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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  13454.89
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   104.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   3.055
   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 
   ------------------------------------------------------------------------
   048/10:50:37.748           1.4               2.6              2.7    
   N/A                       -2.1              -0.3              222.3  
   000/00:07:15.497           0.7               0.1              213.2  
   
 
 
    Coasting Arc #1 (Orbit 2433)
    ---------------------------------------
 
    Vector Time (GMT): 2016/036/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4373996.38                 A    =         6781673.48  meter
     Y    =       -3261919.60  meter          E    =           .0013117
     Z    =       -4039130.79                 I    =           51.63627
     XDOT =       5852.437619                 Wp   =           92.93455
     YDOT =       3012.982193  meter/sec      RA   =          359.15701  deg
     ZDOT =       3914.750297                 TA   =          217.70546
                                              MA   =          217.79747
                                              Ha   =            222.957  n.mi
                                              Hp   =            211.913
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14350381.83                 X    =         4429766.89
     Y    =      -10701835.97  feet           Y    =        -3212694.85  meter
     Z    =      -13251741.44                 Z    =        -4017747.94
     XDOT =      19200.910822                 XDOT =        5799.294923
     YDOT =       9885.112182  feet/sec       YDOT =        3078.130891  meter/sec
     ZDOT =      12843.668952                 ZDOT =        3943.050377
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17738558.37                 X    =         5406712.59
     Y    =        2876225.72  feet           Y    =          876673.60  meter
     Z    =      -13158353.83                 Z    =        -4010666.25
     XDOT =       6463.004036                 XDOT =        1969.923630
     YDOT =      19301.049633  feet/sec       YDOT =        5882.959928  meter/sec
     ZDOT =      12965.753878                 ZDOT =        3951.961782
  
  
    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   16036.50874454  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6401 359.6943 0006595  78.3022 281.8870 15.54418818 24347
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16036.50874454   =   yrday.fracday
    Element set:     900
    Inclination:       51.6401  deg
    RA of node:       359.6943  deg
    Eccentricity:     .0006595     
    Arg of perigee:    78.3022  deg
    Mean anomaly:     281.8870  deg
    Mean motion:   15.54418818  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2434
    Checksum:              321
 
 
    Coasting Arc #2 (Orbit 2449)
    ---------------------------------------
 
    Vector Time (GMT): 2016/037/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5668776.63                 A    =         6785569.34  meter
     Y    =        2651003.61  meter          E    =           .0019916
     Z    =        2602805.38                 I    =           51.61833
     XDOT =      -4171.834093                 Wp   =           96.09984
     YDOT =      -3745.323750  meter/sec      RA   =          354.17125  deg
     ZDOT =      -5238.975896                 TA   =           54.56656
                                              MA   =           54.38077
                                              Ha   =            222.925  n.mi
                                              Hp   =            211.783
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18598348.54                 X    =        -5710642.53
     Y    =        8697518.40  feet           Y    =         2587377.53  meter
     Z    =        8539387.74                 Z    =         2575166.77
     XDOT =     -13687.119728                 XDOT =       -4104.194768
     YDOT =     -12287.807578  feet/sec       YDOT =       -3791.597826  meter/sec
     ZDOT =     -17188.241129                 ZDOT =       -5259.076854
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19367042.14                 X    =        -5903074.44
     Y    =       -6964520.73  feet           Y    =        -2122785.92  meter
     Z    =        8419006.33                 Z    =         2566113.13
     XDOT =      -1488.242615                 XDOT =        -453.616349
     YDOT =     -16874.047251  feet/sec       YDOT =       -5143.209602  meter/sec
     ZDOT =     -17274.624653                 ZDOT =       -5265.305594
  
  
    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   16037.53736281  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6407 354.5632 0006587  81.9205 278.2695 15.54462350 24509
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16037.53736281   =   yrday.fracday
    Element set:     901
    Inclination:       51.6407  deg
    RA of node:       354.5632  deg
    Eccentricity:     .0006587     
    Arg of perigee:    81.9205  deg
    Mean anomaly:     278.2695  deg
    Mean motion:   15.54462350  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2450
    Checksum:              313
 
 
    Coasting Arc #3 (Orbit 2464)
    ---------------------------------------
 
    Vector Time (GMT): 2016/038/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6430294.20                 A    =         6787976.44  meter
     Y    =       -1960976.04  meter          E    =           .0015379
     Z    =        -908991.61                 I    =           51.59509
     XDOT =       2157.492633                 Wp   =           56.84358
     YDOT =       4367.210369  meter/sec      RA   =          349.19365  deg
     ZDOT =       5921.656856                 TA   =          293.31109
                                              MA   =          293.47286
                                              Ha   =            222.870  n.mi
                                              Hp   =            211.712
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21096765.74                 X    =         6456159.79
     Y    =       -6433648.44  feet           Y    =        -1888923.64  meter
     Z    =       -2982255.94                 Z    =         -877692.74
     XDOT =       7078.387904                 XDOT =        2079.732907
     YDOT =      14328.118007  feet/sec       YDOT =        4390.902270  meter/sec
     ZDOT =      19428.008058                 ZDOT =        5931.948169
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19694505.22                 X    =         6002885.19
     Y    =        9969207.03  feet           Y    =         3038614.30  meter
     Z    =       -2846152.27                 Z    =         -867507.21
     XDOT =      -4171.091167                 XDOT =       -1271.348588
     YDOT =      13719.929970  feet/sec       YDOT =        4181.834655  meter/sec
     ZDOT =      19471.734251                 ZDOT =        5934.984600
  
  
    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   16038.50167945  .00016717  00000-0  10270-3 0  9024
    2 25544  51.6409 349.7535 0006561  85.8019 274.3884 15.54482572 24658
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16038.50167945   =   yrday.fracday
    Element set:     902
    Inclination:       51.6409  deg
    RA of node:       349.7535  deg
    Eccentricity:     .0006561     
    Arg of perigee:    85.8019  deg
    Mean anomaly:     274.3884  deg
    Mean motion:   15.54482572  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2465
    Checksum:              336
 
 
    Coasting Arc #4 (Orbit 2480)
    ---------------------------------------
 
    Vector Time (GMT): 2016/039/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6628467.18                 A    =         6787816.61  meter
     Y    =        1083149.51  meter          E    =           .0014663
     Z    =        -958347.83                 I    =           51.56478
     XDOT =         45.129565                 Wp   =          120.32438
     YDOT =      -4885.489011  meter/sec      RA   =          344.21750  deg
     ZDOT =      -5908.627965                 TA   =           70.06481
                                              MA   =           69.90691
                                              Ha   =            222.762  n.mi
                                              Hp   =            211.687
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21746939.57                 X    =        -6635431.47
     Y    =        3553640.14  feet           Y    =         1008986.61  meter
     Z    =       -3144185.79                 Z    =         -990563.41
     XDOT =        148.062876                 XDOT =         128.457792
     YDOT =     -16028.507255  feet/sec       YDOT =       -4884.518722  meter/sec
     ZDOT =     -19385.262352                 ZDOT =       -5908.206110
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18353696.26                 X    =        -5594206.62
     Y    =      -12157315.16  feet           Y    =        -3705549.66  meter
     Z    =       -3284077.44                 Z    =        -1000986.80
     XDOT =      10206.813755                 XDOT =        3111.036833
     YDOT =     -10236.695203  feet/sec       YDOT =       -3120.144698  meter/sec
     ZDOT =     -19382.440344                 ZDOT =       -5907.767817
  
  
    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   16039.53027075  .00016717  00000-0  10270-3 0  9038
    2 25544  51.6421 344.6224 0006514  89.1596 271.0303 15.54501265 24815
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16039.53027075   =   yrday.fracday
    Element set:     903
    Inclination:       51.6421  deg
    RA of node:       344.6224  deg
    Eccentricity:     .0006514     
    Arg of perigee:    89.1596  deg
    Mean anomaly:     271.0303  deg
    Mean motion:   15.54501265  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2481
    Checksum:              287
 
 
    Coasting Arc #5 (Orbit 2496)
    ---------------------------------------
 
    Vector Time (GMT): 2016/040/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6233876.23                 A    =         6785100.18  meter
     Y    =        -106354.50  meter          E    =           .0019884
     Z    =        2655860.54                 I    =           51.52544
     XDOT =      -2137.719377                 Wp   =           82.59838
     YDOT =       5226.802627  meter/sec      RA   =          339.23544  deg
     ZDOT =       5196.118555                 TA   =          307.44032
                                              MA   =          307.62107
                                              Ha   =            222.689  n.mi
                                              Hp   =            211.627
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20452349.82                 X    =         6221701.49
     Y    =        -348932.07  feet           Y    =          -36711.04  meter
     Z    =        8713453.23                 Z    =         2686112.84
     XDOT =      -7013.515018                 XDOT =       -2221.247784
     YDOT =      17148.302581  feet/sec       YDOT =        5202.430564  meter/sec
     ZDOT =      17047.633054                 ZDOT =        5185.531061
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15431395.09                 X    =         4703489.22
     Y    =       13341260.90  feet           Y    =         4066416.32  meter
     Z    =        8844627.59                 Z    =         2695842.49
     XDOT =     -15771.202041                 XDOT =       -4807.062382
     YDOT =       6905.215028  feet/sec       YDOT =        2104.709541  meter/sec
     ZDOT =      17000.678756                 ZDOT =        5181.806885
  
  
    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   16040.55884797  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6421 339.4923 0006499  93.1061 267.0836 15.54524081 24971
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16040.55884797   =   yrday.fracday
    Element set:     904
    Inclination:       51.6421  deg
    RA of node:       339.4923  deg
    Eccentricity:     .0006499     
    Arg of perigee:    93.1061  deg
    Mean anomaly:     267.0836  deg
    Mean motion:   15.54524081  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2497
    Checksum:              330
 
 
    Coasting Arc #6 (Orbit 2511)
    ---------------------------------------
 
    Vector Time (GMT): 2016/041/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5315641.82                 A    =         6780888.14  meter
     Y    =       -1049646.30  meter          E    =           .0013694
     Z    =       -4090205.64                 I    =           51.48260
     XDOT =       3984.336458                 Wp   =           82.07165
     YDOT =      -5303.997959  meter/sec      RA   =          334.24002  deg
     ZDOT =      -3826.079765                 TA   =          148.28589
                                              MA   =          148.20333
                                              Ha   =            222.681  n.mi
                                              Hp   =            211.500
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17439769.74                 X    =        -5283641.32
     Y    =       -3443721.46  feet           Y    =        -1108910.76  meter
     Z    =      -13419309.84                 Z    =        -4115949.32
     XDOT =      13071.970008                 XDOT =        4061.935997
     YDOT =     -17401.568108  feet/sec       YDOT =       -5259.008915  meter/sec
     ZDOT =     -12552.755134                 ZDOT =       -3806.536341
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10876212.24                 X    =        -3315069.49
     Y    =      -13953882.70  feet           Y    =        -4253143.45  meter
     Z    =      -13530699.45                 Z    =        -4124157.19
     XDOT =      20312.965025                 XDOT =        6191.391740
     YDOT =      -3772.755277  feet/sec       YDOT =       -1149.935809  meter/sec
     ZDOT =     -12466.972014                 ZDOT =       -3799.933070
  
  
    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   16041.52312646  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6426 334.6819 0006513  96.0431 264.1464 15.54555202 25129
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16041.52312646   =   yrday.fracday
    Element set:     905
    Inclination:       51.6426  deg
    RA of node:       334.6819  deg
    Eccentricity:     .0006513     
    Arg of perigee:    96.0431  deg
    Mean anomaly:     264.1464  deg
    Mean motion:   15.54555202  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2512
    Checksum:              286
 
 
    Coasting Arc #7 (Orbit 2527)
    ---------------------------------------
 
    Vector Time (GMT): 2016/042/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3993310.56                 A    =         6777291.85  meter
     Y    =        2247093.13  meter          E    =           .0011994
     Z    =        4985245.30                 I    =           51.44227
     XDOT =      -5388.591040                 Wp   =          111.40173
     YDOT =       5080.413874  meter/sec      RA   =          329.23161  deg
     ZDOT =       2018.198578                 TA   =          318.90589
                                              MA   =          318.99617
                                              Ha   =            222.466  n.mi
                                              Hp   =            211.623
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13101412.61                 X    =         3943670.48
     Y    =        7372352.79  feet           Y    =         2291471.90  meter
     Z    =       16355791.67                 Z    =         5004522.67
     XDOT =     -17679.104461                 XDOT =       -5454.804360
     YDOT =      16668.024520  feet/sec       YDOT =        5019.785047  meter/sec
     ZDOT =       6621.386411                 ZDOT =        1991.861313
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5251993.29                 X    =         1600807.55
     Y    =       13988903.07  feet           Y    =         4263817.65  meter
     Z    =       16438907.40                 Z    =         5010578.98
     XDOT =     -23265.918111                 XDOT =       -7091.451840
     YDOT =       1057.750835  feet/sec       YDOT =         322.402454  meter/sec
     ZDOT =       6506.211205                 ZDOT =        1983.093175
  
  
    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   16042.55167558  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6423 329.5517 0006376 100.9978 259.1893 15.54594519 25283
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16042.55167558   =   yrday.fracday
    Element set:     906
    Inclination:       51.6423  deg
    RA of node:       329.5517  deg
    Eccentricity:     .0006376     
    Arg of perigee:   100.9978  deg
    Mean anomaly:     259.1893  deg
    Mean motion:   15.54594519  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2528
    Checksum:              345
 
 
    Coasting Arc #8 (Orbit 2542)
    ---------------------------------------
 
    Vector Time (GMT): 2016/043/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2418491.13                 A    =         6776032.95  meter
     Y    =       -3477394.80  meter          E    =           .0021206
     Z    =       -5307334.86                 I    =           51.41102
     XDOT =       6237.202101                 Wp   =           94.21737
     YDOT =      -4435.090060  meter/sec      RA   =          324.21193  deg
     ZDOT =         62.363200                 TA   =          176.38760
                                              MA   =          176.37226
                                              Ha   =            222.610  n.mi
                                              Hp   =            211.526
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7934682.20                 X    =        -2353645.91
     Y    =      -11408775.58  feet           Y    =        -3504077.90  meter
     Z    =      -17412515.94                 Z    =        -5318925.29
     XDOT =      20463.261486                 XDOT =        6286.029886
     YDOT =     -14550.820408  feet/sec       YDOT =       -4365.068511  meter/sec
     ZDOT =        204.603676                 ZDOT =          92.780560
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1069171.95                 X    =          325883.61
     Y    =      -13793046.80  feet           Y    =        -4204120.67  meter
     Z    =      -17462067.02                 Z    =        -5322438.03
     XDOT =      24056.492186                 XDOT =        7332.418818
     YDOT =       1432.262543  feet/sec       YDOT =         436.553623  meter/sec
     ZDOT =        337.323135                 ZDOT =         102.816092
  
  
    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   16043.51593010  .00016717  00000-0  10270-3 0  9072
    2 25544  51.6426 324.7408 0006441 103.4647 256.7224 15.54586211 25434
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16043.51593010   =   yrday.fracday
    Element set:     907
    Inclination:       51.6426  deg
    RA of node:       324.7408  deg
    Eccentricity:     .0006441     
    Arg of perigee:   103.4647  deg
    Mean anomaly:     256.7224  deg
    Mean motion:   15.54586211  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2543
    Checksum:              290
 
 
    Coasting Arc #9 (Orbit 2558)
    ---------------------------------------
 
    Vector Time (GMT): 2016/044/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         749117.20                 A    =         6777483.94  meter
     Y    =        4567101.54  meter          E    =           .0011555
     Z    =        4941859.14                 I    =           51.39030
     XDOT =      -6544.826800                 Wp   =           81.80347
     YDOT =       3394.348059  meter/sec      RA   =          319.19154  deg
     ZDOT =      -2138.930468                 TA   =           29.11826
                                              MA   =           29.05387
                                              Ha   =            222.480  n.mi
                                              Hp   =            211.633
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2457733.60                 X    =          673985.91
     Y    =       14983928.92  feet           Y    =         4575059.00  meter
     Z    =       16213448.63                 Z    =         4945315.25
     XDOT =     -21472.528870                 XDOT =       -6571.906926
     YDOT =      11136.312530  feet/sec       YDOT =        3321.007868  meter/sec
     ZDOT =      -7017.488412                 ZDOT =       -2170.789308
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7343642.29                 X    =        -2238342.17
     Y    =       13273005.68  feet           Y    =         4045612.13  meter
     Z    =       16227530.15                 Z    =         4946151.19
     XDOT =     -22781.796972                 XDOT =       -6943.891717
     YDOT =      -3831.762238  feet/sec       YDOT =       -1167.921130  meter/sec
     ZDOT =      -7156.239596                 ZDOT =       -2181.221829
  
  
    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   16044.54445317  .00016717  00000-0  10270-3 0  9083
    2 25544  51.6421 319.6100 0006364 106.9532 253.2319 15.54621345 25598
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16044.54445317   =   yrday.fracday
    Element set:     908
    Inclination:       51.6421  deg
    RA of node:       319.6100  deg
    Eccentricity:     .0006364     
    Arg of perigee:   106.9532  deg
    Mean anomaly:     253.2319  deg
    Mean motion:   15.54621345  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2559
    Checksum:              295
 
 
    Coasting Arc #10 (Orbit 2573)
    ---------------------------------------
 
    Vector Time (GMT): 2016/045/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         824900.19                 A    =         6781133.57  meter
     Y    =       -5427875.43  meter          E    =           .0013251
     Z    =       -3994251.64                 I    =           51.37948
     XDOT =       6273.313480                 Wp   =          108.57076
     YDOT =      -1940.496172  meter/sec      RA   =          314.17649  deg
     ZDOT =       3939.189151                 TA   =          202.57966
                                              MA   =          202.63802
                                              Ha   =            222.488  n.mi
                                              Hp   =            211.643
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2706365.45                 X    =          904936.89
     Y    =      -17807990.27  feet           Y    =        -5418203.62  meter
     Z    =      -13104500.12                 Z    =        -3990049.74
     XDOT =      20581.737140                 XDOT =        6275.411647
     YDOT =      -6366.457258  feet/sec       YDOT =       -1870.331812  meter/sec
     ZDOT =      12923.848920                 ZDOT =        3969.668267
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12923371.04                 X    =         3939043.49
     Y    =      -12567425.50  feet           Y    =        -3830551.29  meter
     Z    =      -13085226.49                 Z    =        -3988377.03
     XDOT =      19298.235805                 XDOT =        5882.102273
     YDOT =       6273.228075  feet/sec       YDOT =        1912.079917  meter/sec
     ZDOT =      13056.327611                 ZDOT =        3979.568656
  
  
    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   16045.50868180  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6426 314.7989 0006394 110.5832 249.6008 15.54631294 25746
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16045.50868180   =   yrday.fracday
    Element set:     909
    Inclination:       51.6426  deg
    RA of node:       314.7989  deg
    Eccentricity:     .0006394     
    Arg of perigee:   110.5832  deg
    Mean anomaly:     249.6008  deg
    Mean motion:   15.54631294  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2574
    Checksum:              328
 
 
    Coasting Arc #11 (Orbit 2589)
    ---------------------------------------
 
    Vector Time (GMT): 2016/046/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2222517.70                 A    =         6785265.71  meter
     Y    =        5891734.36  meter          E    =           .0020083
     Z    =        2500980.16                 I    =           51.37134
     XDOT =      -5568.255892                 Wp   =          107.67127
     YDOT =        153.437070  meter/sec      RA   =          309.17250  deg
     ZDOT =      -5280.704683                 TA   =           44.13188
                                              MA   =           43.97181
                                              Ha   =            222.486  n.mi
                                              Hp   =            211.697
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7291724.75                 X    =        -2300383.91
     Y    =       19329837.15  feet           Y    =         5866445.46  meter
     Z    =        8205315.48                 Z    =         2489994.39
     XDOT =     -18268.556075                 XDOT =       -5543.906704
     YDOT =        503.402462  feet/sec       YDOT =          91.304993  meter/sec
     ZDOT =     -17325.146597                 ZDOT =       -5307.694454
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17285927.45                 X    =        -5268750.69
     Y    =       11349289.01  feet           Y    =         3459263.29  meter
     Z    =        8156556.10                 Z    =         2486118.30
     XDOT =     -14172.841184                 XDOT =       -4319.881993
     YDOT =      -8982.161836  feet/sec       YDOT =       -2737.762928  meter/sec
     ZDOT =     -17442.150281                 ZDOT =       -5316.367406
  
  
    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   16046.53717962  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6424 309.6673 0006432 114.8552 245.3270 15.54625442 25906
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16046.53717962   =   yrday.fracday
    Element set:     910
    Inclination:       51.6424  deg
    RA of node:       309.6673  deg
    Eccentricity:     .0006432     
    Arg of perigee:   114.8552  deg
    Mean anomaly:     245.3270  deg
    Mean motion:   15.54625442  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2590
    Checksum:              305
 
 
    Coasting Arc #12 (Orbit 2604)
    ---------------------------------------
 
    Vector Time (GMT): 2016/047/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3287600.31                 A    =         6787530.18  meter
     Y    =       -5889702.03  meter          E    =           .0013307
     Z    =        -736413.75                 I    =           51.36054
     XDOT =       4515.225877                 Wp   =           67.26717
     YDOT =       1790.194258  meter/sec      RA   =          304.17705  deg
     ZDOT =       5930.713239                 TA   =          284.74577
                                              MA   =          284.89320
                                              Ha   =            222.332  n.mi
                                              Hp   =            211.712
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10786090.25                 X    =         3356793.21
     Y    =      -19323169.39  feet           Y    =        -5852551.06  meter
     Z    =       -2416055.62                 Z    =         -720275.30
     XDOT =      14813.733191                 XDOT =        4466.063432
     YDOT =       5873.340741  feet/sec       YDOT =        1840.411892  meter/sec
     ZDOT =      19457.720602                 ZDOT =        5952.527297
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19918568.62                 X    =         6071179.72
     Y    =       -9659900.20  feet           Y    =        -2944337.58  meter
     Z    =       -2344972.36                 Z    =         -714747.57
     XDOT =       7975.463208                 XDOT =        2430.921186
     YDOT =      11773.552010  feet/sec       YDOT =        3588.578653  meter/sec
     ZDOT =      19551.916596                 ZDOT =        5959.424178
  
  
    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   16047.50138261  .00016717  00000-0  10270-3 0  9113
    2 25544  51.6430 304.8564 0006263 118.1132 242.0655 15.54670884 26050
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16047.50138261   =   yrday.fracday
    Element set:     911
    Inclination:       51.6430  deg
    RA of node:       304.8564  deg
    Eccentricity:     .0006263     
    Arg of perigee:   118.1132  deg
    Mean anomaly:     242.0655  deg
    Mean motion:   15.54670884  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2605
    Checksum:              287
 
 
    Coasting Arc #13 (Orbit 2619)
    ---------------------------------------
 
    Vector Time (GMT): 2016/048/10:54:15.497
    Vector Time (MET): N/A
    Weight (LBS)     : 922210.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1781057.61                 A    =         6779692.98  meter
     Y    =       -4542997.41  meter          E    =           .0015016
     Z    =       -4721360.91                 I    =           51.31299
     XDOT =       5240.833200                 Wp   =          114.47411
     YDOT =      -4876.099166  meter/sec      RA   =          299.37976  deg
     ZDOT =       2715.606045                 TA   =          182.54859
                                              MA   =          182.55625
                                              Ha   =            222.275  n.mi
                                              Hp   =            213.233
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5843364.87                 X    =        -1707190.36
     Y    =      -14904847.14  feet           Y    =        -4562501.56  meter
     Z    =      -15490029.23                 Z    =        -4729833.09
     XDOT =      17194.334647                 XDOT =        5281.778414
     YDOT =     -15997.700677  feet/sec       YDOT =       -4817.263641  meter/sec
     ZDOT =       8909.468652                 ZDOT =        2741.163934
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7828765.38                 X    =         2386207.69
     Y    =      -13924725.45  feet           Y    =        -4244256.32  meter
     Z    =      -15525876.48                 Z    =        -4732287.15
     XDOT =      22232.807140                 XDOT =        6776.559616
     YDOT =       2443.941908  feet/sec       YDOT =         744.913494  meter/sec
     ZDOT =       9021.173676                 ZDOT =        2749.653736
  
  
    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   16048.46557501  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6429 300.0444 0004260 129.4194 230.7337 15.54186600 26207
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16048.46557501   =   yrday.fracday
    Element set:     912
    Inclination:       51.6429  deg
    RA of node:       300.0444  deg
    Eccentricity:     .0004260     
    Arg of perigee:   129.4194  deg
    Mean anomaly:     230.7337  deg
    Mean motion:   15.54186600  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2620
    Checksum:              283
 
 
    Coasting Arc #14 (Orbit 2635)
    ---------------------------------------
 
    Vector Time (GMT): 2016/049/10:54:15.497
    Vector Time (MET): N/A
    Weight (LBS)     : 922210.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         670284.82                 A    =         6783381.65  meter
     Y    =        5652864.00  meter          E    =           .0015021
     Z    =        3674576.08                 I    =           51.31016
     XDOT =      -5342.205392                 Wp   =           97.08880
     YDOT =       3440.010697  meter/sec      RA   =          294.36684  deg
     ZDOT =      -4304.203645                 TA   =           38.89817
                                              MA   =           38.79017
                                              Ha   =            222.198  n.mi
                                              Hp   =            213.329
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2199097.19                 X    =          589174.13
     Y    =       18546141.74  feet           Y    =         5659906.23  meter
     Z    =       12055695.79                 Z    =         3677634.82
     XDOT =     -17526.920576                 XDOT =       -5359.367854
     YDOT =      11286.124333  feet/sec       YDOT =        3380.174449  meter/sec
     ZDOT =     -14121.403034                 ZDOT =       -4330.196065
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12709549.15                 X    =        -3873870.58
     Y    =       13673655.66  feet           Y    =         4167730.24  meter
     Z    =       12067879.04                 Z    =         3678289.53
     XDOT =     -18914.565523                 XDOT =       -5765.159572
     YDOT =      -4979.319875  feet/sec       YDOT =       -1517.696698  meter/sec
     ZDOT =     -14234.711300                 ZDOT =       -4338.740004
  
  
    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   16049.49436349  .00016717  00000-0  10270-3 0  9133
    2 25544  51.6425 294.9153 0004292 132.9131 227.2382 15.54198005 26366
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16049.49436349   =   yrday.fracday
    Element set:     913
    Inclination:       51.6425  deg
    RA of node:       294.9153  deg
    Eccentricity:     .0004292     
    Arg of perigee:   132.9131  deg
    Mean anomaly:     227.2382  deg
    Mean motion:   15.54198005  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2636
    Checksum:              313
 
 
    Coasting Arc #15 (Orbit 2650)
    ---------------------------------------
 
    Vector Time (GMT): 2016/050/10:54:15.497
    Vector Time (MET): N/A
    Weight (LBS)     : 922210.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         326321.05                 A    =         6786842.70  meter
     Y    =       -6391861.85  meter          E    =           .0007080
     Z    =       -2261786.17                 I    =           51.31039
     XDOT =       5170.552478                 Wp   =           79.71808
     YDOT =      -1644.867398  meter/sec      RA   =          289.36289  deg
     ZDOT =       5410.150635                 TA   =          255.01211
                                              MA   =          255.09050
                                              Ha   =            222.087  n.mi
                                              Hp   =            213.363
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1070607.10                 X    =          408758.71
     Y    =      -20970675.38  feet           Y    =        -6387751.91  meter
     Z    =       -7420558.31                 Z    =        -2260000.42
     XDOT =      16963.754848                 XDOT =        5162.281927
     YDOT =      -5396.546580  feet/sec       YDOT =       -1587.092778  meter/sec
     ZDOT =      17749.838042                 ZDOT =        5435.247317
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16435568.02                 X    =         5009561.13
     Y    =      -13073642.35  feet           Y    =        -3984846.19  meter
     Z    =       -7411618.61                 Z    =        -2259061.35
     XDOT =      14260.272512                 XDOT =        4346.531062
     YDOT =       7832.180609  feet/sec       YDOT =        2387.248650  meter/sec
     ZDOT =      17858.921650                 ZDOT =        5443.399319
  
  
    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   16050.45883980  .00016717  00000-0  10270-3 0  9149
    2 25544  51.6430 290.1062 0004185 137.2145 222.9334 15.54237740 26519
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16050.45883980   =   yrday.fracday
    Element set:     914
    Inclination:       51.6430  deg
    RA of node:       290.1062  deg
    Eccentricity:     .0004185     
    Arg of perigee:   137.2145  deg
    Mean anomaly:     222.9334  deg
    Mean motion:   15.54237740  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2651
    Checksum:              292
 
 
    Coasting Arc #16 (Orbit 2666)
    ---------------------------------------
 
    Vector Time (GMT): 2016/051/10:54:15.497
    Vector Time (MET): N/A
    Weight (LBS)     : 922210.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1239774.91                 A    =         6788975.11  meter
     Y    =        6642523.06  meter          E    =           .0017199
     Z    =         558360.97                 I    =           51.30716
     XDOT =      -4822.820916                 Wp   =          132.15959
     YDOT =       -390.683103  meter/sec      RA   =          284.36697  deg
     ZDOT =      -5954.127855                 TA   =           41.78390
                                              MA   =           41.65270
                                              Ha   =            222.071  n.mi
                                              Hp   =            213.488
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4067502.99                 X    =        -1316673.32
     Y    =       21793054.67  feet           Y    =         6628229.15  meter
     Z    =        1831892.95                 Z    =          552151.34
     XDOT =     -15822.903269                 XDOT =       -4789.171877
     YDOT =      -1281.768709  feet/sec       YDOT =        -444.427384  meter/sec
     ZDOT =     -19534.540206                 ZDOT =       -5977.473582
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18815665.97                 X    =        -5735014.99
     Y    =       11728378.04  feet           Y    =         3574809.63  meter
     Z    =        1803747.93                 Z    =          549782.37
     XDOT =      -8811.542614                 XDOT =       -2685.758189
     YDOT =     -11061.751657  feet/sec       YDOT =       -3371.621905  meter/sec
     ZDOT =     -19635.655546                 ZDOT =       -5984.947810
  
  
    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   16051.48760380  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6427 284.9767 0004253 142.2297 217.9154 15.54207758 26675
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16051.48760380   =   yrday.fracday
    Element set:     915
    Inclination:       51.6427  deg
    RA of node:       284.9767  deg
    Eccentricity:     .0004253     
    Arg of perigee:   142.2297  deg
    Mean anomaly:     217.9154  deg
    Mean motion:   15.54207758  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2667
    Checksum:              331
 
             

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