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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  22604.21
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   130.0
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.252
   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 3218)
    ---------------------------------------
 
    Vector Time (GMT): 2014/302/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2132902.29                 A    =         6787173.79  meter
     Y    =        3625523.33  meter          E    =           .0013752
     Z    =       -5338088.00                 I    =           51.78678
     XDOT =      -6694.410059                 Wp   =           74.76525
     YDOT =       3705.772944  meter/sec      RA   =          151.94516  deg
     ZDOT =       -154.763769                 TA   =          193.74122
                                              MA   =          193.77869
                                              Ha   =            226.184  n.mi
                                              Hp   =            220.512
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6997710.93                 X    =         2118133.46
     Y    =       11894761.60  feet           Y    =         3649292.12  meter
     Z    =      -17513412.08                 Z    =        -5327762.46
     XDOT =     -21963.287595                 XDOT =       -6734.599520
     YDOT =      12158.047716  feet/sec       YDOT =        3630.686998  meter/sec
     ZDOT =       -507.755147                 ZDOT =        -187.382504
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11568131.73                 X    =        -3525966.55
     Y    =        7625673.09  feet           Y    =         2324305.16  meter
     Z    =      -17469984.33                 Z    =        -5324851.22
     XDOT =     -12558.677728                 XDOT =       -3827.884971
     YDOT =     -20558.453601  feet/sec       YDOT =       -6266.216658  meter/sec
     ZDOT =       -647.308804                 ZDOT =        -197.299723
  
  
    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   14302.67053343  .00016717  00000-0  10270-3 0  9008
    2 25544  51.6419 152.9463 0003666 334.5540  25.5430 15.50767519 32193
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14302.67053343   =   yrday.fracday
    Element set:     900
    Inclination:       51.6419  deg
    RA of node:       152.9463  deg
    Eccentricity:     .0003666     
    Arg of perigee:   334.5540  deg
    Mean anomaly:      25.5430  deg
    Mean motion:   15.50767519  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3219
    Checksum:              295
 
 
    Coasting Arc #2 (Orbit 3234)
    ---------------------------------------
 
    Vector Time (GMT): 2014/303/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1775330.16                 A    =         6787267.36  meter
     Y    =       -3830489.34  meter          E    =           .0004608
     Z    =        5313641.76                 I    =           51.81394
     XDOT =       6628.440108                 Wp   =           15.56733
     YDOT =      -3810.839017  meter/sec      RA   =          146.99025  deg
     ZDOT =       -528.102319                 TA   =           79.48800
                                              MA   =           79.43609
                                              Ha   =            226.338  n.mi
                                              Hp   =            220.384
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5824574.03                 X    =        -1758177.10
     Y    =      -12567222.25  feet           Y    =        -3850246.14  meter
     Z    =       17433207.87                 Z    =         5305059.14
     XDOT =      21746.850749                 XDOT =        6673.126537
     YDOT =     -12502.752679  feet/sec       YDOT =       -3736.465667  meter/sec
     ZDOT =      -1732.619157                 ZDOT =        -495.793188
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12178377.89                 X    =         3711969.58
     Y    =       -6693337.31  feet           Y    =        -2040129.21  meter
     Z    =       17397236.05                 Z    =         5302677.55
     XDOT =      13324.722812                 XDOT =        4061.375513
     YDOT =      20062.133885  feet/sec       YDOT =        6114.938408  meter/sec
     ZDOT =      -1594.348701                 ZDOT =        -485.957484
  
  
    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   14303.70159437  .00016717  00000-0  10270-3 0  9015
    2 25544  51.6417 147.8308 0003734 338.8028  21.2967 15.50754655 32359
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14303.70159437   =   yrday.fracday
    Element set:     901
    Inclination:       51.6417  deg
    RA of node:       147.8308  deg
    Eccentricity:     .0003734     
    Arg of perigee:   338.8028  deg
    Mean anomaly:      21.2967  deg
    Mean motion:   15.50754655  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3235
    Checksum:              308
 
 
    Coasting Arc #3 (Orbit 3249)
    ---------------------------------------
 
    Vector Time (GMT): 2014/304/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1457297.27                 A    =         6787392.04  meter
     Y    =        4080408.54  meter          E    =           .0012842
     Z    =       -5235299.98                 I    =           51.84211
     XDOT =      -6495.532237                 Wp   =           84.42006
     YDOT =       3864.283351  meter/sec      RA   =          142.03957  deg
     ZDOT =       1207.501723                 TA   =          197.13239
                                              MA   =          197.17578
                                              Ha   =            226.234  n.mi
                                              Hp   =            220.221
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4781159.02                 X    =         1436992.60
     Y    =       13387167.13  feet           Y    =         4096591.18  meter
     Z    =      -17176181.03                 Z    =        -5228270.08
     XDOT =     -21310.801301                 XDOT =       -6544.126512
     YDOT =      12678.094985  feet/sec       YDOT =        3791.374456  meter/sec
     ZDOT =       3961.619826                 ZDOT =        1175.828726
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12960859.58                 X    =        -3950470.00
     Y    =        5924364.06  feet           Y    =         1805746.17  meter
     Z    =      -17146864.13                 Z    =        -5226364.19
     XDOT =     -13881.019308                 XDOT =       -4230.934685
     YDOT =     -19329.922616  feet/sec       YDOT =       -5891.760413  meter/sec
     ZDOT =       3826.034634                 ZDOT =        1166.175356
  
  
    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   14304.66818783  .00016717  00000-0  10270-3 0  9028
    2 25544  51.6428 143.0373 0003725 341.2397  18.8616 15.50841287 32506
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14304.66818783   =   yrday.fracday
    Element set:     902
    Inclination:       51.6428  deg
    RA of node:       143.0373  deg
    Eccentricity:     .0003725     
    Arg of perigee:   341.2397  deg
    Mean anomaly:      18.8616  deg
    Mean motion:   15.50841287  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3250
    Checksum:              308
 
 
    Coasting Arc #4 (Orbit 3265)
    ---------------------------------------
 
    Vector Time (GMT): 2014/305/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1137489.87                 A    =         6788113.20  meter
     Y    =       -4371766.94  meter          E    =           .0007707
     Z    =        5065519.53                 I    =           51.86843
     XDOT =       6342.463177                 Wp   =           28.72003
     YDOT =      -3860.250920  meter/sec      RA   =          137.08835  deg
     ZDOT =      -1899.547314                 TA   =           79.69008
                                              MA   =           79.60321
                                              Ha   =            226.365  n.mi
                                              Hp   =            220.094
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3731922.14                 X    =        -1113126.21
     Y    =      -14343067.37  feet           Y    =        -4384350.52  meter
     Z    =       16619158.58                 Z    =         5060053.17
     XDOT =      20808.606223                 XDOT =        6394.385524
     YDOT =     -12664.865222  feet/sec       YDOT =       -3789.035199  meter/sec
     ZDOT =      -6232.110611                 ZDOT =       -1868.609735
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13909229.94                 X    =         4239533.29
     Y    =       -5189897.80  feet           Y    =        -1581880.85  meter
     Z    =       16596552.04                 Z    =         5058629.06
     XDOT =      14221.615387                 XDOT =        4334.748370
     YDOT =      18527.177010  feet/sec       YDOT =        5647.083553  meter/sec
     ZDOT =      -6099.645322                 ZDOT =       -1859.171894
  
  
    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   14305.69919839  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6427 137.9217 0003765 345.8416  14.2629 15.50831799 32668
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14305.69919839   =   yrday.fracday
    Element set:     903
    Inclination:       51.6427  deg
    RA of node:       137.9217  deg
    Eccentricity:     .0003765     
    Arg of perigee:   345.8416  deg
    Mean anomaly:      14.2629  deg
    Mean motion:   15.50831799  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3266
    Checksum:              339
 
 
    Coasting Arc #5 (Orbit 3280)
    ---------------------------------------
 
    Vector Time (GMT): 2014/306/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         878255.22                 A    =         6788843.79  meter
     Y    =        4687274.91  meter          E    =           .0010152
     Z    =       -4840518.52                 I    =           51.89450
     XDOT =      -6138.562395                 Wp   =           89.09472
     YDOT =       3790.168550  meter/sec      RA   =          132.14134  deg
     ZDOT =       2561.201489                 TA   =          206.04114
                                              MA   =          206.09224
                                              Ha   =            226.292  n.mi
                                              Hp   =            219.949
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2881414.77                 X    =          849289.82
     Y    =       15378198.54  feet           Y    =         4696933.81  meter
     Z    =      -15880966.27                 Z    =        -4836322.73
     XDOT =     -20139.640402                 XDOT =       -6192.930402
     YDOT =      12434.936187  feet/sec       YDOT =        3721.219374  meter/sec
     ZDOT =       8402.892023                 ZDOT =        2531.248383
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14942867.42                 X    =        -4554585.99
     Y    =        4695347.58  feet           Y    =         1431141.94  meter
     Z    =      -15863828.53                 Z    =        -4835294.94
     XDOT =     -14289.540656                 XDOT =       -4355.451992
     YDOT =     -17572.572961  feet/sec       YDOT =       -5356.120239  meter/sec
     ZDOT =       8274.620344                 ZDOT =        2522.104281
  
  
    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   14306.66574423  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6433 133.1277 0003866 347.4344  12.6710 15.50909557 32817
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14306.66574423   =   yrday.fracday
    Element set:     904
    Inclination:       51.6433  deg
    RA of node:       133.1277  deg
    Eccentricity:     .0003866     
    Arg of perigee:   347.4344  deg
    Mean anomaly:      12.6710  deg
    Mean motion:   15.50909557  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3281
    Checksum:              303
 
 
    Coasting Arc #6 (Orbit 3296)
    ---------------------------------------
 
    Vector Time (GMT): 2014/307/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -625794.44                 A    =         6790079.07  meter
     Y    =       -5029128.45  meter          E    =           .0010553
     Z    =        4516189.70                 I    =           51.91896
     XDOT =       5927.522281                 Wp   =           47.41234
     YDOT =      -3638.626328  meter/sec      RA   =          127.19465  deg
     ZDOT =      -3218.801994                 TA   =           74.89299
                                              MA   =           74.77627
                                              Ha   =            226.385  n.mi
                                              Hp   =            219.797
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2053131.38                 X    =         -591449.70
     Y    =      -16499765.25  feet           Y    =        -5035934.11  meter
     Z    =       14816895.33                 Z    =         4513233.42
     XDOT =      19447.251579                 XDOT =        5983.405920
     YDOT =     -11937.750419  feet/sec       YDOT =       -3572.028716  meter/sec
     ZDOT =     -10560.373995                 ZDOT =       -3189.870322
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16080416.56                 X    =         4901310.97
     Y    =       -4269326.90  feet           Y    =        -1301290.84  meter
     Z    =       14805101.83                 Z    =         4512595.04
     XDOT =      14058.582810                 XDOT =        4285.056041
     YDOT =      16626.636233  feet/sec       YDOT =        5067.798724  meter/sec
     ZDOT =     -10436.467330                 ZDOT =       -3181.035242
  
  
    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   14307.69670341  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6432 128.0121 0003868 352.4677   7.6415 15.50916231 32974
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14307.69670341   =   yrday.fracday
    Element set:     905
    Inclination:       51.6432  deg
    RA of node:       128.0121  deg
    Eccentricity:     .0003868     
    Arg of perigee:   352.4677  deg
    Mean anomaly:       7.6415  deg
    Mean motion:   15.50916231  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3297
    Checksum:              301
 
 
    Coasting Arc #7 (Orbit 3311)
    ---------------------------------------
 
    Vector Time (GMT): 2014/308/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         447460.60                 A    =         6791280.95  meter
     Y    =        5367206.29  meter          E    =           .0006869
     Z    =       -4141647.46                 I    =           51.94202
     XDOT =      -5691.053306                 Wp   =           77.13252
     YDOT =       3416.195211  meter/sec      RA   =          122.25154  deg
     ZDOT =       3819.042499                 TA   =          232.13542
                                              MA   =          232.19758
                                              Ha   =            226.370  n.mi
                                              Hp   =            219.673
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1468046.59                 X    =          407529.28
     Y    =       17608944.52  feet           Y    =         5371986.53  meter
     Z    =      -13588082.22                 Z    =        -4139571.07
     XDOT =     -18671.434730                 XDOT =       -5747.383150
     YDOT =      11207.989536  feet/sec       YDOT =        3352.239465  meter/sec
     ZDOT =      12529.666993                 ZDOT =        3791.258439
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17188893.69                 X    =        -5239174.80
     Y    =        4121746.80  feet           Y    =         1256308.43  meter
     Z    =      -13580103.22                 Z    =        -4139215.46
     XDOT =     -13539.641673                 XDOT =       -4126.882782
     YDOT =     -15647.984881  feet/sec       YDOT =       -4769.505792  meter/sec
     ZDOT =      12410.674825                 ZDOT =        3782.773687
  
  
    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   14308.66320113  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6435 123.2172 0004073 353.6316   6.4783 15.50974421 33120
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14308.66320113   =   yrday.fracday
    Element set:     906
    Inclination:       51.6435  deg
    RA of node:       123.2172  deg
    Eccentricity:     .0004073     
    Arg of perigee:   353.6316  deg
    Mean anomaly:       6.4783  deg
    Mean motion:   15.50974421  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3312
    Checksum:              275
 
 
    Coasting Arc #8 (Orbit 3327)
    ---------------------------------------
 
    Vector Time (GMT): 2014/309/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -278092.89                 A    =         6792762.73  meter
     Y    =       -5709337.16  meter          E    =           .0012733
     Z    =        3664194.86                 I    =           51.96327
     XDOT =       5464.929045                 Wp   =           67.33358
     YDOT =      -3095.481866  meter/sec      RA   =          117.31002  deg
     ZDOT =      -4391.522235                 TA   =           69.41566
                                              MA   =           69.27911
                                              Ha   =            226.421  n.mi
                                              Hp   =            219.480
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -912378.26                 X    =         -232029.05
     Y    =      -18731421.12  feet           Y    =        -5712189.22  meter
     Z    =       12021636.67                 Z    =         3662956.07
     XDOT =      17929.557234                 XDOT =        5520.470454
     YDOT =     -10155.780399  feet/sec       YDOT =       -3034.059167  meter/sec
     ZDOT =     -14407.881349                 ZDOT =       -4364.838591
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18315532.97                 X    =         5582574.45
     Y    =       -4042791.03  feet           Y    =        -1232242.71  meter
     Z    =       12017296.38                 Z    =         3662871.94
     XDOT =      12676.673357                 XDOT =        3863.850039
     YDOT =      14777.422314  feet/sec       YDOT =        4504.158321  meter/sec
     ZDOT =     -14293.618682                 ZDOT =       -4356.694974
  
  
    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   14309.69410805  .00016717  00000-0  10270-3 0  9074
    2 25544  51.6436 118.1016 0004029 359.2231    .8913 15.51003631 33287
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14309.69410805   =   yrday.fracday
    Element set:     907
    Inclination:       51.6436  deg
    RA of node:       118.1016  deg
    Eccentricity:     .0004029     
    Arg of perigee:   359.2231  deg
    Mean anomaly:        .8913  deg
    Mean motion:   15.51003631  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3328
    Checksum:              275
 
 
    Coasting Arc #9 (Orbit 3342)
    ---------------------------------------
 
    Vector Time (GMT): 2014/310/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         185609.25                 A    =         6794129.05  meter
     Y    =        6016359.83  meter          E    =           .0006944
     Z    =       -3148578.36                 I    =           51.98234
     XDOT =      -5243.755867                 Wp   =           39.90779
     YDOT =       2711.227680  meter/sec      RA   =          112.37122  deg
     ZDOT =       4882.673915                 TA   =          284.05308
                                              MA   =          284.13026
                                              Ha   =            226.469  n.mi
                                              Hp   =            219.366
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         608954.25                 X    =          133614.34
     Y    =       19738713.36  feet           Y    =         6018144.61  meter
     Z    =      -10329981.51                 Z    =        -3147803.17
     XDOT =     -17203.923448                 XDOT =       -5297.402842
     YDOT =       8895.103937  feet/sec       YDOT =        2652.288806  meter/sec
     ZDOT =      16019.271374                 ZDOT =        4857.069373
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19290896.44                 X    =        -5879865.24
     Y    =        4230417.29  feet           Y    =         1289431.19  meter
     Z    =      -10327682.81                 Z    =        -3147877.72
     XDOT =     -11569.156454                 XDOT =       -3526.278887
     YDOT =     -14004.945594  feet/sec       YDOT =       -4268.707417  meter/sec
     ZDOT =      15909.658593                 ZDOT =        4849.263939
  
  
    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   14310.66055696  .00016717  00000-0  10270-3 0  9087
    2 25544  51.6442 113.3060 0004312    .3710 359.7444 15.51041374 33439
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14310.66055696   =   yrday.fracday
    Element set:     908
    Inclination:       51.6442  deg
    RA of node:       113.3060  deg
    Eccentricity:     .0004312     
    Arg of perigee:      .3710  deg
    Mean anomaly:     359.7444  deg
    Mean motion:   15.51041374  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3343
    Checksum:              270
 
 
    Coasting Arc #10 (Orbit 3358)
    ---------------------------------------
 
    Vector Time (GMT): 2014/311/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -95752.07                 A    =         6795469.49  meter
     Y    =       -6300736.23  meter          E    =           .0013712
     Z    =        2533110.50                 I    =           51.99841
     XDOT =       5051.826198                 Wp   =           86.58180
     YDOT =      -2224.144149  meter/sec      RA   =          107.43494  deg
     ZDOT =      -5315.715576                 TA   =           65.16761
                                              MA   =           65.02508
                                              Ha   =            226.475  n.mi
                                              Hp   =            219.145
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -314147.22                 X    =          -37594.03
     Y    =      -20671706.80  feet           Y    =        -6301481.78  meter
     Z    =        8310729.99                 Z    =         2532786.68
     XDOT =      16574.232933                 XDOT =        5102.144373
     YDOT =      -7297.060856  feet/sec       YDOT =       -2167.370077  meter/sec
     ZDOT =     -17440.011732                 ZDOT =       -5291.051593
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20190816.27                 X    =         6154160.80
     Y    =       -4444575.95  feet           Y    =        -1354706.75  meter
     Z    =        8310419.14                 Z    =         2533015.75
     XDOT =      10127.815477                 XDOT =        3086.958157
     YDOT =      13440.059742  feet/sec       YDOT =        4096.530209  meter/sec
     ZDOT =     -17334.477140                 ZDOT =       -5283.548632
  
  
    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   14311.69141098  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6443 108.1906 0004224   6.2123 353.9080 15.51089866 33593
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14311.69141098   =   yrday.fracday
    Element set:     909
    Inclination:       51.6443  deg
    RA of node:       108.1906  deg
    Eccentricity:     .0004224     
    Arg of perigee:     6.2123  deg
    Mean anomaly:     353.9080  deg
    Mean motion:   15.51089866  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3359
    Checksum:              301
 
 
    Coasting Arc #11 (Orbit 3373)
    ---------------------------------------
 
    Vector Time (GMT): 2014/312/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =          73031.72                 A    =         6796577.50  meter
     Y    =        6520331.26  meter          E    =           .0011175
     Z    =       -1898436.03                 I    =           52.01178
     XDOT =      -4894.320751                 Wp   =           27.05009
     YDOT =       1693.044598  meter/sec      RA   =          102.50030  deg
     ZDOT =       5649.303775                 TA   =          312.17641
                                              MA   =          312.27125
                                              Ha   =            226.567  n.mi
                                              Hp   =            219.021
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         239605.39                 X    =            9336.66
     Y    =       21392162.92  feet           Y    =         6520791.82  meter
     Z    =       -6228464.66                 Z    =        -1898235.92
     XDOT =     -16057.482779                 XDOT =       -4940.332197
     YDOT =       5554.608261  feet/sec       YDOT =        1638.055840  meter/sec
     ZDOT =      18534.461203                 ZDOT =        5625.415506
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20834050.31                 X    =        -6350218.53
     Y    =        4860147.26  feet           Y    =         1481372.88  meter
     Z    =       -6228734.50                 Z    =        -1898518.27
     XDOT =      -8541.328380                 XDOT =       -2603.396890
     YDOT =     -13086.866359  feet/sec       YDOT =       -3988.876866  meter/sec
     ZDOT =      18432.312171                 ZDOT =        5618.168750
  
  
    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   14312.65781032  .00016717  00000-0  10270-3 0  9101
    2 25544  51.6452 103.3948 0004542   7.6210 352.5009 15.51114786 33744
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14312.65781032   =   yrday.fracday
    Element set:     910
    Inclination:       51.6452  deg
    RA of node:       103.3948  deg
    Eccentricity:     .0004542     
    Arg of perigee:     7.6210  deg
    Mean anomaly:     352.5009  deg
    Mean motion:   15.51114786  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3374
    Checksum:              279
 
 
    Coasting Arc #12 (Orbit 3389)
    ---------------------------------------
 
    Vector Time (GMT): 2014/313/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -37249.11                 A    =         6797343.89  meter
     Y    =       -6690832.69  meter          E    =           .0012911
     Z    =        1176011.85                 I    =           52.02044
     XDOT =       4781.459559                 Wp   =          103.22776
     YDOT =      -1070.985122  meter/sec      RA   =           97.56800  deg
     ZDOT =      -5890.471366                 TA   =           64.08573
                                              MA   =           63.95271
                                              Ha   =            226.533  n.mi
                                              Hp   =            218.806
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -122208.36                 X    =           31859.30
     Y    =      -21951550.82  feet           Y    =        -6690862.85  meter
     Z    =        3858306.59                 Z    =         1175998.65
     XDOT =      15687.203276                 XDOT =        4821.694829
     YDOT =      -3513.730714  feet/sec       YDOT =       -1017.290678  meter/sec
     ZDOT =     -19325.693457                 ZDOT =       -5867.145490
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21322401.21                 X    =         6499067.89
     Y    =       -5218443.12  feet           Y    =        -1590581.46  meter
     Z    =        3859417.86                 Z    =         1176350.56
     XDOT =       6695.171778                 XDOT =        2040.688358
     YDOT =      13012.604795  feet/sec       YDOT =        3966.241942  meter/sec
     ZDOT =     -19226.039526                 ZDOT =       -5860.096848
  
  
    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   14313.68861083  .00016717  00000-0  10270-3 0  9111
    2 25544  51.6449  98.2795 0004442  13.0270 347.0995 15.51175044 33903
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14313.68861083   =   yrday.fracday
    Element set:     911
    Inclination:       51.6449  deg
    RA of node:        98.2795  deg
    Eccentricity:     .0004442     
    Arg of perigee:    13.0270  deg
    Mean anomaly:     347.0995  deg
    Mean motion:   15.51175044  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3390
    Checksum:              308
 
 
    Coasting Arc #13 (Orbit 3404)
    ---------------------------------------
 
    Vector Time (GMT): 2014/314/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =          47020.58                 A    =         6797774.72  meter
     Y    =        6773855.38  meter          E    =           .0015489
     Z    =        -459284.21                 I    =           52.02614
     XDOT =      -4725.280959                 Wp   =           33.94914
     YDOT =        433.633773  meter/sec      RA   =           92.63592  deg
     ZDOT =       6021.820122                 TA   =          321.12810
                                              MA   =          321.23939
                                              Ha   =            226.642  n.mi
                                              Hp   =            218.653
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         154266.98                 X    =          -26498.65
     Y    =       22223934.96  feet           Y    =         6773970.13  meter
     Z    =       -1506837.97                 Z    =         -459234.23
     XDOT =     -15502.890286                 XDOT =       -4759.031356
     YDOT =       1422.682982  feet/sec       YDOT =         380.603793  meter/sec
     ZDOT =      19756.627696                 ZDOT =        5998.782983
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21489294.06                 X    =        -6549936.83
     Y    =        5668717.83  feet           Y    =         1727825.20  meter
     Z    =       -1507820.57                 Z    =         -459583.71
     XDOT =      -4841.130451                 XDOT =       -1475.576562
     YDOT =     -13219.088195  feet/sec       YDOT =       -4029.178082  meter/sec
     ZDOT =      19658.308349                 ZDOT =        5991.852385
  
  
    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   14314.65495981  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6457  93.4835 0004742  15.0124 345.1167 15.51197351 34059
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14314.65495981   =   yrday.fracday
    Element set:     912
    Inclination:       51.6457  deg
    RA of node:        93.4835  deg
    Eccentricity:     .0004742     
    Arg of perigee:    15.0124  deg
    Mean anomaly:     345.1167  deg
    Mean motion:   15.51197351  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3405
    Checksum:              303
 
 
    Coasting Arc #14 (Orbit 3420)
    ---------------------------------------
 
    Vector Time (GMT): 2014/315/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -20157.23                 A    =         6797627.36  meter
     Y    =       -6787646.96  meter          E    =           .0010139
     Z    =        -322442.56                 I    =           52.02597
     XDOT =       4719.440322                 Wp   =          112.85710
     YDOT =        265.000783  meter/sec      RA   =           87.70486  deg
     ZDOT =      -6027.809377                 TA   =           70.59387
                                              MA   =           70.48432
                                              Ha   =            226.591  n.mi
                                              Hp   =            218.459
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         -66132.66                 X    =           57311.66
     Y    =      -22269182.95  feet           Y    =        -6787439.21  meter
     Z    =       -1057882.41                 Z    =         -322352.41
     XDOT =      15483.728090                 XDOT =        4745.407867
     YDOT =        869.425142  feet/sec       YDOT =         317.921902  meter/sec
     ZDOT =     -19776.277483                 ZDOT =       -6004.819572
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21460059.03                 X    =         6541025.99
     Y    =       -5948959.62  feet           Y    =        -1813242.89  meter
     Z    =       -1056287.63                 Z    =         -321956.47
     XDOT =       2858.789315                 XDOT =         871.358983
     YDOT =      13716.700997  feet/sec       YDOT =        4180.850464  meter/sec
     ZDOT =     -19678.277831                 ZDOT =       -5997.939083
  
  
    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   14315.68570614  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6449  88.3679 0004694  19.5903 340.5428 15.51261590 34213
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14315.68570614   =   yrday.fracday
    Element set:     913
    Inclination:       51.6449  deg
    RA of node:        88.3679  deg
    Eccentricity:     .0004694     
    Arg of perigee:    19.5903  deg
    Mean anomaly:     340.5428  deg
    Mean motion:   15.51261590  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3421
    Checksum:              319
 
 
    Coasting Arc #15 (Orbit 3436)
    ---------------------------------------
 
    Vector Time (GMT): 2014/316/15:41:51.769
    Vector Time (MET): N/A
    Weight (LBS)     : 931508.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =           8815.73                 A    =         6797116.40  meter
     Y    =        6702584.04  meter          E    =           .0017865
     Z    =        1068994.28                 I    =           52.02287
     XDOT =      -4779.930137                 Wp   =           47.65876
     YDOT =       -946.365020  meter/sec      RA   =           82.77249  deg
     ZDOT =       5921.897972                 TA   =          323.86691
                                              MA   =          323.98750
                                              Ha   =            226.687  n.mi
                                              Hp   =            218.277
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =          28922.98                 X    =          -71327.68
     Y    =       21990105.12  feet           Y    =         6702234.51  meter
     Z    =        3507199.07                 Z    =         1068842.46
     XDOT =     -15682.185489                 XDOT =       -4797.759467
     YDOT =      -3104.872114  feet/sec       YDOT =        -999.917009  meter/sec
     ZDOT =      19428.799122                 ZDOT =        5898.634125
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21101744.05                 X    =        -6431811.59
     Y    =        6188291.75  feet           Y    =         1886191.33  meter
     Z    =        3505345.66                 Z    =         1068429.36
     XDOT =      -1013.554350                 XDOT =        -308.931366
     YDOT =     -14500.704536  feet/sec       YDOT =       -4419.814743  meter/sec
     ZDOT =      19329.749106                 ZDOT =        5891.707527
  
  
    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   14316.71642403  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6454  83.2516 0004916  22.5520 337.5847 15.51290245 34376
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14316.71642403   =   yrday.fracday
    Element set:     914
    Inclination:       51.6454  deg
    RA of node:        83.2516  deg
    Eccentricity:     .0004916     
    Arg of perigee:    22.5520  deg
    Mean anomaly:     337.5847  deg
    Mean motion:   15.51290245  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3437
    Checksum:              294
 
             

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