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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  20451.43
   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 
   ------------------------------------------------------------------------
   294/15:33:44.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              225.5  
   000/00:00:00.000           0.0               0.0              221.1  
   
   300/05:39:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              225.6  
   000/00:00:00.000           0.0               0.0              220.6  
   
 
 
    Coasting Arc #1 (Orbit 3030)
    ---------------------------------------
 
    Vector Time (GMT): 2014/290/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1775640.28                 A    =         6792508.64  meter
     Y    =       -5053474.03  meter          E    =           .0007673
     Z    =        4172276.22                 I    =           51.44233
     XDOT =       6670.894050                 Wp   =          107.63546
     YDOT =        720.041880  meter/sec      RA   =          212.25977  deg
     ZDOT =       3703.206560                 TA   =          304.16294
                                              MA   =          304.23566
                                              Ha   =            225.715  n.mi
                                              Hp   =            221.326
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5825591.46                 X    =        -1739266.97
     Y    =      -16579639.19  feet           Y    =        -5073126.61  meter
     Z    =       13688570.27                 Z    =         4163739.15
     XDOT =      21886.135335                 XDOT =        6644.357404
     YDOT =       2362.342125  feet/sec       YDOT =         794.492119  meter/sec
     ZDOT =      12149.627823                 ZDOT =        3735.548624
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12382392.39                 X    =         3774153.20
     Y    =       12508819.85  feet           Y    =         3812688.29  meter
     Z    =       13653010.38                 Z    =         4161437.56
     XDOT =     -19842.146953                 XDOT =       -6047.886391
     YDOT =       6202.130279  feet/sec       YDOT =        1890.409309  meter/sec
     ZDOT =      12287.142936                 ZDOT =        3745.121167
  
  
    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   14290.55525313  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6444 213.0312 0002699 276.1957  83.8886 15.50525691 30318
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14290.55525313   =   yrday.fracday
    Element set:     900
    Inclination:       51.6444  deg
    RA of node:       213.0312  deg
    Eccentricity:     .0002699     
    Arg of perigee:   276.1957  deg
    Mean anomaly:      83.8886  deg
    Mean motion:   15.50525691  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3031
    Checksum:              304
 
 
    Coasting Arc #2 (Orbit 3045)
    ---------------------------------------
 
    Vector Time (GMT): 2014/291/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1605112.54                 A    =         6791240.37  meter
     Y    =        4847176.26  meter          E    =           .0007230
     Z    =       -4485102.49                 I    =           51.46628
     XDOT =      -6913.865135                 Wp   =           58.58046
     YDOT =       -685.372962  meter/sec      RA   =          207.28707  deg
     ZDOT =      -3215.165338                 TA   =          178.94841
                                              MA   =          178.94689
                                              Ha   =            225.649  n.mi
                                              Hp   =            221.247
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5266117.27                 X    =         1572578.44
     Y    =       15902809.25  feet           Y    =         4864943.28  meter
     Z    =      -14714903.17                 Z    =        -4477384.53
     XDOT =     -22683.284563                 XDOT =       -6890.068858
     YDOT =      -2248.598956  feet/sec       YDOT =        -762.555570  meter/sec
     ZDOT =     -10548.442710                 ZDOT =       -3248.694428
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11801523.37                 X    =        -3597104.32
     Y    =      -11928933.16  feet           Y    =        -3635938.83  meter
     Z    =      -14682789.54                 Z    =        -4475314.25
     XDOT =      20434.204667                 XDOT =        6228.345583
     YDOT =      -7057.468785  feet/sec       YDOT =       -2151.116486  meter/sec
     ZDOT =     -10691.027505                 ZDOT =       -3258.625183
  
  
    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   14291.52201747  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6452 208.2376 0002685 281.5567  78.5283 15.50573511 30467
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14291.52201747   =   yrday.fracday
    Element set:     901
    Inclination:       51.6452  deg
    RA of node:       208.2376  deg
    Eccentricity:     .0002685     
    Arg of perigee:   281.5567  deg
    Mean anomaly:      78.5283  deg
    Mean motion:   15.50573511  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3046
    Checksum:              304
 
 
    Coasting Arc #3 (Orbit 3061)
    ---------------------------------------
 
    Vector Time (GMT): 2014/292/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1392897.57                 A    =         6790132.94  meter
     Y    =       -4651873.20  meter          E    =           .0005158
     Z    =        4743778.24                 I    =           51.49095
     XDOT =       7147.313331                 Wp   =          125.20381
     YDOT =        614.502333  meter/sec      RA   =          202.31537  deg
     ZDOT =       2696.244123                 TA   =          298.05157
                                              MA   =          298.10373
                                              Ha   =            225.621  n.mi
                                              Hp   =            221.199
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4569873.93                 X    =        -1363819.79
     Y    =      -15262051.19  feet           Y    =        -4667286.36  meter
     Z    =       15563576.89                 Z    =         4737082.81
     XDOT =      23449.190717                 XDOT =        7126.812948
     YDOT =       2016.083769  feet/sec       YDOT =         694.313908  meter/sec
     ZDOT =       8845.945285                 ZDOT =        2730.915366
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11098218.70                 X    =         3382737.06
     Y    =       11467693.24  feet           Y    =         3495352.90  meter
     Z    =       15535779.14                 Z    =         4735305.48
     XDOT =     -20914.303668                 XDOT =       -6374.679758
     YDOT =       8034.479896  feet/sec       YDOT =        2448.909472  meter/sec
     ZDOT =       8993.414148                 ZDOT =        2741.192632
  
  
    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   14292.55320924  .00016717  00000-0  10270-3 0  9027
    2 25544  51.6451 203.1244 0002738 283.3102  76.7744 15.50599598 30621
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14292.55320924   =   yrday.fracday
    Element set:     902
    Inclination:       51.6451  deg
    RA of node:       203.1244  deg
    Eccentricity:     .0002738     
    Arg of perigee:   283.3102  deg
    Mean anomaly:      76.7744  deg
    Mean motion:   15.50599598  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3062
    Checksum:              302
 
 
    Coasting Arc #4 (Orbit 3076)
    ---------------------------------------
 
    Vector Time (GMT): 2014/293/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1124814.99                 A    =         6789073.61  meter
     Y    =        4493000.89  meter          E    =           .0010250
     Z    =       -4973290.59                 I    =           51.51804
     XDOT =      -7334.660443                 Wp   =           65.74227
     YDOT =       -519.168152  meter/sec      RA   =          197.34445  deg
     ZDOT =      -2127.271223                 TA   =          183.45964
                                              MA   =          183.46673
                                              Ha   =            225.569  n.mi
                                              Hp   =            221.111
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3690337.89                 X    =         1098648.66
     Y    =       14740816.58  feet           Y    =         4505432.40  meter
     Z    =      -16316570.18                 Z    =        -4967890.41
     XDOT =     -24063.846598                 XDOT =       -7317.976080
     YDOT =      -1703.307586  feet/sec       YDOT =        -601.096047  meter/sec
     ZDOT =      -6979.236297                 ZDOT =       -2162.861966
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10276689.24                 X    =        -3132334.88
     Y    =      -11226200.59  feet           Y    =        -3421745.94  meter
     Z    =      -16294256.91                 Z    =        -4966489.51
     XDOT =      21182.345810                 XDOT =        6456.379003
     YDOT =      -9037.888571  feet/sec       YDOT =       -2754.748437  meter/sec
     ZDOT =      -7130.645187                 ZDOT =       -2173.420653
  
  
    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   14293.51992993  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6460 198.3307 0002750 288.7248  71.3604 15.50647467 30771
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14293.51992993   =   yrday.fracday
    Element set:     903
    Inclination:       51.6460  deg
    RA of node:       198.3307  deg
    Eccentricity:     .0002750     
    Arg of perigee:   288.7248  deg
    Mean anomaly:      71.3604  deg
    Mean motion:   15.50647467  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3077
    Checksum:              331
 
 
    Coasting Arc #5 (Orbit 3092)
    ---------------------------------------
 
    Vector Time (GMT): 2014/294/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -818042.34                 A    =         6788242.71  meter
     Y    =       -4357871.92  meter          E    =           .0002268
     Z    =        5139301.28                 I    =           51.54555
     XDOT =       7498.319982                 Wp   =          143.95743
     YDOT =        400.429824  meter/sec      RA   =          192.37460  deg
     ZDOT =       1530.941498                 TA   =          291.25083
                                              MA   =          291.27505
                                              Ha   =            225.528  n.mi
                                              Hp   =            221.068
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2683865.94                 X    =         -794216.38
     Y    =      -14297480.05  feet           Y    =        -4366885.96  meter
     Z    =       16861224.67                 Z    =         5135385.66
     XDOT =      24600.787343                 XDOT =        7485.848015
     YDOT =       1313.746141  feet/sec       YDOT =         484.211347  meter/sec
     ZDOT =       5022.773943                 ZDOT =        1567.337657
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9376101.64                 X    =         2857835.78
     Y    =       11146733.13  feet           Y    =         3397524.26  meter
     Z    =       16845207.87                 Z    =         5134419.36
     XDOT =     -21307.712080                 XDOT =       -6494.590642
     YDOT =      10087.841843  feet/sec       YDOT =        3074.774194  meter/sec
     ZDOT =       5177.640984                 ZDOT =        1578.144972
  
  
    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   14294.55107516  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6459 193.2172 0002824 290.5062  69.5786 15.50676071 30931
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14294.55107516   =   yrday.fracday
    Element set:     904
    Inclination:       51.6459  deg
    RA of node:       193.2172  deg
    Eccentricity:     .0002824     
    Arg of perigee:   290.5062  deg
    Mean anomaly:      69.5786  deg
    Mean motion:   15.50676071  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3093
    Checksum:              316
 
 
    Coasting Arc #6 (Orbit 3094)
    ---------------------------------------
 
    Vector Time (GMT): 2014/294/15:33:44.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929923.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6569966.71                 A    =         6799385.66  meter
     Y    =        1683731.71  meter          E    =           .0008768
     Z    =        -409751.65                 I    =           51.58563
     XDOT =      -1530.360786                 Wp   =          146.92741
     YDOT =       4531.290592  meter/sec      RA   =          191.62820  deg
     ZDOT =      -5985.825027                 TA   =           37.48673
                                              MA   =           37.42561
                                              Ha   =            225.517  n.mi
                                              Hp   =            221.149
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21555008.90                 X    =         6552641.02
     Y    =        5524054.15  feet           Y    =         1757104.41  meter
     Z    =       -1344329.55                 Z    =         -377877.31
     XDOT =      -5020.868722                 XDOT =       -1551.839177
     YDOT =      14866.438949  feet/sec       YDOT =        4514.056298  meter/sec
     ZDOT =     -19638.533554                 ZDOT =       -5993.312167
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8253299.57                 X    =        -2515605.71
     Y    =       20672745.60  feet           Y    =         6301052.86  meter
     Z    =       -1208900.47                 Z    =         -368472.86
     XDOT =     -12603.354037                 XDOT =       -3841.502310
     YDOT =      -6167.580886  feet/sec       YDOT =       -1879.878654  meter/sec
     ZDOT =     -19671.080815                 ZDOT =       -5995.745432
  
  
    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   14294.67996570  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6444 192.5776 0002989 290.1512  69.9317 15.50655157 30953
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14294.67996570   =   yrday.fracday
    Element set:     905
    Inclination:       51.6444  deg
    RA of node:       192.5776  deg
    Eccentricity:     .0002989     
    Arg of perigee:   290.1512  deg
    Mean anomaly:      69.9317  deg
    Mean motion:   15.50655157  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3095
    Checksum:              348
 
 
    Coasting Arc #7 (Orbit 3110)
    ---------------------------------------
 
    Vector Time (GMT): 2014/295/15:33:44.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929923.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6545304.65                 A    =         6798933.38  meter
     Y    =       -1535481.82  meter          E    =           .0012115
     Z    =         965693.66                 I    =           51.61432
     XDOT =       1929.225057                 Wp   =           43.17997
     YDOT =      -4486.168564  meter/sec      RA   =          186.66864  deg
     ZDOT =       5907.536845                 TA   =          327.27067
                                              MA   =          327.34567
                                              Ha   =            225.449  n.mi
                                              Hp   =            221.100
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21474096.64                 X    =        -6532339.21
     Y    =       -5037670.03  feet           Y    =        -1608603.06  meter
     Z    =        3168286.28                 Z    =          933928.40
     XDOT =       6329.478532                 XDOT =        1950.549450
     YDOT =     -14718.400801  feet/sec       YDOT =       -4464.474834  meter/sec
     ZDOT =      19381.682561                 ZDOT =        5916.961262
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7405229.75                 X    =         2257114.03
     Y    =      -20796988.14  feet           Y    =        -6338921.99  meter
     Z    =        3033288.65                 Z    =          924546.38
     XDOT =      12415.299003                 XDOT =        3784.183136
     YDOT =       7271.186495  feet/sec       YDOT =        2216.257644  meter/sec
     ZDOT =      19422.473869                 ZDOT =        5919.970035
  
  
    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   14295.71108378  .00016717  00000-0  10270-3 0  9069
    2 25544  51.6434 187.4626 0003035 293.2172  66.8659 15.50707737 31114
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14295.71108378   =   yrday.fracday
    Element set:     906
    Inclination:       51.6434  deg
    RA of node:       187.4626  deg
    Eccentricity:     .0003035     
    Arg of perigee:   293.2172  deg
    Mean anomaly:      66.8659  deg
    Mean motion:   15.50707737  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3111
    Checksum:              317
 
 
    Coasting Arc #8 (Orbit 3125)
    ---------------------------------------
 
    Vector Time (GMT): 2014/296/15:33:44.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929923.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6463726.58                 A    =         6798241.87  meter
     Y    =        1416972.75  meter          E    =           .0005648
     Z    =       -1545668.99                 I    =           51.64292
     XDOT =      -2354.318804                 Wp   =          155.89809
     YDOT =       4481.567446  meter/sec      RA   =          181.71231  deg
     ZDOT =      -5749.407661                 TA   =           40.96400
                                              MA   =           40.92158
                                              Ha   =            225.478  n.mi
                                              Hp   =            221.009
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21206452.02                 X    =         6454909.82
     Y    =        4648860.74  feet           Y    =         1489204.89  meter
     Z    =       -5071092.49                 Z    =        -1514289.85
     XDOT =      -7724.143057                 XDOT =       -2376.328239
     YDOT =      14703.305270  feet/sec       YDOT =        4455.116319  meter/sec
     ZDOT =     -18862.886027                 ZDOT =       -5760.898797
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6635001.25                 X    =        -2022348.38
     Y    =       20703557.02  feet           Y    =         6310444.18  meter
     Z    =       -4937709.76                 Z    =        -1505013.93
     XDOT =     -12407.298195                 XDOT =       -3781.744490
     YDOT =      -8476.775060  feet/sec       YDOT =       -2583.721038  meter/sec
     ZDOT =     -18912.481781                 ZDOT =       -5764.524447
  
  
    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   14296.67773604  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6429 182.6687 0003044 297.4626  62.6215 15.50738579 31268
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14296.67773604   =   yrday.fracday
    Element set:     907
    Inclination:       51.6429  deg
    RA of node:       182.6687  deg
    Eccentricity:     .0003044     
    Arg of perigee:   297.4626  deg
    Mean anomaly:      62.6215  deg
    Mean motion:   15.50738579  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3126
    Checksum:              338
 
 
    Coasting Arc #9 (Orbit 3141)
    ---------------------------------------
 
    Vector Time (GMT): 2014/297/15:33:44.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929923.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6327270.54                 A    =         6797296.94  meter
     Y    =       -1299987.16  meter          E    =           .0012153
     Z    =        2094643.32                 I    =           51.67037
     XDOT =       2766.979876                 Wp   =           58.67986
     YDOT =      -4533.514492  meter/sec      RA   =          176.75549  deg
     ZDOT =       5527.050935                 TA   =          324.47513
                                              MA   =          324.55599
                                              Ha   =            225.464  n.mi
                                              Hp   =            220.935
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20758761.62                 X    =        -6322438.91
     Y    =       -4265049.73  feet           Y    =        -1370715.62  meter
     Z    =        6872189.39                 Z    =         2063917.32
     XDOT =       9078.017967                 XDOT =        2790.619651
     YDOT =     -14873.735211  feet/sec       YDOT =       -4502.439732  meter/sec
     ZDOT =      18133.369209                 ZDOT =        5540.550672
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5861309.80                 X    =         1786527.23
     Y    =      -20409318.09  feet           Y    =        -6220760.15  meter
     Z    =        6741557.90                 Z    =         2054826.85
     XDOT =      12645.690318                 XDOT =        3854.406409
     YDOT =       9660.040100  feet/sec       YDOT =        2944.380223  meter/sec
     ZDOT =      18191.533939                 ZDOT =        5544.779545
  
  
    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   14297.70880802  .00016717  00000-0  10270-3 0  9081
    2 25544  51.6418 177.5533 0003008 298.4827  61.6021 15.50781176 31426
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14297.70880802   =   yrday.fracday
    Element set:     908
    Inclination:       51.6418  deg
    RA of node:       177.5533  deg
    Eccentricity:     .0003008     
    Arg of perigee:   298.4827  deg
    Mean anomaly:      61.6021  deg
    Mean motion:   15.50781176  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3142
    Checksum:              311
 
 
    Coasting Arc #10 (Orbit 3156)
    ---------------------------------------
 
    Vector Time (GMT): 2014/298/15:33:44.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929923.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6135630.07                 A    =         6796084.01  meter
     Y    =        1230621.20  meter          E    =           .0002082
     Z    =       -2650018.82                 I    =           51.69743
     XDOT =      -3177.911842                 Wp   =          131.10109
     YDOT =       4620.367489  meter/sec      RA   =          171.80103  deg
     ZDOT =      -5216.262062                 TA   =           78.69467
                                              MA   =           78.67128
                                              Ha   =            225.481  n.mi
                                              Hp   =            220.824
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20130019.91                 X    =         6134286.26
     Y    =        4037471.13  feet           Y    =         1299226.13  meter
     Z    =       -8694287.46                 Z    =        -2620215.29
     XDOT =     -10426.219954                 XDOT =       -3204.002038
     YDOT =      15158.685987  feet/sec       YDOT =        4584.683845  meter/sec
     ZDOT =     -17113.720675                 ZDOT =       -5231.763975
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5244879.09                 X    =        -1598639.15
     Y    =       19904714.54  feet           Y    =         6066956.99  meter
     Z    =       -8567560.41                 Z    =        -2611392.41
     XDOT =     -13056.857894                 XDOT =       -3979.730286
     YDOT =     -10829.681240  feet/sec       YDOT =       -3300.886842  meter/sec
     ZDOT =     -17180.435791                 ZDOT =       -5236.596829
  
  
    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   14298.67541714  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6414 172.7588 0002990 304.9928  55.0942 15.50819621 31575
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14298.67541714   =   yrday.fracday
    Element set:     909
    Inclination:       51.6414  deg
    RA of node:       172.7588  deg
    Eccentricity:     .0002990     
    Arg of perigee:   304.9928  deg
    Mean anomaly:      55.0942  deg
    Mean motion:   15.50819621  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3157
    Checksum:              334
 
 
    Coasting Arc #11 (Orbit 3172)
    ---------------------------------------
 
    Vector Time (GMT): 2014/299/15:33:44.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929923.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5891721.64                 A    =         6794747.01  meter
     Y    =       -1183008.05  meter          E    =           .0010818
     Z    =        3159000.48                 I    =           51.72331
     XDOT =       3558.613935                 Wp   =           75.55717
     YDOT =      -4757.210686  meter/sec      RA   =          166.84600  deg
     ZDOT =       4844.249784                 TA   =          320.79367
                                              MA   =          320.87198
                                              Ha   =            225.504  n.mi
                                              Hp   =            220.729
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19329795.40                 X    =        -5893400.89
     Y    =       -3881260.02  feet           Y    =        -1248902.37  meter
     Z    =       10364174.82                 Z    =         3130374.54
     XDOT =      11675.242570                 XDOT =        3588.013248
     YDOT =     -15607.646607  feet/sec       YDOT =       -4717.251385  meter/sec
     ZDOT =      15893.207953                 ZDOT =        4861.609088
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4711512.95                 X    =         1436069.15
     Y    =      -19209771.77  feet           Y    =        -5855138.44  meter
     Z    =       10242441.29                 Z    =         3121896.10
     XDOT =      13692.810277                 XDOT =        4173.568572
     YDOT =      11892.204326  feet/sec       YDOT =        3624.743878  meter/sec
     ZDOT =      15967.867792                 ZDOT =        4867.006103
  
  
    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   14299.70644319  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6406 167.6430 0002944 304.4533  55.6339 15.50854524 31736
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14299.70644319   =   yrday.fracday
    Element set:     910
    Inclination:       51.6406  deg
    RA of node:       167.6430  deg
    Eccentricity:     .0002944     
    Arg of perigee:   304.4533  deg
    Mean anomaly:      55.6339  deg
    Mean motion:   15.50854524  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3173
    Checksum:              307
 
 
    Coasting Arc #12 (Orbit 3181)
    ---------------------------------------
 
    Vector Time (GMT): 2014/300/05:39:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915489.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2525019.65                 A    =         6787423.96  meter
     Y    =       -3547866.97  meter          E    =           .0001260
     Z    =        5205387.10                 I    =           51.71810
     XDOT =       6916.345863                 Wp   =          108.36807
     YDOT =      -3043.978092  meter/sec      RA   =          163.92558  deg
     ZDOT =       1279.624276                 TA   =          329.34771
                                              MA   =          329.35507
                                              Ha   =            225.554  n.mi
                                              Hp   =            220.627
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8284185.20                 X    =        -2510445.64
     Y    =      -11639983.50  feet           Y    =        -3576021.72  meter
     Z    =       17078041.65                 Z    =         5193156.11
     XDOT =      22691.423436                 XDOT =        6943.654129
     YDOT =      -9986.804763  feet/sec       YDOT =       -2966.482302  meter/sec
     ZDOT =       4198.242375                 ZDOT =        1313.290180
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5985116.74                 X    =        -1824263.58
     Y    =       13040451.11  feet           Y    =         3974729.50  meter
     Z    =       17026492.86                 Z    =         5189675.03
     XDOT =     -18915.246372                 XDOT =       -5765.367094
     YDOT =     -14353.541899  feet/sec       YDOT =       -4374.959571  meter/sec
     ZDOT =       4342.100928                 ZDOT =        1323.472363
  
  
    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   14300.28638634  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6418 164.7692 0003113 311.5184  48.5699 15.50872465 31821
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14300.28638634   =   yrday.fracday
    Element set:     911
    Inclination:       51.6418  deg
    RA of node:       164.7692  deg
    Eccentricity:     .0003113     
    Arg of perigee:   311.5184  deg
    Mean anomaly:      48.5699  deg
    Mean motion:   15.50872465  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3182
    Checksum:              312
 
 
    Coasting Arc #13 (Orbit 3196)
    ---------------------------------------
 
    Vector Time (GMT): 2014/301/05:39:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915489.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2106720.98                 A    =         6786938.83  meter
     Y    =        3677195.44  meter          E    =           .0012889
     Z    =       -5312214.63                 I    =           51.74658
     XDOT =      -6950.144511                 Wp   =           74.87273
     YDOT =       3154.601195  meter/sec      RA   =          158.96572  deg
     ZDOT =       -570.507283                 TA   =          189.66815
                                              MA   =          189.69298
                                              Ha   =            225.560  n.mi
                                              Hp   =            220.599
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6911814.25                 X    =         2091250.74
     Y    =       12064289.49  feet           Y    =         3700667.53  meter
     Z    =      -17428525.70                 Z    =        -5302017.92
     XDOT =     -22802.311389                 XDOT =       -6982.132038
     YDOT =      10349.741455  feet/sec       YDOT =        3076.701312  meter/sec
     ZDOT =      -1871.743053                 ZDOT =        -604.348606
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6821539.12                 X    =         2079205.12
     Y    =      -12176995.99  feet           Y    =        -3711548.38  meter
     Z    =      -17385658.97                 Z    =        -5299148.85
     XDOT =      19606.241669                 XDOT =        5975.982461
     YDOT =      13872.249806  feet/sec       YDOT =        4228.261741  meter/sec
     ZDOT =      -2016.388560                 ZDOT =        -614.595233
  
  
    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   14301.25294005  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6419 159.9735 0003128 315.7813  44.3087 15.50886289 31977
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14301.25294005   =   yrday.fracday
    Element set:     912
    Inclination:       51.6419  deg
    RA of node:       159.9735  deg
    Eccentricity:     .0003128     
    Arg of perigee:   315.7813  deg
    Mean anomaly:      44.3087  deg
    Mean motion:   15.50886289  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3197
    Checksum:              317
 
 
    Coasting Arc #14 (Orbit 3212)
    ---------------------------------------
 
    Vector Time (GMT): 2014/302/05:39:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915489.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1673650.57                 A    =         6786663.48  meter
     Y    =       -3853857.29  meter          E    =           .0002705
     Z    =        5329450.13                 I    =           51.77565
     XDOT =       6942.258953                 Wp   =            7.16405
     YDOT =      -3242.655219  meter/sec      RA   =          154.00859  deg
     ZDOT =       -162.083478                 TA   =           84.39401
                                              MA   =           84.36316
                                              Ha   =            225.585  n.mi
                                              Hp   =            220.427
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5490979.55                 X    =        -1656320.67
     Y    =      -12643888.74  feet           Y    =        -3872476.12  meter
     Z    =       17485072.60                 Z    =         5321361.80
     XDOT =      22776.440134                 XDOT =        6978.790471
     YDOT =     -10638.632609  feet/sec       YDOT =       -3164.818127  meter/sec
     ZDOT =       -531.769940                 ZDOT =        -128.269558
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7847829.15                 X    =        -2392018.32
     Y    =       11384782.90  feet           Y    =         3470081.83  meter
     Z    =       17451213.10                 Z    =         5319129.75
     XDOT =     -20148.987537                 XDOT =       -6141.411401
     YDOT =     -13282.460324  feet/sec       YDOT =       -4048.493907  meter/sec
     ZDOT =       -387.205203                 ZDOT =        -118.020146
  
  
    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   14302.28390726  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6425 154.8592 0003226 319.5067  40.5844 15.50935859 32137
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14302.28390726   =   yrday.fracday
    Element set:     913
    Inclination:       51.6425  deg
    RA of node:       154.8592  deg
    Eccentricity:     .0003226     
    Arg of perigee:   319.5067  deg
    Mean anomaly:      40.5844  deg
    Mean motion:   15.50935859  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3213
    Checksum:              309
 
 
    Coasting Arc #15 (Orbit 3227)
    ---------------------------------------
 
    Vector Time (GMT): 2014/303/05:39:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915489.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1267053.76                 A    =         6786843.30  meter
     Y    =        4084593.64  meter          E    =           .0012430
     Z    =       -5280501.47                 I    =           51.80445
     XDOT =      -6854.708900                 Wp   =           85.92622
     YDOT =       3285.348214  meter/sec      RA   =          149.05192  deg
     ZDOT =        899.196416                 TA   =          192.65481
                                              MA   =          192.68604
                                              Ha   =            225.599  n.mi
                                              Hp   =            220.373
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4157000.53                 X    =         1246936.06
     Y    =       13400897.77  feet           Y    =         4098650.02  meter
     Z    =      -17324479.88                 Z    =        -5274395.19
     XDOT =     -22489.202429                 XDOT =       -6895.305036
     YDOT =      10778.701490  feet/sec       YDOT =        3208.467459  meter/sec
     ZDOT =       2950.119476                 ZDOT =         865.798026
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9006707.34                 X    =         2745244.40
     Y    =      -10799197.91  feet           Y    =        -3291595.52  meter
     Z    =      -17299100.11                 Z    =        -5272765.71
     XDOT =      20399.025022                 XDOT =        6217.622827
     YDOT =      12530.278548  feet/sec       YDOT =        3819.228901  meter/sec
     ZDOT =       2807.297797                 ZDOT =         855.664369
  
  
    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   14303.25041759  .00016717  00000-0  10270-3 0  9146
    2 25544  51.6428 150.0634 0003295 323.0379  37.0544 15.50958232 32281
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14303.25041759   =   yrday.fracday
    Element set:     914
    Inclination:       51.6428  deg
    RA of node:       150.0634  deg
    Eccentricity:     .0003295     
    Arg of perigee:   323.0379  deg
    Mean anomaly:      37.0544  deg
    Mean motion:   15.50958232  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3228
    Checksum:              291
 
 
    Coasting Arc #16 (Orbit 3243)
    ---------------------------------------
 
    Vector Time (GMT): 2014/304/05:39:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915489.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -860532.88                 A    =         6787328.63  meter
     Y    =       -4356845.27  meter          E    =           .0006063
     Z    =        5132173.25                 I    =           51.83347
     XDOT =       6730.414649                 Wp   =           22.02887
     YDOT =      -3275.287566  meter/sec      RA   =          144.09847  deg
     ZDOT =      -1645.857841                 TA   =           83.85747
                                              MA   =           83.78840
                                              Ha   =            225.629  n.mi
                                              Hp   =            220.207
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2823270.62                 X    =         -836680.43
     Y    =      -14294111.77  feet           Y    =        -4366334.71  meter
     Z    =       16837838.75                 Z    =         5128050.98
     XDOT =      22081.412889                 XDOT =        6774.534600
     YDOT =     -10745.694115  feet/sec       YDOT =       -3199.777092  meter/sec
     ZDOT =      -5399.796066                 ZDOT =       -1613.054719
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10302259.00                 X    =        -3140128.54
     Y    =       10330740.56  feet           Y    =         3148809.72  meter
     Z    =       16820956.01                 Z    =         5127027.39
     XDOT =     -20413.018487                 XDOT =       -6221.888035
     YDOT =     -11760.340762  feet/sec       YDOT =       -3584.551864  meter/sec
     ZDOT =      -5259.494232                 ZDOT =       -1603.093842
  
  
    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   14304.28133925  .00016717  00000-0  10270-3 0  9158
    2 25544  51.6434 144.9490 0003334 327.2046  32.8898 15.50999242 32440
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14304.28133925   =   yrday.fracday
    Element set:     915
    Inclination:       51.6434  deg
    RA of node:       144.9490  deg
    Eccentricity:     .0003334     
    Arg of perigee:   327.2046  deg
    Mean anomaly:      32.8898  deg
    Mean motion:   15.50999242  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3244
    Checksum:              312
 
 
    Coasting Arc #17 (Orbit 3258)
    ---------------------------------------
 
    Vector Time (GMT): 2014/305/05:39:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915489.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         507526.19                 A    =         6788165.82  meter
     Y    =        4663470.59  meter          E    =           .0009871
     Z    =       -4915208.35                 I    =           51.86154
     XDOT =      -6540.047878                 Wp   =           93.29675
     YDOT =       3200.789324  meter/sec      RA   =          139.14613  deg
     ZDOT =       2365.100351                 TA   =          199.81168
                                              MA   =          199.85005
                                              Ha   =            225.656  n.mi
                                              Hp   =            220.105
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1665112.17                 X    =          479217.26
     Y    =       15300100.37  feet           Y    =         4668987.49  meter
     Z    =      -16126011.66                 Z    =        -4912811.88
     XDOT =     -21456.849993                 XDOT =       -6586.842817
     YDOT =      10501.277310  feet/sec       YDOT =        3127.392769  meter/sec
     ZDOT =       7759.515586                 ZDOT =        2333.215461
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11610538.36                 X    =         3538892.09
     Y    =      -10117641.13  feet           Y    =        -3083857.02  meter
     Z    =      -16116533.71                 Z    =        -4912319.48
     XDOT =      20094.178472                 XDOT =        6124.705598
     YDOT =      10934.704450  feet/sec       YDOT =        3332.897916  meter/sec
     ZDOT =       7623.122979                 ZDOT =        2323.527884
  
  
    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   14305.24780631  .00016717  00000-0  10270-3 0  9168
    2 25544  51.6436 140.1530 0003421 330.6801  29.4158 15.51033039 32590
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14305.24780631   =   yrday.fracday
    Element set:     916
    Inclination:       51.6436  deg
    RA of node:       140.1530  deg
    Eccentricity:     .0003421     
    Arg of perigee:   330.6801  deg
    Mean anomaly:      29.4158  deg
    Mean motion:   15.51033039  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3259
    Checksum:              272
 
             

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