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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  9256.96
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   71.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.07
   ET - UTC  (sec) :   65.18
   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 2242)
    ---------------------------------------
 
    Vector Time (GMT): 2008/130/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         213473.80                 A    =         6715477.05  meter
     Y    =       -4599788.86  meter          E    =           .0010581
     Z    =        4887941.70                 I    =           51.43921
     XDOT =       6887.627628                 Wp   =          157.41052
     YDOT =       2664.431997  meter/sec      RA   =          214.85672  deg
     ZDOT =       2195.354167                 TA   =          271.15777
                                              MA   =          271.27900
                                              Ha   =            187.506  n.mi
                                              Hp   =            180.502
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         700373.36                 X    =          241148.65
     Y    =      -15091170.79  feet           Y    =        -4597247.58  meter
     Z    =       16036554.15                 Z    =         4889045.38
     XDOT =      22597.203505                 XDOT =        6846.656947
     YDOT =       8741.574793  feet/sec       YDOT =        2741.224018  meter/sec
     ZDOT =       7202.605534                 ZDOT =        2228.715248
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10607075.96                 X    =        -3233036.75
     Y    =      -10751900.35  feet           Y    =        -3277179.23  meter
     Z    =       16040311.91                 Z    =         4889087.07
     XDOT =      21006.359462                 XDOT =        6402.738364
     YDOT =      -9731.818552  feet/sec       YDOT =       -2966.258295  meter/sec
     ZDOT =       7330.989741                 ZDOT =        2234.485673
  
  
    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   08130.55138401  .00020000  00000-0  20000-3 0  9008
    2 25544  51.6409 215.5337 0006386 192.6751 167.4254 15.76207648 22433
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08130.55138401   =   yrday.fracday
    Element set:     900
    Inclination:       51.6409  deg
    RA of node:       215.5337  deg
    Eccentricity:     .0006386     
    Arg of perigee:   192.6751  deg
    Mean anomaly:     167.4254  deg
    Mean motion:   15.76207648  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2243
    Checksum:              283
 
 
    Coasting Arc #2 (Orbit 2257)
    ---------------------------------------
 
    Vector Time (GMT): 2008/131/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6162633.98                 A    =         6725319.13  meter
     Y    =       -2408145.20  meter          E    =           .0004049
     Z    =       -1203364.35                 I    =           51.49652
     XDOT =        782.369713                 Wp   =           69.57242
     YDOT =      -4924.759337  meter/sec      RA   =          209.66306  deg
     ZDOT =       5865.947790                 TA   =          277.20961
                                              MA   =          277.25564
                                              Ha   =            187.335  n.mi
                                              Hp   =            180.733
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20218615.42                 X    =        -6129401.97
     Y    =       -7900738.86  feet           Y    =        -2476873.36  meter
     Z    =       -3948045.78                 Z    =        -1233222.01
     XDOT =       2566.829767                 XDOT =         808.885264
     YDOT =     -16157.346907  feet/sec       YDOT =       -4915.862835  meter/sec
     ZDOT =      19245.235531                 ZDOT =        5869.812398
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19400529.75                 X    =        -5913281.47
     Y    =        9690866.66  feet           Y    =         2953776.16  meter
     Z    =       -4062966.71                 Z    =        -1238392.25
     XDOT =      -9636.110057                 XDOT =       -2937.086346
     YDOT =     -11239.297033  feet/sec       YDOT =       -3425.737736  meter/sec
     ZDOT =      19259.559056                 ZDOT =        5870.313600
  
  
    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   08131.50239849  .00020000  00000-0  20000-3 0  9013
    2 25544  51.6403 210.6345 0006099 196.9589 163.1372 15.76174627 22589
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08131.50239849   =   yrday.fracday
    Element set:     901
    Inclination:       51.6403  deg
    RA of node:       210.6345  deg
    Eccentricity:     .0006099     
    Arg of perigee:   196.9589  deg
    Mean anomaly:     163.1372  deg
    Mean motion:   15.76174627  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2258
    Checksum:              304
 
 
    Coasting Arc #3 (Orbit 2273)
    ---------------------------------------
 
    Vector Time (GMT): 2008/132/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1216464.82                 A    =         6713884.76  meter
     Y    =        4029818.22  meter          E    =           .0013511
     Z    =       -5240915.63                 I    =           51.48350
     XDOT =      -7145.192114                 Wp   =          110.46711
     YDOT =      -2812.644158  meter/sec      RA   =          204.51633  deg
     ZDOT =       -509.923934                 TA   =          154.70807
                                              MA   =          154.64186
                                              Ha   =            187.136  n.mi
                                              Hp   =            180.802
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3991026.32                 X    =        -1235977.07
     Y    =       13221188.39  feet           Y    =         4016106.39  meter
     Z    =      -17194605.10                 Z    =        -5246872.25
     XDOT =     -23442.231344                 XDOT =       -7110.732522
     YDOT =      -9227.835164  feet/sec       YDOT =       -2892.353064  meter/sec
     ZDOT =      -1672.978787                 ZDOT =        -544.551813
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7402543.75                 X    =         2256295.34
     Y    =       11625742.48  feet           Y    =         3543526.31  meter
     Z    =      -17217055.96                 Z    =        -5247758.66
     XDOT =     -21511.003366                 XDOT =       -6556.553826
     YDOT =      11049.544541  feet/sec       YDOT =        3367.901176  meter/sec
     ZDOT =      -1806.279139                 ZDOT =        -550.553882
  
  
    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   08132.51679482  .00020000  00000-0  20000-3 0  9027
    2 25544  51.6395 205.4079 0006152 200.8933 159.1980 15.76218254 22746
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08132.51679482   =   yrday.fracday
    Element set:     902
    Inclination:       51.6395  deg
    RA of node:       205.4079  deg
    Eccentricity:     .0006152     
    Arg of perigee:   200.8933  deg
    Mean anomaly:     159.1980  deg
    Mean motion:   15.76218254  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2274
    Checksum:              295
 
 
    Coasting Arc #4 (Orbit 2289)
    ---------------------------------------
 
    Vector Time (GMT): 2008/133/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6239207.20                 A    =         6725696.31  meter
     Y    =        2465221.07  meter          E    =           .0015115
     Z    =        -325264.52                 I    =           51.55110
     XDOT =      -2030.777869                 Wp   =          158.83513
     YDOT =       4357.843401  meter/sec      RA   =          199.35365  deg
     ZDOT =      -6026.068256                 TA   =           24.71009
                                              MA   =           24.63776
                                              Ha   =            186.970  n.mi
                                              Hp   =            180.860
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20469839.89                 X    =         6212757.07
     Y    =        8087995.64  feet           Y    =         2534843.59  meter
     Z    =       -1067140.82                 Z    =         -295018.51
     XDOT =      -6662.657049                 XDOT =       -2050.083458
     YDOT =      14297.386487  feet/sec       YDOT =        4335.026551  meter/sec
     ZDOT =     -19770.565144                 ZDOT =       -6035.980376
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19379159.86                 X    =         5906767.92
     Y    =      -10445723.99  feet           Y    =        -3183856.67  meter
     Z    =        -950695.36                 Z    =         -289771.95
     XDOT =       5950.567328                 XDOT =        1813.732922
     YDOT =      12808.770434  feet/sec       YDOT =        3904.113228  meter/sec
     ZDOT =     -19808.173628                 ZDOT =       -6037.531322
  
  
    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   08133.53117264  .00020000  00000-0  20000-3 0  9036
    2 25544  51.6396 200.1812 0005982 203.4523 156.6370 15.76269579 22907
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08133.53117264   =   yrday.fracday
    Element set:     903
    Inclination:       51.6396  deg
    RA of node:       200.1812  deg
    Eccentricity:     .0005982     
    Arg of perigee:   203.4523  deg
    Mean anomaly:     156.6370  deg
    Mean motion:   15.76269579  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2290
    Checksum:              285
 
 
    Coasting Arc #5 (Orbit 2305)
    ---------------------------------------
 
    Vector Time (GMT): 2008/134/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2342842.94                 A    =         6713950.27  meter
     Y    =       -3622114.48  meter          E    =           .0002976
     Z    =        5143893.03                 I    =           51.54057
     XDOT =       7067.728678                 Wp   =          172.61509
     YDOT =       2806.434975  meter/sec      RA   =          194.18073  deg
     ZDOT =      -1245.725566                 TA   =          289.28310
                                              MA   =          289.31529
                                              Ha   =            186.653  n.mi
                                              Hp   =            181.012
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7686492.59                 X    =         2358183.68
     Y    =      -11883577.69  feet           Y    =        -3595829.97  meter
     Z    =       16876289.46                 Z    =         5155311.67
     XDOT =      23188.086215                 XDOT =        7041.872923
     YDOT =       9207.463829  feet/sec       YDOT =        2885.325861  meter/sec
     ZDOT =      -4087.026136                 ZDOT =       -1211.453067
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4427053.80                 X    =        -1349366.00
     Y    =      -13387810.97  feet           Y    =        -4080604.78  meter
     Z    =       16919764.92                 Z    =         5157144.35
     XDOT =      20815.105478                 XDOT =        6344.444150
     YDOT =     -11869.901092  feet/sec       YDOT =       -3617.945853  meter/sec
     ZDOT =      -3955.066487                 ZDOT =       -1205.504265
  
  
    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   08134.54552997  .00020000  00000-0  20000-3 0  9045
    2 25544  51.6400 194.9542 0005994 209.1928 150.8902 15.76327109 23067
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08134.54552997   =   yrday.fracday
    Element set:     904
    Inclination:       51.6400  deg
    RA of node:       194.9542  deg
    Eccentricity:     .0005994     
    Arg of perigee:   209.1928  deg
    Mean anomaly:     150.8902  deg
    Mean motion:   15.76327109  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2306
    Checksum:              304
 
 
    Coasting Arc #6 (Orbit 2321)
    ---------------------------------------
 
    Vector Time (GMT): 2008/135/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5991732.27                 A    =         6724224.00  meter
     Y    =       -2428862.29  meter          E    =           .0009999
     Z    =        1837399.76                 I    =           51.60299
     XDOT =       3364.710745                 Wp   =           84.96355
     YDOT =      -4002.707185  meter/sec      RA   =          189.05000  deg
     ZDOT =       5655.654648                 TA   =          295.45077
                                              MA   =          295.55420
                                              Ha   =            186.605  n.mi
                                              Hp   =            181.160
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19657914.28                 X    =        -5973052.86
     Y    =       -7968708.30  feet           Y    =        -2495760.91  meter
     Z    =        6028214.43                 Z    =         1808336.95
     XDOT =      11039.077246                 XDOT =        3381.745207
     YDOT =     -13132.241419  feet/sec       YDOT =       -3964.986089  meter/sec
     ZDOT =      18555.297402                 ZDOT =        5672.041728
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18430477.45                 X    =        -5617609.53
     Y    =       10563529.63  feet           Y    =         3219763.83  meter
     Z    =        5916301.03                 Z    =         1803288.55
     XDOT =      -2803.355763                 XDOT =        -854.462837
     YDOT =     -15365.957174  feet/sec       YDOT =       -4683.543747  meter/sec
     ZDOT =      18617.821637                 ZDOT =        5674.712035
  
  
    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   08135.55987296  .00020000  00000-0  20000-3 0  9052
    2 25544  51.6395 189.7270 0005679 211.4440 148.6385 15.76302181 23226
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08135.55987296   =   yrday.fracday
    Element set:     905
    Inclination:       51.6395  deg
    RA of node:       189.7270  deg
    Eccentricity:     .0005679     
    Arg of perigee:   211.4440  deg
    Mean anomaly:     148.6385  deg
    Mean motion:   15.76302181  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2322
    Checksum:              310
 
 
    Coasting Arc #7 (Orbit 2336)
    ---------------------------------------
 
    Vector Time (GMT): 2008/136/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3516258.05                 A    =         6716202.96  meter
     Y    =        3416476.50  meter          E    =           .0010622
     Z    =       -4600007.59                 I    =           51.60589
     XDOT =      -6548.635874                 Wp   =          140.87911
     YDOT =      -2775.983071  meter/sec      RA   =          183.85502  deg
     ZDOT =       2939.621288                 TA   =          158.30924
                                              MA   =          158.26422
                                              Ha   =            186.351  n.mi
                                              Hp   =            181.106
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11536279.68                 X    =        -3531854.00
     Y    =       11208912.39  feet           Y    =         3377068.72  meter
     Z    =      -15091888.42                 Z    =        -4617127.49
     XDOT =     -21485.025834                 XDOT =       -6531.388010
     YDOT =      -9107.556007  feet/sec       YDOT =       -2849.117380  meter/sec
     ZDOT =       9644.426798                 ZDOT =        2907.849369
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2015584.40                 X    =          614350.13
     Y    =       15896048.47  feet           Y    =         4845115.57  meter
     Z    =      -15157296.08                 Z    =        -4619943.85
     XDOT =     -19110.594464                 XDOT =       -5824.909192
     YDOT =      11516.483492  feet/sec       YDOT =        3510.224168  meter/sec
     ZDOT =       9522.061610                 ZDOT =        2902.324379
  
  
    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   08136.51080025  .00020000  00000-0  20000-3 0  9064
    2 25544  51.6396 184.8264 0005636 215.5282 144.5508 15.76350772 23375
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08136.51080025   =   yrday.fracday
    Element set:     906
    Inclination:       51.6396  deg
    RA of node:       184.8264  deg
    Eccentricity:     .0005636     
    Arg of perigee:   215.5282  deg
    Mean anomaly:     144.5508  deg
    Mean motion:   15.76350772  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2337
    Checksum:              291
 
 
    Coasting Arc #8 (Orbit 2352)
    ---------------------------------------
 
    Vector Time (GMT): 2008/137/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5350320.38                 A    =         6720882.57  meter
     Y    =        2449195.66  meter          E    =           .0005111
     Z    =       -3242828.78                 I    =           51.65154
     XDOT =      -4655.343320                 Wp   =          168.22624
     YDOT =       3871.050036  meter/sec      RA   =          178.74828  deg
     ZDOT =      -4763.373448                 TA   =           49.75764
                                              MA   =           49.71295
                                              Ha   =            186.251  n.mi
                                              Hp   =            181.303
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17553544.56                 X    =         5338288.78
     Y    =        8035418.82  feet           Y    =         2508958.94  meter
     Z    =      -10639202.03                 Z    =        -3216865.56
     XDOT =     -15273.436088                 XDOT =       -4675.144025
     YDOT =      12700.295394  feet/sec       YDOT =        3818.880923  meter/sec
     ZDOT =     -15627.865644                 ZDOT =       -4786.037322
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16883363.15                 X    =         5146049.09
     Y    =       -9474447.30  feet           Y    =        -2887811.54  meter
     Z    =      -10539183.99                 Z    =        -3212343.28
     XDOT =        597.482437                 XDOT =         182.112647
     YDOT =      18522.303816  feet/sec       YDOT =        5645.598203  meter/sec
     ZDOT =     -15714.532555                 ZDOT =       -4789.789523
  
  
    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   08137.52510631  .00020000  00000-0  20000-3 0  9078
    2 25544  51.6400 179.5991 0005562 218.8350 141.2415 15.76389579 23535
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08137.52510631   =   yrday.fracday
    Element set:     907
    Inclination:       51.6400  deg
    RA of node:       179.5991  deg
    Eccentricity:     .0005562     
    Arg of perigee:   218.8350  deg
    Mean anomaly:     141.2415  deg
    Mean motion:   15.76389579  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2353
    Checksum:              295
 
 
    Coasting Arc #9 (Orbit 2368)
    ---------------------------------------
 
    Vector Time (GMT): 2008/138/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4542347.80                 A    =         6719506.80  meter
     Y    =       -3382714.65  meter          E    =           .0008665
     Z    =        3606366.16                 I    =           51.67565
     XDOT =       5637.445300                 Wp   =          110.62773
     YDOT =       2867.011623  meter/sec      RA   =          173.54523  deg
     ZDOT =      -4405.874775                 TA   =           26.16397
                                              MA   =           26.12022
                                              Ha   =            185.856  n.mi
                                              Hp   =            181.330
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14902715.88                 X    =         4562316.84
     Y    =      -11098145.17  feet           Y    =        -3331808.17  meter
     Z    =       11831909.99                 Z    =         3628481.53
     XDOT =      18495.555446                 XDOT =        5626.370288
     YDOT =       9406.206111  feet/sec       YDOT =        2929.991212  meter/sec
     ZDOT =     -14454.969733                 ZDOT =       -4378.514196
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -519858.34                 X    =         -158452.82
     Y    =      -18519716.32  feet           Y    =        -5644809.53  meter
     Z    =       11916531.18                 Z    =         3632158.70
     XDOT =      17043.046804                 XDOT =        5194.720666
     YDOT =      -9723.112974  feet/sec       YDOT =       -2963.604834  meter/sec
     ZDOT =     -14349.533032                 ZDOT =       -4373.737668
  
  
    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   08138.53939355  .00020000  00000-0  20000-3 0  9089
    2 25544  51.6389 174.3719 0005492 223.8315 136.2414 15.76432258 23694
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08138.53939355   =   yrday.fracday
    Element set:     908
    Inclination:       51.6389  deg
    RA of node:       174.3719  deg
    Eccentricity:     .0005492     
    Arg of perigee:   223.8315  deg
    Mean anomaly:     136.2414  deg
    Mean motion:   15.76432258  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2369
    Checksum:              315
 
 
    Coasting Arc #10 (Orbit 2384)
    ---------------------------------------
 
    Vector Time (GMT): 2008/139/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4402505.92                 A    =         6717109.57  meter
     Y    =       -2607875.93  meter          E    =           .0008636
     Z    =        4351189.41                 I    =           51.69559
     XDOT =       5695.060121                 Wp   =          143.01536
     YDOT =      -3911.627592  meter/sec      RA   =          168.44463  deg
     ZDOT =       3407.541362                 TA   =          272.62511
                                              MA   =          272.72396
                                              Ha   =            185.882  n.mi
                                              Hp   =            181.409
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14443917.07                 X    =        -4394154.76
     Y    =       -8556023.41  feet           Y    =        -2657061.04  meter
     Z    =       14275555.80                 Z    =         4329821.60
     XDOT =      18684.580450                 XDOT =        5721.823725
     YDOT =     -12833.423858  feet/sec       YDOT =       -3847.792892  meter/sec
     ZDOT =      11179.597645                 ZDOT =        3435.273126
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15241510.44                 X    =        -4645612.38
     Y    =        7202365.00  feet           Y    =         2195280.85  meter
     Z    =       14193169.78                 Z    =         4326078.15
     XDOT =        379.883597                 XDOT =         115.788520
     YDOT =     -21502.820751  feet/sec       YDOT =       -6554.059765  meter/sec
     ZDOT =      11285.757883                 ZDOT =        3439.899003
  
  
    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   08139.55366473  .00020000  00000-0  20000-3 0  9098
    2 25544  51.6383 169.1438 0005356 226.3990 133.6731 15.76431267 23854
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08139.55366473   =   yrday.fracday
    Element set:     909
    Inclination:       51.6383  deg
    RA of node:       169.1438  deg
    Eccentricity:     .0005356     
    Arg of perigee:   226.3990  deg
    Mean anomaly:     133.6731  deg
    Mean motion:   15.76431267  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2385
    Checksum:              314
 
 
    Coasting Arc #11 (Orbit 2399)
    ---------------------------------------
 
    Vector Time (GMT): 2008/140/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5309715.75                 A    =         6722797.10  meter
     Y    =        3452787.75  meter          E    =           .0000755
     Z    =       -2252759.75                 I    =           51.74503
     XDOT =      -4389.238832                 Wp   =          358.37021
     YDOT =      -3182.164942  meter/sec      RA   =          163.25188  deg
     ZDOT =       5468.775077                 TA   =          336.36793
                                              MA   =          336.37139
                                              Ha   =            185.588  n.mi
                                              Hp   =            181.371
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17420327.26                 X    =        -5336987.01
     Y    =       11328043.81  feet           Y    =         3393259.28  meter
     Z    =       -7390944.08                 Z    =        -2278620.68
     XDOT =     -14400.389869                 XDOT =       -4379.895995
     YDOT =     -10440.173694  feet/sec       YDOT =       -3231.196379  meter/sec
     ZDOT =      17942.175449                 ZDOT =        5447.474013
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         -44221.90                 X    =          -13478.84
     Y    =       20744076.68  feet           Y    =         6322794.57  meter
     Z    =       -7489977.29                 Z    =        -2282945.08
     XDOT =     -15166.469553                 XDOT =       -4622.739920
     YDOT =       6415.484854  feet/sec       YDOT =        1955.439783  meter/sec
     ZDOT =      17859.981515                 ZDOT =        5443.722366
  
  
    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   08140.50452668  .00020000  00000-0  20000-3 0  9109
    2 25544  51.6391 164.2431 0005395 229.8014 130.2679 15.76499141 24007
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08140.50452668   =   yrday.fracday
    Element set:     910
    Inclination:       51.6391  deg
    RA of node:       164.2431  deg
    Eccentricity:     .0005395     
    Arg of perigee:   229.8014  deg
    Mean anomaly:     130.2679  deg
    Mean motion:   15.76499141  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2400
    Checksum:              278
 
 
    Coasting Arc #12 (Orbit 2415)
    ---------------------------------------
 
    Vector Time (GMT): 2008/141/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 615213.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3214303.74                 A    =         6714002.10  meter
     Y    =        3018585.74  meter          E    =           .0008760
     Z    =       -5070482.78                 I    =           51.74207
     XDOT =      -6374.060232                 Wp   =           90.85950
     YDOT =       3979.701126  meter/sec      RA   =          158.13899  deg
     ZDOT =      -1674.060955                 TA   =          163.07846
                                              MA   =          163.04923
                                              Ha   =            185.445  n.mi
                                              Hp   =            181.678
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10545615.95                 X    =         3204942.48
     Y    =        9903496.54  feet           Y    =         3054478.32  meter
     Z    =      -16635442.21                 Z    =        -5054889.71
     XDOT =     -20912.271101                 XDOT =       -6409.955705
     YDOT =      13056.762223  feet/sec       YDOT =        3908.222280  meter/sec
     ZDOT =      -5492.325967                 ZDOT =       -1705.113320
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14052373.83                 X    =         4283163.54
     Y    =       -3717627.58  feet           Y    =        -1133132.89  meter
     Z    =      -16575199.30                 Z    =        -5052120.75
     XDOT =       -364.540034                 XDOT =        -111.111802
     YDOT =      23601.949669  feet/sec       YDOT =        7193.874259  meter/sec
     ZDOT =      -5611.275091                 ZDOT =       -1710.316648
  
  
    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   08141.51876241  .00020000  00000-0  20000-3 0  9119
    2 25544  51.6386 159.0150 0005417 235.2106 124.8549 15.76481403 24163
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      08141.51876241   =   yrday.fracday
    Element set:     911
    Inclination:       51.6386  deg
    RA of node:       159.0150  deg
    Eccentricity:     .0005417     
    Arg of perigee:   235.2106  deg
    Mean anomaly:     124.8549  deg
    Mean motion:   15.76481403  rev/day
    Decay rate:    2.00000E-04  rev/day^2
    Epoch rev:            2416
    Checksum:              274
 
             

Curator: Kim Dismukes | Responsible NASA Official: John I. Petty | Updated: 01/02/2004
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