =         1192073.21  meter
     Z    =      -10361409.92                 Z    =        -3158157.74
     XDOT =       4958.283745                 XDOT =        1511.284885
     YDOT =      17495.241855  feet/sec       YDOT =        5332.549717  meter/sec
     ZDOT =      15878.101123                 ZDOT =        4839.645222
  
  
    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   14106.46484592  .00016717  00000-0  10270-3 0  9102
    2 25544  51.6470  45.4583 0004024 298.8099  61.2647 15.49834133  1759
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14106.46484592   =   yrday.fracday
    Element set:     910
    Inclination:       51.6470  deg
    RA of node:        45.4583  deg
    Eccentricity:     .0004024     
    Arg of perigee:   298.8099  deg
    Mean anomaly:      61.2647  deg
    Mean motion:   15.49834133  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             175
    Checksum:              315
 
 
    Coasting Arc #12 (Orbit 190)
    ---------------------------------------
 
    Vector Time (GMT): 2014/107/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925957.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5833062.08                 A    =         6798105.58  meter
     Y    =       -1874617.04  meter          E    =           .0009683
     Z    =        2937343.27                 I    =           51.88919
     XDOT =       -699.852979                 Wp   =           88.65099
     YDOT =      -5732.753768  meter/sec      RA   =           39.90597  deg
     ZDOT =      -5033.891799                 TA   =           58.02084
                                              MA   =           57.92675
                                              Ha   =            226.756  n.mi
                                              Hp   =            222.626
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19137342.78                 X    =        -5825935.11
     Y    =       -6150318.36  feet           Y    =        -1939806.08  meter
     Z    =        9636953.00                 Z    =         2909023.94
     XDOT =      -2296.105573                 XDOT =        -611.242509
     YDOT =     -18808.247271  feet/sec       YDOT =       -5740.084787  meter/sec
     ZDOT =     -16515.393040                 ZDOT =       -5037.076119
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19957732.58                 X    =        -6083116.89
     Y    =       -2835782.67  feet           Y    =         -864346.56  meter
     Z    =        9517479.44                 Z    =         2900927.73
     XDOT =      -5529.407520                 XDOT =       -1685.363412
     YDOT =     -16718.249488  feet/sec       YDOT =       -5095.722444  meter/sec
     ZDOT =     -16527.879938                 ZDOT =       -5037.697805
  
  
    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   14107.49650616  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6479  40.3488 0004044 302.2300  57.8458 15.49898488  1915
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14107.49650616   =   yrday.fracday
    Element set:     911
    Inclination:       51.6479  deg
    RA of node:        40.3488  deg
    Eccentricity:     .0004044     
    Arg of perigee:   302.2300  deg
    Mean anomaly:      57.8458  deg
    Mean motion:   15.49898488  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             191
    Checksum:              318
 
 
    Coasting Arc #13 (Orbit 205)
    ---------------------------------------
 
    Vector Time (GMT): 2014/108/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925957.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6024033.19                 A    =         6798640.72  meter
     Y    =        1645099.14  meter          E    =           .0005360
     Z    =       -2680781.62                 I    =           51.86667
     XDOT =        800.508277                 Wp   =            6.84833
     YDOT =       5554.723116  meter/sec      RA   =           34.96943  deg
     ZDOT =       5213.823864                 TA   =          323.05133
                                              MA   =          323.08823
                                              Ha   =            226.844  n.mi
                                              Hp   =            222.592
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19763888.42                 X    =         6018212.20
     Y    =        5397306.89  feet           Y    =         1712431.11  meter
     Z    =       -8795215.29                 Z    =        -2651531.40
     XDOT =       2626.339493                 XDOT =         713.007087
     YDOT =      18224.157204  feet/sec       YDOT =        5563.185843  meter/sec
     ZDOT =      17105.721340                 ZDOT =        5217.499962
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20474815.24                 X    =         6240723.69
     Y    =        1637187.20  feet           Y    =          499014.66  meter
     Z    =       -8671769.03                 Z    =        -2643155.20
     XDOT =       5966.676772                 XDOT =        1818.643080
     YDOT =      15951.937226  feet/sec       YDOT =        4862.150466  meter/sec
     ZDOT =      17120.308844                 ZDOT =        5218.270136
  
  
    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   14108.46366157  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6477  35.5585 0004116 305.1758  54.9006 15.49919981  2062
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14108.46366157   =   yrday.fracday
    Element set:     912
    Inclination:       51.6477  deg
    RA of node:        35.5585  deg
    Eccentricity:     .0004116     
    Arg of perigee:   305.1758  deg
    Mean anomaly:      54.9006  deg
    Mean motion:   15.49919981  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             206
    Checksum:              318
 
 
    Coasting Arc #14 (Orbit 221)
    ---------------------------------------
 
    Vector Time (GMT): 2014/109/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925957.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6202896.99                 A    =         6799106.70  meter
     Y    =       -1425219.63  meter          E    =           .0010092
     Z    =        2380705.55                 I    =           51.84366
     XDOT =       -840.319532                 Wp   =           98.05116
     YDOT =      -5378.147092  meter/sec      RA   =           30.03129  deg
     ZDOT =      -5390.918107                 TA   =           55.49015
                                              MA   =           55.39490
                                              Ha   =            226.786  n.mi
                                              Hp   =            222.407
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20350711.91                 X    =        -6198063.71
     Y    =       -4675917.42  feet           Y    =        -1494557.33  meter
     Z    =        7810713.76                 Z    =         2350584.10
     XDOT =      -2756.953846                 XDOT =        -753.929705
     YDOT =     -17644.839540  feet/sec       YDOT =       -5387.061166  meter/sec
     ZDOT =     -17686.739197                 ZDOT =       -5394.790366
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20923036.25                 X    =        -6377341.45
     Y    =        -461077.21  feet           Y    =         -140536.33  meter
     Z    =        7683546.73                 Z    =         2341945.04
     XDOT =      -6187.544418                 XDOT =       -1885.963539
     YDOT =     -15223.118737  feet/sec       YDOT =       -4640.006591  meter/sec
     ZDOT =     -17702.179107                 ZDOT =       -5395.624192
  
  
    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   14109.49526683  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6485  30.4485 0004084 308.6358  51.4426 15.49978863  2222
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14109.49526683   =   yrday.fracday
    Element set:     913
    Inclination:       51.6485  deg
    RA of node:        30.4485  deg
    Eccentricity:     .0004084     
    Arg of perigee:   308.6358  deg
    Mean anomaly:      51.4426  deg
    Mean motion:   15.49978863  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             222
    Checksum:              325
 
 
    Coasting Arc #15 (Orbit 236)
    ---------------------------------------
 
    Vector Time (GMT): 2014/110/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925957.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6361390.12                 A    =         6799580.42  meter
     Y    =        1171034.67  meter          E    =           .0007869
     Z    =       -2081682.52                 I    =           51.81780
     XDOT =        851.760619                 Wp   =            8.18319
     YDOT =       5215.762389  meter/sec      RA   =           25.09112  deg
     ZDOT =       5547.137777                 TA   =          328.87846
                                              MA   =          328.92504
                                              Ha   =            226.881  n.mi
                                              Hp   =            222.328
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20870702.49                 X    =         6357934.79
     Y    =        3841977.27  feet           Y    =         1242152.46  meter
     Z    =       -6829667.07                 Z    =        -2050787.89
     XDOT =       2794.490219                 XDOT =         766.426999
     YDOT =      17112.081330  feet/sec       YDOT =        5224.810292  meter/sec
     ZDOT =      18199.270922                 ZDOT =        5551.068189
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21246922.94                 X    =         6476062.11
     Y    =        -824940.00  feet           Y    =         -251441.71  meter
     Z    =       -6699186.79                 Z    =        -2041912.13
     XDOT =       6297.951351                 XDOT =        1919.615572
     YDOT =      14563.841913  feet/sec       YDOT =        4439.059015  meter/sec
     ZDOT =      18214.979688                 ZDOT =        5551.925809
  
  
    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   14110.46237077  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6481  25.6577 0004174 311.4849  48.5943 15.50005000  2376
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14110.46237077   =   yrday.fracday
    Element set:     914
    Inclination:       51.6481  deg
    RA of node:        25.6577  deg
    Eccentricity:     .0004174     
    Arg of perigee:   311.4849  deg
    Mean anomaly:      48.5943  deg
    Mean motion:   15.50005000  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             237
    Checksum:              285
 
 
    Coasting Arc #16 (Orbit 252)
    ---------------------------------------
 
    Vector Time (GMT): 2014/111/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925957.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6503941.27                 A    =         6799984.43  meter
     Y    =        -929781.20  meter          E    =           .0010107
     Z    =        1737292.87                 I    =           51.79189
     XDOT =       -802.337215                 Wp   =          107.68032
     YDOT =      -5065.775852  meter/sec      RA   =           20.14924  deg
     ZDOT =      -5690.599147                 TA   =           53.33372
                                              MA   =           53.24087
                                              Ha   =            226.827  n.mi
                                              Hp   =            222.170
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21338390.01                 X    =        -6501500.12
     Y    =       -3050463.24  feet           Y    =        -1002498.75  meter
     Z    =        5699779.76                 Z    =         1705703.39
     XDOT =      -2632.339944                 XDOT =        -717.987657
     YDOT =     -16619.999513  feet/sec       YDOT =       -5074.276612  meter/sec
     ZDOT =     -18669.944708                 ZDOT =       -5694.291811
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21490917.55                 X    =        -6550431.67
     Y    =        2067909.63  feet           Y    =          630298.85  meter
     Z    =        5566319.77                 Z    =         1696614.26
     XDOT =      -6207.235293                 XDOT =       -1891.965317
     YDOT =     -13994.957840  feet/sec       YDOT =       -4265.663150  meter/sec
     ZDOT =     -18684.670890                 ZDOT =       -5695.087687
  
  
    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   14111.49392149  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6488  20.5470 0004111 314.8600  45.2216 15.50054435  2533
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14111.49392149   =   yrday.fracday
    Element set:     915
    Inclination:       51.6488  deg
    RA of node:        20.5470  deg
    Eccentricity:     .0004111     
    Arg of perigee:   314.8600  deg
    Mean anomaly:      45.2216  deg
    Mean motion:   15.50054435  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             253
    Checksum:              269
 
 
    Coasting Arc #17 (Orbit 267)
    ---------------------------------------
 
    Vector Time (GMT): 2014/112/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925957.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6616421.31                 A    =         6800320.27  meter
     Y    =         657786.51  meter          E    =           .0010322
     Z    =       -1396766.51                 I    =           51.76383
     XDOT =        731.220913                 Wp   =           13.57907
     YDOT =       4942.751031  meter/sec      RA   =           15.20521  deg
     ZDOT =       5809.967648                 TA   =          331.24796
                                              MA   =          331.30482
                                              Ha   =            226.917  n.mi
                                              Hp   =            222.038
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21707419.01                 X    =         6615359.12
     Y    =        2158092.23  feet           Y    =          731769.59  meter
     Z    =       -4582567.30                 Z    =        -1364627.35
     XDOT =       2399.018743                 XDOT =         647.672535
     YDOT =      16216.374773  feet/sec       YDOT =        4950.461091  meter/sec
     ZDOT =      19061.573648                 ZDOT =        5813.316705
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21577538.38                 X    =         6576833.70
     Y    =       -3392003.77  feet           Y    =        -1033882.75  meter
     Z    =       -4446737.38                 Z    =        -1355365.55
     XDOT =       6047.516790                 XDOT =        1843.283118
     YDOT =      13545.860710  feet/sec       YDOT =        4128.778344  meter/sec
     ZDOT =      19074.866494                 ZDOT =        5814.019307
  
  
    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   14112.46097449  .00016717  00000-0  10270-3 0  9166
    2 25544  51.6487  15.7556 0004220 317.8982  42.1844 15.50088959  2687
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14112.46097449   =   yrday.fracday
    Element set:     916
    Inclination:       51.6487  deg
    RA of node:        15.7556  deg
    Eccentricity:     .0004220     
    Arg of perigee:   317.8982  deg
    Mean anomaly:      42.1844  deg
    Mean motion:   15.50088959  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             268
    Checksum:              327
 
             

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