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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  17659.2714
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   77.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.664
   ET - UTC  (sec) :   68.18
   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 
   ------------------------------------------------------------------------
   182/20:55:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.5  
   000/00:00:00.000           0.0               0.0              214.8  
   
   183/12:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.4  
   000/00:00:00.000           0.0               0.0              215.0  
   
 
 
    Coasting Arc #1 (Orbit 2272)
    ---------------------------------------
 
    Vector Time (GMT): 2017/174/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6610367.84                 A    =         6789178.13  meter
     Y    =       -1334559.02  meter          E    =           .0005204
     Z    =        -760466.78                 I    =           51.70366
     XDOT =       1601.705322                 Wp   =          147.95838
     YDOT =      -4553.643381  meter/sec      RA   =            6.30524  deg
     ZDOT =      -5954.554644                 TA   =           40.25037
                                              MA   =           40.21185
                                              Ha   =            220.445  n.mi
                                              Hp   =            216.103
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21687558.52                 X    =        -6591259.17
     Y    =       -4378474.46  feet           Y    =        -1408373.66  meter
     Z    =       -2494969.76                 Z    =         -792531.79
     XDOT =       5254.938722                 XDOT =        1681.430680
     YDOT =     -14939.774873  feet/sec       YDOT =       -4535.285249  meter/sec
     ZDOT =     -19535.940433                 ZDOT =       -5946.581167
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4006232.67                 X    =        -1221099.72
     Y    =       21742727.76  feet           Y    =         6627183.42  meter
     Z    =       -2636284.64                 Z    =         -803539.56
     XDOT =     -13446.177051                 XDOT =       -4098.394765
     YDOT =      -4833.221028  feet/sec       YDOT =       -1473.165769  meter/sec
     ZDOT =     -19499.832019                 ZDOT =       -5943.548800
  
  
    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   17174.53062184  .00016717  00000-0  10270-3 0  9006
    2 25544  51.6393   6.7155 0005170 312.4359  47.6356 15.54085089 22733
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17174.53062184   =   yrday.fracday
    Element set:     900
    Inclination:       51.6393  deg
    RA of node:         6.7155  deg
    Eccentricity:     .0005170     
    Arg of perigee:   312.4359  deg
    Mean anomaly:      47.6356  deg
    Mean motion:   15.54085089  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2273
    Checksum:              303
 
 
    Coasting Arc #2 (Orbit 2288)
    ---------------------------------------
 
    Vector Time (GMT): 2017/175/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6021652.91                 A    =         6786968.23  meter
     Y    =        2017516.46  meter          E    =           .0012118
     Z    =        2373176.25                 I    =           51.66286
     XDOT =      -3525.673392                 Wp   =           52.51979
     YDOT =       4176.513870  meter/sec      RA   =            1.33458  deg
     ZDOT =       5383.747728                 TA   =          333.98525
                                              MA   =          334.04610
                                              Ha   =            220.428  n.mi
                                              Hp   =            215.952
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19756079.09                 X    =         5987117.29
     Y    =        6619148.48  feet           Y    =         2084661.15  meter
     Z    =        7786011.33                 Z    =         2402343.93
     XDOT =     -11567.169922                 XDOT =       -3598.265733
     YDOT =      13702.473326  feet/sec       YDOT =        4136.680593  meter/sec
     ZDOT =      17663.214330                 ZDOT =        5366.445561
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5939003.20                 X    =         1810208.18
     Y    =      -19920550.04  feet           Y    =        -6071783.65  meter
     Z    =        7914397.47                 Z    =         2412308.35
     XDOT =      12644.677363                 XDOT =        3854.097660
     YDOT =      10771.616790  feet/sec       YDOT =        3283.188798  meter/sec
     ZDOT =      17585.990724                 ZDOT =        5360.209973
  
  
    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   17175.55948959  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6383   1.5856 0005006 314.8881  45.1864 15.54092457 22898
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17175.55948959   =   yrday.fracday
    Element set:     901
    Inclination:       51.6383  deg
    RA of node:         1.5856  deg
    Eccentricity:     .0005006     
    Arg of perigee:   314.8881  deg
    Mean anomaly:      45.1864  deg
    Mean motion:   15.54092457  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2289
    Checksum:              335
 
 
    Coasting Arc #3 (Orbit 2303)
    ---------------------------------------
 
    Vector Time (GMT): 2017/176/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4983554.67                 A    =         6783346.79  meter
     Y    =       -2665451.30  meter          E    =           .0005887
     Z    =       -3758315.50                 I    =           51.61777
     XDOT =       5187.978825                 Wp   =           27.11929
     YDOT =      -3703.745254  meter/sec      RA   =          356.35475  deg
     ZDOT =      -4250.055130                 TA   =          197.82377
                                              MA   =          197.84442
                                              Ha   =            220.697  n.mi
                                              Hp   =            215.688
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16350244.99                 X    =        -4935122.63
     Y    =       -8744918.95  feet           Y    =        -2720909.38  meter
     Z    =      -12330431.43                 Z    =        -3782406.64
     XDOT =      17020.927902                 XDOT =        5249.653988
     YDOT =     -12151.395191  feet/sec       YDOT =       -3645.384234  meter/sec
     ZDOT =     -13943.750426                 ZDOT =       -4224.704556
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7895880.45                 X    =        -2406664.36
     Y    =       16698437.02  feet           Y    =         5089683.60  meter
     Z    =      -12436274.80                 Z    =        -3790576.56
     XDOT =     -11800.764001                 XDOT =       -3596.872867
     YDOT =     -15886.847969  feet/sec       YDOT =       -4842.311261  meter/sec
     ZDOT =     -13831.086452                 ZDOT =       -4215.715151
  
  
    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   17176.52405320  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6378 356.7775 0004947 320.8204  39.2590 15.54093443 23040
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17176.52405320   =   yrday.fracday
    Element set:     902
    Inclination:       51.6378  deg
    RA of node:       356.7775  deg
    Eccentricity:     .0004947     
    Arg of perigee:   320.8204  deg
    Mean anomaly:      39.2590  deg
    Mean motion:   15.54093443  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2304
    Checksum:              306
 
 
    Coasting Arc #4 (Orbit 2319)
    ---------------------------------------
 
    Vector Time (GMT): 2017/177/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3570483.46                 A    =         6779832.82  meter
     Y    =        3265708.86  meter          E    =           .0003602
     Z    =        4745699.35                 I    =           51.57376
     XDOT =      -6457.245920                 Wp   =           82.55227
     YDOT =       3142.869764  meter/sec      RA   =          351.36174  deg
     ZDOT =       2694.152497                 TA   =          340.80247
                                              MA   =          340.81603
                                              Ha   =            220.723  n.mi
                                              Hp   =            215.773
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11714184.56                 X    =         3510648.08
     Y    =       10714267.91  feet           Y    =         3305301.20  meter
     Z    =       15569879.77                 Z    =         4762898.57
     XDOT =     -21185.190027                 XDOT =       -6504.997110
     YDOT =      10311.252506  feet/sec       YDOT =        3070.393095  meter/sec
     ZDOT =       8839.082995                 ZDOT =        2662.670039
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9892455.13                 X    =         3015220.32
     Y    =      -12320982.79  feet           Y    =        -3755435.55  meter
     Z    =       15645175.85                 Z    =         4768649.60
     XDOT =      10848.805223                 XDOT =        3306.715832
     YDOT =      19762.398002  feet/sec       YDOT =        6023.578911  meter/sec
     ZDOT =       8699.461317                 ZDOT =        2651.595809
  
  
    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   17177.55291819  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6382 351.6481 0005052 322.8428  37.2374 15.54074156 23207
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17177.55291819   =   yrday.fracday
    Element set:     903
    Inclination:       51.6382  deg
    RA of node:       351.6481  deg
    Eccentricity:     .0005052     
    Arg of perigee:   322.8428  deg
    Mean anomaly:      37.2374  deg
    Mean motion:   15.54074156  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2320
    Checksum:              304
 
 
    Coasting Arc #5 (Orbit 2334)
    ---------------------------------------
 
    Vector Time (GMT): 2017/178/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1932672.99                 A    =         6777675.96  meter
     Y    =       -3829652.48  meter          E    =           .0013227
     Z    =       -5258441.61                 I    =           51.53563
     XDOT =       7205.367095                 Wp   =           63.97109
     YDOT =      -2450.972402  meter/sec      RA   =          346.35941  deg
     ZDOT =       -859.235479                 TA   =          197.76834
                                              MA   =          197.81463
                                              Ha   =            220.907  n.mi
                                              Hp   =            215.447
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6340790.64                 X    =        -1864162.58
     Y    =      -12564476.65  feet           Y    =        -3850881.27  meter
     Z    =      -17252105.02                 Z    =        -5267663.86
     XDOT =      23639.655823                 XDOT =        7236.412687
     YDOT =      -8041.248038  feet/sec       YDOT =       -2370.223417  meter/sec
     ZDOT =      -2819.014038                 ZDOT =        -824.159374
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11984878.65                 X    =        -3652991.01
     Y    =        7283798.45  feet           Y    =         2220101.77  meter
     Z    =      -17292073.06                 Z    =        -5270623.87
     XDOT =      -9511.933712                 XDOT =       -2899.237395
     YDOT =     -22005.806488  feet/sec       YDOT =       -6707.369818  meter/sec
     ZDOT =      -2663.670156                 ZDOT =        -811.886663
  
  
    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   17178.51747640  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6392 346.8403 0004822 328.6769  31.4095 15.54094296 23353
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17178.51747640   =   yrday.fracday
    Element set:     904
    Inclination:       51.6392  deg
    RA of node:       346.8403  deg
    Eccentricity:     .0004822     
    Arg of perigee:   328.6769  deg
    Mean anomaly:      31.4095  deg
    Mean motion:   15.54094296  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2335
    Checksum:              326
 
 
    Coasting Arc #6 (Orbit 2350)
    ---------------------------------------
 
    Vector Time (GMT): 2017/179/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         180366.63                 A    =         6777997.17  meter
     Y    =        4320481.85  meter          E    =           .0006428
     Z    =        5219577.14                 I    =           51.50351
     XDOT =      -7421.519818                 Wp   =            8.47121
     YDOT =       1608.018206  meter/sec      RA   =          341.35122  deg
     ZDOT =      -1068.175340                 TA   =           91.81763
                                              MA   =           91.74401
                                              Ha   =            221.111  n.mi
                                              Hp   =            215.469
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         591754.05                 X    =          106686.62
     Y    =       14174809.22  feet           Y    =         4322086.36  meter
     Z    =       17124596.91                 Z    =         5220274.75
     XDOT =     -24348.818302                 XDOT =       -7433.760912
     YDOT =       5275.650281  feet/sec       YDOT =        1524.957397  meter/sec
     ZDOT =      -3504.512271                 ZDOT =       -1104.255933
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14051544.80                 X    =         4282910.85
     Y    =       -1937198.05  feet           Y    =         -590457.96  meter
     Z    =       17126837.45                 Z    =         5220260.05
     XDOT =       7611.211782                 XDOT =        2319.897351
     YDOT =      22628.092082  feet/sec       YDOT =        6897.042467  meter/sec
     ZDOT =      -3664.116232                 ZDOT =       -1116.822628
  
  
    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   17179.54633770  .00016717  00000-0  10270-3 0  9052
    2 25544  51.6380 341.7112 0004777 332.4442  27.6457 15.54048640 23510
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17179.54633770   =   yrday.fracday
    Element set:     905
    Inclination:       51.6380  deg
    RA of node:       341.7112  deg
    Eccentricity:     .0004777     
    Arg of perigee:   332.4442  deg
    Mean anomaly:      27.6457  deg
    Mean motion:   15.54048640  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2351
    Checksum:              306
 
 
    Coasting Arc #7 (Orbit 2365)
    ---------------------------------------
 
    Vector Time (GMT): 2017/180/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1487307.63                 A    =         6780270.00  meter
     Y    =       -4701050.09  meter          E    =           .0007862
     Z    =       -4660392.04                 I    =           51.48263
     XDOT =       7077.753303                 Wp   =           83.51322
     YDOT =       -603.810211  meter/sec      RA   =          336.34574  deg
     ZDOT =       2872.902685                 TA   =          215.09390
                                              MA   =          215.14573
                                              Ha   =            221.118  n.mi
                                              Hp   =            215.346
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4879618.21                 X    =         1562403.15
     Y    =      -15423392.67  feet           Y    =        -4683997.74  meter
     Z    =      -15290000.13                 Z    =        -4652985.22
     XDOT =      23220.975404                 XDOT =        7070.024219
     YDOT =      -1981.004629  feet/sec       YDOT =        -524.705425  meter/sec
     ZDOT =       9425.533744                 ZDOT =        2907.265070
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15911082.15                 X    =        -4849697.84
     Y    =       -3091230.83  feet           Y    =         -942207.16  meter
     Z    =      -15256394.60                 Z    =        -4650149.07
     XDOT =      -4972.195575                 XDOT =       -1515.525211
     YDOT =     -21593.234685  feet/sec       YDOT =       -6581.617932  meter/sec
     ZDOT =       9577.347345                 ZDOT =        2919.175471
  
  
    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   17180.51089122  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6397 336.9038 0004809 335.0162  25.0757 15.54093538 23662
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17180.51089122   =   yrday.fracday
    Element set:     906
    Inclination:       51.6397  deg
    RA of node:       336.9038  deg
    Eccentricity:     .0004809     
    Arg of perigee:   335.0162  deg
    Mean anomaly:      25.0757  deg
    Mean motion:   15.54093538  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2366
    Checksum:              314
 
 
    Coasting Arc #8 (Orbit 2381)
    ---------------------------------------
 
    Vector Time (GMT): 2017/181/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2995740.95                 A    =         6784030.27  meter
     Y    =        4904742.26  meter          E    =           .0011497
     Z    =        3600447.98                 I    =           51.46522
     XDOT =      -6252.638157                 Wp   =           63.03494
     YDOT =       -577.009081  meter/sec      RA   =          331.34537  deg
     ZDOT =      -4400.476445                 TA   =           74.22381
                                              MA   =           74.09706
                                              Ha   =            221.279  n.mi
                                              Hp   =            215.229
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9828546.42                 X    =        -3067853.51
     Y    =       16091674.09  feet           Y    =         4870838.37  meter
     Z    =       11812493.39                 Z    =         3585720.93
     XDOT =     -20513.904714                 XDOT =       -6224.345967
     YDOT =      -1893.074413  feet/sec       YDOT =        -646.771790  meter/sec
     ZDOT =     -14437.258678                 ZDOT =       -4430.780956
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17299125.84                 X    =         5272773.56
     Y    =        7605017.46  feet           Y    =         2318009.32  meter
     Z    =       11746542.23                 Z    =         3580346.07
     XDOT =       1478.383943                 XDOT =         450.611426
     YDOT =      19224.455220  feet/sec       YDOT =        5859.613951  meter/sec
     ZDOT =     -14570.922956                 ZDOT =       -4441.217317
  
  
    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   17181.53974685  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6393 331.7744 0004826 339.0051  21.0903 15.54082507 23826
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17181.53974685   =   yrday.fracday
    Element set:     907
    Inclination:       51.6393  deg
    RA of node:       331.7744  deg
    Eccentricity:     .0004826     
    Arg of perigee:   339.0051  deg
    Mean anomaly:      21.0903  deg
    Mean motion:   15.54082507  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2382
    Checksum:              309
 
 
    Coasting Arc #9 (Orbit 2396)
    ---------------------------------------
 
    Vector Time (GMT): 2017/182/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4171029.74                 A    =         6787419.54  meter
     Y    =       -4877104.34  meter          E    =           .0009678
     Z    =       -2194976.60                 I    =           51.44928
     XDOT =       5049.546386                 Wp   =           16.36514
     YDOT =       1867.260578  meter/sec      RA   =          326.35459  deg
     ZDOT =       5461.497583                 TA   =          319.19020
                                              MA   =          319.26264
                                              Ha   =            221.379  n.mi
                                              Hp   =            215.059
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13684480.77                 X    =         4235918.88
     Y    =      -16000998.48  feet           Y    =        -4830098.06  meter
     Z    =       -7201366.79                 Z    =        -2174557.88
     XDOT =      16566.753235                 XDOT =        5001.761716
     YDOT =       6126.182998  feet/sec       YDOT =        1923.460413  meter/sec
     ZDOT =      17918.299156                 ZDOT =        5485.910717
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17927151.64                 X    =        -5464195.82
     Y    =      -11100334.55  feet           Y    =        -3383381.97  meter
     Z    =       -7110306.39                 Z    =        -2167221.39
     XDOT =       2709.280626                 XDOT =         825.788735
     YDOT =     -15889.980349  feet/sec       YDOT =       -4843.266011  meter/sec
     ZDOT =      18025.705166                 ZDOT =        5494.234935
  
  
    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   17182.50429648  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6399 326.9672 0004855 343.2924  16.8068 15.54099077 23976
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17182.50429648   =   yrday.fracday
    Element set:     908
    Inclination:       51.6399  deg
    RA of node:       326.9672  deg
    Eccentricity:     .0004855     
    Arg of perigee:   343.2924  deg
    Mean anomaly:      16.8068  deg
    Mean motion:   15.54099077  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2397
    Checksum:              352
 
 
    Coasting Arc #10 (Orbit 2402)
    ---------------------------------------
 
    Vector Time (GMT): 2017/182/20:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922738.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3753479.80                 A    =         6778173.64  meter
     Y    =       -2361177.58  meter          E    =           .0014440
     Z    =       -5138693.17                 I    =           51.40823
     XDOT =       5354.358186                 Wp   =           57.66628
     YDOT =      -5269.772968  meter/sec      RA   =          324.53302  deg
     ZDOT =      -1485.095821                 TA   =          197.94237
                                              MA   =          197.99339
                                              Ha   =            221.481  n.mi
                                              Hp   =            214.837
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12314566.28                 X    =        -3701836.35
     Y    =       -7746645.61  feet           Y    =        -2402862.36  meter
     Z    =      -16859229.56                 Z    =        -5156801.13
     XDOT =      17566.791950                 XDOT =        5420.102075
     YDOT =     -17289.281391  feet/sec       YDOT =       -5209.529184  meter/sec
     ZDOT =      -4872.361616                 ZDOT =       -1458.926828
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13533930.96                 X    =         4125142.16
     Y    =       -5079914.10  feet           Y    =        -1548357.82  meter
     Z    =      -16938709.16                 Z    =        -5162918.55
     XDOT =       2840.096706                 XDOT =         865.661476
     YDOT =      23473.788114  feet/sec       YDOT =        7154.810617  meter/sec
     ZDOT =      -4755.848199                 ZDOT =       -1449.582531
  
  
    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   17182.89011485  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6398 325.0483 0005159 345.8322  14.2685 15.54088336 24034
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17182.89011485   =   yrday.fracday
    Element set:     909
    Inclination:       51.6398  deg
    RA of node:       325.0483  deg
    Eccentricity:     .0005159     
    Arg of perigee:   345.8322  deg
    Mean anomaly:      14.2685  deg
    Mean motion:   15.54088336  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2403
    Checksum:              319
 
 
    Coasting Arc #11 (Orbit 2412)
    ---------------------------------------
 
    Vector Time (GMT): 2017/183/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 901313.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5009439.40                 A    =         6789265.52  meter
     Y    =        4547127.63  meter          E    =           .0009434
     Z    =         532575.61                 I    =           51.42837
     XDOT =      -3574.571181                 Wp   =          111.31009
     YDOT =      -3230.059352  meter/sec      RA   =          321.36887  deg
     ZDOT =      -5962.390214                 TA   =           62.92904
                                              MA   =           62.83281
                                              Ha   =            221.406  n.mi
                                              Hp   =            214.955
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16435168.64                 X    =        -5062501.26
     Y    =       14918397.74  feet           Y    =         4490811.95  meter
     Z    =        1747295.32                 Z    =          508112.86
     XDOT =     -11727.595738                 XDOT =       -3509.223812
     YDOT =     -10597.307584  feet/sec       YDOT =       -3269.666725  meter/sec
     ZDOT =     -19561.647683                 ZDOT =       -5979.595918
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17512948.74                 X    =         5337946.77
     Y    =       13650585.55  feet           Y    =         4160698.48  meter
     Z    =        1638456.93                 Z    =          499401.67
     XDOT =      -7462.243566                 XDOT =       -2274.491839
     YDOT =      11965.085430  feet/sec       YDOT =        3646.958039  meter/sec
     ZDOT =     -19636.979038                 ZDOT =       -5985.351211
  
  
    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   17183.53314757  .00016717  00000-0  10270-3 0  9103
    2 25544  51.6392 321.8383 0004924 345.8751  14.2263 15.54113211 24130
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17183.53314757   =   yrday.fracday
    Element set:     910
    Inclination:       51.6392  deg
    RA of node:       321.8383  deg
    Eccentricity:     .0004924     
    Arg of perigee:   345.8751  deg
    Mean anomaly:      14.2263  deg
    Mean motion:   15.54113211  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2413
    Checksum:              287
 
 
    Coasting Arc #12 (Orbit 2428)
    ---------------------------------------
 
    Vector Time (GMT): 2017/184/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 901313.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5425761.06                 A    =         6788751.65  meter
     Y    =       -3896606.18  meter          E    =           .0016220
     Z    =        1154916.40                 I    =           51.40374
     XDOT =       2007.009601                 Wp   =           41.45325
     YDOT =       4539.550796  meter/sec      RA   =          316.38323  deg
     ZDOT =       5852.039944                 TA   =          331.13712
                                              MA   =          331.22674
                                              Ha   =            221.458  n.mi
                                              Hp   =            214.748
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17801053.34                 X    =         5463320.66
     Y    =      -12784141.00  feet           Y    =        -3835721.74  meter
     Z    =        3789095.80                 Z    =         1181363.90
     XDOT =       6584.677167                 XDOT =        1927.671651
     YDOT =      14893.539358  feet/sec       YDOT =        4561.550347  meter/sec
     ZDOT =      19199.606116                 ZDOT =        5861.597130
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15898549.88                 X    =        -4845878.00
     Y    =      -15054696.44  feet           Y    =        -4588671.47  meter
     Z    =        3906563.07                 Z    =         1190720.42
     XDOT =      12317.051976                 XDOT =        3754.237442
     YDOT =      -7985.519926  feet/sec       YDOT =       -2433.986473  meter/sec
     ZDOT =      19240.932423                 ZDOT =        5864.636203
  
  
    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   17184.56199558  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6410 316.7095 0004904 350.5842   9.5218 15.54122497 24296
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17184.56199558   =   yrday.fracday
    Element set:     911
    Inclination:       51.6410  deg
    RA of node:       316.7095  deg
    Eccentricity:     .0004904     
    Arg of perigee:   350.5842  deg
    Mean anomaly:       9.5218  deg
    Mean motion:   15.54122497  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2429
    Checksum:              318
 
 
    Coasting Arc #13 (Orbit 2443)
    ---------------------------------------
 
    Vector Time (GMT): 2017/185/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 901313.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5486945.49                 A    =         6786063.73  meter
     Y    =        2900134.00  meter          E    =           .0004427
     Z    =       -2751510.16                 I    =           51.37154
     XDOT =       -440.267195                 Wp   =           54.41255
     YDOT =      -5684.521718  meter/sec      RA   =          311.39196  deg
     ZDOT =      -5116.903696                 TA   =          156.83991
                                              MA   =          156.81995
                                              Ha   =            221.641  n.mi
                                              Hp   =            214.555
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18001789.65                 X    =        -5505602.26
     Y    =        9514875.32  feet           Y    =         2838671.25  meter
     Z    =       -9027264.31                 Z    =        -2778209.03
     XDOT =      -1444.446178                 XDOT =        -351.813253
     YDOT =     -18650.005636  feet/sec       YDOT =       -5688.949928  meter/sec
     ZDOT =     -16787.741786                 ZDOT =       -5118.828182
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12988928.83                 X    =         3959025.51
     Y    =       15611971.25  feet           Y    =         4758528.84  meter
     Z    =       -9145647.34                 Z    =        -2787593.31
     XDOT =     -16843.751526                 XDOT =       -5133.975465
     YDOT =       4181.221772  feet/sec       YDOT =        1274.436396  meter/sec
     ZDOT =     -16795.169368                 ZDOT =       -5119.167624
  
  
    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   17185.52653844  .00016717  00000-0  10270-3 0  9129
    2 25544  51.6407 311.9017 0004985 354.7271   5.3828 15.54118573 24442
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17185.52653844   =   yrday.fracday
    Element set:     912
    Inclination:       51.6407  deg
    RA of node:       311.9017  deg
    Eccentricity:     .0004985     
    Arg of perigee:   354.7271  deg
    Mean anomaly:       5.3828  deg
    Mean motion:   15.54118573  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2444
    Checksum:              315
 
 
    Coasting Arc #14 (Orbit 2459)
    ---------------------------------------
 
    Vector Time (GMT): 2017/186/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 901313.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5198290.10                 A    =         6782236.06  meter
     Y    =       -1608673.16  meter          E    =           .0010462
     Z    =        4037556.19                 I    =           51.33858
     XDOT =       -982.783060                 Wp   =           75.27952
     YDOT =       6552.667003  meter/sec      RA   =          306.38983  deg
     ZDOT =       3870.277113                 TA   =          334.45969
                                              MA   =          334.51134
                                              Ha   =            221.506  n.mi
                                              Hp   =            214.505
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17054757.56                 X    =         5196279.92
     Y    =       -5277799.08  feet           Y    =        -1550554.10  meter
     Z    =       13246575.44                 Z    =         4062802.77
     XDOT =      -3224.353870                 XDOT =       -1074.783547
     YDOT =      21498.251323  feet/sec       YDOT =        6541.161964  meter/sec
     ZDOT =      12697.759558                 ZDOT =        3865.280432
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8907479.51                 X    =        -2714999.76
     Y    =      -15375441.88  feet           Y    =        -4686434.69  meter
     Z    =       13358303.59                 Z    =         4071610.94
     XDOT =      20576.364114                 XDOT =        6271.675782
     YDOT =       -892.444518  feet/sec       YDOT =        -272.017089  meter/sec
     ZDOT =      12674.484990                 ZDOT =        3863.183025
  
  
    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   17186.55538042  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6410 306.7733 0004941 357.3787   2.7339 15.54146191 24609
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17186.55538042   =   yrday.fracday
    Element set:     913
    Inclination:       51.6410  deg
    RA of node:       306.7733  deg
    Eccentricity:     .0004941     
    Arg of perigee:   357.3787  deg
    Mean anomaly:       2.7339  deg
    Mean motion:   15.54146191  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2460
    Checksum:              309
 
 
    Coasting Arc #15 (Orbit 2474)
    ---------------------------------------
 
    Vector Time (GMT): 2017/187/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 901313.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4672596.69                 A    =         6778994.33  meter
     Y    =          88150.84  meter          E    =           .0014644
     Z    =       -4923881.27                 I    =           51.30978
     XDOT =       2196.753883                 Wp   =           54.49397
     YDOT =      -6995.671322  meter/sec      RA   =          301.37665  deg
     ZDOT =      -2206.187451                 TA   =          193.82395
                                              MA   =          193.86409
                                              Ha   =            221.803  n.mi
                                              Hp   =            214.274
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15330041.62                 X    =        -4649317.42
     Y    =         289208.79  feet           Y    =           36029.52  meter
     Z    =      -16154466.12                 Z    =        -4946522.68
     XDOT =       7207.197779                 XDOT =        2285.534594
     YDOT =     -22951.677566  feet/sec       YDOT =       -6970.609029  meter/sec
     ZDOT =      -7238.147806                 ZDOT =       -2195.301646
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3909899.95                 X    =         1191737.51
     Y    =       14716226.48  feet           Y    =         4485505.83  meter
     Z    =      -16254413.37                 Z    =        -4954345.20
     XDOT =     -22946.965847                 XDOT =       -6994.235190
     YDOT =      -1856.832927  feet/sec       YDOT =        -565.962676  meter/sec
     ZDOT =      -7188.808144                 ZDOT =       -2191.148722
  
  
    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   17187.51991932  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6419 301.9660 0005029    .8624 359.2536 15.54113909 24758
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17187.51991932   =   yrday.fracday
    Element set:     914
    Inclination:       51.6419  deg
    RA of node:       301.9660  deg
    Eccentricity:     .0005029     
    Arg of perigee:      .8624  deg
    Mean anomaly:     359.2536  deg
    Mean motion:   15.54113909  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2475
    Checksum:              317
 
 
    Coasting Arc #16 (Orbit 2490)
    ---------------------------------------
 
    Vector Time (GMT): 2017/188/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 901313.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3949470.65                 A    =         6777271.40  meter
     Y    =        1559586.10  meter          E    =           .0005386
     Z    =        5279412.20                 I    =           51.28866
     XDOT =      -3173.072837                 Wp   =           32.26775
     YDOT =       6977.257005  meter/sec      RA   =          296.35386  deg
     ZDOT =        316.923594                 TA   =           54.72258
                                              MA   =           54.67221
                                              Ha   =            221.735  n.mi
                                              Hp   =            214.218
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12957580.86                 X    =         3906092.77
     Y    =        5116752.29  feet           Y    =         1603508.48  meter
     Z    =       17320906.18                 Z    =         5298492.26
     XDOT =     -10410.343954                 XDOT =       -3252.397983
     YDOT =      22891.263141  feet/sec       YDOT =        6941.329975  meter/sec
     ZDOT =       1039.775572                 ZDOT =         301.318190
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1671927.49                 X    =          509603.50
     Y    =      -13724803.77  feet           Y    =        -4183320.19  meter
     Z    =       17404834.57                 Z    =         5304993.58
     XDOT =      23790.673439                 XDOT =        7251.397264
     YDOT =       4109.817531  feet/sec       YDOT =        1252.672383  meter/sec
     ZDOT =        969.619267                 ZDOT =         295.539952
  
  
    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   17188.54875502  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6422 296.8369 0005152   4.9903 355.1300 15.54163114 24917
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17188.54875502   =   yrday.fracday
    Element set:     915
    Inclination:       51.6422  deg
    RA of node:       296.8369  deg
    Eccentricity:     .0005152     
    Arg of perigee:     4.9903  deg
    Mean anomaly:     355.1300  deg
    Mean motion:   15.54163114  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2491
    Checksum:              305
 
             

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