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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  30138.95
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   130.0
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.252
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 3138)
    ---------------------------------------
 
    Vector Time (GMT): 2014/297/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -367220.93                 A    =         6787026.42  meter
     Y    =        4223703.10  meter          E    =           .0012121
     Z    =       -5310354.28                 I    =           51.63648
     XDOT =      -7638.516212                 Wp   =           86.71143
     YDOT =        -50.971195  meter/sec      RA   =          177.47586  deg
     ZDOT =        489.321726                 TA   =          187.95551
                                              MA   =          187.97475
                                              Ha   =            225.381  n.mi
                                              Hp   =            220.778
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1204793.08                 X    =         -388627.36
     Y    =       13857293.65  feet           Y    =         4219476.49  meter
     Z    =      -17422422.19                 Z    =        -5312190.57
     XDOT =     -25060.748728                 XDOT =       -7639.755556
     YDOT =       -167.228331  feet/sec       YDOT =        -136.396924  meter/sec
     ZDOT =       1605.386240                 ZDOT =         452.210861
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6410094.38                 X    =        -1953796.77
     Y    =      -12332562.35  feet           Y    =        -3758965.01  meter
     Z    =      -17430877.90                 Z    =        -5312931.58
     XDOT =      20454.165036                 XDOT =        6234.429503
     YDOT =     -12669.568694  feet/sec       YDOT =       -3861.684538  meter/sec
     ZDOT =       1447.382621                 ZDOT =         441.162223
  
  
    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   14297.51536800  .00016717  00000-0  10270-3 0  9008
    2 25544  51.6462 178.5197 0003116 302.4915  57.5934 15.50834477 31392
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14297.51536800   =   yrday.fracday
    Element set:     900
    Inclination:       51.6462  deg
    RA of node:       178.5197  deg
    Eccentricity:     .0003116     
    Arg of perigee:   302.4915  deg
    Mean anomaly:      57.5934  deg
    Mean motion:   15.50834477  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3139
    Checksum:              314
 
 
    Coasting Arc #2 (Orbit 3154)
    ---------------------------------------
 
    Vector Time (GMT): 2014/298/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         797708.49                 A    =         6787203.84  meter
     Y    =       -4266171.64  meter          E    =           .0004043
     Z    =        5218334.32                 I    =           51.66868
     XDOT =       7570.135977                 Wp   =            9.21276
     YDOT =        -45.678591  meter/sec      RA   =          172.51164  deg
     ZDOT =      -1190.537222                 TA   =           92.23315
                                              MA   =           92.18686
                                              Ha   =            225.272  n.mi
                                              Hp   =            220.706
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2617153.82                 X    =          820004.82
     Y    =      -13996626.12  feet           Y    =        -4257126.17  meter
     Z    =       17120519.42                 Z    =         5222264.00
     XDOT =      24836.404125                 XDOT =        7575.867539
     YDOT =       -149.864144  feet/sec       YDOT =          39.007550  meter/sec
     ZDOT =      -3905.962015                 ZDOT =       -1153.747617
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5510609.50                 X    =         1679633.78
     Y    =       13106973.46  feet           Y    =         3995005.51  meter
     Z    =       17137901.03                 Z    =         5223632.23
     XDOT =     -19819.851561                 XDOT =       -6041.090756
     YDOT =      13252.539390  feet/sec       YDOT =        4039.374006  meter/sec
     ZDOT =      -3749.294374                 ZDOT =       -1142.784925
  
  
    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   14298.54638240  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6460 173.4055 0003216 304.9838  55.1011 15.50897795 31559
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14298.54638240   =   yrday.fracday
    Element set:     901
    Inclination:       51.6460  deg
    RA of node:       173.4055  deg
    Eccentricity:     .0003216     
    Arg of perigee:   304.9838  deg
    Mean anomaly:      55.1011  deg
    Mean motion:   15.50897795  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3155
    Checksum:              307
 
 
    Coasting Arc #3 (Orbit 3169)
    ---------------------------------------
 
    Vector Time (GMT): 2014/299/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1217903.59                 A    =         6787794.00  meter
     Y    =        4363976.71  meter          E    =           .0010208
     Z    =       -5063466.16                 I    =           51.70097
     XDOT =      -7418.945099                 Wp   =           96.47461
     YDOT =        113.848735  meter/sec      RA   =          167.54877  deg
     ZDOT =       1884.728554                 TA   =          191.79629
                                              MA   =          191.82023
                                              Ha   =            225.314  n.mi
                                              Hp   =            220.579
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3995746.69                 X    =        -1242014.72
     Y    =       14317508.90  feet           Y    =         4350222.30  meter
     Z    =      -16612421.77                 Z    =        -5069441.47
     XDOT =     -24340.371060                 XDOT =       -7428.822435
     YDOT =        373.519471  feet/sec       YDOT =          30.830137  meter/sec
     ZDOT =       6183.492630                 ZDOT =        1848.663402
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4768334.10                 X    =        -1453388.23
     Y    =      -14048191.43  feet           Y    =        -4281888.75  meter
     Z    =      -16638537.11                 Z    =        -5071426.11
     XDOT =      18988.706282                 XDOT =        5787.757675
     YDOT =     -13578.682155  feet/sec       YDOT =       -4138.782321  meter/sec
     ZDOT =       6029.880634                 ZDOT =        1837.907617
  
  
    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   14299.51292801  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6451 168.6098 0003283 308.4714  51.6142 15.50931764 31706
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14299.51292801   =   yrday.fracday
    Element set:     902
    Inclination:       51.6451  deg
    RA of node:       168.6098  deg
    Eccentricity:     .0003283     
    Arg of perigee:   308.4714  deg
    Mean anomaly:      51.6142  deg
    Mean motion:   15.50931764  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3170
    Checksum:              302
 
 
    Coasting Arc #4 (Orbit 3185)
    ---------------------------------------
 
    Vector Time (GMT): 2014/300/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1647124.77                 A    =         6788593.25  meter
     Y    =       -4494758.60  meter          E    =           .0006921
     Z    =        4812519.77                 I    =           51.73473
     XDOT =       7214.318879                 Wp   =           33.31658
     YDOT =       -128.301702  meter/sec      RA   =          162.58903  deg
     ZDOT =      -2581.581183                 TA   =           82.13021
                                              MA   =           82.05166
                                              Ha   =            225.209  n.mi
                                              Hp   =            220.496
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5403952.66                 X    =         1673885.54
     Y    =      -14746583.34  feet           Y    =        -4476189.62  meter
     Z    =       15789106.85                 Z    =         4820586.59
     XDOT =      23669.025195                 XDOT =        7227.758185
     YDOT =       -420.937342  feet/sec       YDOT =         -47.551447  meter/sec
     ZDOT =      -8469.754538                 ZDOT =       -2546.501542
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4096430.62                 X    =         1248592.05
     Y    =       15125328.74  feet           Y    =         4610200.20  meter
     Z    =       15824158.94                 Z    =         4823203.65
     XDOT =     -18101.861019                 XDOT =       -5517.447239
     YDOT =      13632.686512  feet/sec       YDOT =        4155.242849  meter/sec
     ZDOT =      -8320.317546                 ZDOT =       -2536.032788
  
  
    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   14300.54387486  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6451 163.4950 0003412 311.5264  48.5594 15.51004973 31862
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14300.54387486   =   yrday.fracday
    Element set:     903
    Inclination:       51.6451  deg
    RA of node:       163.4950  deg
    Eccentricity:     .0003412     
    Arg of perigee:   311.5264  deg
    Mean anomaly:      48.5594  deg
    Mean motion:   15.51004973  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3186
    Checksum:              299
 
 
    Coasting Arc #5 (Orbit 3200)
    ---------------------------------------
 
    Vector Time (GMT): 2014/301/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2036016.28                 A    =         6789775.49  meter
     Y    =        4668505.01  meter          E    =           .0006607
     Z    =       -4496271.22                 I    =           51.76738
     XDOT =      -6936.903843                 Wp   =           98.69442
     YDOT =         93.394798  meter/sec      RA   =          157.63100  deg
     ZDOT =       3241.262494                 TA   =          203.89719
                                              MA   =          203.92787
                                              Ha   =            225.271  n.mi
                                              Hp   =            220.362
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6679843.43                 X    =        -2066227.37
     Y    =       15316617.50  feet           Y    =         4645567.94  meter
     Z    =      -14751546.01                 Z    =        -4506235.59
     XDOT =     -22758.870875                 XDOT =       -6953.177971
     YDOT =        306.413378  feet/sec       YDOT =          15.730923  meter/sec
     ZDOT =      10634.063302                 ZDOT =        3207.523766
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3652032.02                 X    =        -1113139.36
     Y    =      -16266720.18  feet           Y    =        -4958096.31  meter
     Z    =      -14794717.52                 Z    =        -4509429.90
     XDOT =      17117.267254                 XDOT =        5217.343059
     YDOT =     -13374.805316  feet/sec       YDOT =       -4076.640660  meter/sec
     ZDOT =      10490.323375                 ZDOT =        3197.450565
  
  
    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   14301.51035790  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6440 158.6986 0003412 314.4878  45.5993 15.51028300 32016
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14301.51035790   =   yrday.fracday
    Element set:     904
    Inclination:       51.6440  deg
    RA of node:       158.6986  deg
    Eccentricity:     .0003412     
    Arg of perigee:   314.4878  deg
    Mean anomaly:      45.5993  deg
    Mean motion:   15.51028300  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3201
    Checksum:              290
 
 
    Coasting Arc #6 (Orbit 3216)
    ---------------------------------------
 
    Vector Time (GMT): 2014/302/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2416878.22                 A    =         6791043.95  meter
     Y    =       -4860310.64  meter          E    =           .0009347
     Z    =        4077742.41                 I    =           51.80139
     XDOT =       6608.801202                 Wp   =           57.92173
     YDOT =         21.818024  meter/sec      RA   =          152.67711  deg
     ZDOT =      -3879.677691                 TA   =           72.23478
                                              MA   =           72.13280
                                              Ha   =            225.191  n.mi
                                              Hp   =            220.260
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7929390.47                 X    =         2451239.01
     Y    =      -15945901.05  feet           Y    =        -4833091.33  meter
     Z    =       13378419.99                 Z    =         4089567.04
     XDOT =      21682.418643                 XDOT =        6626.912587
     YDOT =         71.581445  feet/sec       YDOT =          95.823098  meter/sec
     ZDOT =     -12728.601349                 ZDOT =       -3847.528537
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3303293.40                 X    =         1006843.83
     Y    =       17460365.96  feet           Y    =         5321919.54  meter
     Z    =       13429556.52                 Z    =         4093328.83
     XDOT =     -16169.647567                 XDOT =       -4928.508578
     YDOT =      12772.440589  feet/sec       YDOT =        3893.039891  meter/sec
     ZDOT =     -12591.632352                 ZDOT =       -3837.929541
  
  
    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   14302.54123778  .00016717  00000-0  10270-3 0  9059
    2 25544  51.6444 153.5833 0003596 317.8471  42.2404 15.51108503 32176
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14302.54123778   =   yrday.fracday
    Element set:     905
    Inclination:       51.6444  deg
    RA of node:       153.5833  deg
    Eccentricity:     .0003596     
    Arg of perigee:   317.8471  deg
    Mean anomaly:      42.2404  deg
    Mean motion:   15.51108503  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3217
    Checksum:              289
 
 
    Coasting Arc #7 (Orbit 3231)
    ---------------------------------------
 
    Vector Time (GMT): 2014/303/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2732240.91                 A    =         6792548.87  meter
     Y    =        5071808.62  meter          E    =           .0003682
     Z    =       -3599540.07                 I    =           51.83269
     XDOT =      -6231.116907                 Wp   =           58.41877
     YDOT =       -201.943556  meter/sec      RA   =          147.72521  deg
     ZDOT =       4450.434311                 TA   =          259.20636
                                              MA   =          259.24781
                                              Ha   =            225.250  n.mi
                                              Hp   =            220.128
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8964044.97                 X    =        -2771266.33
     Y    =       16639792.06  feet           Y    =         5041036.61  meter
     Z    =      -11809514.68                 Z    =        -3612908.05
     XDOT =     -20443.296938                 XDOT =       -6250.014689
     YDOT =       -662.544476  feet/sec       YDOT =        -271.729461  meter/sec
     ZDOT =      14601.162439                 ZDOT =        4420.118115
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3205179.61                 X    =         -976938.75
     Y    =      -18590216.23  feet           Y    =        -5666297.91  meter
     Z    =      -11867270.25                 Z    =        -3617143.97
     XDOT =      15255.234398                 XDOT =        4649.795445
     YDOT =     -11857.660130  feet/sec       YDOT =       -3614.214808  meter/sec
     ZDOT =      14472.014812                 ZDOT =        4411.070115
  
  
    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   14303.50765858  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6431 148.7863 0003496 320.6277  39.4620 15.51124306 32320
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14303.50765858   =   yrday.fracday
    Element set:     906
    Inclination:       51.6431  deg
    RA of node:       148.7863  deg
    Eccentricity:     .0003496     
    Arg of perigee:   320.6277  deg
    Mean anomaly:      39.4620  deg
    Mean motion:   15.51124306  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3232
    Checksum:              302
 
 
    Coasting Arc #8 (Orbit 3247)
    ---------------------------------------
 
    Vector Time (GMT): 2014/304/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3025998.10                 A    =         6793920.97  meter
     Y    =       -5276034.45  meter          E    =           .0010914
     Z    =        3019805.49                 I    =           51.86457
     XDOT =       5814.632417                 Wp   =           82.00765
     YDOT =        481.510795  meter/sec      RA   =          142.77794  deg
     ZDOT =      -4968.454853                 TA   =           63.56354
                                              MA   =           63.45160
                                              Ha   =            225.204  n.mi
                                              Hp   =            219.988
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9927815.29                 X    =         3070101.62
     Y    =      -17309824.30  feet           Y    =        -5241949.03  meter
     Z    =        9907498.33                 Z    =         3034612.93
     XDOT =      19076.878009                 XDOT =        5832.951347
     YDOT =       1579.759827  feet/sec       YDOT =         546.635969  meter/sec
     ZDOT =     -16300.704898                 ZDOT =       -4940.163370
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3185614.71                 X    =          970975.36
     Y    =       19666532.57  feet           Y    =         5994359.13  meter
     Z    =        9971429.82                 Z    =         3039291.81
     XDOT =     -14486.644874                 XDOT =       -4415.529358
     YDOT =      10578.168832  feet/sec       YDOT =        3224.225860  meter/sec
     ZDOT =     -16180.215480                 ZDOT =       -4931.729678
  
  
    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   14304.53847152  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6436 143.6707 0003742 324.2765  35.8135 15.51211718 32484
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14304.53847152   =   yrday.fracday
    Element set:     907
    Inclination:       51.6436  deg
    RA of node:       143.6707  deg
    Eccentricity:     .0003742     
    Arg of perigee:   324.2765  deg
    Mean anomaly:      35.8135  deg
    Mean motion:   15.51211718  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3248
    Checksum:              299
 
 
    Coasting Arc #9 (Orbit 3262)
    ---------------------------------------
 
    Vector Time (GMT): 2014/305/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3239228.85                 A    =         6795330.09  meter
     Y    =        5468205.85  meter          E    =           .0007082
     Z    =       -2394999.51                 I    =           51.89224
     XDOT =      -5381.379705                 Wp   =           17.93722
     YDOT =       -831.162485  meter/sec      RA   =          137.83234  deg
     ZDOT =       5391.400474                 TA   =          315.43786
                                              MA   =          315.49478
                                              Ha   =            225.258  n.mi
                                              Hp   =            219.871
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10627391.23                 X    =        -3288500.56
     Y    =       17940307.92  feet           Y    =         5431707.05  meter
     Z    =       -7857609.94                 Z    =        -2410855.47
     XDOT =     -17655.445228                 XDOT =       -5397.875529
     YDOT =      -2726.911040  feet/sec       YDOT =        -891.432443  meter/sec
     ZDOT =      17688.321766                 ZDOT =        5365.218137
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3380840.21                 X    =        -1030480.10
     Y    =      -20549593.01  feet           Y    =        -6263515.95  meter
     Z    =       -7926050.29                 Z    =        -2415860.13
     XDOT =      13884.947023                 XDOT =        4232.131853
     YDOT =      -9050.285193  feet/sec       YDOT =       -2758.526927  meter/sec
     ZDOT =      17576.865871                 ZDOT =        5357.428718
  
  
    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   14305.50482977  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6422 138.8733 0003546 327.3182  32.7749 15.51219182 32630
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14305.50482977   =   yrday.fracday
    Element set:     908
    Inclination:       51.6422  deg
    RA of node:       138.8733  deg
    Eccentricity:     .0003546     
    Arg of perigee:   327.3182  deg
    Mean anomaly:      32.7749  deg
    Mean motion:   15.51219182  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3263
    Checksum:              314
 
 
    Coasting Arc #10 (Orbit 3278)
    ---------------------------------------
 
    Vector Time (GMT): 2014/306/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3425055.42                 A    =         6796291.20  meter
     Y    =       -5619999.36  meter          E    =           .0011033
     Z    =        1679063.13                 I    =           51.91914
     XDOT =       4928.981987                 Wp   =          104.26224
     YDOT =       1284.934126  meter/sec      RA   =          132.89109  deg
     ZDOT =      -5724.824225                 TA   =           57.43420
                                              MA   =           57.32770
                                              Ha   =            225.241  n.mi
                                              Hp   =            219.669
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11237058.47                 X    =         3479488.52
     Y    =      -18438318.11  feet           Y    =        -5581393.69  meter
     Z    =        5508737.31                 Z    =         1695834.47
     XDOT =      16171.200745                 XDOT =        4942.057017
     YDOT =       4215.663142  feet/sec       YDOT =        1340.125868  meter/sec
     ZDOT =     -18782.231708                 ZDOT =       -5700.847888
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3587371.32                 X    =         1093430.78
     Y    =       21273720.36  feet           Y    =         6484229.97  meter
     Z    =        5581114.01                 Z    =         1701123.55
     XDOT =     -13526.279845                 XDOT =       -4122.810097
     YDOT =       7206.119159  feet/sec       YDOT =        2196.425120  meter/sec
     ZDOT =     -18680.243001                 ZDOT =       -5693.738067
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14306.53557509  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6424 133.7571 0003836 331.5381  28.5560 15.51317527 32799
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14306.53557509   =   yrday.fracday
    Element set:     909
    Inclination:       51.6424  deg
    RA of node:       133.7571  deg
    Eccentricity:     .0003836     
    Arg of perigee:   331.5381  deg
    Mean anomaly:      28.5560  deg
    Mean motion:   15.51317527  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3279
    Checksum:              312
 
 
    Coasting Arc #11 (Orbit 3293)
    ---------------------------------------
 
    Vector Time (GMT): 2014/307/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3529249.34                 A    =         6797120.30  meter
     Y    =        5724256.71  meter          E    =           .0011844
     Z    =        -941782.20                 I    =           51.94125
     XDOT =      -4495.734414                 Wp   =           23.42882
     YDOT =      -1800.171977  meter/sec      RA   =          127.95062  deg
     ZDOT =       5941.904402                 TA   =          326.42587
                                              MA   =          326.50087
                                              Ha   =            225.299  n.mi
                                              Hp   =            219.572
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11578902.04                 X    =        -3588422.04
     Y    =       18780369.78  feet           Y    =         5684459.43  meter
     Z    =       -3089836.63                 Z    =         -959071.31
     XDOT =     -14749.784824                 XDOT =       -4504.134769
     YDOT =      -5906.076041  feet/sec       YDOT =       -1850.492700  meter/sec
     ZDOT =      19494.437013                 ZDOT =        5920.044066
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3915035.05                 X    =        -1193302.68
     Y    =      -21702053.20  feet           Y    =        -6614785.82  meter
     Z    =       -3164449.31                 Z    =         -964524.15
     XDOT =      13436.253131                 XDOT =        4095.369954
     YDOT =      -5236.002585  feet/sec       YDOT =       -1595.933588  meter/sec
     ZDOT =      19401.545940                 ZDOT =        5913.591203
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14307.50186969  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6411 128.9591 0003571 334.9928  25.1050 15.51316903 32944
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14307.50186969   =   yrday.fracday
    Element set:     910
    Inclination:       51.6411  deg
    RA of node:       128.9591  deg
    Eccentricity:     .0003571     
    Arg of perigee:   334.9928  deg
    Mean anomaly:      25.1050  deg
    Mean motion:   15.51316903  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3294
    Checksum:              305
 
 
    Coasting Arc #12 (Orbit 3309)
    ---------------------------------------
 
    Vector Time (GMT): 2014/308/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3611207.95                 A    =         6797197.03  meter
     Y    =       -5752915.56  meter          E    =           .0009109
     Z    =         135769.72                 I    =           51.96099
     XDOT =       4066.585614                 Wp   =          122.12227
     YDOT =       2403.444205  meter/sec      RA   =          123.01329  deg
     ZDOT =      -6032.199839                 TA   =           56.42374
                                              MA   =           56.33680
                                              Ha   =            225.297  n.mi
                                              Hp   =            219.314
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11847795.12                 X    =         3674610.45
     Y    =      -18874394.88  feet           Y    =        -5712178.18  meter
     Z    =         445438.73                 Z    =          153467.28
     XDOT =      13341.816320                 XDOT =        4068.710686
     YDOT =       7885.315632  feet/sec       YDOT =        2448.930860  meter/sec
     ZDOT =     -19790.681886                 ZDOT =       -6012.439480
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4142385.45                 X    =         1262599.08
     Y    =       21894743.71  feet           Y    =         6673517.88  meter
     Z    =         521811.73                 Z    =          159048.22
     XDOT =     -13639.097554                 XDOT =       -4157.196934
     YDOT =       3069.534350  feet/sec       YDOT =         935.594070  meter/sec
     ZDOT =     -19706.838479                 ZDOT =       -6006.644368
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14308.53254645  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6411 123.8421 0003862 340.0056  20.0944 15.51421219 33105
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14308.53254645   =   yrday.fracday
    Element set:     911
    Inclination:       51.6411  deg
    RA of node:       123.8421  deg
    Eccentricity:     .0003862     
    Arg of perigee:   340.0056  deg
    Mean anomaly:      20.0944  deg
    Mean motion:   15.51421219  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3310
    Checksum:              258
 
 
    Coasting Arc #13 (Orbit 3325)
    ---------------------------------------
 
    Vector Time (GMT): 2014/309/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3625506.26                 A    =         6797033.20  meter
     Y    =        5701264.78  meter          E    =           .0014814
     Z    =         659425.21                 I    =           51.97624
     XDOT =      -3687.321166                 Wp   =           39.05575
     YDOT =      -3045.187385  meter/sec      RA   =          118.07579  deg
     ZDOT =       5993.452806                 TA   =          328.02747
                                              MA   =          328.11728
                                              Ha   =            225.350  n.mi
                                              Hp   =            219.223
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11894705.59                 X    =        -3692193.03
     Y    =       18704936.93  feet           Y    =         5660349.18  meter
     Z    =        2163468.54                 Z    =          641650.25
     XDOT =     -12097.510387                 XDOT =       -3682.110167
     YDOT =      -9990.772260  feet/sec       YDOT =       -3086.391934  meter/sec
     ZDOT =      19663.559074                 ZDOT =        5975.552667
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4355514.76                 X    =        -1327560.90
     Y    =      -21741992.06  feet           Y    =        -6626959.18  meter
     Z    =        2086757.12                 Z    =          636043.57
     XDOT =      14149.022872                 XDOT =        4312.622171
     YDOT =       -934.249630  feet/sec       YDOT =        -284.759287  meter/sec
     ZDOT =      19587.751834                 ZDOT =        5970.346759
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14309.56319006  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6406 118.7238 0003583 343.5953  16.5081 15.51425006 33269
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14309.56319006   =   yrday.fracday
    Element set:     912
    Inclination:       51.6406  deg
    RA of node:       118.7238  deg
    Eccentricity:     .0003583     
    Arg of perigee:   343.5953  deg
    Mean anomaly:      16.5081  deg
    Mean motion:   15.51425006  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3326
    Checksum:              290
 
 
    Coasting Arc #14 (Orbit 3340)
    ---------------------------------------
 
    Vector Time (GMT): 2014/310/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3634434.55                 A    =         6796027.02  meter
     Y    =       -5545134.49  meter          E    =           .0005241
     Z    =       -1487891.12                 I    =           51.98803
     XDOT =       3332.151887                 Wp   =          123.57863
     YDOT =       3735.032574  meter/sec      RA   =          113.13950  deg
     ZDOT =      -5797.996529                 TA   =           72.55761
                                              MA   =           72.50032
                                              Ha   =            225.348  n.mi
                                              Hp   =            218.974
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11923997.88                 X    =         3703399.31
     Y    =      -18192698.45  feet           Y    =        -5504106.34  meter
     Z    =       -4881532.54                 Z    =        -1470067.34
     XDOT =      10932.256848                 XDOT =        3318.303826
     YDOT =      12254.043879  feet/sec       YDOT =        3772.217219  meter/sec
     ZDOT =     -19022.298325                 ZDOT =       -5781.842722
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4335168.54                 X    =         1321359.37
     Y    =       21333244.00  feet           Y    =         6502372.77  meter
     Z    =       -4804620.34                 Z    =        -1464448.28
     XDOT =     -14919.904134                 XDOT =       -4547.586780
     YDOT =      -1223.755923  feet/sec       YDOT =        -373.000805  meter/sec
     ZDOT =     -18954.053967                 ZDOT =       -5777.195649
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14310.52938306  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6409 113.9260 0003828 348.8289  11.2777 15.51514636 33415
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14310.52938306   =   yrday.fracday
    Element set:     913
    Inclination:       51.6409  deg
    RA of node:       113.9260  deg
    Eccentricity:     .0003828     
    Arg of perigee:   348.8289  deg
    Mean anomaly:      11.2777  deg
    Mean motion:   15.51514636  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3341
    Checksum:              305
 
 
    Coasting Arc #15 (Orbit 3356)
    ---------------------------------------
 
    Vector Time (GMT): 2014/311/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 946559.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3602472.43                 A    =         6794736.59  meter
     Y    =        5285594.52  meter          E    =           .0014894
     Z    =        2266629.10                 I    =           51.99568
     XDOT =      -3043.957037                 Wp   =           57.93220
     YDOT =      -4428.705548  meter/sec      RA   =          108.20198  deg
     ZDOT =       5470.932432                 TA   =          327.14774
                                              MA   =          327.24024
                                              Ha   =            225.389  n.mi
                                              Hp   =            218.851
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11819135.26                 X    =        -3672320.29
     Y    =       17341189.36  feet           Y    =         5244918.83  meter
     Z    =        7436447.18                 Z    =         2248958.57
     XDOT =      -9986.735687                 XDOT =       -3020.784753
     YDOT =     -14529.873844  feet/sec       YDOT =       -4462.615398  meter/sec
     ZDOT =      17949.253386                 ZDOT =        5456.201264
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4153283.07                 X    =        -1265920.68
     Y    =      -20598229.51  feet           Y    =        -6278340.36  meter
     Z    =        7360212.91                 Z    =         2243392.90
     XDOT =      15953.667449                 XDOT =        4862.677838
     YDOT =       3196.659126  feet/sec       YDOT =         974.341702  meter/sec
     ZDOT =      17887.196721                 ZDOT =        5452.017560
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   14311.55995508  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6412 108.8078 0003623 351.6919   8.4172 15.51541188 33570
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14311.55995508   =   yrday.fracday
    Element set:     914
    Inclination:       51.6412  deg
    RA of node:       108.8078  deg
    Eccentricity:     .0003623     
    Arg of perigee:   351.6919  deg
    Mean anomaly:       8.4172  deg
    Mean motion:   15.51541188  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3357
    Checksum:              312
 
             

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