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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  31215.34
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   133.2
   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 8)
    ---------------------------------------
 
    Vector Time (GMT): 2014/353/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2110790.31                 A    =         6788183.13  meter
     Y    =       -5241247.73  meter          E    =           .0016833
     Z    =        3755465.38                 I    =           51.28907
     XDOT =       4289.758317                 Wp   =          116.54759
     YDOT =       4759.966478  meter/sec      RA   =          259.74855  deg
     ZDOT =       4209.986171                 TA   =          288.63667
                                              MA   =          288.81938
                                              Ha   =            225.674  n.mi
                                              Hp   =            215.635
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6925165.05                 X    =         2150999.30
     Y    =      -17195694.66  feet           Y    =        -5217419.01  meter
     Z    =       12321080.66                 Z    =         3765816.59
     XDOT =      14074.010225                 XDOT =        4215.761520
     YDOT =      15616.687921  feet/sec       YDOT =        4807.523232  meter/sec
     ZDOT =      13812.290588                 ZDOT =        4230.646054
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16836417.00                 X    =         5131739.90
     Y    =        7685793.45  feet           Y    =         2342629.84  meter
     Z    =       12366183.56                 Z    =         3769212.75
     XDOT =     -15727.475889                 XDOT =       -4793.734651
     YDOT =      11972.452178  feet/sec       YDOT =        3649.203424  meter/sec
     ZDOT =      13899.513956                 ZDOT =        4236.571854
  
  
    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   14353.55630475  .00016717  00000-0  10270-3 0  9008
    2 25544  51.6466 260.3224 0007153 150.1250 210.0312 15.52456825    90
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14353.55630475   =   yrday.fracday
    Element set:     900
    Inclination:       51.6466  deg
    RA of node:       260.3224  deg
    Eccentricity:     .0007153     
    Arg of perigee:   150.1250  deg
    Mean anomaly:     210.0312  deg
    Mean motion:   15.52456825  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:               9
    Checksum:              262
 
 
    Coasting Arc #2 (Orbit 23)
    ---------------------------------------
 
    Vector Time (GMT): 2014/354/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2539249.66                 A    =         6785348.28  meter
     Y    =        4404950.41  meter          E    =           .0012518
     Z    =       -4502211.29                 I    =           51.28756
     XDOT =      -4151.027273                 Wp   =          103.96209
     YDOT =      -5608.037347  meter/sec      RA   =          254.74870  deg
     ZDOT =      -3156.080184                 TA   =          134.20653
                                              MA   =          134.10364
                                              Ha   =            225.443  n.mi
                                              Hp   =            215.615
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8330871.58                 X    =        -2566447.72
     Y    =       14451937.05  feet           Y    =         4376403.27  meter
     Z    =      -14771034.42                 Z    =        -4514612.27
     XDOT =     -13618.855884                 XDOT =       -4072.677082
     YDOT =     -18399.072662  feet/sec       YDOT =       -5654.018419  meter/sec
     ZDOT =     -10354.593780                 ZDOT =       -3176.055659
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14178975.08                 X    =        -4321751.60
     Y    =       -8696526.68  feet           Y    =        -2650701.33  meter
     Z    =      -14824724.38                 Z    =        -4518575.99
     XDOT =      18191.042523                 XDOT =        5544.629761
     YDOT =     -11922.163923  feet/sec       YDOT =       -3633.875564  meter/sec
     ZDOT =     -10438.756139                 ZDOT =       -3181.732871
  
  
    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   14354.52185305  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6473 255.5211 0007081 153.9962 206.1547 15.52531076   246
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14354.52185305   =   yrday.fracday
    Element set:     901
    Inclination:       51.6473  deg
    RA of node:       255.5211  deg
    Eccentricity:     .0007081     
    Arg of perigee:   153.9962  deg
    Mean anomaly:     206.1547  deg
    Mean motion:   15.52531076  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              24
    Checksum:              284
 
 
    Coasting Arc #3 (Orbit 39)
    ---------------------------------------
 
    Vector Time (GMT): 2014/355/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2985540.69                 A    =         6783191.90  meter
     Y    =       -3477527.00  meter          E    =           .0012412
     Z    =        4996965.80                 I    =           51.28944
     XDOT =       3982.353024                 Wp   =          142.83001
     YDOT =       6253.485095  meter/sec      RA   =          249.74495  deg
     ZDOT =       1960.353832                 TA   =          287.97913
                                              MA   =          288.11438
                                              Ha   =            225.274  n.mi
                                              Hp   =            215.747
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9795081.00                 X    =         2999931.66
     Y    =      -11409209.32  feet           Y    =        -3444060.84  meter
     Z    =       16394244.76                 Z    =         5011503.71
     XDOT =      13065.462677                 XDOT =        3902.606344
     YDOT =      20516.683384  feet/sec       YDOT =        6297.572241  meter/sec
     ZDOT =       6431.607062                 ZDOT =        1979.506550
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11262303.79                 X    =         3432750.19
     Y    =        9859844.02  feet           Y    =         3005280.46  meter
     Z    =       16456880.62                 Z    =         5016057.21
     XDOT =     -19989.718058                 XDOT =       -6092.866064
     YDOT =      11896.732096  feet/sec       YDOT =        3626.123943  meter/sec
     ZDOT =       6512.159099                 ZDOT =        1984.906093
  
  
    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   14355.55173794  .00016717  00000-0  10270-3 0  9028
    2 25544  51.6468 250.3997 0007118 158.4236 201.7218 15.52572759   406
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14355.55173794   =   yrday.fracday
    Element set:     902
    Inclination:       51.6468  deg
    RA of node:       250.3997  deg
    Eccentricity:     .0007118     
    Arg of perigee:   158.4236  deg
    Mean anomaly:     201.7218  deg
    Mean motion:   15.52572759  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              40
    Checksum:              318
 
 
    Coasting Arc #4 (Orbit 54)
    ---------------------------------------
 
    Vector Time (GMT): 2014/356/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3521965.15                 A    =         6781841.84  meter
     Y    =        2436025.90  meter          E    =           .0017590
     Z    =       -5272834.37                 I    =           51.29730
     XDOT =      -3698.022339                 Wp   =          108.10284
     YDOT =      -6672.829412  meter/sec      RA   =          244.73747  deg
     ZDOT =       -619.811345                 TA   =          155.98232
                                              MA   =          155.90018
                                              Ha   =            225.093  n.mi
                                              Hp   =            215.698
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11555003.78                 X    =        -3523330.00
     Y    =        7992210.94  feet           Y    =         2396633.95  meter
     Z    =      -17299325.37                 Z    =        -5289946.55
     XDOT =     -12132.619223                 XDOT =       -3620.119527
     YDOT =     -21892.484949  feet/sec       YDOT =       -6713.747449  meter/sec
     ZDOT =      -2033.501789                 ZDOT =        -637.587246
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8017253.59                 X    =        -2443658.90
     Y    =      -11426774.93  feet           Y    =        -3482881.00  meter
     Z    =      -17372756.43                 Z    =        -5295216.16
     XDOT =      21031.124859                 XDOT =        6410.286857
     YDOT =     -11585.879699  feet/sec       YDOT =       -3531.376132  meter/sec
     ZDOT =      -2108.124529                 ZDOT =        -642.556357
  
  
    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   14356.51722317  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6468 245.5978 0007010 162.3148 197.8249 15.52635516   554
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14356.51722317   =   yrday.fracday
    Element set:     903
    Inclination:       51.6468  deg
    RA of node:       245.5978  deg
    Eccentricity:     .0007010     
    Arg of perigee:   162.3148  deg
    Mean anomaly:     197.8249  deg
    Mean motion:   15.52635516  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              55
    Checksum:              315
 
 
    Coasting Arc #5 (Orbit 70)
    ---------------------------------------
 
    Vector Time (GMT): 2014/357/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4057985.55                 A    =         6781679.00  meter
     Y    =       -1386861.58  meter          E    =           .0006879
     Z    =        5249311.53                 I    =           51.31124
     XDOT =       3315.960884                 Wp   =          141.52337
     YDOT =       6875.566729  meter/sec      RA   =          239.73000  deg
     ZDOT =       -751.650350                 TA   =          315.66132
                                              MA   =          315.71640
                                              Ha   =            224.779  n.mi
                                              Hp   =            215.918
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13313600.87                 X    =         4047692.94
     Y    =       -4550070.79  feet           Y    =        -1341540.62  meter
     Z    =       17222150.68                 Z    =         5268999.32
     XDOT =      10879.136760                 XDOT =        3242.481481
     YDOT =      22557.633626  feet/sec       YDOT =        6912.237183  meter/sec
     ZDOT =      -2466.044457                 ZDOT =        -735.719826
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4805503.31                 X    =         1464717.41
     Y    =       13113111.53  feet           Y    =         3996876.40  meter
     Z    =       17306386.98                 Z    =         5274986.75
     XDOT =     -21384.102605                 XDOT =       -6517.874474
     YDOT =      10982.581417  feet/sec       YDOT =        3347.490816  meter/sec
     ZDOT =      -2399.309199                 ZDOT =        -731.309444
  
  
    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   14357.54704006  .00016717  00000-0  10270-3 0  9047
    2 25544  51.6464 240.4758 0006975 167.3193 192.8135 15.52700024   718
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14357.54704006   =   yrday.fracday
    Element set:     904
    Inclination:       51.6464  deg
    RA of node:       240.4758  deg
    Eccentricity:     .0006975     
    Arg of perigee:   167.3193  deg
    Mean anomaly:     192.8135  deg
    Mean motion:   15.52700024  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              71
    Checksum:              299
 
 
    Coasting Arc #6 (Orbit 85)
    ---------------------------------------
 
    Vector Time (GMT): 2014/358/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4629070.53                 A    =         6782897.82  meter
     Y    =         331307.87  meter          E    =           .0016665
     Z    =       -4961474.19                 I    =           51.33171
     XDOT =      -2756.201975                 Wp   =          127.90728
     YDOT =      -6821.014222  meter/sec      RA   =          234.72327  deg
     ZDOT =       2110.893384                 TA   =          162.80659
                                              MA   =          162.75008
                                              Ha   =            224.732  n.mi
                                              Hp   =            215.881
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15187239.27                 X    =        -4608330.32
     Y    =        1086968.07  feet           Y    =          279658.97  meter
     Z    =      -16277802.45                 Z    =        -4983910.86
     XDOT =      -9042.657398                 XDOT =       -2689.976859
     YDOT =     -22378.655584  feet/sec       YDOT =       -6851.465749  meter/sec
     ZDOT =       6925.503228                 ZDOT =        2097.664610
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1638707.09                 X    =         -499477.92
     Y    =      -15033989.60  feet           Y    =        -4582360.03  meter
     Z    =      -16373588.01                 Z    =        -4990669.63
     XDOT =      20932.923155                 XDOT =        6380.354978
     YDOT =      -9782.496171  feet/sec       YDOT =       -2981.704833  meter/sec
     ZDOT =       6870.263989                 ZDOT =        2094.056464
  
  
    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   14358.51246389  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6459 235.6730 0006911 171.1164 189.0111 15.52727517   863
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14358.51246389   =   yrday.fracday
    Element set:     905
    Inclination:       51.6459  deg
    RA of node:       235.6730  deg
    Eccentricity:     .0006911     
    Arg of perigee:   171.1164  deg
    Mean anomaly:     189.0111  deg
    Mean motion:   15.52727517  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              86
    Checksum:              308
 
 
    Coasting Arc #7 (Orbit 101)
    ---------------------------------------
 
    Vector Time (GMT): 2014/359/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5136412.10                 A    =         6784929.15  meter
     Y    =         651305.76  meter          E    =           .0010003
     Z    =        4374772.60                 I    =           51.35813
     XDOT =       2041.359058                 Wp   =          111.27865
     YDOT =       6581.213807  meter/sec      RA   =          229.72178  deg
     ZDOT =      -3373.879133                 TA   =           12.99907
                                              MA   =           12.97330
                                              Ha   =            224.324  n.mi
                                              Hp   =            216.108
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16851745.75                 X    =         5107496.37
     Y    =        2136829.93  feet           Y    =          708582.51  meter
     Z    =       14352928.47                 Z    =         4399654.01
     XDOT =       6697.372237                 XDOT =        1984.003651
     YDOT =      21591.908815  feet/sec       YDOT =        6603.721127  meter/sec
     ZDOT =     -11069.157259                 ZDOT =       -3364.101539
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1231472.94                 X    =         -375352.95
     Y    =       16851563.31  feet           Y    =         5136356.50  meter
     Z    =       14458984.09                 Z    =         4407098.35
     XDOT =     -19965.833981                 XDOT =       -6085.586197
     YDOT =       8011.158642  feet/sec       YDOT =        2441.801154  meter/sec
     ZDOT =     -11028.582746                 ZDOT =       -3361.512021
  
  
    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   14359.54221495  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6458 230.5504 0006780 175.5675 184.5538 15.52807875  1022
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14359.54221495   =   yrday.fracday
    Element set:     906
    Inclination:       51.6458  deg
    RA of node:       230.5504  deg
    Eccentricity:     .0006780     
    Arg of perigee:   175.5675  deg
    Mean anomaly:     184.5538  deg
    Mean motion:   15.52807875  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             102
    Checksum:              323
 
 
    Coasting Arc #8 (Orbit 116)
    ---------------------------------------
 
    Vector Time (GMT): 2014/360/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5584203.56                 A    =         6787718.10  meter
     Y    =       -1541247.78  meter          E    =           .0009119
     Z    =       -3549335.07                 I    =           51.38784
     XDOT =      -1137.388362                 Wp   =          145.02904
     YDOT =      -6126.725175  meter/sec      RA   =          224.72551  deg
     ZDOT =       4448.279439                 TA   =          173.01219
                                              MA   =          172.99947
                                              Ha   =            224.345  n.mi
                                              Hp   =            216.157
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18320877.83                 X    =        -5549312.65
     Y    =       -5056587.22  feet           Y    =        -1603498.73  meter
     Z    =      -11644800.10                 Z    =        -3576377.30
     XDOT =      -3731.589113                 XDOT =       -1090.401372
     YDOT =     -20100.804379  feet/sec       YDOT =       -6139.181669  meter/sec
     ZDOT =      14594.092648                 ZDOT =        4442.868095
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3747904.79                 X    =         1142361.38
     Y    =      -18560230.38  feet           Y    =        -5657158.22  meter
     Z    =      -11759934.79                 Z    =        -3584428.13
     XDOT =      18423.402587                 XDOT =        5615.453108
     YDOT =      -5516.065138  feet/sec       YDOT =       -1681.296654  meter/sec
     ZDOT =      14572.056256                 ZDOT =        4441.562747
  
  
    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   14360.50757768  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6451 225.7468 0006812 179.9205 180.1949 15.52815982  1175
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14360.50757768   =   yrday.fracday
    Element set:     907
    Inclination:       51.6451  deg
    RA of node:       225.7468  deg
    Eccentricity:     .0006812     
    Arg of perigee:   179.9205  deg
    Mean anomaly:     180.1949  deg
    Mean motion:   15.52815982  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             117
    Checksum:              332
 
 
    Coasting Arc #9 (Orbit 132)
    ---------------------------------------
 
    Vector Time (GMT): 2014/361/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5872469.21                 A    =         6790273.12  meter
     Y    =        2305288.22  meter          E    =           .0016377
     Z    =        2483797.58                 I    =           51.42015
     XDOT =         67.202804                 Wp   =          128.43672
     YDOT =       5550.979239  meter/sec      RA   =          219.73734  deg
     ZDOT =      -5297.198157                 TA   =           23.61865
                                              MA   =           23.54355
                                              Ha   =            224.032  n.mi
                                              Hp   =            216.301
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19266631.25                 X    =         5834189.12
     Y    =        7563281.55  feet           Y    =         2370743.86  meter
     Z    =        8148942.19                 Z    =         2512231.99
     XDOT =        220.481641                 XDOT =          30.857258
     YDOT =      18211.874145  feet/sec       YDOT =        5551.527700  meter/sec
     ZDOT =     -17379.259046                 ZDOT =       -5296.959796
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5839299.98                 X    =        -1779818.63
     Y    =       19807142.36  feet           Y    =         6037216.99  meter
     Z    =        8269900.46                 Z    =         2520665.66
     XDOT =     -16665.760212                 XDOT =       -5079.723713
     YDOT =       2361.506332  feet/sec       YDOT =         719.787130  meter/sec
     ZDOT =     -17379.190148                 ZDOT =       -5297.177157
  
  
    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   14361.53726504  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6453 220.6237 0006729 183.1898 176.9212 15.52879388  1331
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14361.53726504   =   yrday.fracday
    Element set:     908
    Inclination:       51.6453  deg
    RA of node:       220.6237  deg
    Eccentricity:     .0006729     
    Arg of perigee:   183.1898  deg
    Mean anomaly:     176.9212  deg
    Mean motion:   15.52879388  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             133
    Checksum:              327
 
 
    Coasting Arc #10 (Orbit 147)
    ---------------------------------------
 
    Vector Time (GMT): 2014/362/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5997827.62                 A    =         6792145.61  meter
     Y    =       -2920464.16  meter          E    =           .0004457
     Z    =       -1279590.74                 I    =           51.45045
     XDOT =       1128.185451                 Wp   =           86.11069
     YDOT =      -4856.958829  meter/sec      RA   =          214.75425  deg
     ZDOT =       5814.943753                 TA   =          259.95134
                                              MA   =          260.00163
                                              Ha   =            223.940  n.mi
                                              Hp   =            216.467
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19677912.14                 X    =        -5958508.75
     Y    =       -9581575.32  feet           Y    =        -2987315.88  meter
     Z    =       -4198132.36                 Z    =        -1308631.70
     XDOT =       3701.395835                 XDOT =        1154.166353
     YDOT =     -15934.904295  feet/sec       YDOT =       -4844.197637  meter/sec
     ZDOT =      19077.899452                 ZDOT =        5820.487232
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7458471.05                 X    =         2273341.98
     Y    =      -20551063.51  feet           Y    =        -6263964.16  meter
     Z    =       -4321588.29                 Z    =        -1317220.11
     XDOT =      14723.100100                 XDOT =        4487.600911
     YDOT =       1338.372510  feet/sec       YDOT =         407.935941  meter/sec
     ZDOT =      19102.384397                 ZDOT =        5822.406764
  
  
    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   14362.50256641  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6443 215.8195 0006722 188.2308 171.8734 15.52905321  1480
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14362.50256641   =   yrday.fracday
    Element set:     909
    Inclination:       51.6443  deg
    RA of node:       215.8195  deg
    Eccentricity:     .0006722     
    Arg of perigee:   188.2308  deg
    Mean anomaly:     171.8734  deg
    Mean motion:   15.52905321  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             148
    Checksum:              305
 
 
    Coasting Arc #11 (Orbit 163)
    ---------------------------------------
 
    Vector Time (GMT): 2014/363/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5868444.00                 A    =         6792788.34  meter
     Y    =        3400249.87  meter          E    =           .0016778
     Z    =         -46298.75                 I    =           51.47910
     XDOT =      -2426.105071                 Wp   =          154.82771
     YDOT =       4116.560866  meter/sec      RA   =          209.77719  deg
     ZDOT =      -6002.142786                 TA   =           25.67220
                                              MA   =           25.58900
                                              Ha   =            223.793  n.mi
                                              Hp   =            216.567
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19253425.19                 X    =         5830210.35
     Y    =       11155675.41  feet           Y    =         3465660.84  meter
     Z    =        -151898.78                 Z    =          -17883.56
     XDOT =      -7959.662307                 XDOT =       -2442.800779
     YDOT =      13505.777120  feet/sec       YDOT =        4089.337457  meter/sec
     ZDOT =     -19692.069509                 ZDOT =       -6013.968800
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8714326.66                 X    =        -2656126.77
     Y    =       20475011.28  feet           Y    =         6240783.44  meter
     Z    =         -31181.40                 Z    =           -9504.09
     XDOT =     -12868.598021                 XDOT =       -3922.348677
     YDOT =      -5487.190364  feet/sec       YDOT =       -1672.495623  meter/sec
     ZDOT =     -19743.245628                 ZDOT =       -6017.741267
  
  
    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   14363.53219000  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6442 210.6962 0006805 191.7835 168.3159 15.52941109  1644
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14363.53219000   =   yrday.fracday
    Element set:     910
    Inclination:       51.6442  deg
    RA of node:       210.6962  deg
    Eccentricity:     .0006805     
    Arg of perigee:   191.7835  deg
    Mean anomaly:     168.3159  deg
    Mean motion:   15.52941109  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             164
    Checksum:              293
 
 
    Coasting Arc #12 (Orbit 179)
    ---------------------------------------
 
    Vector Time (GMT): 2014/364/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 929709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5507079.82                 A    =         6791793.45  meter
     Y    =       -3732859.15  meter          E    =           .0009994
     Z    =        1356211.81                 I    =           51.50319
     XDOT =       3715.857007                 Wp   =           87.82216
     YDOT =      -3362.386881  meter/sec      RA   =          204.79994  deg
     ZDOT =       5797.385148                 TA   =          286.96417
                                              MA   =          287.07369
                                              Ha   =            223.528  n.mi
                                              Hp   =            216.690
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18067847.18                 X    =        -5471516.83
     Y    =      -12246913.21  feet           Y    =        -3794244.11  meter
     Z    =        4449513.81                 Z    =         1329545.48
     XDOT =      12191.131914                 XDOT =        3725.018105
     YDOT =     -11031.453022  feet/sec       YDOT =       -3320.782825  meter/sec
     ZDOT =      19020.292479                 ZDOT =        5815.458274
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9602600.71                 X    =         2926872.70
     Y    =      -19626988.60  feet           Y    =        -5982306.13  meter
     Z    =        4336304.42                 Z    =         1321705.59
     XDOT =      11174.386328                 XDOT =        3405.952953
     YDOT =       9713.827459  feet/sec       YDOT =        2960.774609  meter/sec
     ZDOT =      19098.014385                 ZDOT =        5821.074784
  
  
    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   14364.56177819  .00016717  00000-0  10270-3 0  9111
    2 25544  51.6431 205.5712 0006795 196.5399 163.5533 15.53026960  1805
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14364.56177819   =   yrday.fracday
    Element set:     911
    Inclination:       51.6431  deg
    RA of node:       205.5712  deg
    Eccentricity:     .0006795     
    Arg of perigee:   196.5399  deg
    Mean anomaly:     163.5533  deg
    Mean motion:   15.53026960  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             180
    Checksum:              320
 
             

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