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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  28524.36
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.423
   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 2269)
    ---------------------------------------
 
    Vector Time (GMT): 2014/241/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1844882.46                 A    =         6797228.92  meter
     Y    =        5793147.03  meter          E    =           .0007865
     Z    =       -3041064.33                 I    =           52.00982
     XDOT =      -4268.836439                 Wp   =           63.28533
     YDOT =       3961.873860  meter/sec      RA   =           95.33060  deg
     ZDOT =       4970.882420                 TA   =          262.13031
                                              MA   =          262.21960
                                              Ha   =            228.497  n.mi
                                              Hp   =            220.020
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6052763.98                 X    =         1794737.51
     Y    =       19006387.91  feet           Y    =         5813497.03  meter
     Z    =       -9977245.19                 Z    =        -3032224.55
     XDOT =     -14005.368894                 XDOT =       -4336.968630
     YDOT =      12998.273818  feet/sec       YDOT =        3913.756514  meter/sec
     ZDOT =      16308.669357                 ZDOT =        4949.979203
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1870278.12                 X    =          570060.77
     Y    =      -19877407.23  feet           Y    =        -6058633.73  meter
     Z    =       -9940568.20                 Z    =        -3029885.19
     XDOT =      16639.890036                 XDOT =        5071.838483
     YDOT =      -6523.437012  feet/sec       YDOT =       -1988.343601  meter/sec
     ZDOT =      16219.071585                 ZDOT =        4943.573019
  
  
    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   14241.50620882  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6440  96.1823 0003434  53.3543 306.7923 15.50086510 22700
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14241.50620882   =   yrday.fracday
    Element set:     900
    Inclination:       51.6440  deg
    RA of node:        96.1823  deg
    Eccentricity:     .0003434     
    Arg of perigee:    53.3543  deg
    Mean anomaly:     306.7923  deg
    Mean motion:   15.50086510  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2270
    Checksum:              274
 
 
    Coasting Arc #2 (Orbit 2285)
    ---------------------------------------
 
    Vector Time (GMT): 2014/242/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2068514.94                 A    =         6797834.71  meter
     Y    =       -5878085.86  meter          E    =           .0016068
     Z    =        2701657.62                 I    =           52.01487
     XDOT =       4096.012889                 Wp   =           92.66437
     YDOT =      -3848.294050  meter/sec      RA   =           90.40133  deg
     ZDOT =      -5210.814051                 TA   =           57.02519
                                              MA   =           56.87083
                                              Ha   =            228.409  n.mi
                                              Hp   =            219.859
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6786466.33                 X    =        -2015754.87
     Y    =      -19285058.59  feet           Y    =        -5900922.09  meter
     Z    =        8863706.10                 Z    =         2691737.75
     XDOT =      13438.362498                 XDOT =        4164.053422
     YDOT =     -12625.636646  feet/sec       YDOT =       -3802.109817  meter/sec
     ZDOT =     -17095.846624                 ZDOT =       -5190.750600
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -960846.45                 X    =         -292866.00
     Y    =       20439567.54  feet           Y    =         6229980.19  meter
     Z    =        8822457.06                 Z    =         2689084.91
     XDOT =     -15825.147307                 XDOT =       -4823.504899
     YDOT =       6635.050699  feet/sec       YDOT =        2022.363453  meter/sec
     ZDOT =     -17009.832368                 ZDOT =       -5184.596906
  
  
    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   14242.53771354  .00016717  00000-0  10270-3 0  9016
    2 25544  51.6443  91.0708 0003486  54.5282 305.6194 15.50162387 22861
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14242.53771354   =   yrday.fracday
    Element set:     901
    Inclination:       51.6443  deg
    RA of node:        91.0708  deg
    Eccentricity:     .0003486     
    Arg of perigee:    54.5282  deg
    Mean anomaly:     305.6194  deg
    Mean motion:   15.50162387  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2286
    Checksum:              301
 
 
    Coasting Arc #3 (Orbit 2300)
    ---------------------------------------
 
    Vector Time (GMT): 2014/243/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2335384.37                 A    =         6798533.03  meter
     Y    =        5922083.97  meter          E    =           .0008956
     Z    =       -2382605.59                 I    =           52.01518
     XDOT =      -3941.859065                 Wp   =           50.98410
     YDOT =       3722.898427  meter/sec      RA   =           85.47115  deg
     ZDOT =       5408.806303                 TA   =          282.60958
                                              MA   =          282.70973
                                              Ha   =            228.409  n.mi
                                              Hp   =            219.871
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7662022.22                 X    =         2280562.64
     Y    =       19429409.34  feet           Y    =         5947893.04  meter
     Z    =       -7816947.46                 Z    =        -2371394.22
     XDOT =     -12932.608480                 XDOT =       -4009.470669
     YDOT =      12214.233684  feet/sec       YDOT =        3678.440388  meter/sec
     ZDOT =      17745.427503                 ZDOT =        5389.492785
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -148474.53                 X    =          -45255.04
     Y    =      -20902507.65  feet           Y    =        -6371084.33  meter
     Z    =       -7770220.63                 Z    =        -2368363.25
     XDOT =      15059.302522                 XDOT =        4590.075409
     YDOT =      -6649.378552  feet/sec       YDOT =       -2026.730583  meter/sec
     ZDOT =      17662.616240                 ZDOT =        5383.565430
  
  
    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   14243.50472877  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6431  86.2778 0003350  59.5359 300.6122 15.50154967 23010
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14243.50472877   =   yrday.fracday
    Element set:     902
    Inclination:       51.6431  deg
    RA of node:        86.2778  deg
    Eccentricity:     .0003350     
    Arg of perigee:    59.5359  deg
    Mean anomaly:     300.6122  deg
    Mean motion:   15.50154967  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2301
    Checksum:              297
 
 
    Coasting Arc #4 (Orbit 2316)
    ---------------------------------------
 
    Vector Time (GMT): 2014/244/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2571666.79                 A    =         6799017.86  meter
     Y    =       -5962657.77  meter          E    =           .0016190
     Z    =        1993863.73                 I    =           52.01475
     XDOT =       3845.085888                 Wp   =          102.39705
     YDOT =      -3543.580708  meter/sec      RA   =           80.54249  deg
     ZDOT =      -5602.832905                 TA   =           55.73834
                                              MA   =           55.58512
                                              Ha   =            228.285  n.mi
                                              Hp   =            219.727
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8437226.99                 X    =        -2514485.39
     Y    =      -19562525.48  feet           Y    =        -5991095.96  meter
     Z    =        6541547.69                 Z    =         1981510.20
     XDOT =      12615.111182                 XDOT =        3911.642025
     YDOT =     -11625.920958  feet/sec       YDOT =       -3500.210686  meter/sec
     ZDOT =     -18381.997719                 ZDOT =       -5583.992130
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1181602.11                 X    =          360152.32
     Y    =       21287438.90  feet           Y    =         6488411.38  meter
     Z    =        6489977.68                 Z    =         1978145.20
     XDOT =     -14416.466231                 XDOT =       -4394.138907
     YDOT =       6414.963039  feet/sec       YDOT =        1955.280734  meter/sec
     ZDOT =     -18301.219029                 ZDOT =       -5578.211560
  
  
    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   14244.53618591  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6436  81.1662 0003381  59.5407 300.6078 15.50236830 23176
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14244.53618591   =   yrday.fracday
    Element set:     903
    Inclination:       51.6436  deg
    RA of node:        81.1662  deg
    Eccentricity:     .0003381     
    Arg of perigee:    59.5407  deg
    Mean anomaly:     300.6078  deg
    Mean motion:   15.50236830  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2317
    Checksum:              293
 
 
    Coasting Arc #5 (Orbit 2331)
    ---------------------------------------
 
    Vector Time (GMT): 2014/245/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2841544.81                 A    =         6799596.77  meter
     Y    =        5954802.10  meter          E    =           .0010957
     Z    =       -1629622.51                 I    =           52.00941
     XDOT =      -3774.717988                 Wp   =           46.09185
     YDOT =       3366.954751  meter/sec      RA   =           75.61236  deg
     ZDOT =       5752.667474                 TA   =          296.19527
                                              MA   =          296.30789
                                              Ha   =            228.325  n.mi
                                              Hp   =            219.706
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9322653.56                 X    =         2782661.82
     Y    =       19536752.30  feet           Y    =         5986248.77  meter
     Z    =       -5346530.54                 Z    =        -1615962.03
     XDOT =     -12384.245367                 XDOT =       -3840.032078
     YDOT =      11046.439473  feet/sec       YDOT =        3324.378513  meter/sec
     ZDOT =      18873.580952                 ZDOT =        5734.171640
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2384776.65                 X    =         -726879.92
     Y    =      -21529444.14  feet           Y    =        -6562174.57  meter
     Z    =       -5289406.77                 Z    =        -1612211.18
     XDOT =      13878.405939                 XDOT =        4230.138130
     YDOT =      -6129.136197  feet/sec       YDOT =       -1868.160713  meter/sec
     ZDOT =      18794.291263                 ZDOT =        5728.499977
  
  
    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   14245.50315679  .00016717  00000-0  10270-3 0  9043
    2 25544  51.6425  76.3729 0003311  66.4763 293.6736 15.50225496 23324
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14245.50315679   =   yrday.fracday
    Element set:     904
    Inclination:       51.6425  deg
    RA of node:        76.3729  deg
    Eccentricity:     .0003311     
    Arg of perigee:    66.4763  deg
    Mean anomaly:     293.6736  deg
    Mean motion:   15.50225496  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2332
    Checksum:              311
 
 
    Coasting Arc #6 (Orbit 2347)
    ---------------------------------------
 
    Vector Time (GMT): 2014/246/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3071680.10                 A    =         6799860.17  meter
     Y    =       -5940673.76  meter          E    =           .0015739
     Z    =        1195147.81                 I    =           52.00290
     XDOT =       3769.326995                 Wp   =          111.76451
     YDOT =      -3144.198191  meter/sec      RA   =           70.68337  deg
     ZDOT =      -5884.757704                 TA   =           55.33639
                                              MA   =           55.18815
                                              Ha   =            228.173  n.mi
                                              Hp   =            219.573
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10077690.61                 X    =        -3010827.44
     Y    =      -19490399.46  feet           Y    =        -5974682.97  meter
     Z    =        3921088.61                 Z    =         1180374.16
     XDOT =      12366.558384                 XDOT =        3832.792134
     YDOT =     -10315.610863  feet/sec       YDOT =       -3101.692545  meter/sec
     ZDOT =     -19306.947849                 ZDOT =       -5866.292638
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3477646.58                 X    =         1059986.68
     Y    =       21675395.09  feet           Y    =         6606660.42  meter
     Z    =        3859232.70                 Z    =         1176294.13
     XDOT =     -13513.592574                 XDOT =       -4118.943017
     YDOT =       5625.037099  feet/sec       YDOT =        1714.511308  meter/sec
     ZDOT =     -19227.819271                 ZDOT =       -5860.639314
  
  
    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   14246.53456539  .00016717  00000-0  10270-3 0  9059
    2 25544  51.6429  71.2610 0003331  65.4315 294.7183 15.50313522 23488
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14246.53456539   =   yrday.fracday
    Element set:     905
    Inclination:       51.6429  deg
    RA of node:        71.2610  deg
    Eccentricity:     .0003331     
    Arg of perigee:    65.4315  deg
    Mean anomaly:     294.7183  deg
    Mean motion:   15.50313522  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2348
    Checksum:              291
 
 
    Coasting Arc #7 (Orbit 2362)
    ---------------------------------------
 
    Vector Time (GMT): 2014/247/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3323254.56                 A    =         6800225.43  meter
     Y    =        5874210.29  meter          E    =           .0013233
     Z    =        -790337.85                 I    =           51.99200
     XDOT =      -3794.192327                 Wp   =           47.77075
     YDOT =       2940.223253  meter/sec      RA   =           65.75246  deg
     ZDOT =       5971.713415                 TA   =          303.74063
                                              MA   =          303.86666
                                              Ha   =            228.242  n.mi
                                              Hp   =            219.523
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10903066.13                 X    =         3261159.97
     Y    =       19272343.46  feet           Y    =         5911025.84  meter
     Z    =       -2592971.94                 Z    =         -774345.17
     XDOT =     -12448.137557                 XDOT =       -3855.797019
     YDOT =       9646.401749  feet/sec       YDOT =        2897.449970  meter/sec
     ZDOT =      19592.235612                 ZDOT =        5953.132144
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4694826.86                 X    =        -1430983.23
     Y    =      -21647214.49  feet           Y    =        -6598070.98  meter
     Z    =       -2525922.10                 Z    =         -769901.06
     XDOT =      13292.924100                 XDOT =        4051.683266
     YDOT =      -5131.337920  feet/sec       YDOT =       -1564.031798  meter/sec
     ZDOT =      19512.641276                 ZDOT =        5947.453061
  
  
    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   14247.50149062  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6420  66.4675 0003329  73.8618 286.2899 15.50300755 23633
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14247.50149062   =   yrday.fracday
    Element set:     906
    Inclination:       51.6420  deg
    RA of node:        66.4675  deg
    Eccentricity:     .0003329     
    Arg of perigee:    73.8618  deg
    Mean anomaly:     286.2899  deg
    Mean motion:   15.50300755  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2363
    Checksum:              315
 
 
    Coasting Arc #8 (Orbit 2378)
    ---------------------------------------
 
    Vector Time (GMT): 2014/248/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3523278.17                 A    =         6800184.30  meter
     Y    =       -5801208.00  meter          E    =           .0014601
     Z    =         317131.92                 I    =           51.97913
     XDOT =       3887.296969                 Wp   =          119.99814
     YDOT =      -2701.200557  meter/sec      RA   =           60.82183  deg
     ZDOT =      -6025.201332                 TA   =           56.60531
                                              MA   =           56.46571
                                              Ha   =            228.082  n.mi
                                              Hp   =            219.397
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11559311.59                 X    =        -3459686.38
     Y    =      -19032834.65  feet           Y    =        -5840251.99  meter
     Z    =        1040459.07                 Z    =          300171.34
     XDOT =      12753.598980                 XDOT =        3946.481664
     YDOT =      -8862.206551  feet/sec       YDOT =       -2657.399729  meter/sec
     ZDOT =     -19767.720906                 ZDOT =       -6006.173692
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5754161.73                 X    =         1753868.49
     Y    =       21515091.25  feet           Y    =         6557799.81  meter
     Z    =         969281.01                 Z    =          295436.85
     XDOT =     -13280.169471                 XDOT =       -4047.795655
     YDOT =       4470.366702  feet/sec       YDOT =        1362.567771  meter/sec
     ZDOT =     -19686.263917                 ZDOT =       -6000.373242
  
  
    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   14248.53284935  .00016717  00000-0  10270-3 0  9072
    2 25544  51.6421  61.3549 0003352  72.2904 287.8612 15.50389053 23790
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14248.53284935   =   yrday.fracday
    Element set:     907
    Inclination:       51.6421  deg
    RA of node:        61.3549  deg
    Eccentricity:     .0003352     
    Arg of perigee:    72.2904  deg
    Mean anomaly:     287.8612  deg
    Mean motion:   15.50389053  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2379
    Checksum:              316
 
 
    Coasting Arc #9 (Orbit 2394)
    ---------------------------------------
 
    Vector Time (GMT): 2014/249/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3731145.07                 A    =         6800228.64  meter
     Y    =        5676378.55  meter          E    =           .0015258
     Z    =         120244.76                 I    =           51.96306
     XDOT =      -4010.139357                 Wp   =           53.82237
     YDOT =       2496.990999  meter/sec      RA   =           55.88916  deg
     ZDOT =       6033.959453                 TA   =          307.46527
                                              MA   =          307.60395
                                              Ha   =            228.141  n.mi
                                              Hp   =            219.334
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12241289.60                 X    =         3666809.09
     Y    =       18623289.19  feet           Y    =         5717742.91  meter
     Z    =         394503.80                 Z    =          138213.17
     XDOT =     -13156.625186                 XDOT =       -4067.073890
     YDOT =       8192.227687  feet/sec       YDOT =        2451.829178  meter/sec
     ZDOT =      19796.454898                 ZDOT =        6014.340533
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6880614.84                 X    =        -2097211.40
     Y    =      -21195941.92  feet           Y    =        -6460523.10  meter
     Z    =         469989.78                 Z    =          143252.89
     XDOT =      13428.900752                 XDOT =        4093.128949
     YDOT =      -3890.195421  feet/sec       YDOT =       -1185.731564  meter/sec
     ZDOT =      19712.514908                 ZDOT =        6008.374544
  
  
    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   14249.56418456  .00016717  00000-0  10270-3 0  9084
    2 25544  51.6419  56.2416 0003375  81.3821 278.7712 15.50384123 23958
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14249.56418456   =   yrday.fracday
    Element set:     908
    Inclination:       51.6419  deg
    RA of node:        56.2416  deg
    Eccentricity:     .0003375     
    Arg of perigee:    81.3821  deg
    Mean anomaly:     278.7712  deg
    Mean motion:   15.50384123  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2395
    Checksum:              316
 
 
    Coasting Arc #10 (Orbit 2409)
    ---------------------------------------
 
    Vector Time (GMT): 2014/250/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3874307.77                 A    =         6799838.86  meter
     Y    =       -5548411.74  meter          E    =           .0012714
     Z    =        -620859.96                 I    =           51.94427
     XDOT =       4198.069974                 Wp   =          125.72433
     YDOT =      -2271.276422  meter/sec      RA   =           50.95572  deg
     ZDOT =      -5992.431585                 TA   =           60.93858
                                              MA   =           60.81129
                                              Ha   =            228.002  n.mi
                                              Hp   =            219.226
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12710983.49                 X    =        -3808960.30
     Y    =      -18203450.58  feet           Y    =        -5591371.44  meter
     Z    =       -2036942.11                 Z    =         -639521.24
     XDOT =      13773.195453                 XDOT =        4252.264828
     YDOT =      -7451.694299  feet/sec       YDOT =       -2224.028500  meter/sec
     ZDOT =     -19660.208611                 ZDOT =       -5971.906350
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7793181.35                 X    =         2375361.68
     Y    =       20781609.04  feet           Y    =         6334234.44  meter
     Z    =       -2115395.39                 Z    =         -644772.52
     XDOT =     -13794.434942                 XDOT =       -4204.543770
     YDOT =       3210.601066  feet/sec       YDOT =         978.591205  meter/sec
     ZDOT =     -19572.451030                 ZDOT =       -5965.683074
  
  
    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   14250.53103449  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6419  51.4479 0003401  79.6932 280.4603 15.50458894 24101
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14250.53103449   =   yrday.fracday
    Element set:     909
    Inclination:       51.6419  deg
    RA of node:        51.4479  deg
    Eccentricity:     .0003401     
    Arg of perigee:    79.6932  deg
    Mean anomaly:     280.4603  deg
    Mean motion:   15.50458894  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2410
    Checksum:              302
 
 
    Coasting Arc #11 (Orbit 2425)
    ---------------------------------------
 
    Vector Time (GMT): 2014/251/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4011607.14                 A    =         6799464.71  meter
     Y    =        5373987.32  meter          E    =           .0016620
     Z    =        1078581.78                 I    =           51.92352
     XDOT =      -4410.900461                 Wp   =           62.71795
     YDOT =       2094.437304  meter/sec      RA   =           46.02046  deg
     ZDOT =       5907.824353                 TA   =          308.91975
                                              MA   =          309.06781
                                              Ha   =            228.001  n.mi
                                              Hp   =            219.162
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13161440.75                 X    =         3945976.47
     Y    =       17631192.01  feet           Y    =         5418480.88  meter
     Z    =        3538654.14                 Z    =         1097909.31
     XDOT =     -14471.458206                 XDOT =       -4462.691131
     YDOT =       6871.513465  feet/sec       YDOT =        2044.822927  meter/sec
     ZDOT =      19382.625831                 ZDOT =        5886.270989
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8710724.71                 X    =        -2655028.89
     Y    =      -20189691.37  feet           Y    =        -6153817.93  meter
     Z    =        3619967.52                 Z    =         1103366.10
     XDOT =      14313.970265                 XDOT =        4362.898137
     YDOT =      -2681.077133  feet/sec       YDOT =        -817.192310  meter/sec
     ZDOT =      19290.525933                 ZDOT =        5879.752304
  
  
    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   14251.56231650  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6427  46.3347 0003395  88.0128 272.1411 15.50473634 24261
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14251.56231650   =   yrday.fracday
    Element set:     910
    Inclination:       51.6427  deg
    RA of node:        46.3347  deg
    Eccentricity:     .0003395     
    Arg of perigee:    88.0128  deg
    Mean anomaly:     272.1411  deg
    Mean motion:   15.50473634  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2426
    Checksum:              284
 
 
    Coasting Arc #12 (Orbit 2440)
    ---------------------------------------
 
    Vector Time (GMT): 2014/252/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4071753.92                 A    =         6798723.17  meter
     Y    =       -5204253.97  meter          E    =           .0010263
     Z    =       -1590241.27                 I    =           51.89948
     XDOT =       4677.539502                 Wp   =          125.88773
     YDOT =      -1910.368597  meter/sec      RA   =           41.08352  deg
     ZDOT =      -5756.592358                 TA   =           71.40973
                                              MA   =           71.29828
                                              Ha   =            227.908  n.mi
                                              Hp   =            219.086
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13358772.69                 X    =        -4005531.29
     Y    =      -17074324.04  feet           Y    =        -5249416.90  meter
     Z    =       -5217327.01                 Z    =        -1609859.60
     XDOT =      15346.258208                 XDOT =        4726.517554
     YDOT =      -6267.613506  feet/sec       YDOT =       -1857.788260  meter/sec
     ZDOT =     -18886.457868                 ZDOT =       -5733.750442
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9358411.96                 X    =         2852443.96
     Y    =       19533075.63  feet           Y    =         5953681.45  meter
     Z    =       -5299899.29                 Z    =        -1615409.30
     XDOT =     -15024.512700                 XDOT =       -4579.471471
     YDOT =       2128.244564  feet/sec       YDOT =         648.688943  meter/sec
     ZDOT =     -18788.910430                 ZDOT =       -5726.859899
  
  
    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   14252.52911756  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6429  41.5408 0003417  86.9504 273.2038 15.50523265 24418
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14252.52911756   =   yrday.fracday
    Element set:     911
    Inclination:       51.6429  deg
    RA of node:        41.5408  deg
    Eccentricity:     .0003417     
    Arg of perigee:    86.9504  deg
    Mean anomaly:     273.2038  deg
    Mean motion:   15.50523265  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2441
    Checksum:              291
 
 
    Coasting Arc #13 (Orbit 2456)
    ---------------------------------------
 
    Vector Time (GMT): 2014/253/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4113703.56                 A    =         6797890.00  meter
     Y    =        4998218.88  meter          E    =           .0017022
     Z    =        2051203.75                 I    =           51.87425
     XDOT =      -4960.556286                 Wp   =           73.57564
     YDOT =       1785.191178  meter/sec      RA   =           36.14471  deg
     ZDOT =       5564.879634                 TA   =          309.00515
                                              MA   =          309.15661
                                              Ha   =            227.823  n.mi
                                              Hp   =            219.023
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13496402.77                 X    =         4047542.51
     Y    =       16398355.92  feet           Y    =         5043851.33  meter
     Z    =        6729671.10                 Z    =         2071026.14
     XDOT =     -16274.790965                 XDOT =       -5007.182401
     YDOT =       5856.926437  feet/sec       YDOT =        1729.459086  meter/sec
     ZDOT =      18257.479114                 ZDOT =        5540.668482
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9952011.26                 X    =        -3033373.03
     Y    =      -18731953.04  feet           Y    =        -5709499.29  meter
     Z    =        6813137.67                 Z    =         2076644.36
     XDOT =      15857.435642                 XDOT =        4833.346384
     YDOT =      -1782.325648  feet/sec       YDOT =        -543.252858  meter/sec
     ZDOT =      18154.131570                 ZDOT =        5533.379303
  
  
    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   14253.56034477  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6442  36.4279 0003362  93.5898 266.5637 15.50565654 24576
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14253.56034477   =   yrday.fracday
    Element set:     912
    Inclination:       51.6442  deg
    RA of node:        36.4279  deg
    Eccentricity:     .0003362     
    Arg of perigee:    93.5898  deg
    Mean anomaly:     266.5637  deg
    Mean motion:   15.50565654  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2457
    Checksum:              331
 
 
    Coasting Arc #14 (Orbit 2471)
    ---------------------------------------
 
    Vector Time (GMT): 2014/254/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4069328.75                 A    =         6796831.47  meter
     Y    =       -4809205.88  meter          E    =           .0008132
     Z    =       -2552378.73                 I    =           51.84547
     XDOT =       5277.344389                 Wp   =          114.19063
     YDOT =      -1665.127846  meter/sec      RA   =           31.20340  deg
     ZDOT =      -5292.912549                 TA   =           94.33337
                                              MA   =           94.24044
                                              Ha   =            227.784  n.mi
                                              Hp   =            218.979
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13350816.09                 X    =        -4002849.98
     Y    =      -15778234.52  feet           Y    =        -4854340.37  meter
     Z    =       -8373945.96                 Z    =        -2571984.93
     XDOT =      17314.122011                 XDOT =        5321.283354
     YDOT =      -5463.017868  feet/sec       YDOT =       -1605.868159  meter/sec
     ZDOT =     -17365.198653                 ZDOT =       -5267.168947
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10231283.12                 X    =         3118495.10
     Y    =       17920048.76  feet           Y    =         5462030.86  meter
     Z    =       -8456514.88                 Z    =        -2577545.74
     XDOT =     -16816.549910                 XDOT =       -5125.684412
     YDOT =       1483.760548  feet/sec       YDOT =         452.250215  meter/sec
     ZDOT =     -17255.356074                 ZDOT =       -5259.432531
  
  
    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   14254.52709563  .00016717  00000-0  10270-3 0  9134
    2 25544  51.6444  31.6343 0003369  93.3731 266.7805 15.50588418 24727
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14254.52709563   =   yrday.fracday
    Element set:     913
    Inclination:       51.6444  deg
    RA of node:        31.6343  deg
    Eccentricity:     .0003369     
    Arg of perigee:    93.3731  deg
    Mean anomaly:     266.7805  deg
    Mean motion:   15.50588418  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2472
    Checksum:              315
 
 
    Coasting Arc #15 (Orbit 2487)
    ---------------------------------------
 
    Vector Time (GMT): 2014/255/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3997332.42                 A    =         6795597.37  meter
     Y    =        4598042.08  meter          E    =           .0016311
     Z    =        2994319.67                 I    =           51.81598
     XDOT =      -5599.379863                 Wp   =           85.80339
     YDOT =       1608.000424  meter/sec      RA   =           26.25957  deg
     ZDOT =       4983.571285                 TA   =          308.33135
                                              MA   =          308.47786
                                              Ha   =            227.631  n.mi
                                              Hp   =            218.913
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13114607.67                 X    =         3931073.44
     Y    =       15085439.89  feet           Y    =         4642372.69  meter
     Z    =        9823883.44                 Z    =         3013576.79
     XDOT =     -18370.668842                 XDOT =       -5641.153445
     YDOT =       5275.591943  feet/sec       YDOT =        1545.151518  meter/sec
     ZDOT =      16350.299491                 ZDOT =        4956.268512
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10409276.12                 X    =        -3172747.36
     Y    =      -17017937.02  feet           Y    =        -5187067.20  meter
     Z    =        9904994.05                 Z    =         3019042.19
     XDOT =      17846.622247                 XDOT =        5439.650461
     YDOT =      -1425.455233  feet/sec       YDOT =        -434.478755  meter/sec
     ZDOT =      16233.836935                 ZDOT =        4948.073498
  
  
    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   14255.55826695  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6456  26.5214 0003297  97.9137 262.2388 15.50655427 24889
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14255.55826695   =   yrday.fracday
    Element set:     914
    Inclination:       51.6456  deg
    RA of node:        26.5214  deg
    Eccentricity:     .0003297     
    Arg of perigee:    97.9137  deg
    Mean anomaly:     262.2388  deg
    Mean motion:   15.50655427  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2488
    Checksum:              338
 
             

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