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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  9687.52
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   126.0
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.637
   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 
   ------------------------------------------------------------------------
   186/07:13:02.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.6  
   000/00:00:00.000           0.0               0.0              211.5  
   
   191/02:58:39.135           3.2               3.9              3.9    
   N/A                       -2.1              -0.4              219.4  
   000/00:11:54.271           0.5              -0.0              214.0  
   
 
 
    Coasting Arc #1 (Orbit 3029)
    ---------------------------------------
 
    Vector Time (GMT): 2015/182/16:01:04.389
    Vector Time (MET): N/A
    Weight (LBS)     : 877726.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3937404.35                 A    =         6778865.76  meter
     Y    =        3906509.90  meter          E    =           .0013981
     Z    =        3888095.72                 I    =           51.71681
     XDOT =      -6139.348189                 Wp   =          103.09233
     YDOT =       2088.055933  meter/sec      RA   =           11.18203  deg
     ZDOT =       4103.760262                 TA   =          303.89993
                                              MA   =          304.03282
                                              Ha   =            219.797  n.mi
                                              Hp   =            211.541
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12917993.26                 X    =         3874541.39
     Y    =       12816633.52  feet           Y    =         3950188.47  meter
     Z    =       12756219.55                 Z    =         3907070.64
     XDOT =     -20142.218468                 XDOT =       -6182.175444
     YDOT =       6850.577207  feet/sec       YDOT =        2019.161656  meter/sec
     ZDOT =      13463.780388                 ZDOT =        4073.832967
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7337975.24                 X    =        -2236614.85
     Y    =      -16589981.59  feet           Y    =        -5056626.39  meter
     Z    =       12836993.89                 Z    =         3912715.74
     XDOT =      20126.938889                 XDOT =        6134.690973
     YDOT =       1454.751188  feet/sec       YDOT =         443.408162  meter/sec
     ZDOT =      13334.625670                 ZDOT =        4064.393904
  
  
    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   15182.72319628  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6434  11.4347 0002972 119.2870 240.8581 15.55490380 30307
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15182.72319628   =   yrday.fracday
    Element set:     900
    Inclination:       51.6434  deg
    RA of node:        11.4347  deg
    Eccentricity:     .0002972     
    Arg of perigee:   119.2870  deg
    Mean anomaly:     240.8581  deg
    Mean motion:   15.55490380  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3030
    Checksum:              293
 
 
    Coasting Arc #2 (Orbit 3044)
    ---------------------------------------
 
    Vector Time (GMT): 2015/183/16:01:04.389
    Vector Time (MET): N/A
    Weight (LBS)     : 877726.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1817689.99                 A    =         6774699.86  meter
     Y    =       -4187867.13  meter          E    =           .0015092
     Z    =       -5018948.50                 I    =           51.67148
     XDOT =       7350.134485                 Wp   =           82.72833
     YDOT =       -795.468742  meter/sec      RA   =            6.18170  deg
     ZDOT =      -2001.515671                 TA   =          167.83168
                                              MA   =          167.79518
                                              Ha   =            219.843  n.mi
                                              Hp   =            211.558
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5963549.83                 X    =        -1746345.25
     Y    =      -13739721.55  feet           Y    =        -4207794.12  meter
     Z    =      -16466366.47                 Z    =        -5027605.69
     XDOT =      24114.614451                 XDOT =        7368.205840
     YDOT =      -2609.805585  feet/sec       YDOT =        -713.173405  meter/sec
     ZDOT =      -6566.652465                 ZDOT =       -1965.766732
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         754542.74                 X    =          229984.63
     Y    =       14918995.51  feet           Y    =         4547309.83  meter
     Z    =      -16502706.99                 Z    =        -5030025.09
     XDOT =     -22484.085245                 XDOT =       -6853.149183
     YDOT =      -5944.374943  feet/sec       YDOT =       -1811.845483  meter/sec
     ZDOT =      -6412.736377                 ZDOT =       -1954.602048
  
  
    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   15183.68689498  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6436   6.6211 0002886 120.2333 239.9106 15.55475606 30457
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15183.68689498   =   yrday.fracday
    Element set:     901
    Inclination:       51.6436  deg
    RA of node:         6.6211  deg
    Eccentricity:     .0002886     
    Arg of perigee:   120.2333  deg
    Mean anomaly:     239.9106  deg
    Mean motion:   15.55475606  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3045
    Checksum:              315
 
 
    Coasting Arc #3 (Orbit 3060)
    ---------------------------------------
 
    Vector Time (GMT): 2015/184/16:01:04.389
    Vector Time (MET): N/A
    Weight (LBS)     : 877726.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -554856.11                 A    =         6773379.28  meter
     Y    =        4181255.94  meter          E    =           .0004977
     Z    =        5295496.22                 I    =           51.63630
     XDOT =      -7648.252048                 Wp   =           96.18651
     YDOT =       -486.473742  meter/sec      RA   =            1.16825  deg
     ZDOT =       -417.449984                 TA   =          357.79007
                                              MA   =          357.79227
                                              Ha   =            219.773  n.mi
                                              Hp   =            211.590
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1820394.06                 X    =         -627293.86
     Y    =       13718031.31  feet           Y    =         4174645.49  meter
     Z    =       17373675.26                 Z    =         5292625.45
     XDOT =     -25092.690447                 XDOT =       -7640.215962
     YDOT =      -1596.042462  feet/sec       YDOT =        -571.956520  meter/sec
     ZDOT =      -1369.586562                 ZDOT =        -454.583742
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6337669.26                 X    =         1931721.59
     Y    =      -12320383.80  feet           Y    =        -3755252.98  meter
     Z    =       17360440.69                 Z    =         5291462.32
     XDOT =      22263.172078                 XDOT =        6785.814849
     YDOT =       9298.415486  feet/sec       YDOT =        2834.157040  meter/sec
     ZDOT =      -1529.183634                 ZDOT =        -466.095172
  
  
    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   15184.71482728  .00016717  00000-0  10270-3 0  9027
    2 25544  51.6442   1.4856 0002834 122.2815 237.8613 15.55514997 30617
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15184.71482728   =   yrday.fracday
    Element set:     902
    Inclination:       51.6442  deg
    RA of node:         1.4856  deg
    Eccentricity:     .0002834     
    Arg of perigee:   122.2815  deg
    Mean anomaly:     237.8613  deg
    Mean motion:   15.55514997  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3061
    Checksum:              308
 
 
    Coasting Arc #4 (Orbit 3075)
    ---------------------------------------
 
    Vector Time (GMT): 2015/185/16:01:04.389
    Vector Time (MET): N/A
    Weight (LBS)     : 877726.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2874488.76                 A    =         6775904.01  meter
     Y    =       -3939079.50  meter          E    =           .0013537
     Z    =       -4717808.70                 I    =           51.61323
     XDOT =       6926.081217                 Wp   =          112.32215
     YDOT =       1735.690030  meter/sec      RA   =          356.15607  deg
     ZDOT =       2772.106614                 TA   =          185.16940
                                              MA   =          185.18339
                                              Ha   =            219.718  n.mi
                                              Hp   =            211.656
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9430737.42                 X    =         2941239.85
     Y    =      -12923489.18  feet           Y    =        -3906561.36  meter
     Z    =      -15478374.99                 Z    =        -4703683.49
     XDOT =      22723.363572                 XDOT =        6892.691909
     YDOT =       5694.521095  feet/sec       YDOT =        1812.955022  meter/sec
     ZDOT =       9094.837972                 ZDOT =        2805.670743
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13093257.74                 X    =        -3990824.96
     Y    =        9296478.56  feet           Y    =         2833566.67  meter
     Z    =      -15416794.78                 Z    =        -4699039.05
     XDOT =     -19069.005031                 XDOT =       -5812.232734
     YDOT =     -11543.165937  feet/sec       YDOT =       -3518.356978  meter/sec
     ZDOT =       9238.815491                 ZDOT =        2815.990962
  
  
    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   15185.67850351  .00016717  00000-0  10270-3 0  9035
    2 25544  51.6445 356.6724 0002860 125.9246 234.2174 15.55529936 30764
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15185.67850351   =   yrday.fracday
    Element set:     903
    Inclination:       51.6445  deg
    RA of node:       356.6724  deg
    Eccentricity:     .0002860     
    Arg of perigee:   125.9246  deg
    Mean anomaly:     234.2174  deg
    Mean motion:   15.55529936  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3076
    Checksum:              323
 
 
    Coasting Arc #5 (Orbit 3085)
    ---------------------------------------
 
    Vector Time (GMT): 2015/186/07:13:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3167792.99                 A    =         6775092.96  meter
     Y    =       -3502987.91  meter          E    =           .0013839
     Z    =       -4870304.68                 I    =           51.59156
     XDOT =       6733.275820                 Wp   =           79.45165
     YDOT =      -2745.917423  meter/sec      RA   =          353.03392  deg
     ZDOT =      -2407.859683                 TA   =          166.91607
                                              MA   =          166.88013
                                              Ha   =            219.594  n.mi
                                              Hp   =            211.545
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10393021.61                 X    =        -3104728.55
     Y    =      -11492742.49  feet           Y    =        -3538059.18  meter
     Z    =      -15978689.89                 Z    =        -4885540.12
     XDOT =      22090.799934                 XDOT =        6775.177197
     YDOT =      -9008.915429  feet/sec       YDOT =       -2670.387014  meter/sec
     ZDOT =      -7899.802110                 ZDOT =       -2375.049718
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14691821.22                 X    =        -4478067.11
     Y    =       -4708929.38  feet           Y    =        -1435281.67  meter
     Z    =      -16043470.08                 Z    =        -4890049.68
     XDOT =      14197.423119                 XDOT =        4327.374567
     YDOT =     -17900.935520  feet/sec       YDOT =       -5456.205146  meter/sec
     ZDOT =      -7758.124192                 ZDOT =       -2364.676254
  
  
    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   15186.32094749  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6452 353.4661 0002431 116.9398 243.2004 15.55541613 30868
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15186.32094749   =   yrday.fracday
    Element set:     904
    Inclination:       51.6452  deg
    RA of node:       353.4661  deg
    Eccentricity:     .0002431     
    Arg of perigee:   116.9398  deg
    Mean anomaly:     243.2004  deg
    Mean motion:   15.55541613  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3086
    Checksum:              302
 
 
    Coasting Arc #6 (Orbit 3101)
    ---------------------------------------
 
    Vector Time (GMT): 2015/187/07:13:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         879523.88                 A    =         6773184.22  meter
     Y    =        4116604.58  meter          E    =           .0004635
     Z    =        5302340.24                 I    =           51.55407
     XDOT =      -7506.834754                 Wp   =          104.17993
     YDOT =       1596.915081  meter/sec      RA   =          348.01592  deg
     ZDOT =          4.272816                 TA   =          345.77282
                                              MA   =          345.78587
                                              Ha   =            219.526  n.mi
                                              Hp   =            211.645
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2885577.03                 X    =          807669.22
     Y    =       13505920.55  feet           Y    =         4126037.84  meter
     Z    =       17396129.39                 Z    =         5306438.52
     XDOT =     -24628.722945                 XDOT =       -7524.154674
     YDOT =       5239.222708  feet/sec       YDOT =        1512.871895  meter/sec
     ZDOT =         14.018424                 ZDOT =         -32.235384
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9401620.36                 X    =         2865613.89
     Y    =       10087746.28  feet           Y    =         3074745.07  meter
     Z    =       17412888.10                 Z    =         5307448.29
     XDOT =     -17563.642059                 XDOT =       -5353.398100
     YDOT =      16610.101034  feet/sec       YDOT =        5062.758795  meter/sec
     ZDOT =       -143.311977                 ZDOT =         -43.681491
  
  
    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   15187.34884922  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6455 348.3312 0002434 121.3005 238.8387 15.55557572 31029
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15187.34884922   =   yrday.fracday
    Element set:     905
    Inclination:       51.6455  deg
    RA of node:       348.3312  deg
    Eccentricity:     .0002434     
    Arg of perigee:   121.3005  deg
    Mean anomaly:     238.8387  deg
    Mean motion:   15.55557572  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3102
    Checksum:              307
 
 
    Coasting Arc #7 (Orbit 3116)
    ---------------------------------------
 
    Vector Time (GMT): 2015/188/07:13:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1472719.80                 A    =         6775144.13  meter
     Y    =       -4493267.27  meter          E    =           .0013970
     Z    =       -4865416.44                 I    =           51.52904
     XDOT =       7268.176655                 Wp   =          109.81137
     YDOT =       -222.883878  meter/sec      RA   =          342.99476  deg
     ZDOT =       2406.852734                 TA   =          183.84600
                                              MA   =          183.85675
                                              Ha   =            219.467  n.mi
                                              Hp   =            211.712
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4831757.86                 X    =         1546489.25
     Y    =      -14741690.50  feet           Y    =        -4476385.57  meter
     Z    =      -15962652.35                 Z    =        -4858083.43
     XDOT =      23845.723935                 XDOT =        7258.437345
     YDOT =       -731.246320  feet/sec       YDOT =        -141.660971  meter/sec
     ZDOT =       7896.498472                 ZDOT =        2442.136088
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3724196.28                 X    =        -1135135.03
     Y    =      -15094016.03  feet           Y    =        -4600656.09  meter
     Z    =      -15930180.01                 Z    =        -4855518.87
     XDOT =      18607.733017                 XDOT =        5671.637024
     YDOT =     -13081.784007  feet/sec       YDOT =       -3987.327765  meter/sec
     ZDOT =       8048.264133                 ZDOT =        2453.110908
  
  
    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   15188.31249631  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6448 343.5163 0002289 124.1651 235.9719 15.55573532 31175
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15188.31249631   =   yrday.fracday
    Element set:     906
    Inclination:       51.6448  deg
    RA of node:       343.5163  deg
    Eccentricity:     .0002289     
    Arg of perigee:   124.1651  deg
    Mean anomaly:     235.9719  deg
    Mean motion:   15.55573532  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3117
    Checksum:              314
 
 
    Coasting Arc #8 (Orbit 3132)
    ---------------------------------------
 
    Vector Time (GMT): 2015/189/07:13:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3567583.75                 A    =         6779625.29  meter
     Y    =        4510615.15  meter          E    =           .0013866
     Z    =        3577737.28                 I    =           51.51445
     XDOT =      -6127.100426                 Wp   =           92.32795
     YDOT =      -1321.252070  meter/sec      RA   =          337.98462  deg
     ZDOT =      -4429.660182                 TA   =           45.23090
                                              MA   =           45.11818
                                              Ha   =            219.395  n.mi
                                              Hp   =            211.681
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11704671.08                 X    =        -3635136.56
     Y    =       14798606.13  feet           Y    =         4470342.16  meter
     Z    =       11737983.22                 Z    =         3560242.97
     XDOT =     -20102.035519                 XDOT =       -6090.353008
     YDOT =      -4334.816503  feet/sec       YDOT =       -1389.563583  meter/sec
     ZDOT =     -14533.005848                 ZDOT =       -4459.335072
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1704416.98                 X    =         -519506.30
     Y    =       18838131.96  feet           Y    =         5741862.62  meter
     Z    =       11661820.85                 Z    =         3554523.00
     XDOT =     -17724.697103                 XDOT =       -5402.487677
     YDOT =       7501.067849  feet/sec       YDOT =        2286.325480  meter/sec
     ZDOT =     -14660.325334                 ZDOT =       -4468.467162
  
  
    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   15189.34037417  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6450 338.3814 0002147 125.0223 235.1133 15.55619948 31333
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15189.34037417   =   yrday.fracday
    Element set:     907
    Inclination:       51.6450  deg
    RA of node:       338.3814  deg
    Eccentricity:     .0002147     
    Arg of perigee:   125.0223  deg
    Mean anomaly:     235.1133  deg
    Mean motion:   15.55619948  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3133
    Checksum:              294
 
 
    Coasting Arc #9 (Orbit 3147)
    ---------------------------------------
 
    Vector Time (GMT): 2015/190/07:13:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 892160.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5103364.76                 A    =         6783893.54  meter
     Y    =       -4127288.96  meter          E    =           .0007946
     Z    =       -1708605.44                 I    =           51.49803
     XDOT =       4247.060230                 Wp   =           52.90655
     YDOT =       2908.608172  meter/sec      RA   =          332.98768  deg
     ZDOT =       5682.324235                 TA   =          288.31478
                                              MA   =          288.40121
                                              Ha   =            219.367  n.mi
                                              Hp   =            211.788
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16743322.70                 X    =         5157437.53
     Y    =      -13540974.26  feet           Y    =        -4069917.33  meter
     Z    =       -5605660.88                 Z    =        -1683683.33
     XDOT =      13933.924640                 XDOT =        4186.617328
     YDOT =       9542.677730  feet/sec       YDOT =        2955.763226  meter/sec
     ZDOT =      18642.796045                 ZDOT =        5702.808949
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6218230.06                 X    =         1895316.52
     Y    =      -20645332.44  feet           Y    =        -6292697.33  meter
     Z    =       -5497648.26                 Z    =        -1675683.19
     XDOT =      15285.582330                 XDOT =        4659.045494
     YDOT =       -363.326489  feet/sec       YDOT =        -110.741914  meter/sec
     ZDOT =      18730.265784                 ZDOT =        5708.985011
  
  
    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   15190.30400019  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6437 333.5662 0002107 130.3782 229.7555 15.55587411 31483
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15190.30400019   =   yrday.fracday
    Element set:     908
    Inclination:       51.6437  deg
    RA of node:       333.5662  deg
    Eccentricity:     .0002107     
    Arg of perigee:   130.3782  deg
    Mean anomaly:     229.7555  deg
    Mean motion:   15.55587411  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3148
    Checksum:              295
 
 
    Coasting Arc #10 (Orbit 3160)
    ---------------------------------------
 
    Vector Time (GMT): 2015/191/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         837473.52                 A    =         6777986.90  meter
     Y    =       -4852743.06  meter          E    =           .0009773
     Z    =       -4666955.13                 I    =           51.44874
     XDOT =       6941.627969                 Wp   =          118.36489
     YDOT =      -1543.356059  meter/sec      RA   =          328.83650  deg
     ZDOT =       2850.462139                 TA   =          180.04378
                                              MA   =          180.04387
                                              Ha   =            219.407  n.mi
                                              Hp   =            214.002
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2747616.55                 X    =          914346.08
     Y    =      -15921073.04  feet           Y    =        -4842947.68  meter
     Z    =      -15311532.59                 Z    =        -4662700.55
     XDOT =      22774.369978                 XDOT =        6944.523787
     YDOT =      -5063.504132  feet/sec       YDOT =       -1465.714273  meter/sec
     ZDOT =       9351.909905                 ZDOT =        2884.190048
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9754497.01                 X    =         2973170.69
     Y    =      -12902341.18  feet           Y    =        -3932633.59  meter
     Z    =      -15292232.46                 Z    =        -4661072.45
     XDOT =      21600.267389                 XDOT =        6583.761500
     YDOT =       5073.974624  feet/sec       YDOT =        1546.547465  meter/sec
     ZDOT =       9497.240552                 ZDOT =        2894.758920
  
  
    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   15191.13913636  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6444 329.3927 0001787 229.4285 130.6713 15.54864409 31614
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15191.13913636   =   yrday.fracday
    Element set:     909
    Inclination:       51.6444  deg
    RA of node:       329.3927  deg
    Eccentricity:     .0001787     
    Arg of perigee:   229.4285  deg
    Mean anomaly:     130.6713  deg
    Mean motion:   15.54864409  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3161
    Checksum:              323
 
 
    Coasting Arc #11 (Orbit 3176)
    ---------------------------------------
 
    Vector Time (GMT): 2015/192/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2566173.48                 A    =         6782258.76  meter
     Y    =        5256243.11  meter          E    =           .0011089
     Z    =        3422422.22                 I    =           51.43600
     XDOT =      -6157.534159                 Wp   =           95.21657
     YDOT =        -18.379190  meter/sec      RA   =          323.82859  deg
     ZDOT =      -4576.956942                 TA   =           44.55253
                                              MA   =           44.46344
                                              Ha   =            219.407  n.mi
                                              Hp   =            214.019
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8419204.34                 X    =        -2641384.13
     Y    =       17244892.10  feet           Y    =         5227125.61  meter
     Z    =       11228419.35                 Z    =         3409774.12
     XDOT =     -20201.883724                 XDOT =       -6134.637915
     YDOT =        -60.299181  feet/sec       YDOT =         -87.108293  meter/sec
     ZDOT =     -15016.262933                 ZDOT =       -4606.813363
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15185976.51                 X    =        -4628685.64
     Y    =       11785498.06  feet           Y    =         3592219.81  meter
     Z    =       11172952.13                 Z    =         3405515.81
     XDOT =     -17188.599093                 XDOT =       -5239.085004
     YDOT =      -7753.639164  feet/sec       YDOT =       -2363.309217  meter/sec
     ZDOT =     -15144.621019                 ZDOT =       -4616.080487
  
  
    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   15192.16747783  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6441 324.2607 0001757 232.6570 127.4423 15.54867037 31779
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15192.16747783   =   yrday.fracday
    Element set:     910
    Inclination:       51.6441  deg
    RA of node:       324.2607  deg
    Eccentricity:     .0001757     
    Arg of perigee:   232.6570  deg
    Mean anomaly:     127.4423  deg
    Mean motion:   15.54867037  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3177
    Checksum:              312
 
 
    Coasting Arc #12 (Orbit 3191)
    ---------------------------------------
 
    Vector Time (GMT): 2015/193/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3919603.08                 A    =         6785834.38  meter
     Y    =       -5259287.90  meter          E    =           .0006040
     Z    =       -1728750.64                 I    =           51.42402
     XDOT =       4854.702008                 Wp   =           31.23463
     YDOT =       1759.730404  meter/sec      RA   =          318.83120  deg
     ZDOT =       5667.515146                 TA   =          309.73949
                                              MA   =          309.79269
                                              Ha   =            219.256  n.mi
                                              Hp   =            214.019
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12859590.16                 X    =         3986519.97
     Y    =      -17254881.57  feet           Y    =        -5215081.98  meter
     Z    =       -5671754.06                 Z    =        -1709548.12
     XDOT =      15927.500027                 XDOT =        4807.132935
     YDOT =       5773.393714  feet/sec       YDOT =        1813.752245  meter/sec
     ZDOT =      18594.209798                 ZDOT =        5690.982899
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18977589.31                 X    =         5784369.22
     Y    =      -10192787.29  feet           Y    =        -3106761.57  meter
     Z    =       -5588110.78                 Z    =        -1703256.17
     XDOT =      11146.101806                 XDOT =        3397.331830
     YDOT =      10528.793021  feet/sec       YDOT =        3209.176113  meter/sec
     ZDOT =      18694.740668                 ZDOT =        5698.156956
  
  
    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   15193.13153640  .00016717  00000-0  10270-3 0  9111
    2 25544  51.6448 319.4486 0001796 240.3857 119.7117 15.54906097 31925
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15193.13153640   =   yrday.fracday
    Element set:     911
    Inclination:       51.6448  deg
    RA of node:       319.4486  deg
    Eccentricity:     .0001796     
    Arg of perigee:   240.3857  deg
    Mean anomaly:     119.7117  deg
    Mean motion:   15.54906097  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3192
    Checksum:              320
 
 
    Coasting Arc #13 (Orbit 3207)
    ---------------------------------------
 
    Vector Time (GMT): 2015/194/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4826600.33                 A    =         6787108.91  meter
     Y    =        4757313.91  meter          E    =           .0011202
     Z    =        -233100.15                 I    =           51.40511
     XDOT =      -3217.795796                 Wp   =          145.50025
     YDOT =      -3550.759935  meter/sec      RA   =          313.84109  deg
     ZDOT =      -5989.338221                 TA   =           37.02055
                                              MA   =           36.94331
                                              Ha   =            219.215  n.mi
                                              Hp   =            214.080
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15835302.91                 X    =        -4878306.73
     Y    =       15607985.28  feet           Y    =         4703050.63  meter
     Z    =        -764764.27                 Z    =         -256671.67
     XDOT =     -10557.072822                 XDOT =       -3148.757468
     YDOT =     -11649.474854  feet/sec       YDOT =       -3586.356697  meter/sec
     ZDOT =     -19650.059779                 ZDOT =       -6004.802268
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20810174.66                 X    =        -6342941.23
     Y    =        7818931.13  feet           Y    =         2383210.21  meter
     Z    =        -867083.58                 Z    =         -264287.08
     XDOT =      -4219.983154                 XDOT =       -1286.250865
     YDOT =     -13369.674993  feet/sec       YDOT =       -4075.076938  meter/sec
     ZDOT =     -19715.814483                 ZDOT =       -6009.380254
  
  
    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   15194.15985599  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6451 314.3162 0001851 242.9082 117.1882 15.54882514 32080
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15194.15985599   =   yrday.fracday
    Element set:     912
    Inclination:       51.6451  deg
    RA of node:       314.3162  deg
    Eccentricity:     .0001851     
    Arg of perigee:   242.9082  deg
    Mean anomaly:     117.1882  deg
    Mean motion:   15.54882514  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3208
    Checksum:              315
 
 
    Coasting Arc #14 (Orbit 3223)
    ---------------------------------------
 
    Vector Time (GMT): 2015/195/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5221092.93                 A    =         6785038.12  meter
     Y    =       -3758075.43  meter          E    =           .0012169
     Z    =        2139111.60                 I    =           51.37738
     XDOT =       1462.995036                 Wp   =           69.72475
     YDOT =       5164.213355  meter/sec      RA   =          308.84766  deg
     ZDOT =       5480.621350                 TA   =          314.09584
                                              MA   =          314.19592
                                              Ha   =            219.113  n.mi
                                              Hp   =            214.004
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17129569.97                 X    =         5252337.71
     Y    =      -12329643.81  feet           Y    =        -3699515.31  meter
     Z    =        7018082.68                 Z    =         2164549.80
     XDOT =       4799.852479                 XDOT =        1378.516338
     YDOT =      16942.957200  feet/sec       YDOT =        5180.100511  meter/sec
     ZDOT =      17981.041173                 ZDOT =        5487.523651
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20545070.68                 X    =         6262137.54
     Y    =       -4667369.06  feet           Y    =        -1422614.09  meter
     Z    =        7128218.93                 Z    =         2172681.13
     XDOT =      -2653.533735                 XDOT =        -808.797083
     YDOT =      15929.436678  feet/sec       YDOT =        4855.292300  meter/sec
     ZDOT =      18009.661933                 ZDOT =        5489.344957
  
  
    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   15195.18816365  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6452 309.1835 0001737 255.5286 104.5674 15.54916864 32242
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15195.18816365   =   yrday.fracday
    Element set:     913
    Inclination:       51.6452  deg
    RA of node:       309.1835  deg
    Eccentricity:     .0001737     
    Arg of perigee:   255.5286  deg
    Mean anomaly:     104.5674  deg
    Mean motion:   15.54916864  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3224
    Checksum:              326
 
 
    Coasting Arc #15 (Orbit 3238)
    ---------------------------------------
 
    Vector Time (GMT): 2015/196/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5158037.43                 A    =         6780823.83  meter
     Y    =        2268492.93  meter          E    =           .0004165
     Z    =       -3776478.60                 I    =           51.34454
     XDOT =        253.558967                 Wp   =           74.07900
     YDOT =      -6407.337728  meter/sec      RA   =          303.84318  deg
     ZDOT =      -4197.889098                 TA   =          151.39407
                                              MA   =          151.37121
                                              Ha   =            219.000  n.mi
                                              Hp   =            213.989
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16922694.99                 X    =        -5164676.47
     Y    =        7442562.12  feet           Y    =         2210775.69  meter
     Z    =      -12390021.66                 Z    =        -3801550.84
     XDOT =        831.886375                 XDOT =         345.579973
     YDOT =     -21021.449240  feet/sec       YDOT =       -6403.987261  meter/sec
     ZDOT =     -13772.602029                 ZDOT =       -4196.434610
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18404858.00                 X    =        -5609800.72
     Y    =         579830.36  feet           Y    =          176732.29  meter
     Z    =      -12498278.77                 Z    =        -3809475.37
     XDOT =       8780.642860                 XDOT =        2676.339944
     YDOT =     -17800.580853  feet/sec       YDOT =       -5425.617044  meter/sec
     ZDOT =     -13765.050510                 ZDOT =       -4195.587395
  
  
    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   15196.15219128  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6455 304.3721 0001949 260.0555 100.0378 15.54937188 32391
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15196.15219128   =   yrday.fracday
    Element set:     914
    Inclination:       51.6455  deg
    RA of node:       304.3721  deg
    Eccentricity:     .0001949     
    Arg of perigee:   260.0555  deg
    Mean anomaly:     100.0378  deg
    Mean motion:   15.54937188  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3239
    Checksum:              308
 
 
    Coasting Arc #16 (Orbit 3254)
    ---------------------------------------
 
    Vector Time (GMT): 2015/197/03:04:36.271
    Vector Time (MET): N/A
    Weight (LBS)     : 891730.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4692335.68                 A    =         6776744.73  meter
     Y    =        -443177.96  meter          E    =           .0005392
     Z    =        4867141.84                 I    =           51.31412
     XDOT =      -1762.793167                 Wp   =          132.18787
     YDOT =       7089.667669  meter/sec      RA   =          298.82325  deg
     ZDOT =       2339.805523                 TA   =          294.78268
                                              MA   =          294.83877
                                              Ha   =            218.916  n.mi
                                              Hp   =            214.008
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15394802.12                 X    =         4673300.34
     Y    =       -1453995.92  feet           Y    =         -390812.12  meter
     Z    =       15968313.12                 Z    =         4889889.61
     XDOT =      -5783.442149                 XDOT =       -1853.306215
     YDOT =      23260.064531  feet/sec       YDOT =        7069.448629  meter/sec
     ZDOT =       7676.527306                 ZDOT =        2331.023261
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14794248.51                 X    =         4509286.95
     Y    =        4136210.78  feet           Y    =         1260717.05  meter
     Z    =       16066207.75                 Z    =         4896980.12
     XDOT =     -13494.800673                 XDOT =       -4113.215245
     YDOT =      18535.917678  feet/sec       YDOT =        5649.747708  meter/sec
     ZDOT =       7637.345378                 ZDOT =        2327.862871
  
  
    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   15197.18047852  .00016717  00000-0  10270-3 0  9151
    2 25544  51.6455 299.2397 0001767 265.7883  94.3068 15.54952632 32556
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15197.18047852   =   yrday.fracday
    Element set:     915
    Inclination:       51.6455  deg
    RA of node:       299.2397  deg
    Eccentricity:     .0001767     
    Arg of perigee:   265.7883  deg
    Mean anomaly:      94.3068  deg
    Mean motion:   15.54952632  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3255
    Checksum:              351
 
             

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