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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  6996.54
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   128.2
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.453
   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 1726)
    ---------------------------------------
 
    Vector Time (GMT): 2014/206/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2305163.48                 A    =         6796894.90  meter
     Y    =       -5777820.54  meter          E    =           .0005346
     Z    =       -2729746.45                 I    =           51.29565
     XDOT =       4026.200586                 Wp   =          332.83332
     YDOT =      -4027.721646  meter/sec      RA   =          268.83564  deg
     ZDOT =       5125.845218                 TA   =          356.17489
                                              MA   =          356.17898
                                              Ha   =            225.227  n.mi
                                              Hp   =            223.027
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7562872.32                 X    =        -2227123.26
     Y    =      -18956104.14  feet           Y    =        -5803161.80  meter
     Z    =       -8955861.05                 Z    =        -2740755.31
     XDOT =      13209.319509                 XDOT =        4046.041013
     YDOT =     -13214.309861  feet/sec       YDOT =       -3982.587549  meter/sec
     ZDOT =      16817.077487                 ZDOT =        5145.451443
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12014868.20                 X    =        -3662131.83
     Y    =       16472799.22  feet           Y    =         5020909.20  meter
     Z    =       -9001566.36                 Z    =        -2743677.43
     XDOT =     -16968.280991                 XDOT =       -5171.932046
     YDOT =      -3141.934338  feet/sec       YDOT =        -957.661586  meter/sec
     ZDOT =      16900.967264                 ZDOT =        5151.414822
  
  
    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   14206.50555242  .00016717  00000-0  10270-3 0  9008
    2 25544  51.6467 269.6596 0006864 288.5807  71.4598 15.50439307 17274
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14206.50555242   =   yrday.fracday
    Element set:     900
    Inclination:       51.6467  deg
    RA of node:       269.6596  deg
    Eccentricity:     .0006864     
    Arg of perigee:   288.5807  deg
    Mean anomaly:      71.4598  deg
    Mean motion:   15.50439307  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1727
    Checksum:              336
 
 
    Coasting Arc #2 (Orbit 1742)
    ---------------------------------------
 
    Vector Time (GMT): 2014/207/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2480378.40                 A    =         6797719.84  meter
     Y    =        5896727.67  meter          E    =           .0006988
     Z    =        2290541.32                 I    =           51.30044
     XDOT =      -3939.392103                 Wp   =          101.25017
     YDOT =       3755.989370  meter/sec      RA   =          263.85621  deg
     ZDOT =      -5390.763310                 TA   =           53.15929
                                              MA   =           53.09523
                                              Ha   =            225.558  n.mi
                                              Hp   =            222.849
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8137724.43                 X    =         2403129.01
     Y    =       19346219.39  feet           Y    =         5924032.78  meter
     Z    =        7514899.33                 Z    =         2302403.16
     XDOT =     -12924.514775                 XDOT =       -3954.913590
     YDOT =      12322.799771  feet/sec       YDOT =        3711.850118  meter/sec
     ZDOT =     -17686.231333                 ZDOT =       -5409.937389
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11735395.35                 X    =         3576948.50
     Y    =      -17379170.27  feet           Y    =        -5297171.10  meter
     Z    =        7564219.22                 Z    =         2305574.02
     XDOT =      16063.960546                 XDOT =        4896.295175
     YDOT =       3095.711084  feet/sec       YDOT =         943.572738  meter/sec
     ZDOT =     -17768.236691                 ZDOT =       -5415.758544
  
  
    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   14207.53683225  .00016717  00000-0  10270-3 0  9016
    2 25544  51.6468 264.5473 0006900 294.0081  66.0347 15.50477596 17432
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14207.53683225   =   yrday.fracday
    Element set:     901
    Inclination:       51.6468  deg
    RA of node:       264.5473  deg
    Eccentricity:     .0006900     
    Arg of perigee:   294.0081  deg
    Mean anomaly:      66.0347  deg
    Mean motion:   15.50477596  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1743
    Checksum:              312
 
 
    Coasting Arc #3 (Orbit 1757)
    ---------------------------------------
 
    Vector Time (GMT): 2014/208/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2675132.18                 A    =         6798607.48  meter
     Y    =       -5966360.00  meter          E    =           .0008920
     Z    =       -1840158.93                 I    =           51.30641
     XDOT =       3896.107574                 Wp   =          349.99168
     YDOT =      -3475.756765  meter/sec      RA   =          258.87729  deg
     ZDOT =       5610.009782                 TA   =          349.69882
                                              MA   =          349.71708
                                              Ha   =            225.717  n.mi
                                              Hp   =            222.763
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8776680.39                 X    =        -2599277.44
     Y    =      -19574671.91  feet           Y    =        -5995850.83  meter
     Z    =       -6037266.81                 Z    =        -1852970.13
     XDOT =      12782.505164                 XDOT =        3907.433663
     YDOT =     -11403.401459  feet/sec       YDOT =       -3432.124932  meter/sec
     ZDOT =      18405.543904                 ZDOT =        5628.963465
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11258464.18                 X    =        -3431579.88
     Y    =       18242747.13  feet           Y    =         5560389.33  meter
     Z    =       -6090619.92                 Z    =        -1856420.95
     XDOT =     -15223.997936                 XDOT =       -4640.274571
     YDOT =      -3228.324597  feet/sec       YDOT =        -983.993337  meter/sec
     ZDOT =      18486.562471                 ZDOT =        5634.704241
  
  
    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   14208.50365329  .00016717  00000-0  10270-3 0  9027
    2 25544  51.6459 259.7543 0006867 297.7887  62.2567 15.50443007 17580
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14208.50365329   =   yrday.fracday
    Element set:     902
    Inclination:       51.6459  deg
    RA of node:       259.7543  deg
    Eccentricity:     .0006867     
    Arg of perigee:   297.7887  deg
    Mean anomaly:      62.2567  deg
    Mean motion:   15.50443007  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1758
    Checksum:              341
 
 
    Coasting Arc #4 (Orbit 1773)
    ---------------------------------------
 
    Vector Time (GMT): 2014/209/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2867002.27                 A    =         6799126.45  meter
     Y    =        6009965.52  meter          E    =           .0006959
     Z    =        1358592.85                 I    =           51.31567
     XDOT =      -3900.952358                 Wp   =          117.03382
     YDOT =       3171.875923  meter/sec      RA   =          253.89933  deg
     ZDOT =      -5779.408524                 TA   =           48.12743
                                              MA   =           48.06807
                                              Ha   =            225.951  n.mi
                                              Hp   =            222.477
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9406175.41                 X    =         2792984.90
     Y    =       19717734.65  feet           Y    =         6041612.29  meter
     Z    =        4457325.64                 Z    =         1372340.49
     XDOT =     -12798.400125                 XDOT =       -3908.057140
     YDOT =      10406.417069  feet/sec       YDOT =        3128.213428  meter/sec
     ZDOT =     -18961.314055                 ZDOT =       -5798.375565
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10690695.50                 X    =         3258523.99
     Y    =      -19038377.14  feet           Y    =        -5802897.35  meter
     Z    =        4514662.00                 Z    =         1376068.98
     XDOT =      14426.107004                 XDOT =        4397.077415
     YDOT =       3569.904567  feet/sec       YDOT =        1088.106912  meter/sec
     ZDOT =     -19042.334798                 ZDOT =       -5804.103647
  
  
    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   14209.53492241  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6460 254.6416 0006851 302.7259  57.3231 15.50489935 17749
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14209.53492241   =   yrday.fracday
    Element set:     903
    Inclination:       51.6460  deg
    RA of node:       254.6416  deg
    Eccentricity:     .0006851     
    Arg of perigee:   302.7259  deg
    Mean anomaly:      57.3231  deg
    Mean motion:   15.50489935  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1774
    Checksum:              309
 
 
    Coasting Arc #5 (Orbit 1788)
    ---------------------------------------
 
    Vector Time (GMT): 2014/210/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3063262.21                 A    =         6799695.30  meter
     Y    =       -5998164.50  meter          E    =           .0011908
     Z    =        -876004.99                 I    =           51.32631
     XDOT =       3953.556056                 Wp   =            4.20262
     YDOT =      -2878.659604  meter/sec      RA   =          248.92216  deg
     ZDOT =       5902.446465                 TA   =          346.28817
                                              MA   =          346.32049
                                              Ha   =            226.133  n.mi
                                              Hp   =            222.384
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10050072.87                 X    =        -2991706.42
     Y    =      -19679017.39  feet           Y    =        -6032019.76  meter
     Z    =       -2874032.11                 Z    =         -890711.91
     XDOT =      12970.984436                 XDOT =        3956.780405
     YDOT =      -9444.421273  feet/sec       YDOT =       -2834.430471  meter/sec
     ZDOT =      19364.981842                 ZDOT =        5921.659701
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9943810.34                 X    =        -3030873.39
     Y    =       19723880.81  feet           Y    =         6011838.87  meter
     Z    =       -2935457.74                 Z    =         -894727.52
     XDOT =     -13773.124470                 XDOT =       -4198.048338
     YDOT =      -4057.492078  feet/sec       YDOT =       -1236.723586  meter/sec
     ZDOT =      19446.996116                 ZDOT =        5927.444416
  
  
    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   14210.50173331  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6456 249.8484 0006860 306.9020  53.1502 15.50453650 17893
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14210.50173331   =   yrday.fracday
    Element set:     904
    Inclination:       51.6456  deg
    RA of node:       249.8484  deg
    Eccentricity:     .0006860     
    Arg of perigee:   306.9020  deg
    Mean anomaly:      53.1502  deg
    Mean motion:   15.50453650  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1789
    Checksum:              289
 
 
    Coasting Arc #6 (Orbit 1804)
    ---------------------------------------
 
    Vector Time (GMT): 2014/211/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3242781.33                 A    =         6799850.59  meter
     Y    =        5962213.95  meter          E    =           .0005969
     Z    =         368158.26                 I    =           51.33938
     XDOT =      -4053.438040                 Wp   =          130.66982
     YDOT =       2576.744875  meter/sec      RA   =          243.94596  deg
     ZDOT =      -5966.429209                 TA   =           45.35263
                                              MA   =           45.30398
                                              Ha   =            226.298  n.mi
                                              Hp   =            222.105
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10639046.37                 X    =         3174081.11
     Y    =       19561069.39  feet           Y    =         5998092.69  meter
     Z    =        1207868.32                 Z    =          383744.15
     XDOT =     -13298.681232                 XDOT =       -4052.968013
     YDOT =       8453.887386  feet/sec       YDOT =        2531.419379  meter/sec
     ZDOT =     -19574.898981                 ZDOT =       -5986.118761
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9146436.46                 X    =         2787833.83
     Y    =      -20297924.63  feet           Y    =        -6186807.43  meter
     Z    =        1273045.40                 Z    =          388024.24
     XDOT =      13219.896259                 XDOT =        4029.424380
     YDOT =       4712.324054  feet/sec       YDOT =        1436.316372  meter/sec
     ZDOT =     -19658.883792                 ZDOT =       -5992.027780
  
  
    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   14211.53299198  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6457 244.7353 0006785 311.0444  49.0120 15.50493137 18059
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14211.53299198   =   yrday.fracday
    Element set:     905
    Inclination:       51.6457  deg
    RA of node:       244.7353  deg
    Eccentricity:     .0006785     
    Arg of perigee:   311.0444  deg
    Mean anomaly:      49.0120  deg
    Mean motion:   15.50493137  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1805
    Checksum:              300
 
 
    Coasting Arc #7 (Orbit 1820)
    ---------------------------------------
 
    Vector Time (GMT): 2014/212/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3410210.27                 A    =         6799967.17  meter
     Y    =       -5871043.98  meter          E    =           .0013944
     Z    =         130222.11                 I    =           51.35404
     XDOT =       4199.951877                 Wp   =           17.38325
     YDOT =      -2303.385247  meter/sec      RA   =          238.97100  deg
     ZDOT =       5985.836197                 TA   =          344.02366
                                              MA   =          344.06759
                                              Ha   =            226.478  n.mi
                                              Hp   =            221.974
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11188353.89                 X    =        -3344938.02
     Y    =      -19261955.32  feet           Y    =        -5908814.19  meter
     Z    =         427237.88                 Z    =          113814.56
     XDOT =      13779.369675                 XDOT =        4196.319832
     YDOT =      -7557.038211  feet/sec       YDOT =       -2256.438971  meter/sec
     ZDOT =      19638.570199                 ZDOT =        6006.229880
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8214686.60                 X    =        -2503836.47
     Y    =       20706885.03  feet           Y    =         6311458.56  meter
     Z    =         358544.80                 Z    =          109284.45
     XDOT =     -12872.726251                 XDOT =       -3923.606961
     YDOT =      -5458.700210  feet/sec       YDOT =       -1663.811824  meter/sec
     ZDOT =      19725.499197                 ZDOT =        6012.332155
  
  
    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   14212.56424633  .00016717  00000-0  10270-3 0  9066
    2 25544  51.6457 239.6225 0006858 315.6366  44.4235 15.50476032 18213
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14212.56424633   =   yrday.fracday
    Element set:     906
    Inclination:       51.6457  deg
    RA of node:       239.6225  deg
    Eccentricity:     .0006858     
    Arg of perigee:   315.6366  deg
    Mean anomaly:      44.4235  deg
    Mean motion:   15.50476032  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1821
    Checksum:              303
 
 
    Coasting Arc #8 (Orbit 1835)
    ---------------------------------------
 
    Vector Time (GMT): 2014/213/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3548558.51                 A    =         6799742.86  meter
     Y    =        5762096.02  meter          E    =           .0003934
     Z    =        -646202.41                 I    =           51.37016
     XDOT =      -4385.712771                 Wp   =          140.18816
     YDOT =       2037.526640  meter/sec      RA   =          233.99680  deg
     ZDOT =      -5938.481087                 TA   =           46.80114
                                              MA   =           46.76828
                                              Ha   =            226.616  n.mi
                                              Hp   =            221.757
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11642252.32                 X    =         3487000.70
     Y    =       18904514.49  feet           Y    =         5801434.09  meter
     Z    =       -2120086.65                 Z    =         -629113.73
     XDOT =     -14388.821426                 XDOT =       -4379.323968
     YDOT =       6684.798689  feet/sec       YDOT =        1988.518469  meter/sec
     ZDOT =     -19483.205666                 ZDOT =       -5959.770534
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7286595.08                 X    =         2220954.18
     Y    =      -20979198.45  feet           Y    =        -6394459.69  meter
     Z    =       -2048472.45                 Z    =         -624374.40
     XDOT =      12664.653812                 XDOT =        3860.186482
     YDOT =       6302.343843  feet/sec       YDOT =        1920.954403  meter/sec
     ZDOT =     -19573.895757                 ZDOT =       -5966.123427
  
  
    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   14213.53104085  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6455 234.8290 0006773 318.9802  41.0839 15.50494928 18360
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14213.53104085   =   yrday.fracday
    Element set:     907
    Inclination:       51.6455  deg
    RA of node:       234.8290  deg
    Eccentricity:     .0006773     
    Arg of perigee:   318.9802  deg
    Mean anomaly:      41.0839  deg
    Mean motion:   15.50494928  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1836
    Checksum:              315
 
 
    Coasting Arc #9 (Orbit 1851)
    ---------------------------------------
 
    Vector Time (GMT): 2014/214/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3658907.51                 A    =         6799356.50  meter
     Y    =       -5604248.86  meter          E    =           .0014806
     Z    =        1142593.08                 I    =           51.38797
     XDOT =       4612.325326                 Wp   =           29.89873
     YDOT =      -1814.467202  meter/sec      RA   =          229.02413  deg
     ZDOT =       5850.069213                 TA   =          342.53807
                                              MA   =          342.58893
                                              Ha   =            226.764  n.mi
                                              Hp   =            221.578
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12004289.73                 X    =        -3601517.89
     Y    =      -18386643.23  feet           Y    =        -5644844.23  meter
     Z    =        3748664.95                 Z    =         1124958.14
     XDOT =      15132.300938                 XDOT =        4603.854771
     YDOT =      -5952.976384  feet/sec       YDOT =       -1762.936569  meter/sec
     ZDOT =      19193.140461                 ZDOT =        5872.454498
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6288683.68                 X    =        -1916790.79
     Y    =       21051678.83  feet           Y    =         6416551.71  meter
     Z    =        3674695.38                 Z    =         1120047.15
     XDOT =     -12696.497773                 XDOT =       -3869.892521
     YDOT =      -7171.497238  feet/sec       YDOT =       -2185.872358  meter/sec
     ZDOT =      19288.450320                 ZDOT =        5879.119658
  
  
    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   14214.56228363  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6455 229.7164 0006884 323.2576  36.8102 15.50505673 18526
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14214.56228363   =   yrday.fracday
    Element set:     908
    Inclination:       51.6455  deg
    RA of node:       229.7164  deg
    Eccentricity:     .0006884     
    Arg of perigee:   323.2576  deg
    Mean anomaly:      36.8102  deg
    Mean motion:   15.50505673  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1852
    Checksum:              312
 
 
    Coasting Arc #10 (Orbit 1866)
    ---------------------------------------
 
    Vector Time (GMT): 2014/215/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3731358.78                 A    =         6798769.69  meter
     Y    =        5439209.56  meter          E    =           .0001204
     Z    =       -1647364.35                 I    =           51.40653
     XDOT =      -4863.022750                 Wp   =          115.38655
     YDOT =       1613.900158  meter/sec      RA   =          224.05189  deg
     ZDOT =      -5690.034013                 TA   =           82.67373
                                              MA   =           82.66005
                                              Ha   =            226.918  n.mi
                                              Hp   =            221.407
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12241990.74                 X    =         3678261.29
     Y    =       17845175.73  feet           Y    =         5480639.15  meter
     Z    =       -5404738.69                 Z    =        -1629366.95
     XDOT =     -15954.799050                 XDOT =       -4853.068119
     YDOT =       5294.948025  feet/sec       YDOT =        1559.574420  meter/sec
     ZDOT =     -18668.090593                 ZDOT =       -5713.633565
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5354578.06                 X    =         1632075.39
     Y    =      -20987044.27  feet           Y    =        -6396851.09  meter
     Z    =       -5329193.29                 Z    =        -1624338.11
     XDOT =      12878.512661                 XDOT =        3925.370659
     YDOT =       8048.450882  feet/sec       YDOT =        2453.167829  meter/sec
     ZDOT =     -18768.529387                 ZDOT =       -5720.647757
  
  
    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   14215.52906885  .00016717  00000-0  10270-3 0  9092
    2 25544  51.6449 224.9228 0006846 326.8000  33.2720 15.50503390 18673
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14215.52906885   =   yrday.fracday
    Element set:     909
    Inclination:       51.6449  deg
    RA of node:       224.9228  deg
    Eccentricity:     .0006846     
    Arg of perigee:   326.8000  deg
    Mean anomaly:      33.2720  deg
    Mean motion:   15.50503390  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1867
    Checksum:              309
 
 
    Coasting Arc #11 (Orbit 1882)
    ---------------------------------------
 
    Vector Time (GMT): 2014/216/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3762189.53                 A    =         6797934.69  meter
     Y    =       -5236719.10  meter          E    =           .0014460
     Z    =        2123127.76                 I    =           51.42675
     XDOT =       5145.405047                 Wp   =           41.69682
     YDOT =      -1465.000055  meter/sec      RA   =          219.08128  deg
     ZDOT =       5493.226805                 TA   =          341.88334
                                              MA   =          341.93481
                                              Ha   =            227.025  n.mi
                                              Hp   =            221.200
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12343141.49                 X    =        -3713665.14
     Y    =      -17180836.95  feet           Y    =        -5278519.07  meter
     Z    =        6965642.24                 Z    =         2104969.40
     XDOT =      16881.250153                 XDOT =        5134.720404
     YDOT =      -4806.430628  feet/sec       YDOT =       -1407.520692  meter/sec
     ZDOT =      18022.397655                 ZDOT =        5518.196341
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4425663.55                 X    =        -1348942.25
     Y    =       20712424.98  feet           Y    =         6313147.13  meter
     Z    =        6889370.48                 Z    =         2099880.12
     XDOT =     -13303.813037                 XDOT =       -4055.002214
     YDOT =      -8884.748471  feet/sec       YDOT =       -2708.071334  meter/sec
     ZDOT =      18128.637764                 ZDOT =        5525.608790
  
  
    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   14216.56029997  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6446 219.8103 0006953 330.3041  29.7715 15.50535652 18837
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14216.56029997   =   yrday.fracday
    Element set:     910
    Inclination:       51.6446  deg
    RA of node:       219.8103  deg
    Eccentricity:     .0006953     
    Arg of perigee:   330.3041  deg
    Mean anomaly:      29.7715  deg
    Mean motion:   15.50535652  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1883
    Checksum:              310
 
 
    Coasting Arc #12 (Orbit 1897)
    ---------------------------------------
 
    Vector Time (GMT): 2014/217/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3751589.26                 A    =         6797043.40  meter
     Y    =        5040835.35  meter          E    =           .0003261
     Z    =       -2597113.10                 I    =           51.44756
     XDOT =      -5430.837911                 Wp   =           18.86128
     YDOT =       1349.777578  meter/sec      RA   =          214.11070  deg
     ZDOT =      -5223.957622                 TA   =          190.37626
                                              MA   =          190.38299
                                              Ha   =            227.210  n.mi
                                              Hp   =            221.035
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12308363.71                 X    =         3707558.51
     Y    =       16538173.73  feet           Y    =         5082541.95  meter
     Z    =       -8520712.26                 Z    =        -2578995.27
     XDOT =     -17817.709683                 XDOT =       -5420.151660
     YDOT =       4428.404127  feet/sec       YDOT =        1289.106400  meter/sec
     ZDOT =     -17138.968577                 ZDOT =       -5250.313690
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3616723.73                 X    =         1102377.39
     Y    =      -20327766.55  feet           Y    =        -6195903.24  meter
     Z    =       -8444569.95                 Z    =        -2573904.92
     XDOT =      13856.276084                 XDOT =        4223.392950
     YDOT =       9633.388108  feet/sec       YDOT =        2936.256695  meter/sec
     ZDOT =     -17251.088938                 ZDOT =       -5258.131908
  
  
    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   14217.52707554  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6437 215.0164 0006975 334.6658  25.4150 15.50519725 18982
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14217.52707554   =   yrday.fracday
    Element set:     911
    Inclination:       51.6437  deg
    RA of node:       215.0164  deg
    Eccentricity:     .0006975     
    Arg of perigee:   334.6658  deg
    Mean anomaly:      25.4150  deg
    Mean motion:   15.50519725  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1898
    Checksum:              315
 
 
    Coasting Arc #13 (Orbit 1913)
    ---------------------------------------
 
    Vector Time (GMT): 2014/218/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3689421.30                 A    =         6795891.17  meter
     Y    =       -4822495.38  meter          E    =           .0013046
     Z    =        3033307.33                 I    =           51.46996
     XDOT =       5736.879160                 Wp   =           52.30539
     YDOT =      -1288.821561  meter/sec      RA   =          209.14184  deg
     ZDOT =       4922.044539                 TA   =          342.53402
                                              MA   =          342.57885
                                              Ha   =            227.285  n.mi
                                              Hp   =            220.824
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12104400.61                 X    =        -3649955.54
     Y    =      -15821835.24  feet           Y    =        -4863532.35  meter
     Z    =        9951795.69                 Z    =         3015480.42
     XDOT =      18821.782020                 XDOT =        5726.955195
     YDOT =      -4228.417196  feet/sec       YDOT =       -1224.723813  meter/sec
     ZDOT =      16148.440090                 ZDOT =        4949.889063
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2887895.23                 X    =         -880230.46
     Y    =       19748247.65  feet           Y    =         6019265.88  meter
     Z    =        9876841.48                 Z    =         3010461.28
     XDOT =     -14626.306481                 XDOT =       -4458.098215
     YDOT =     -10285.661050  feet/sec       YDOT =       -3135.069488  meter/sec
     ZDOT =      16266.885346                 ZDOT =        4958.146653
  
  
    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   14218.55829492  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6433 209.9037 0007055 337.3165  22.7673 15.50560905 19147
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14218.55829492   =   yrday.fracday
    Element set:     912
    Inclination:       51.6433  deg
    RA of node:       209.9037  deg
    Eccentricity:     .0007055     
    Arg of perigee:   337.3165  deg
    Mean anomaly:      22.7673  deg
    Mean motion:   15.50560905  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1914
    Checksum:              311
 
 
    Coasting Arc #14 (Orbit 1928)
    ---------------------------------------
 
    Vector Time (GMT): 2014/219/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3588800.11                 A    =         6794807.91  meter
     Y    =        4626060.24  meter          E    =           .0007367
     Z    =       -3457468.28                 I    =           51.49329
     XDOT =      -6021.447877                 Wp   =           22.19196
     YDOT =       1266.818669  meter/sec      RA   =          204.17267  deg
     ZDOT =      -4551.690288                 TA   =          198.33387
                                              MA   =          198.36044
                                              Ha   =            227.481  n.mi
                                              Hp   =            220.652
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11774278.58                 X    =         3553598.76
     Y    =       15177362.98  feet           Y    =         4665995.87  meter
     Z    =      -11343399.86                 Z    =        -3440119.88
     XDOT =     -19755.406419                 XDOT =       -6013.055857
     YDOT =       4156.229228  feet/sec       YDOT =        1199.530119  meter/sec
     ZDOT =     -14933.367085                 ZDOT =       -4580.920791
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2320456.69                 X    =          707275.20
     Y    =      -19111554.81  feet           Y    =        -5825201.91  meter
     Z    =      -11270432.86                 Z    =        -3435227.94
     XDOT =      15466.804358                 XDOT =        4714.281968
     YDOT =      10764.528485  feet/sec       YDOT =        3281.028282  meter/sec
     ZDOT =     -15057.711065                 ZDOT =       -4589.590333
  
  
    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   14219.52506006  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6428 205.1095 0007119 342.3827  17.7076 15.50539808 19290
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14219.52506006   =   yrday.fracday
    Element set:     913
    Inclination:       51.6428  deg
    RA of node:       205.1095  deg
    Eccentricity:     .0007119     
    Arg of perigee:   342.3827  deg
    Mean anomaly:      17.7076  deg
    Mean motion:   15.50539808  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1929
    Checksum:              306
 
 
    Coasting Arc #15 (Orbit 1944)
    ---------------------------------------
 
    Vector Time (GMT): 2014/220/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3431280.24                 A    =         6793505.82  meter
     Y    =       -4423837.80  meter          E    =           .0010845
     Z    =        3835449.71                 I    =           51.51806
     XDOT =       6315.068113                 Wp   =           60.36825
     YDOT =      -1295.254149  meter/sec      RA   =          199.20552  deg
     ZDOT =       4152.053549                 TA   =          345.85007
                                              MA   =          345.88043
                                              Ha   =            227.539  n.mi
                                              Hp   =            220.442
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11257481.10                 X    =        -3400187.89
     Y    =      -14513903.53  feet           Y    =        -4462034.91  meter
     Z    =       12583496.43                 Z    =         3818856.66
     XDOT =      20718.727406                 XDOT =        6308.913618
     YDOT =      -4249.521485  feet/sec       YDOT =       -1224.669580  meter/sec
     ZDOT =      13622.222930                 ZDOT =        4182.715701
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1897856.05                 X    =         -578466.52
     Y    =       18317596.23  feet           Y    =         5583203.33  meter
     Z    =       12513691.27                 Z    =         3814173.10
     XDOT =     -16474.994230                 XDOT =       -5021.578241
     YDOT =     -11110.200687  feet/sec       YDOT =       -3386.389169  meter/sec
     ZDOT =      13752.669393                 ZDOT =        4191.813631
  
  
    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   14220.55626751  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6427 199.9966 0007167 344.4880  15.6050 15.50582278 19457
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14220.55626751   =   yrday.fracday
    Element set:     914
    Inclination:       51.6427  deg
    RA of node:       199.9966  deg
    Eccentricity:     .0007167     
    Arg of perigee:   344.4880  deg
    Mean anomaly:      15.6050  deg
    Mean motion:   15.50582278  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1945
    Checksum:              329
 
             

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