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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14531.28
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   132.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.186
   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 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 634)
    ---------------------------------------
 
    Vector Time (GMT): 2015/028/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         306385.94                 A    =         6782781.32  meter
     Y    =       -5518511.41  meter          E    =           .0005357
     Z    =       -3936697.56                 I    =           51.95825
     XDOT =       5627.176359                 Wp   =           10.32979
     YDOT =       3225.865833  meter/sec      RA   =           59.30719  deg
     ZDOT =      -4079.834261                 TA   =          217.11601
                                              MA   =          217.15307
                                              Ha   =            220.112  n.mi
                                              Hp   =            216.709
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1005203.21                 X    =          387195.26
     Y    =      -18105352.40  feet           Y    =        -5514633.35  meter
     Z    =      -12915674.41                 Z    =        -3935012.97
     XDOT =      18461.864696                 XDOT =        5610.503845
     YDOT =      10583.549321  feet/sec       YDOT =        3288.699384  meter/sec
     ZDOT =     -13385.283010                 ZDOT =       -4052.539293
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15005679.76                 X    =        -4573731.19
     Y    =      -10191038.87  feet           Y    =        -3106228.65  meter
     Z    =      -12907407.42                 Z    =        -3934177.78
     XDOT =      17833.368667                 XDOT =        5435.610770
     YDOT =      -9434.903336  feet/sec       YDOT =       -2875.758537  meter/sec
     ZDOT =     -13269.074081                 ZDOT =       -4044.413780
  
  
    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   15028.83571020  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6456  59.8551 0006351 302.3258  57.7280 15.54125802  6356
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15028.83571020   =   yrday.fracday
    Element set:     900
    Inclination:       51.6456  deg
    RA of node:        59.8551  deg
    Eccentricity:     .0006351     
    Arg of perigee:   302.3258  deg
    Mean anomaly:      57.7280  deg
    Mean motion:   15.54125802  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             635
    Checksum:              289
 
 
    Coasting Arc #2 (Orbit 650)
    ---------------------------------------
 
    Vector Time (GMT): 2015/029/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1494882.43                 A    =         6779237.21  meter
     Y    =        4466440.34  meter          E    =           .0000821
     Z    =        4875140.21                 I    =           51.92938
     XDOT =      -5647.010650                 Wp   =           80.54928
     YDOT =      -4570.401892  meter/sec      RA   =           54.33657  deg
     ZDOT =       2455.465486                 TA   =          345.44989
                                              MA   =          345.45225
                                              Ha   =            220.301  n.mi
                                              Hp   =            216.527
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4904469.91                 X    =        -1568397.40
     Y    =       14653675.64  feet           Y    =         4449312.48  meter
     Z    =       15994554.48                 Z    =         4867699.95
     XDOT =     -18526.937829                 XDOT =       -5607.411219
     YDOT =     -14994.756863  feet/sec       YDOT =       -4633.329058  meter/sec
     ZDOT =       8055.989126                 ZDOT =        2428.129887
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10237411.13                 X    =         3120362.91
     Y    =       11620011.95  feet           Y    =         3541779.64  meter
     Z    =       15961846.50                 Z    =         4865170.81
     XDOT =     -21390.652704                 XDOT =       -6519.870944
     YDOT =       7937.891466  feet/sec       YDOT =        2419.469319  meter/sec
     ZDOT =       7939.869298                 ZDOT =        2420.072162
  
  
    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   15029.86454626  .00016717  00000-0  10270-3 0  9016
    2 25544  51.6454  54.7262 0006344 305.5243  54.5318 15.54144728  6511
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15029.86454626   =   yrday.fracday
    Element set:     901
    Inclination:       51.6454  deg
    RA of node:        54.7262  deg
    Eccentricity:     .0006344     
    Arg of perigee:   305.5243  deg
    Mean anomaly:      54.5318  deg
    Mean motion:   15.54144728  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             651
    Checksum:              301
 
 
    Coasting Arc #3 (Orbit 665)
    ---------------------------------------
 
    Vector Time (GMT): 2015/030/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2742296.16                 A    =         6777308.03  meter
     Y    =       -3202591.98  meter          E    =           .0011087
     Z    =       -5314997.17                 I    =           51.90463
     XDOT =       5306.623369                 Wp   =           61.98061
     YDOT =       5496.266971  meter/sec      RA   =           49.35696  deg
     ZDOT =       -569.675873                 TA   =          202.57326
                                              MA   =          202.62207
                                              Ha   =            220.398  n.mi
                                              Hp   =            216.414
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8997034.64                 X    =         2803722.32
     Y    =      -10507191.55  feet           Y    =        -3171582.31  meter
     Z    =      -17437654.76                 Z    =        -5301526.70
     XDOT =      17410.181658                 XDOT =        5247.535648
     YDOT =      18032.371953  feet/sec       YDOT =        5555.278716  meter/sec
     ZDOT =      -1869.015331                 ZDOT =        -544.041189
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4827004.79                 X    =        -1471271.06
     Y    =      -13041351.30  feet           Y    =        -3975003.88  meter
     Z    =      -17379375.45                 Z    =        -5297233.64
     XDOT =      23240.899761                 XDOT =        7083.826247
     YDOT =      -6237.976412  feet/sec       YDOT =       -1901.335210  meter/sec
     ZDOT =      -1760.360036                 ZDOT =        -536.557739
  
  
    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   15030.82906540  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6460  49.9179 0006363 310.0097  50.0497 15.54176804  6665
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15030.82906540   =   yrday.fracday
    Element set:     902
    Inclination:       51.6460  deg
    RA of node:        49.9179  deg
    Eccentricity:     .0006363     
    Arg of perigee:   310.0097  deg
    Mean anomaly:      50.0497  deg
    Mean motion:   15.54176804  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             666
    Checksum:              301
 
 
    Coasting Arc #4 (Orbit 681)
    ---------------------------------------
 
    Vector Time (GMT): 2015/031/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3967626.05                 A    =         6777746.47  meter
     Y    =        1813874.96  meter          E    =           .0007118
     Z    =        5189437.71                 I    =           51.88490
     XDOT =      -4569.409132                 Wp   =          351.22361
     YDOT =      -5997.071471  meter/sec      RA   =           44.37369  deg
     ZDOT =      -1390.804016                 TA   =          112.14493
                                              MA   =          112.06937
                                              Ha   =            220.546  n.mi
                                              Hp   =            216.143
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13017145.82                 X    =        -4012822.18
     Y    =        5951033.34  feet           Y    =         1769253.63  meter
     Z    =       17025714.29                 Z    =         5170054.38
     XDOT =     -14991.499776                 XDOT =       -4495.252992
     YDOT =     -19675.431334  feet/sec       YDOT =       -6047.754931  meter/sec
     ZDOT =      -4563.005301                 ZDOT =       -1412.820821
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -853131.77                 X    =         -260034.56
     Y    =       14386218.52  feet           Y    =         4384919.40  meter
     Z    =       16942393.96                 Z    =         5164041.68
     XDOT =     -23333.329723                 XDOT =       -7111.998900
     YDOT =       4125.308129  feet/sec       YDOT =        1257.393918  meter/sec
     ZDOT =      -4656.072980                 ZDOT =       -1419.171044
  
  
    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   15031.85786828  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6456  44.7888 0006506 313.2851  46.7758 15.54222138  6824
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15031.85786828   =   yrday.fracday
    Element set:     903
    Inclination:       51.6456  deg
    RA of node:        44.7888  deg
    Eccentricity:     .0006506     
    Arg of perigee:   313.2851  deg
    Mean anomaly:      46.7758  deg
    Mean motion:   15.54222138  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             682
    Checksum:              330
 
 
    Coasting Arc #5 (Orbit 696)
    ---------------------------------------
 
    Vector Time (GMT): 2015/032/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5033660.92                 A    =         6780532.00  meter
     Y    =        -459789.84  meter          E    =           .0004741
     Z    =       -4522672.39                 I    =           51.87128
     XDOT =       3425.763900                 Wp   =           72.18347
     YDOT =       6063.910071  meter/sec      RA   =           39.39328  deg
     ZDOT =       3200.510094                 TA   =          229.85659
                                              MA   =          229.89813
                                              Ha   =            220.733  n.mi
                                              Hp   =            216.084
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16514635.57                 X    =         5060397.24
     Y    =       -1508496.85  feet           Y    =         -403350.68  meter
     Z    =      -14838164.01                 Z    =        -4498155.46
     XDOT =      11239.382874                 XDOT =        3342.154697
     YDOT =      19894.718081  feet/sec       YDOT =        6101.751708  meter/sec
     ZDOT =      10500.361200                 ZDOT =        3216.948334
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6141816.46                 X    =         1872025.66
     Y    =      -15504602.41  feet           Y    =        -4725802.81  meter
     Z    =      -14733134.66                 Z    =        -4490659.44
     XDOT =      21665.557817                 XDOT =        6603.662023
     YDOT =      -1448.189463  feet/sec       YDOT =        -441.408148  meter/sec
     ZDOT =      10569.534187                 ZDOT =        3221.594020
  
  
    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   15032.82235751  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6460  39.9800 0006478 317.2385  42.8263 15.54213354  6977
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15032.82235751   =   yrday.fracday
    Element set:     904
    Inclination:       51.6460  deg
    RA of node:        39.9800  deg
    Eccentricity:     .0006478     
    Arg of perigee:   317.2385  deg
    Mean anomaly:      42.8263  deg
    Mean motion:   15.54213354  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             697
    Checksum:              306
 
 
    Coasting Arc #6 (Orbit 712)
    ---------------------------------------
 
    Vector Time (GMT): 2015/033/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5841131.56                 A    =         6784360.12  meter
     Y    =        -812151.40  meter          E    =           .0009810
     Z    =        3351586.49                 I    =           51.85909
     XDOT =      -1897.065584                 Wp   =           61.23255
     YDOT =      -5762.111800  meter/sec      RA   =           34.42081  deg
     ZDOT =      -4687.484765                 TA   =           79.84750
                                              MA   =           79.73686
                                              Ha   =            220.787  n.mi
                                              Hp   =            215.795
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19163817.47                 X    =        -5847896.13
     Y    =       -2664538.71  feet           Y    =         -877508.50  meter
     Z    =       10996018.68                 Z    =         3323195.69
     XDOT =      -6223.968450                 XDOT =       -1809.721813
     YDOT =     -18904.566273  feet/sec       YDOT =       -5782.837729  meter/sec
     ZDOT =     -15378.887024                 ZDOT =       -4696.487879
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10774158.52                 X    =        -3283963.52
     Y    =       16153123.25  feet           Y    =         4923471.97  meter
     Z    =       10874659.10                 Z    =         3314596.10
     XDOT =     -18509.014423                 XDOT =       -5641.547596
     YDOT =      -1933.478523  feet/sec       YDOT =        -589.324254  meter/sec
     ZDOT =     -15416.292303                 ZDOT =       -4698.885894
  
  
    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   15033.85112897  .00016717  00000-0  10270-3 0  9055
    2 25544  51.6458  34.8506 0006419 321.8212  38.2485 15.54236417  7135
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15033.85112897   =   yrday.fracday
    Element set:     905
    Inclination:       51.6458  deg
    RA of node:        34.8506  deg
    Eccentricity:     .0006419     
    Arg of perigee:   321.8212  deg
    Mean anomaly:      38.2485  deg
    Mean motion:   15.54236417  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             713
    Checksum:              304
 
 
    Coasting Arc #7 (Orbit 727)
    ---------------------------------------
 
    Vector Time (GMT): 2015/034/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6252504.33                 A    =         6787555.97  meter
     Y    =        1878867.94  meter          E    =           .0011132
     Z    =       -1831178.80                 I    =           51.84400
     XDOT =        102.031196                 Wp   =            3.82316
     YDOT =       5170.180981  meter/sec      RA   =           29.45611  deg
     ZDOT =       5666.013019                 TA   =          336.09010
                                              MA   =          336.14176
                                              Ha   =            220.924  n.mi
                                              Hp   =            215.580
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20513465.65                 X    =         6239924.65
     Y    =        6164264.90  feet           Y    =         1948717.12  meter
     Z    =       -6007804.45                 Z    =        -1800836.72
     XDOT =        334.748017                 XDOT =          16.686754
     YDOT =      16962.536028  feet/sec       YDOT =        5170.844963  meter/sec
     ZDOT =      18589.281559                 ZDOT =        5666.301192
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14224784.84                 X    =         4335714.42
     Y    =      -16062227.83  feet           Y    =        -4895767.04  meter
     Z    =       -5878306.09                 Z    =        -1791707.69
     XDOT =      14315.473245                 XDOT =        4363.356245
     YDOT =       5890.348147  feet/sec       YDOT =        1795.378115  meter/sec
     ZDOT =      18589.500492                 ZDOT =        5666.079750
  
  
    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   15034.81558525  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6463  30.0411 0006527 324.6544  35.4175 15.54269564  7283
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15034.81558525   =   yrday.fracday
    Element set:     906
    Inclination:       51.6463  deg
    RA of node:        30.0411  deg
    Eccentricity:     .0006527     
    Arg of perigee:   324.6544  deg
    Mean anomaly:      35.4175  deg
    Mean motion:   15.54269564  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             728
    Checksum:              302
 
 
    Coasting Arc #8 (Orbit 743)
    ---------------------------------------
 
    Vector Time (GMT): 2015/035/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6201863.84                 A    =         6788969.96  meter
     Y    =       -2755209.14  meter          E    =           .0006184
     Z    =          81948.65                 I    =           51.82070
     XDOT =       1853.465372                 Wp   =          119.79764
     YDOT =      -4361.299413  meter/sec      RA   =           24.49748  deg
     ZDOT =      -6024.433972                 TA   =           59.32223
                                              MA   =           59.26129
                                              Ha   =            220.934  n.mi
                                              Hp   =            215.491
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20347322.32                 X    =        -6170991.58
     Y    =       -9039400.05  feet           Y    =        -2824389.79  meter
     Z    =         268860.40                 Z    =           51897.06
     XDOT =       6080.923135                 XDOT =        1931.360424
     YDOT =     -14308.725107  feet/sec       YDOT =       -4340.137529  meter/sec
     ZDOT =     -19765.203320                 ZDOT =       -6015.240999
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16494664.02                 X    =        -5027573.59
     Y    =       14956697.62  feet           Y    =         4558801.44  meter
     Z    =         140782.62                 Z    =           42910.54
     XDOT =      -9488.972481                 XDOT =       -2892.238812
     YDOT =     -10259.134216  feet/sec       YDOT =       -3126.984109  meter/sec
     ZDOT =     -19725.002526                 ZDOT =       -6012.180770
  
  
    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   15035.84432345  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6463  24.9118 0006361 327.5989  32.4773 15.54250418  7447
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15035.84432345   =   yrday.fracday
    Element set:     907
    Inclination:       51.6463  deg
    RA of node:        24.9118  deg
    Eccentricity:     .0006361     
    Arg of perigee:   327.5989  deg
    Mean anomaly:      32.4773  deg
    Mean motion:   15.54250418  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             744
    Checksum:              312
 
 
    Coasting Arc #9 (Orbit 759)
    ---------------------------------------
 
    Vector Time (GMT): 2015/036/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5630659.24                 A    =         6787548.50  meter
     Y    =        3386868.11  meter          E    =           .0015127
     Z    =        1662712.87                 I    =           51.78744
     XDOT =      -3769.389267                 Wp   =           38.07668
     YDOT =       3446.981206  meter/sec      RA   =           19.53589  deg
     ZDOT =       5727.358862                 TA   =          340.11610
                                              MA   =          340.17499
                                              Ha   =            220.986  n.mi
                                              Hp   =            215.158
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18473291.47                 X    =         5584291.35
     Y    =       11111772.00  feet           Y    =         3449574.66  meter
     Z    =        5455094.70                 Z    =         1689952.05
     XDOT =     -12366.762686                 XDOT =       -3835.474811
     YDOT =      11308.993458  feet/sec       YDOT =        3404.460316  meter/sec
     ZDOT =      18790.547446                 ZDOT =        5708.887575
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17402842.43                 X    =         5304386.37
     Y    =      -12672687.34  feet           Y    =        -3862635.10  meter
     Z    =        5571005.64                 Z    =         1698042.52
     XDOT =       4647.277798                 XDOT =        1416.490273
     YDOT =      14630.011950  feet/sec       YDOT =        4459.227642  meter/sec
     ZDOT =      18710.820236                 ZDOT =        5703.058008
  
  
    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   15036.87304156  .00016717  00000-0  10270-3 0  9084
    2 25544  51.6461  19.7813 0006594 331.7302  28.3493 15.54322013  7605
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15036.87304156   =   yrday.fracday
    Element set:     908
    Inclination:       51.6461  deg
    RA of node:        19.7813  deg
    Eccentricity:     .0006594     
    Arg of perigee:   331.7302  deg
    Mean anomaly:      28.3493  deg
    Mean motion:   15.54322013  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             760
    Checksum:              293
 
 
    Coasting Arc #10 (Orbit 774)
    ---------------------------------------
 
    Vector Time (GMT): 2015/037/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4567389.77                 A    =         6784217.15  meter
     Y    =       -3831125.53  meter          E    =           .0005657
     Z    =       -3245920.10                 I    =           51.74599
     XDOT =       5462.552383                 Wp   =           17.59567
     YDOT =      -2467.310436  meter/sec      RA   =           14.56670  deg
     ZDOT =      -4771.221160                 TA   =          199.91842
                                              MA   =          199.94051
                                              Ha   =            221.105  n.mi
                                              Hp   =            214.989
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14984874.56                 X    =        -4508442.61
     Y    =      -12569309.48  feet           Y    =        -3881871.72  meter
     Z    =      -10649344.18                 Z    =        -3267963.68
     XDOT =      17921.759786                 XDOT =        5512.912788
     YDOT =      -8094.850512  feet/sec       YDOT =       -2405.943406  meter/sec
     ZDOT =     -15653.612729                 ZDOT =       -4744.563163
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17223261.30                 X    =        -5249650.05
     Y    =        9159221.21  feet           Y    =         2791730.62  meter
     Z    =      -10742926.73                 Z    =        -3274444.07
     XDOT =       -130.817831                 XDOT =         -39.873275
     YDOT =     -18483.656863  feet/sec       YDOT =       -5633.818612  meter/sec
     ZDOT =     -15539.048629                 ZDOT =       -4736.302022
  
  
    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   15037.83745015  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6457  14.9725 0006564 334.3284  25.7542 15.54324557  7751
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15037.83745015   =   yrday.fracday
    Element set:     909
    Inclination:       51.6457  deg
    RA of node:        14.9725  deg
    Eccentricity:     .0006564     
    Arg of perigee:   334.3284  deg
    Mean anomaly:      25.7542  deg
    Mean motion:   15.54324557  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             775
    Checksum:              320
 
 
    Coasting Arc #11 (Orbit 790)
    ---------------------------------------
 
    Vector Time (GMT): 2015/038/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3062963.99                 A    =         6780219.09  meter
     Y    =        4084688.50  meter          E    =           .0006788
     Z    =        4454556.70                 I    =           51.70196
     XDOT =      -6770.323366                 Wp   =           64.30834
     YDOT =       1490.093207  meter/sec      RA   =            9.58343  deg
     ZDOT =       3287.901331                 TA   =          352.59113
                                              MA   =          352.60115
                                              Ha   =            221.232  n.mi
                                              Hp   =            214.782
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10049094.44                 X    =         2995422.19
     Y    =       13401208.99  feet           Y    =         4118563.28  meter
     Z    =       14614687.32                 Z    =         4469271.34
     XDOT =     -22212.347001                 XDOT =       -6802.453882
     YDOT =       4888.757241  feet/sec       YDOT =        1414.203662  meter/sec
     ZDOT =      10787.077858                 ZDOT =        3254.934806
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16071753.16                 X    =         4898670.36
     Y    =       -4522669.65  feet           Y    =        -1378509.71  meter
     Z    =       14676852.42                 Z    =         4473504.62
     XDOT =      -3706.332223                 XDOT =       -1129.690062
     YDOT =      21387.219235  feet/sec       YDOT =        6518.824423  meter/sec
     ZDOT =      10645.718449                 ZDOT =        3244.814983
  
  
    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   15038.86613604  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6457   9.8419 0006614 339.8984  20.1907 15.54337323  7914
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15038.86613604   =   yrday.fracday
    Element set:     910
    Inclination:       51.6457  deg
    RA of node:         9.8419  deg
    Eccentricity:     .0006614     
    Arg of perigee:   339.8984  deg
    Mean anomaly:      20.1907  deg
    Mean motion:   15.54337323  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             791
    Checksum:              317
 
 
    Coasting Arc #12 (Orbit 805)
    ---------------------------------------
 
    Vector Time (GMT): 2015/039/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1274151.91                 A    =         6777193.15  meter
     Y    =       -4205435.65  meter          E    =           .0014597
     Z    =       -5171453.69                 I    =           51.65993
     XDOT =       7508.140050                 Wp   =           52.50708
     YDOT =       -523.060276  meter/sec      RA   =            4.58787  deg
     ZDOT =      -1418.587092                 TA   =          203.79976
                                              MA   =          203.86733
                                              Ha   =            221.241  n.mi
                                              Hp   =            214.543
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4180288.42                 X    =        -1201910.40
     Y    =      -13797361.05  feet           Y    =        -4219280.55  meter
     Z    =      -16966711.57                 Z    =        -5177467.37
     XDOT =      24633.005413                 XDOT =        7520.321884
     YDOT =      -1716.077020  feet/sec       YDOT =        -439.031368  meter/sec
     ZDOT =      -4654.157125                 ZDOT =       -1382.084878
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14361119.22                 X    =        -4377269.14
     Y    =        -868581.61  feet           Y    =         -264743.68  meter
     Z    =      -16991618.68                 Z    =        -5179045.37
     XDOT =       6719.203475                 XDOT =        2048.013219
     YDOT =     -22725.809221  feet/sec       YDOT =       -6926.826651  meter/sec
     ZDOT =      -4497.868739                 ZDOT =       -1370.950392
  
  
    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   15039.83050998  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6446   5.0322 0006580 342.2505  17.8417 15.54399479  8068
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15039.83050998   =   yrday.fracday
    Element set:     911
    Inclination:       51.6446  deg
    RA of node:         5.0322  deg
    Eccentricity:     .0006580     
    Arg of perigee:   342.2505  deg
    Mean anomaly:      17.8417  deg
    Mean motion:   15.54399479  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             806
    Checksum:              311
 
 
    Coasting Arc #13 (Orbit 821)
    ---------------------------------------
 
    Vector Time (GMT): 2015/040/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -680806.24                 A    =         6776679.14  meter
     Y    =        4188522.36  meter          E    =           .0007712
     Z    =        5283367.72                 I    =           51.62707
     XDOT =      -7631.231305                 Wp   =            7.75049
     YDOT =       -440.730871  meter/sec      RA   =          359.58517  deg
     ZDOT =       -626.365408                 TA   =           88.27309
                                              MA   =           88.18477
                                              Ha   =            221.367  n.mi
                                              Hp   =            214.411
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2233616.28                 X    =         -753257.02
     Y    =       13741871.26  feet           Y    =         4180504.46  meter
     Z    =       17333883.61                 Z    =         5279884.23
     XDOT =     -25036.848113                 XDOT =       -7622.693166
     YDOT =      -1445.967424  feet/sec       YDOT =        -526.020581  meter/sec
     ZDOT =      -2055.004619                 ZDOT =        -663.415257
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12241125.79                 X    =         3731095.14
     Y    =        6672917.30  feet           Y    =         2033905.19  meter
     Z    =       17318158.17                 Z    =         5278574.61
     XDOT =      -8994.955535                 XDOT =       -2741.662447
     YDOT =      22309.916601  feet/sec       YDOT =        6800.062580  meter/sec
     ZDOT =      -2213.436520                 ZDOT =        -674.655451
  
  
    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   15040.85915968  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6450 359.9023 0006497 345.8883  14.2087 15.54409996  8225
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15040.85915968   =   yrday.fracday
    Element set:     912
    Inclination:       51.6450  deg
    RA of node:       359.9023  deg
    Eccentricity:     .0006497     
    Arg of perigee:   345.8883  deg
    Mean anomaly:      14.2087  deg
    Mean motion:   15.54409996  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             822
    Checksum:              340
 
 
    Coasting Arc #14 (Orbit 836)
    ---------------------------------------
 
    Vector Time (GMT): 2015/041/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2550769.64                 A    =         6778700.20  meter
     Y    =       -4061397.88  meter          E    =           .0009918
     Z    =       -4797602.69                 I    =           51.60121
     XDOT =       7075.670338                 Wp   =           73.40304
     YDOT =       1391.625793  meter/sec      RA   =          354.58126  deg
     ZDOT =       2591.098665                 TA   =          222.11992
                                              MA   =          222.19619
                                              Ha   =            221.385  n.mi
                                              Hp   =            214.249
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8368666.81                 X    =         2619300.31
     Y    =      -13324796.21  feet           Y    =        -4032490.68  meter
     Z    =      -15740166.29                 Z    =        -4785044.92
     XDOT =      23214.141530                 XDOT =        7046.996506
     YDOT =       4565.701420  feet/sec       YDOT =        1470.590407  meter/sec
     ZDOT =       8500.979873                 ZDOT =        2625.400823
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10071202.04                 X    =        -3069702.38
     Y    =      -12160142.51  feet           Y    =        -3706411.44  meter
     Z    =      -15685644.28                 Z    =        -4780984.38
     XDOT =      10589.198855                 XDOT =        3227.587811
     YDOT =     -19894.050149  feet/sec       YDOT =       -6063.706486  meter/sec
     ZDOT =       8647.460288                 ZDOT =        2635.745896
  
  
    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   15041.82350134  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6436 355.0916 0006446 349.5537  10.5481 15.54452579  8376
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15041.82350134   =   yrday.fracday
    Element set:     913
    Inclination:       51.6436  deg
    RA of node:       355.0916  deg
    Eccentricity:     .0006446     
    Arg of perigee:   349.5537  deg
    Mean anomaly:      10.5481  deg
    Mean motion:   15.54452579  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             837
    Checksum:              308
 
 
    Coasting Arc #15 (Orbit 852)
    ---------------------------------------
 
    Vector Time (GMT): 2015/042/19:29:22.676
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4225179.00                 A    =         6782464.67  meter
     Y    =        3778132.18  meter          E    =           .0013140
     Z    =        3722372.25                 I    =           51.58324
     XDOT =      -5904.367823                 Wp   =           54.66116
     YDOT =      -2367.018121  meter/sec      RA   =          349.58522  deg
     ZDOT =      -4281.318367                 TA   =           80.86265
                                              MA   =           80.71400
                                              Ha   =            221.424  n.mi
                                              Hp   =            214.050
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13862135.83                 X    =        -4285194.66
     Y    =       12395446.80  feet           Y    =         3730548.13  meter
     Z    =       12212507.38                 Z    =         3701701.35
     XDOT =     -19371.285509                 XDOT =       -5856.663596
     YDOT =      -7765.807485  feet/sec       YDOT =       -2432.778134  meter/sec
     ZDOT =     -14046.320103                 ZDOT =       -4309.884363
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7794753.63                 X    =         2375840.91
     Y    =       16947501.54  feet           Y    =         5165598.47  meter
     Z    =       12123335.14                 Z    =         3695192.55
     XDOT =     -11814.720861                 XDOT =       -3601.126919
     YDOT =      15611.915106  feet/sec       YDOT =        4758.511724  meter/sec
     ZDOT =     -14168.062298                 ZDOT =       -4318.425388
  
  
    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   15042.85211351  .00016717  00000-0  10270-3 0  9140
    2 25544  51.6440 349.9613 0006523 351.9183   8.1864 15.54498732  8534
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15042.85211351   =   yrday.fracday
    Element set:     914
    Inclination:       51.6440  deg
    RA of node:       349.9613  deg
    Eccentricity:     .0006523     
    Arg of perigee:   351.9183  deg
    Mean anomaly:       8.1864  deg
    Mean motion:   15.54498732  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             853
    Checksum:              308
 
             

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