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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  23680.6
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   74.8
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   0.74
   ET - UTC  (sec) :   66.18
   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 320)
    ---------------------------------------
 
    Vector Time (GMT): 2010/039/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4922221.80                 A    =         6720268.20  meter
     Y    =       -2322063.96  meter          E    =           .0003611
     Z    =        3938698.29                 I    =           51.69615
     XDOT =       5144.124780                 Wp   =           18.92155
     YDOT =      -4090.661888  meter/sec      RA   =          170.39220  deg
     ZDOT =       4019.328552                 TA   =           29.41841
                                              MA   =           29.39809
                                              Ha   =            187.233  n.mi
                                              Hp   =            183.190
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16149021.64                 X    =        -4915023.31
     Y    =       -7618320.09  feet           Y    =        -2377067.09  meter
     Z    =       12922238.50                 Z    =         3914804.03
     XDOT =      16877.049804                 XDOT =        5169.960213
     YDOT =     -13420.806718  feet/sec       YDOT =       -4032.992967  meter/sec
     ZDOT =      13186.773463                 ZDOT =        4044.380740
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6877532.16                 X    =        -2096271.80
     Y    =      -16552117.00  feet           Y    =        -5045085.26  meter
     Z    =       12827350.57                 Z    =         3909776.45
     XDOT =      20250.799409                 XDOT =        6172.443660
     YDOT =       1875.886024  feet/sec       YDOT =         571.770060  meter/sec
     ZDOT =      13286.001569                 ZDOT =        4049.573278
  
  
    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   10039.55498280  .00016717  00000-0  10270-3 0  9001
    2 25544  51.6441 171.1159 0011231 298.8801  61.1236 15.75843839  3210
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10039.55498280   =   yrday.fracday
    Element set:     900
    Inclination:       51.6441  deg
    RA of node:       171.1159  deg
    Eccentricity:     .0011231     
    Arg of perigee:   298.8801  deg
    Mean anomaly:      61.1236  deg
    Mean motion:   15.75843839  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             321
    Checksum:              295
 
 
    Coasting Arc #2 (Orbit 335)
    ---------------------------------------
 
    Vector Time (GMT): 2010/040/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4718391.10                 A    =         6722909.95  meter
     Y    =        3708083.70  meter          E    =           .0009130
     Z    =       -3016943.92                 I    =           51.73522
     XDOT =      -5262.658732                 Wp   =          326.41875
     YDOT =      -2658.604806  meter/sec      RA   =          165.19855  deg
     ZDOT =       4963.312465                 TA   =          358.68648
                                              MA   =          358.68887
                                              Ha   =            187.408  n.mi
                                              Hp   =            182.900
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15480285.75                 X    =        -4744849.47
     Y    =       12165628.93  feet           Y    =         3655172.04  meter
     Z    =       -9898109.97                 Z    =        -3039929.39
     XDOT =     -17265.940723                 XDOT =       -5256.648873
     YDOT =      -8722.456714  feet/sec       YDOT =       -2717.421576  meter/sec
     ZDOT =      16283.833547                 ZDOT =        4937.761606
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19615087.08                 X    =        -5978678.54
     Y    =       -1038882.34  feet           Y    =         -316651.34  meter
     Z    =       -9989166.00                 Z    =        -3044697.80
     XDOT =      -7362.249485                 XDOT =       -2244.013643
     YDOT =     -16580.638274  feet/sec       YDOT =       -5053.778546  meter/sec
     ZDOT =      16182.346736                 ZDOT =        4932.379285
  
  
    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   10040.50621736  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6445 166.2187 0011310 303.5452  56.4632 15.75835825  3363
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10040.50621736   =   yrday.fracday
    Element set:     901
    Inclination:       51.6445  deg
    RA of node:       166.2187  deg
    Eccentricity:     .0011310     
    Arg of perigee:   303.5452  deg
    Mean anomaly:      56.4632  deg
    Mean motion:   15.75835825  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             336
    Checksum:              280
 
 
    Coasting Arc #3 (Orbit 351)
    ---------------------------------------
 
    Vector Time (GMT): 2010/041/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4216254.39                 A    =         6717462.24  meter
     Y    =        2382277.31  meter          E    =           .0010520
     Z    =       -4661119.36                 I    =           51.74646
     XDOT =      -5635.652584                 Wp   =            6.55699
     YDOT =       4414.359495  meter/sec      RA   =          160.10284  deg
     ZDOT =      -2831.990806                 TA   =          235.45980
                                              MA   =          235.55914
                                              Ha   =            187.654  n.mi
                                              Hp   =            182.717
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13832855.61                 X    =         4211944.21
     Y    =        7815870.43  feet           Y    =         2429402.00  meter
     Z    =      -15292386.35                 Z    =        -4640647.78
     XDOT =     -18489.673833                 XDOT =       -5670.838978
     YDOT =      14482.806743  feet/sec       YDOT =        4351.141634  meter/sec
     ZDOT =      -9291.308418                 ZDOT =       -2859.453356
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5559592.71                 X    =         1694563.86
     Y    =       14966882.80  feet           Y    =         4561905.88  meter
     Z    =      -15211053.66                 Z    =        -4636329.16
     XDOT =     -22335.186569                 XDOT =       -6807.764866
     YDOT =      -1289.117103  feet/sec       YDOT =        -392.922893  meter/sec
     ZDOT =      -9400.113803                 ZDOT =       -2865.154687
  
  
    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   10041.52084199  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6450 160.9944 0011319 307.2783  52.7348 15.75883317  3528
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10041.52084199   =   yrday.fracday
    Element set:     902
    Inclination:       51.6450  deg
    RA of node:       160.9944  deg
    Eccentricity:     .0011319     
    Arg of perigee:   307.2783  deg
    Mean anomaly:      52.7348  deg
    Mean motion:   15.75883317  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             352
    Checksum:              305
 
 
    Coasting Arc #4 (Orbit 367)
    ---------------------------------------
 
    Vector Time (GMT): 2010/042/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5071386.66                 A    =         6725132.90  meter
     Y    =       -4000216.64  meter          E    =           .0004979
     Z    =        1872958.41                 I    =           51.80129
     XDOT =       4360.748099                 Wp   =           67.61735
     YDOT =       2873.610210  meter/sec      RA   =          154.92380  deg
     ZDOT =      -5656.402846                 TA   =           91.62716
                                              MA   =           91.57013
                                              Ha   =            187.764  n.mi
                                              Hp   =            182.343
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16638407.66                 X    =         5106642.66
     Y    =      -13124070.33  feet           Y    =        -3943308.28  meter
     Z    =        6144876.69                 Z    =         1897680.03
     XDOT =      14306.916334                 XDOT =        4355.767715
     YDOT =       9427.855021  feet/sec       YDOT =        2922.346905  meter/sec
     ZDOT =     -18557.752118                 ZDOT =       -5635.231047
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21159571.52                 X    =         6449437.40
     Y    =         370034.45  feet           Y    =          112786.50  meter
     Z    =        6242831.80                 Z    =         1902815.13
     XDOT =       5203.170959                 XDOT =        1585.926508
     YDOT =      14885.509060  feet/sec       YDOT =        4537.103161  meter/sec
     ZDOT =     -18473.610567                 ZDOT =       -5630.756501
  
  
    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   10042.53544153  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6454 155.7700 0011236 311.5406  48.4793 15.75922245  3689
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10042.53544153   =   yrday.fracday
    Element set:     903
    Inclination:       51.6454  deg
    RA of node:       155.7700  deg
    Eccentricity:     .0011236     
    Arg of perigee:   311.5406  deg
    Mean anomaly:      48.4793  deg
    Mean motion:   15.75922245  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             368
    Checksum:              290
 
 
    Coasting Arc #5 (Orbit 383)
    ---------------------------------------
 
    Vector Time (GMT): 2010/043/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3383825.10                 A    =         6715074.39  meter
     Y    =       -2705355.29  meter          E    =           .0006895
     Z    =        5133053.20                 I    =           51.79584
     XDOT =       5914.317943                 Wp   =          322.55727
     YDOT =      -4727.402042  meter/sec      RA   =          149.81408  deg
     ZDOT =       1413.645639                 TA   =          113.97204
                                              MA   =          113.89983
                                              Ha   =            187.949  n.mi
                                              Hp   =            182.018
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11101788.39                 X    =        -3378256.50
     Y    =       -8875837.55  feet           Y    =        -2743164.06  meter
     Z    =       16840725.73                 Z    =         5116628.64
     XDOT =      19403.930259                 XDOT =        5959.874011
     YDOT =     -15509.849219  feet/sec       YDOT =       -4661.009906  meter/sec
     ZDOT =       4637.945009                 ZDOT =        1442.487166
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3278744.99                 X    =         -999361.47
     Y    =      -13909536.72  feet           Y    =        -4239626.79  meter
     Z    =       16775424.29                 Z    =         5113149.32
     XDOT =      23804.523695                 XDOT =        7255.618822
     YDOT =         94.957423  feet/sec       YDOT =          28.943022  meter/sec
     ZDOT =       4752.232161                 ZDOT =        1448.480363
  
  
    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   10043.55001386  .00016717  00000-0  10270-3 0  9047
    2 25544  51.6464 150.5449 0011359 315.8069  44.2187 15.76005019  3842
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10043.55001386   =   yrday.fracday
    Element set:     904
    Inclination:       51.6464  deg
    RA of node:       150.5449  deg
    Eccentricity:     .0011359     
    Arg of perigee:   315.8069  deg
    Mean anomaly:      44.2187  deg
    Mean motion:   15.76005019  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             384
    Checksum:              293
 
 
    Coasting Arc #6 (Orbit 398)
    ---------------------------------------
 
    Vector Time (GMT): 2010/044/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5186588.31                 A    =         6726373.95  meter
     Y    =        4226579.23  meter          E    =           .0017163
     Z    =        -570150.42                 I    =           51.85965
     XDOT =      -3416.599353                 Wp   =          359.67568
     YDOT =      -3381.422398  meter/sec      RA   =          144.66003  deg
     ZDOT =       6029.502148                 TA   =          354.12675
                                              MA   =          354.14685
                                              Ha   =            188.186  n.mi
                                              Hp   =            181.687
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17016365.85                 X    =        -5230695.59
     Y    =       13866729.76  feet           Y    =         4168333.09  meter
     Z    =       -1870572.23                 Z    =         -595453.32
     XDOT =     -11209.315461                 XDOT =       -3407.823086
     YDOT =     -11093.905505  feet/sec       YDOT =       -3419.579613  meter/sec
     ZDOT =      19781.831195                 ZDOT =        6012.926227
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21930853.07                 X    =        -6684524.02
     Y    =         703852.88  feet           Y    =          214534.36  meter
     Z    =       -1970841.54                 Z    =         -600712.50
     XDOT =      -2219.562592                 XDOT =        -676.522678
     YDOT =     -14090.610770  feet/sec       YDOT =       -4294.818163  meter/sec
     ZDOT =      19715.895070                 ZDOT =        6009.404817
  
  
    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   10044.50115481  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6467 145.6473 0011469 320.5238  39.5089 15.75987312  3998
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10044.50115481   =   yrday.fracday
    Element set:     905
    Inclination:       51.6467  deg
    RA of node:       145.6473  deg
    Eccentricity:     .0011469     
    Arg of perigee:   320.5238  deg
    Mean anomaly:      39.5089  deg
    Mean motion:   15.75987312  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             399
    Checksum:              318
 
 
    Coasting Arc #7 (Orbit 414)
    ---------------------------------------
 
    Vector Time (GMT): 2010/045/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2583354.89                 A    =         6714263.13  meter
     Y    =        3251924.36  meter          E    =           .0012356
     Z    =       -5282660.44                 I    =           51.84309
     XDOT =      -5924.866483                 Wp   =           42.83237
     YDOT =       4913.893983  meter/sec      RA   =          139.53007  deg
     ZDOT =        136.564357                 TA   =          228.40729
                                              MA   =          228.51325
                                              Ha   =            188.335  n.mi
                                              Hp   =            181.415
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8475573.78                 X    =         2572460.77
     Y    =       10669043.19  feet           Y    =         3280751.83  meter
     Z    =      -17331563.12                 Z    =        -5270137.47
     XDOT =     -19438.538329                 XDOT =       -5980.037556
     YDOT =      16121.699419  feet/sec       YDOT =        4847.330140  meter/sec
     ZDOT =        448.045792                 ZDOT =         107.647964
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         579622.14                 X    =          176668.83
     Y    =       13676739.89  feet           Y    =         4168670.32  meter
     Z    =      -17281716.86                 Z    =        -5267467.30
     XDOT =     -24216.689251                 XDOT =       -7381.246884
     YDOT =       1409.998226  feet/sec       YDOT =         429.767459  meter/sec
     ZDOT =        333.453090                 ZDOT =         101.636502
  
  
    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   10045.51567929  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6465 140.4232 0011484 324.2054  35.8339 15.76049045  4155
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10045.51567929   =   yrday.fracday
    Element set:     906
    Inclination:       51.6465  deg
    RA of node:       140.4232  deg
    Eccentricity:     .0011484     
    Arg of perigee:   324.2054  deg
    Mean anomaly:      35.8339  deg
    Mean motion:   15.76049045  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             415
    Checksum:              296
 
 
    Coasting Arc #8 (Orbit 430)
    ---------------------------------------
 
    Vector Time (GMT): 2010/046/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5113494.81                 A    =         6725971.24  meter
     Y    =       -4291698.47  meter          E    =           .0001747
     Z    =        -829282.83                 I    =           51.90427
     XDOT =       2507.300556                 Wp   =           19.80996
     YDOT =       4143.028609  meter/sec      RA   =          134.40489  deg
     ZDOT =      -5982.586054                 TA   =          169.20209
                                              MA   =          169.19834
                                              Ha   =            188.399  n.mi
                                              Hp   =            181.139
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16776557.79                 X    =         5165133.71
     Y    =      -14080375.56  feet           Y    =        -4234227.66  meter
     Z    =       -2720744.19                 Z    =         -804316.42
     XDOT =       8226.051693                 XDOT =        2489.847716
     YDOT =      13592.613545  feet/sec       YDOT =        4170.968795  meter/sec
     ZDOT =     -19627.907001                 ZDOT =       -5970.448532
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21843931.48                 X    =         6658030.31
     Y    =       -1755315.94  feet           Y    =         -535020.30  meter
     Z    =       -2621800.82                 Z    =         -799124.89
     XDOT =      -1198.579953                 XDOT =        -365.327170
     YDOT =      14318.645312  feet/sec       YDOT =        4364.323091  meter/sec
     ZDOT =     -19579.552477                 ZDOT =       -5967.847595
  
  
    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   10046.53017895  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6456 135.1982 0011409 328.4034  31.6444 15.76082618  4311
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10046.53017895   =   yrday.fracday
    Element set:     907
    Inclination:       51.6456  deg
    RA of node:       135.1982  deg
    Eccentricity:     .0011409     
    Arg of perigee:   328.4034  deg
    Mean anomaly:      31.6444  deg
    Mean motion:   15.76082618  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             431
    Checksum:              298
 
 
    Coasting Arc #9 (Orbit 446)
    ---------------------------------------
 
    Vector Time (GMT): 2010/047/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1834332.67                 A    =         6714929.96  meter
     Y    =       -4024510.21  meter          E    =           .0013338
     Z    =        5056964.46                 I    =           51.88865
     XDOT =       5730.163773                 Wp   =          355.37224
     YDOT =      -4835.369229  meter/sec      RA   =          129.24890  deg
     ZDOT =      -1756.934251                 TA   =          111.55484
                                              MA   =          111.41263
                                              Ha   =            188.522  n.mi
                                              Hp   =            180.735
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6018151.80                 X    =        -1813758.85
     Y    =      -13203773.65  feet           Y    =        -4044907.43  meter
     Z    =       16591090.74                 Z    =         5048103.70
     XDOT =      18799.749911                 XDOT =        5792.342542
     YDOT =     -15864.072272  feet/sec       YDOT =       -4770.943597  meter/sec
     ZDOT =      -5764.219982                 ZDOT =       -1728.946348
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2413532.86                 X    =          735644.81
     Y    =      -14349357.94  feet           Y    =        -4373684.30  meter
     Z    =       16555750.29                 Z    =         5046192.69
     XDOT =      23455.993667                 XDOT =        7149.386870
     YDOT =      -2625.477742  feet/sec       YDOT =        -800.245616  meter/sec
     ZDOT =      -5653.296030                 ZDOT =       -1723.124630
  
  
    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   10047.54465121  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6462 129.9721 0011596 332.2780  27.7765 15.76163206  4470
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10047.54465121   =   yrday.fracday
    Element set:     908
    Inclination:       51.6462  deg
    RA of node:       129.9721  deg
    Eccentricity:     .0011596     
    Arg of perigee:   332.2780  deg
    Mean anomaly:      27.7765  deg
    Mean motion:   15.76163206  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             447
    Checksum:              309
 
 
    Coasting Arc #10 (Orbit 462)
    ---------------------------------------
 
    Vector Time (GMT): 2010/048/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4855212.15                 A    =         6723946.44  meter
     Y    =        4073448.21  meter          E    =           .0017520
     Z    =        2210837.82                 I    =           51.93646
     XDOT =      -1762.065387                 Wp   =           30.12358
     YDOT =      -5095.658572  meter/sec      RA   =          124.15101  deg
     ZDOT =       5515.189432                 TA   =          354.60662
                                              MA   =          354.62546
                                              Ha   =            188.765  n.mi
                                              Hp   =            180.418
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15929173.72                 X    =        -4911140.99
     Y    =       13364331.38  feet           Y    =         4018841.78  meter
     Z    =        7253404.93                 Z    =         2187115.47
     XDOT =      -5781.054418                 XDOT =       -1731.745213
     YDOT =     -16718.039934  feet/sec       YDOT =       -5115.193118  meter/sec
     ZDOT =      18094.453518                 ZDOT =        5506.703466
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20691287.23                 X    =        -6306704.35
     Y    =        2360030.28  feet           Y    =          719337.23  meter
     Z    =        7159378.59                 Z    =         2182178.59
     XDOT =       4464.239119                 XDOT =        1360.700083
     YDOT =     -15687.572565  feet/sec       YDOT =       -4781.572118  meter/sec
     ZDOT =      18060.560879                 ZDOT =        5504.858956
  
  
    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   10048.55910059  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6455 124.7468 0011555 336.9383  23.1261 15.76166175  4635
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10048.55910059   =   yrday.fracday
    Element set:     909
    Inclination:       51.6455  deg
    RA of node:       124.7468  deg
    Eccentricity:     .0011555     
    Arg of perigee:   336.9383  deg
    Mean anomaly:      23.1261  deg
    Mean motion:   15.76166175  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             463
    Checksum:              312
 
 
    Coasting Arc #11 (Orbit 477)
    ---------------------------------------
 
    Vector Time (GMT): 2010/049/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1293084.88                 A    =         6717225.21  meter
     Y    =        4861880.80  meter          E    =           .0009225
     Z    =       -4451315.09                 I    =           51.92943
     XDOT =      -5385.961054                 Wp   =           34.82623
     YDOT =       4424.582970  meter/sec      RA   =          118.97697  deg
     ZDOT =       3278.804461                 TA   =          267.85108
                                              MA   =          267.95672
                                              Ha   =            188.835  n.mi
                                              Hp   =            180.056
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4242404.48                 X    =         1260245.77
     Y    =       15951052.48  feet           Y    =         4876156.94  meter
     Z    =      -14604052.13                 Z    =        -4445113.44
     XDOT =     -17670.475900                 XDOT =       -5450.964866
     YDOT =      14516.348326  feet/sec       YDOT =        4363.990709  meter/sec
     ZDOT =      10757.232484                 ZDOT =        3252.481629
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4900443.51                 X    =        -1493655.18
     Y    =       15784287.61  feet           Y    =         4811050.86  meter
     Z    =      -14579243.04                 Z    =        -4443753.28
     XDOT =     -21601.548519                 XDOT =       -6584.151989
     YDOT =       3100.576308  feet/sec       YDOT =         945.055659  meter/sec
     ZDOT =      10652.885888                 ZDOT =        3246.999619
  
  
    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   10049.51012277  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6444 119.8480 0011602 341.1812  18.8922 15.76227399  4787
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10049.51012277   =   yrday.fracday
    Element set:     910
    Inclination:       51.6444  deg
    RA of node:       119.8480  deg
    Eccentricity:     .0011602     
    Arg of perigee:   341.1812  deg
    Mean anomaly:      18.8922  deg
    Mean motion:   15.76227399  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             478
    Checksum:              298
 
 
    Coasting Arc #12 (Orbit 493)
    ---------------------------------------
 
    Vector Time (GMT): 2010/050/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4542873.31                 A    =         6720649.22  meter
     Y    =       -3543324.83  meter          E    =           .0011674
     Z    =       -3473453.61                 I    =           51.95417
     XDOT =       1227.097845                 Wp   =           10.17296
     YDOT =       6064.395179  meter/sec      RA   =          113.89499  deg
     ZDOT =      -4572.569294                 TA   =          210.79399
                                              MA   =          210.86253
                                              Ha   =            188.945  n.mi
                                              Hp   =            179.901
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14904439.98                 X    =         4599031.00
     Y    =      -11625081.45  feet           Y    =        -3492209.90  meter
     Z    =      -11395845.17                 Z    =        -3451247.97
     XDOT =       4025.911564                 XDOT =        1181.405994
     YDOT =      19896.309642  feet/sec       YDOT =        6077.861608  meter/sec
     ZDOT =     -15001.867764                 ZDOT =       -4566.719404
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18837148.63                 X    =         5741562.90
     Y    =       -2108447.40  feet           Y    =         -642654.77  meter
     Z    =      -11307803.42                 Z    =        -3446618.48
     XDOT =      -7022.722494                 XDOT =       -2140.525816
     YDOT =      17746.817380  feet/sec       YDOT =        5409.229937  meter/sec
     ZDOT =     -14978.417255                 ZDOT =       -4565.421579
  
  
    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   10050.52452229  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6441 114.6214 0011639 345.2095  14.8727 15.76237020  4949
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10050.52452229   =   yrday.fracday
    Element set:     911
    Inclination:       51.6441  deg
    RA of node:       114.6214  deg
    Eccentricity:     .0011639     
    Arg of perigee:   345.2095  deg
    Mean anomaly:      14.8727  deg
    Mean motion:   15.76237020  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             494
    Checksum:              279
 
 
    Coasting Arc #13 (Orbit 509)
    ---------------------------------------
 
    Vector Time (GMT): 2010/051/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -906112.44                 A    =         6720459.73  meter
     Y    =       -5705337.50  meter          E    =           .0015579
     Z    =        3437146.93                 I    =           51.96606
     XDOT =       5019.693592                 Wp   =           40.72081
     YDOT =      -3586.547293  meter/sec      RA   =          108.71333  deg
     ZDOT =      -4606.830356                 TA   =           98.79933
                                              MA   =           98.62288
                                              Ha   =            189.028  n.mi
                                              Hp   =            179.434
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2972809.86                 X    =         -858943.89
     Y    =      -18718298.89  feet           Y    =        -5715206.34  meter
     Z    =       11276728.76                 Z    =         3432859.84
     XDOT =      16468.810996                 XDOT =        5081.804876
     YDOT =     -11766.887443  feet/sec       YDOT =       -3530.066973  meter/sec
     ZDOT =     -15114.272821                 ZDOT =       -4582.293916
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6868590.67                 X    =         2093546.44
     Y    =      -17675489.41  feet           Y    =        -5387489.17  meter
     Z    =       11259505.29                 Z    =         3431897.21
     XDOT =      18948.408405                 XDOT =        5775.474882
     YDOT =      -2251.291097  feet/sec       YDOT =        -686.193526  meter/sec
     ZDOT =     -15016.966664                 ZDOT =       -4577.171439
  
  
    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   10051.53889414  .00016717  00000-0  10270-3 0  9129
    2 25544  51.6446 109.3948 0011864 348.8356  11.2544 15.76318459  5101
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10051.53889414   =   yrday.fracday
    Element set:     912
    Inclination:       51.6446  deg
    RA of node:       109.3948  deg
    Eccentricity:     .0011864     
    Arg of perigee:   348.8356  deg
    Mean anomaly:      11.2544  deg
    Mean motion:   15.76318459  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             510
    Checksum:              314
 
 
    Coasting Arc #14 (Orbit 525)
    ---------------------------------------
 
    Vector Time (GMT): 2010/052/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4244395.33                 A    =         6716873.64  meter
     Y    =        2637956.00  meter          E    =           .0010844
     Z    =        4477656.54                 I    =           51.96226
     XDOT =       -914.401814                 Wp   =           40.41722
     YDOT =      -6943.491933  meter/sec      RA   =          103.63234  deg
     ZDOT =       3227.670012                 TA   =           17.49932
                                              MA   =           17.46199
                                              Ha   =            189.264  n.mi
                                              Hp   =            179.125
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13925181.53                 X    =        -4295329.40
     Y    =        8654711.29  feet           Y    =         2590207.94  meter
     Z    =       14690474.22                 Z    =         4456913.71
     XDOT =      -3000.005951                 XDOT =        -852.369778
     YDOT =     -22780.485344  feet/sec       YDOT =       -6953.370425  meter/sec
     ZDOT =      10589.468543                 ZDOT =        3223.378678
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16456428.42                 X    =        -5015919.38
     Y    =         641494.08  feet           Y    =          195527.39  meter
     Z    =       14608189.14                 Z    =         4452576.05
     XDOT =       8588.753548                 XDOT =        2617.852082
     YDOT =     -20138.927195  feet/sec       YDOT =       -6138.345009  meter/sec
     ZDOT =      10572.195323                 ZDOT =        3222.405134
  
  
    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   10052.55324261  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6443 104.1681 0011759 353.5378   6.5633 15.76333097  5263
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10052.55324261   =   yrday.fracday
    Element set:     913
    Inclination:       51.6443  deg
    RA of node:       104.1681  deg
    Eccentricity:     .0011759     
    Arg of perigee:   353.5378  deg
    Mean anomaly:       6.5633  deg
    Mean motion:   15.76333097  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             526
    Checksum:              294
 
 
    Coasting Arc #15 (Orbit 540)
    ---------------------------------------
 
    Vector Time (GMT): 2010/053/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 764580.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         735096.03                 A    =         6723487.44  meter
     Y    =        6327688.25  meter          E    =           .0017033
     Z    =       -2121564.21                 I    =           51.99121
     XDOT =      -4757.767451                 Wp   =           12.57742
     YDOT =       2411.202930  meter/sec      RA   =           98.46048  deg
     ZDOT =       5567.569605                 TA   =          323.77987
                                              MA   =          323.89508
                                              Ha   =            189.285  n.mi
                                              Hp   =            178.812
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2411732.37                 X    =          674590.10
     Y    =       20760132.04  feet           Y    =         6335570.22  meter
     Z    =       -6960512.51                 Z    =        -2118140.14
     XDOT =     -15609.473266                 XDOT =       -4811.422250
     YDOT =       7910.770767  feet/sec       YDOT =        2357.698757  meter/sec
     ZDOT =      18266.304479                 ZDOT =        5544.326335
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7745862.88                 X    =        -2360939.01
     Y    =       19416309.16  feet           Y    =         5918091.03  meter
     Z    =       -6946712.65                 Z    =        -2117358.02
     XDOT =     -16171.137898                 XDOT =       -4928.962831
     YDOT =         22.175518  feet/sec       YDOT =           6.759098  meter/sec
     ZDOT =      18174.071245                 ZDOT =        5539.456915
  
  
    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   10053.50417101  .00016717  00000-0  10270-3 0  9140
    2 25544  51.6447  99.2683 0011839 357.4912   2.6191 15.76367404  5411
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      10053.50417101   =   yrday.fracday
    Element set:     914
    Inclination:       51.6447  deg
    RA of node:        99.2683  deg
    Eccentricity:     .0011839     
    Arg of perigee:   357.4912  deg
    Mean anomaly:       2.6191  deg
    Mean motion:   15.76367404  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             541
    Checksum:              295
 
             

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