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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  5381.96
   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 1773)
    ---------------------------------------
 
    Vector Time (GMT): 2014/209/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3691479.88                 A    =         6796888.83  meter
     Y    =       -5042135.94  meter          E    =           .0006541
     Z    =       -2662642.99                 I    =           51.30796
     XDOT =       2900.331018                 Wp   =          346.55748
     YDOT =      -4852.963185  meter/sec      RA   =          253.74515  deg
     ZDOT =       5172.517151                 TA   =          343.29566
                                              MA   =          343.31719
                                              Ha   =            225.813  n.mi
                                              Hp   =            222.418
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12111154.45                 X    =        -3621889.20
     Y    =      -16542440.74  feet           Y    =        -5083027.25  meter
     Z    =       -8735705.35                 Z    =        -2680406.45
     XDOT =       9515.521712                 XDOT =        2929.256493
     YDOT =     -15921.795226  feet/sec       YDOT =       -4820.368254  meter/sec
     ZDOT =      16970.200628                 ZDOT =        5186.676360
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2854395.25                 X    =         -870019.67
     Y    =       20270099.89  feet           Y    =         6178326.45  meter
     Z    =       -8810245.97                 Z    =        -2685362.97
     XDOT =     -16357.471526                 XDOT =       -4985.757321
     YDOT =       5093.818599  feet/sec       YDOT =        1552.595909  meter/sec
     ZDOT =      17031.099112                 ZDOT =        5191.079009
  
  
    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   14209.53493196  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6456 254.6440 0006626 302.6240  57.4270 15.50486889 17749
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14209.53493196   =   yrday.fracday
    Element set:     900
    Inclination:       51.6456  deg
    RA of node:       254.6440  deg
    Eccentricity:     .0006626     
    Arg of perigee:   302.6240  deg
    Mean anomaly:      57.4270  deg
    Mean motion:   15.50486889  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1774
    Checksum:              316
 
 
    Coasting Arc #2 (Orbit 1789)
    ---------------------------------------
 
    Vector Time (GMT): 2014/210/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3887975.71                 A    =         6797849.36  meter
     Y    =        5115237.42  meter          E    =           .0007796
     Z    =        2212685.32                 I    =           51.31978
     XDOT =      -2895.451794                 Wp   =           92.36488
     YDOT =       4558.020076  meter/sec      RA   =          248.76646  deg
     ZDOT =      -5433.111666                 TA   =           62.98302
                                              MA   =           62.90345
                                              Ha   =            226.156  n.mi
                                              Hp   =            222.250
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12755825.81                 X    =         3819738.68
     Y    =       16782275.00  feet           Y    =         5158333.70  meter
     Z    =        7259466.29                 Z    =         2231406.56
     XDOT =      -9499.513760                 XDOT =       -2919.813610
     YDOT =      14954.134108  feet/sec       YDOT =        4525.505150  meter/sec
     ZDOT =     -17825.169509                 ZDOT =       -5447.236190
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2191740.86                 X    =          668042.61
     Y    =      -20938114.35  feet           Y    =        -6381937.26  meter
     Z    =        7338074.43                 Z    =         2236645.09
     XDOT =      15545.081746                 XDOT =        4738.140916
     YDOT =      -4659.734093  feet/sec       YDOT =       -1420.286951  meter/sec
     ZDOT =     -17885.864515                 ZDOT =       -5451.611504
  
  
    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   14210.56620089  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6447 249.5311 0006718 307.5871  52.4669 15.50478585 17904
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14210.56620089   =   yrday.fracday
    Element set:     901
    Inclination:       51.6447  deg
    RA of node:       249.5311  deg
    Eccentricity:     .0006718     
    Arg of perigee:   307.5871  deg
    Mean anomaly:      52.4669  deg
    Mean motion:   15.50478585  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1790
    Checksum:              320
 
 
    Coasting Arc #3 (Orbit 1804)
    ---------------------------------------
 
    Vector Time (GMT): 2014/211/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4091858.38                 A    =         6798544.41  meter
     Y    =       -5128275.69  meter          E    =           .0010153
     Z    =       -1757290.76                 I    =           51.33520
     XDOT =       2933.052795                 Wp   =          357.85139
     YDOT =      -4272.290374  meter/sec      RA   =          243.78921  deg
     ZDOT =       5647.023507                 TA   =          342.79721
                                              MA   =          342.83160
                                              Ha   =            226.163  n.mi
                                              Hp   =            222.079
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13424732.21                 X    =        -4025672.49
     Y    =      -16825051.48  feet           Y    =        -5173663.41  meter
     Z    =       -5765389.65                 Z    =        -1777007.38
     XDOT =       9622.876623                 XDOT =        2953.177558
     YDOT =     -14016.700702  feet/sec       YDOT =       -4239.378593  meter/sec
     ZDOT =      18526.980011                 ZDOT =        5661.320490
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1356801.99                 X    =         -413553.25
     Y    =       21459327.88  feet           Y    =         6540803.14  meter
     Z    =       -5848234.38                 Z    =        -1782541.84
     XDOT =     -14886.508881                 XDOT =       -4537.407907
     YDOT =       4116.760700  feet/sec       YDOT =        1254.788661  meter/sec
     ZDOT =      18588.354175                 ZDOT =        5665.730353
  
  
    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   14211.53301230  .00016717  00000-0  10270-3 0  9025
    2 25544  51.6454 244.7380 0006647 310.8732  49.1842 15.50503488 18053
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14211.53301230   =   yrday.fracday
    Element set:     902
    Inclination:       51.6454  deg
    RA of node:       244.7380  deg
    Eccentricity:     .0006647     
    Arg of perigee:   310.8732  deg
    Mean anomaly:      49.1842  deg
    Mean motion:   15.50503488  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1805
    Checksum:              282
 
 
    Coasting Arc #4 (Orbit 1820)
    ---------------------------------------
 
    Vector Time (GMT): 2014/212/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4284470.62                 A    =         6799244.18  meter
     Y    =        5121750.51  meter          E    =           .0007456
     Z    =        1266837.90                 I    =           51.35076
     XDOT =      -3024.503088                 Wp   =          107.47503
     YDOT =       3973.187723  meter/sec      RA   =          238.81310  deg
     ZDOT =      -5808.259270                 TA   =           58.71728
                                              MA   =           58.64428
                                              Ha   =            226.501  n.mi
                                              Hp   =            221.885
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14056662.15                 X    =         4220725.80
     Y    =       16803643.40  feet           Y    =         5169305.81  meter
     Z    =        4156292.33                 Z    =         1287496.14
     XDOT =      -9922.910394                 XDOT =       -3040.493117
     YDOT =      13035.392792  feet/sec       YDOT =        3939.276360  meter/sec
     ZDOT =     -19055.968734                 ZDOT =       -5822.990532
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         489786.96                 X    =          149287.07
     Y    =      -21885674.59  feet           Y    =        -6670753.62  meter
     Z    =        4243147.96                 Z    =         1293311.50
     XDOT =      14361.658194                 XDOT =        4377.433418
     YDOT =      -3401.680646  feet/sec       YDOT =       -1036.832261  meter/sec
     ZDOT =     -19119.133483                 ZDOT =       -5827.511886
  
  
    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   14212.56427344  .00016717  00000-0  10270-3 0  9035
    2 25544  51.6443 239.6247 0006723 315.8541  44.2073 15.50481420 18215
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14212.56427344   =   yrday.fracday
    Element set:     903
    Inclination:       51.6443  deg
    RA of node:       239.6247  deg
    Eccentricity:     .0006723     
    Arg of perigee:   315.8541  deg
    Mean anomaly:      44.2073  deg
    Mean motion:   15.50481420  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1821
    Checksum:              284
 
 
    Coasting Arc #5 (Orbit 1835)
    ---------------------------------------
 
    Vector Time (GMT): 2014/213/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4467560.38                 A    =         6799559.72  meter
     Y    =       -5054636.30  meter          E    =           .0013088
     Z    =        -781368.59                 I    =           51.36975
     XDOT =       3157.576883                 Wp   =            9.54073
     YDOT =      -3702.380528  meter/sec      RA   =          233.83913  deg
     ZDOT =       5923.660043                 TA   =          341.98964
                                              MA   =          342.03597
                                              Ha   =            226.483  n.mi
                                              Hp   =            221.726
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14657350.33                 X    =        -4406910.64
     Y    =      -16583452.44  feet           Y    =        -5104256.33  meter
     Z    =       -2563545.25                 Z    =         -802923.82
     XDOT =      10359.504210                 XDOT =        3169.968129
     YDOT =     -12146.917742  feet/sec       YDOT =       -3667.001159  meter/sec
     ZDOT =      19434.580194                 ZDOT =        5939.029063
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         495579.42                 X    =          151052.61
     Y    =       22116284.37  feet           Y    =         6741043.48  meter
     Z    =       -2654231.40                 Z    =         -809009.73
     XDOT =     -14043.464779                 XDOT =       -4280.448064
     YDOT =       2644.737540  feet/sec       YDOT =         806.116002  meter/sec
     ZDOT =      19500.406364                 ZDOT =        5943.723860
  
  
    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   14213.53107678  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6449 234.8318 0006698 318.6948  41.3695 15.50521419 18367
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14213.53107678   =   yrday.fracday
    Element set:     904
    Inclination:       51.6449  deg
    RA of node:       234.8318  deg
    Eccentricity:     .0006698     
    Arg of perigee:   318.6948  deg
    Mean anomaly:      41.3695  deg
    Mean motion:   15.50521419  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1836
    Checksum:              330
 
 
    Coasting Arc #6 (Orbit 1851)
    ---------------------------------------
 
    Vector Time (GMT): 2014/214/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4626937.10                 A    =         6799888.69  meter
     Y    =        4972832.76  meter          E    =           .0006102
     Z    =         267500.24                 I    =           51.38858
     XDOT =      -3338.634192                 Wp   =          118.38994
     YDOT =       3433.369419  meter/sec      RA   =          228.86588  deg
     ZDOT =      -5976.736687                 TA   =           58.72340
                                              MA   =           58.66365
                                              Ha   =            226.825  n.mi
                                              Hp   =            221.530
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15180239.83                 X    =         4569686.44
     Y    =       16315068.11  feet           Y    =         5024254.05  meter
     Z    =         877625.47                 Z    =          289838.03
     XDOT =     -10953.524252                 XDOT =       -3347.745929
     YDOT =      11264.335364  feet/sec       YDOT =        3395.983714  meter/sec
     ZDOT =     -19608.716164                 ZDOT =       -5992.977312
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1459140.43                 X    =         -444746.00
     Y    =      -22233266.61  feet           Y    =        -6776699.66  meter
     Z    =         971658.43                 Z    =          296161.49
     XDOT =      13888.693959                 XDOT =        4233.273919
     YDOT =      -1784.632403  feet/sec       YDOT =        -543.955957  meter/sec
     ZDOT =     -19678.199432                 ZDOT =       -5997.915187
  
  
    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   14214.56233003  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6439 229.7183 0006826 323.8096  36.2592 15.50488876 18520
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14214.56233003   =   yrday.fracday
    Element set:     905
    Inclination:       51.6439  deg
    RA of node:       229.7183  deg
    Eccentricity:     .0006826     
    Arg of perigee:   323.8096  deg
    Mean anomaly:      36.2592  deg
    Mean motion:   15.50488876  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1852
    Checksum:              320
 
 
    Coasting Arc #7 (Orbit 1867)
    ---------------------------------------
 
    Vector Time (GMT): 2014/215/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4760458.35                 A    =         6799770.46  meter
     Y    =       -4836303.76  meter          E    =           .0015052
     Z    =         231167.66                 I    =           51.40995
     XDOT =       3555.957325                 Wp   =           21.36700
     YDOT =      -3208.781819  meter/sec      RA   =          223.89511  deg
     ZDOT =       5987.141338                 TA   =          341.12939
                                              MA   =          341.18512
                                              Ha   =            226.788  n.mi
                                              Hp   =            221.371
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15618301.69                 X    =        -4707146.82
     Y    =      -15867138.31  feet           Y    =        -4889240.19  meter
     Z    =         758424.09                 Z    =          208171.59
     XDOT =      11666.526658                 XDOT =        3562.490926
     YDOT =     -10527.499405  feet/sec       YDOT =       -3168.980343  meter/sec
     ZDOT =      19642.852158                 ZDOT =        6004.431417
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2470771.41                 X    =          753091.13
     Y    =       22129849.88  feet           Y    =         6745178.24  meter
     Z    =         661563.03                 Z    =          201644.41
     XDOT =     -13966.148809                 XDOT =       -4256.882157
     YDOT =        957.568714  feet/sec       YDOT =         291.866944  meter/sec
     ZDOT =      19716.757430                 ZDOT =        6009.667665
  
  
    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   14215.59357664  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6440 224.6059 0006778 326.4296  33.6425 15.50539545 18688
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14215.59357664   =   yrday.fracday
    Element set:     906
    Inclination:       51.6440  deg
    RA of node:       224.6059  deg
    Eccentricity:     .0006778     
    Arg of perigee:   326.4296  deg
    Mean anomaly:      33.6425  deg
    Mean motion:   15.50539545  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1868
    Checksum:              333
 
 
    Coasting Arc #8 (Orbit 1882)
    ---------------------------------------
 
    Vector Time (GMT): 2014/216/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4860562.95                 A    =         6799667.65  meter
     Y    =        4694154.01  meter          E    =           .0003887
     Z    =        -749997.77                 I    =           51.43157
     XDOT =      -3808.054495                 Wp   =          119.00203
     YDOT =       3000.022716  meter/sec      RA   =          218.92469  deg
     ZDOT =      -5927.517222                 TA   =           69.10899
                                              MA   =           69.06738
                                              Ha   =            227.131  n.mi
                                              Hp   =            221.172
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15946728.85                 X    =         4811353.83
     Y    =       15400767.74  feet           Y    =         4748232.83  meter
     Z    =       -2460622.61                 Z    =         -726505.37
     XDOT =     -12493.617110                 XDOT =       -3812.524591
     YDOT =       9842.594211  feet/sec       YDOT =        2957.413747  meter/sec
     ZDOT =     -19447.234979                 ZDOT =       -5946.026902
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3403248.37                 X    =        -1037310.10
     Y    =      -21917507.31  feet           Y    =        -6680456.23  meter
     Z    =       -2361619.20                 Z    =         -719821.53
     XDOT =      14205.452761                 XDOT =        4329.822002
     YDOT =       -111.076109  feet/sec       YDOT =         -33.855998  meter/sec
     ZDOT =     -19526.290069                 ZDOT =       -5951.613213
  
  
    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   14216.56037050  .00016717  00000-0  10270-3 0  9074
    2 25544  51.6432 219.8119 0006987 331.5717  28.5052 15.50501817 18836
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14216.56037050   =   yrday.fracday
    Element set:     907
    Inclination:       51.6432  deg
    RA of node:       219.8119  deg
    Eccentricity:     .0006987     
    Arg of perigee:   331.5717  deg
    Mean anomaly:      28.5052  deg
    Mean motion:   15.50501817  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1883
    Checksum:              304
 
 
    Coasting Arc #9 (Orbit 1898)
    ---------------------------------------
 
    Vector Time (GMT): 2014/217/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4920906.98                 A    =         6799128.70  meter
     Y    =       -4508574.31  meter          E    =           .0015892
     Z    =        1243867.75                 I    =           51.45467
     XDOT =       4087.696221                 Wp   =           33.10285
     YDOT =      -2847.031728  meter/sec      RA   =          213.95674  deg
     ZDOT =       5829.775534                 TA   =          340.44525
                                              MA   =          340.50614
                                              Ha   =            227.100  n.mi
                                              Hp   =            221.010
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16144707.95                 X    =        -4876167.61
     Y    =      -14791910.47  feet           Y    =        -4563352.96  meter
     Z    =        4080930.92                 Z    =         1220071.32
     XDOT =      13411.076840                 XDOT =        4090.909587
     YDOT =      -9340.655275  feet/sec       YDOT =       -2801.302735  meter/sec
     ZDOT =      19126.560151                 ZDOT =        5849.640551
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4307503.97                 X    =         1312927.21
     Y    =       21487356.61  feet           Y    =         6549346.29  meter
     Z    =        3980593.32                 Z    =         1213284.84
     XDOT =     -14673.605743                 XDOT =       -4472.515031
     YDOT =       -631.235408  feet/sec       YDOT =        -192.400552  meter/sec
     ZDOT =      19211.353123                 ZDOT =        5855.620432
  
  
    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   14217.59160862  .00016717  00000-0  10270-3 0  9087
    2 25544  51.6428 214.6995 0006895 333.8603  26.2199 15.50552446 18991
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14217.59160862   =   yrday.fracday
    Element set:     908
    Inclination:       51.6428  deg
    RA of node:       214.6995  deg
    Eccentricity:     .0006895     
    Arg of perigee:   333.8603  deg
    Mean anomaly:      26.2199  deg
    Mean motion:   15.50552446  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1899
    Checksum:              342
 
 
    Coasting Arc #10 (Orbit 1913)
    ---------------------------------------
 
    Vector Time (GMT): 2014/218/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4942612.02                 A    =         6798595.31  meter
     Y    =        4329742.33  meter          E    =           .0002251
     Z    =       -1748516.41                 I    =           51.47864
     XDOT =      -4382.580999                 Wp   =           72.28532
     YDOT =       2720.412858  meter/sec      RA   =          208.98889  deg
     ZDOT =      -5657.415083                 TA   =          126.90350
                                              MA   =          126.88287
                                              Ha   =            227.414  n.mi
                                              Hp   =            220.813
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16215918.71                 X    =         4902322.16
     Y    =       14205191.38  feet           Y    =         4384788.62  meter
     Z    =       -5736602.39                 Z    =        -1724603.76
     XDOT =     -14378.546584                 XDOT =       -4385.193913
     YDOT =       8925.239034  feet/sec       YDOT =        2671.389685  meter/sec
     ZDOT =     -18561.073106                 ZDOT =       -5678.711054
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5081676.50                 X    =        -1548895.00
     Y    =      -20977779.45  feet           Y    =        -6394027.18  meter
     Z    =       -5635727.28                 Z    =        -1717769.67
     XDOT =      15267.393655                 XDOT =        4653.501586
     YDOT =       1307.686759  feet/sec       YDOT =         398.582924  meter/sec
     ZDOT =     -18651.932052                 ZDOT =       -5685.108889
  
  
    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   14218.55839419  .00016717  00000-0  10270-3 0  9096
    2 25544  51.6425 209.9053 0007156 339.0970  20.9887 15.50517829 19145
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14218.55839419   =   yrday.fracday
    Element set:     909
    Inclination:       51.6425  deg
    RA of node:       209.9053  deg
    Eccentricity:     .0007156     
    Arg of perigee:   339.0970  deg
    Mean anomaly:      20.9887  deg
    Mean motion:   15.50517829  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1914
    Checksum:              335
 
 
    Coasting Arc #11 (Orbit 1929)
    ---------------------------------------
 
    Vector Time (GMT): 2014/219/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4914528.98                 A    =         6797703.46  meter
     Y    =       -4122719.02  meter          E    =           .0015571
     Z    =        2219003.24                 I    =           51.50339
     XDOT =       4694.408548                 Wp   =           44.40795
     YDOT =      -2654.965146  meter/sec      RA   =          204.02333  deg
     ZDOT =       5451.918661                 TA   =          340.28173
                                              MA   =          340.34187
                                              Ha   =            227.418  n.mi
                                              Hp   =            220.642
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16123782.74                 X    =        -4878841.59
     Y    =      -13525981.03  feet           Y    =        -4177477.03  meter
     Z    =        7280194.37                 Z    =         2195215.94
     XDOT =      15401.602849                 XDOT =        4697.264772
     YDOT =      -8710.515571  feet/sec       YDOT =       -2602.453560  meter/sec
     ZDOT =      17886.872249                 ZDOT =        5474.729926
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5755899.84                 X    =         1754398.27
     Y    =       20279295.57  feet           Y    =         6181129.29  meter
     Z    =        7179801.58                 Z    =         2188403.52
     XDOT =     -16060.378793                 XDOT =       -4895.203456
     YDOT =      -1823.275579  feet/sec       YDOT =        -555.734397  meter/sec
     ZDOT =      17984.167322                 ZDOT =        5481.574200
  
  
    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   14219.58962369  .00016717  00000-0  10270-3 0  9103
    2 25544  51.6422 204.7926 0007041 341.3526  18.7366 15.50559948 19303
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14219.58962369   =   yrday.fracday
    Element set:     910
    Inclination:       51.6422  deg
    RA of node:       204.7926  deg
    Eccentricity:     .0007041     
    Arg of perigee:   341.3526  deg
    Mean anomaly:      18.7366  deg
    Mean motion:   15.50559948  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1930
    Checksum:              320
 
 
    Coasting Arc #12 (Orbit 1944)
    ---------------------------------------
 
    Vector Time (GMT): 2014/220/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4848474.30                 A    =         6796810.36  meter
     Y    =        3936508.87  meter          E    =           .0004783
     Z    =       -2690170.43                 I    =           51.52932
     XDOT =      -4997.545343                 Wp   =           29.07269
     YDOT =       2621.074671  meter/sec      RA   =          199.05783  deg
     ZDOT =      -5171.431019                 TA   =          181.27832
                                              MA   =          181.27954
                                              Ha   =            227.666  n.mi
                                              Hp   =            220.466
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15907067.90                 X    =         4817162.75
     Y    =       12915055.36  feet           Y    =         3990552.68  meter
     Z    =       -8826018.46                 Z    =        -2666693.53
     XDOT =     -16396.146137                 XDOT =       -5001.362683
     YDOT =       8599.326348  feet/sec       YDOT =        2565.167779  meter/sec
     ZDOT =     -16966.637200                 ZDOT =       -5195.717106
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6265896.56                 X    =        -1909845.27
     Y    =      -19552797.34  feet           Y    =        -5959692.63  meter
     Z    =       -8726896.49                 Z    =        -2659958.05
     XDOT =      16910.449892                 XDOT =        5154.305127
     YDOT =       2200.030328  feet/sec       YDOT =         670.569244  meter/sec
     ZDOT =     -17070.203135                 ZDOT =       -5202.997916
  
  
    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   14220.55640025  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6425 199.9983 0007302 346.2722  13.8229 15.50534625 19451
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14220.55640025   =   yrday.fracday
    Element set:     911
    Inclination:       51.6425  deg
    RA of node:       199.9983  deg
    Eccentricity:     .0007302     
    Arg of perigee:   346.2722  deg
    Mean anomaly:      13.8229  deg
    Mean motion:   15.50534625  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1945
    Checksum:              300
 
 
    Coasting Arc #13 (Orbit 1960)
    ---------------------------------------
 
    Vector Time (GMT): 2014/221/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4727367.08                 A    =         6795671.82  meter
     Y    =       -3739475.86  meter          E    =           .0014173
     Z    =        3118585.76                 I    =           51.55586
     XDOT =       5306.765791                 Wp   =           54.66191
     YDOT =      -2647.341476  meter/sec      RA   =          194.09458  deg
     ZDOT =       4862.363374                 TA   =          341.26239
                                              MA   =          341.31451
                                              Ha   =            227.718  n.mi
                                              Hp   =            220.273
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15509734.52                 X    =        -4700348.81
     Y    =      -12268621.59  feet           Y    =        -3792189.33  meter
     Z    =       10231580.59                 Z    =         3095686.92
     XDOT =      17410.648919                 XDOT =        5312.355285
     YDOT =      -8685.503531  feet/sec       YDOT =       -2587.966662  meter/sec
     ZDOT =      15952.635741                 ZDOT =        4888.155840
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6618045.80                 X    =         2017180.36
     Y    =       18688021.66  feet           Y    =         5696109.00  meter
     Z    =       10134865.47                 Z    =         3089106.99
     XDOT =     -17910.007082                 XDOT =       -5458.970158
     YDOT =      -2382.163303  feet/sec       YDOT =        -726.083375  meter/sec
     ZDOT =      16062.616594                 ZDOT =        4895.885538
  
  
    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   14221.58762093  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6428 194.8855 0007184 348.7570  11.3420 15.50566333 19617
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14221.58762093   =   yrday.fracday
    Element set:     912
    Inclination:       51.6428  deg
    RA of node:       194.8855  deg
    Eccentricity:     .0007184     
    Arg of perigee:   348.7570  deg
    Mean anomaly:      11.3420  deg
    Mean motion:   15.50566333  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1961
    Checksum:              311
 
 
    Coasting Arc #14 (Orbit 1975)
    ---------------------------------------
 
    Vector Time (GMT): 2014/222/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4575656.08                 A    =         6794560.49  meter
     Y    =        3576950.70  meter          E    =           .0008752
     Z    =       -3537471.83                 I    =           51.58318
     XDOT =      -5581.756146                 Wp   =           28.89720
     YDOT =       2703.818538  meter/sec      RA   =          189.13152  deg
     ZDOT =      -4483.073847                 TA   =          192.70233
                                              MA   =          192.72440
                                              Ha   =            227.890  n.mi
                                              Hp   =            220.128
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15011995.02                 X    =         4552501.22
     Y    =       11735402.56  feet           Y    =         3627989.16  meter
     Z    =      -11605878.71                 Z    =        -3515300.72
     XDOT =     -18312.848247                 XDOT =       -5589.799203
     YDOT =       8870.795729  feet/sec       YDOT =        2641.354756  meter/sec
     ZDOT =     -14708.247530                 ZDOT =       -4510.208133
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6797526.47                 X    =        -2071886.07
     Y    =      -17861653.15  feet           Y    =        -5444231.88  meter
     Z    =      -11512213.90                 Z    =        -3508922.80
     XDOT =      18874.053234                 XDOT =        5752.811426
     YDOT =       2377.578489  feet/sec       YDOT =         724.685923  meter/sec
     ZDOT =     -14823.948664                 ZDOT =       -4518.339553
  
  
    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   14222.55438833  .00016717  00000-0  10270-3 0  9131
    2 25544  51.6435 190.0913 0007413 353.1782   6.9267 15.50551152 19766
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14222.55438833   =   yrday.fracday
    Element set:     913
    Inclination:       51.6435  deg
    RA of node:       190.0913  deg
    Eccentricity:     .0007413     
    Arg of perigee:   353.1782  deg
    Mean anomaly:       6.9267  deg
    Mean motion:   15.50551152  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1976
    Checksum:              301
 
 
    Coasting Arc #15 (Orbit 1991)
    ---------------------------------------
 
    Vector Time (GMT): 2014/223/12:42:29.731
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4368563.10                 A    =         6793311.88  meter
     Y    =       -3421146.60  meter          E    =           .0011957
     Z    =        3905651.79                 I    =           51.61098
     XDOT =       5853.322654                 Wp   =           62.57970
     YDOT =      -2813.182839  meter/sec      RA   =          184.17078  deg
     ZDOT =       4078.671392                 TA   =          344.67231
                                              MA   =          344.70850
                                              Ha   =            227.973  n.mi
                                              Hp   =            219.912
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14332556.10                 X    =        -4348954.35
     Y    =      -11224234.25  feet           Y    =        -3469888.94  meter
     Z    =       12813818.20                 Z    =         3884478.12
     XDOT =      19203.814481                 XDOT =        5864.532850
     YDOT =      -9229.602491  feet/sec       YDOT =       -2747.664412  meter/sec
     ZDOT =      13381.467823                 ZDOT =        4107.132678
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6781665.61                 X    =         2067051.68
     Y    =       16961702.63  feet           Y    =         5169926.96  meter
     Z    =       12724354.26                 Z    =         3878383.18
     XDOT =     -19926.598444                 XDOT =       -6073.627206
     YDOT =      -2172.903644  feet/sec       YDOT =        -662.301031  meter/sec
     ZDOT =      13502.833794                 ZDOT =        4115.663740
  
  
    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   14223.58559992  .00016717  00000-0  10270-3 0  9146
    2 25544  51.6443 184.9787 0007298 355.9567   4.1524 15.50576599 19924
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14223.58559992   =   yrday.fracday
    Element set:     914
    Inclination:       51.6443  deg
    RA of node:       184.9787  deg
    Eccentricity:     .0007298     
    Arg of perigee:   355.9567  deg
    Mean anomaly:       4.1524  deg
    Mean motion:   15.50576599  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1992
    Checksum:              364
 
             

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