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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  24756.99
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   128.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.453
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 1859)
    ---------------------------------------
 
    Vector Time (GMT): 2015/107/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5338449.23                 A    =         6777448.10  meter
     Y    =        -933204.30  meter          E    =           .0006164
     Z    =       -4076004.85                 I    =           51.81009
     XDOT =       3898.525910                 Wp   =          158.28610
     YDOT =       5338.069825  meter/sec      RA   =           26.35793  deg
     ZDOT =       3880.132569                 TA   =          151.82766
                                              MA   =          151.79430
                                              Ha   =            217.588  n.mi
                                              Hp   =            213.758
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17514597.22                 X    =         5368287.76
     Y    =       -3061693.89  feet           Y    =         -873339.88  meter
     Z    =      -13372719.32                 Z    =        -4049998.76
     XDOT =      12790.439338                 XDOT =        3819.696102
     YDOT =      17513.352445  feet/sec       YDOT =        5381.225349  meter/sec
     ZDOT =      12730.093729                 ZDOT =        3898.879059
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10788865.42                 X    =         3288446.18
     Y    =      -14237637.07  feet           Y    =        -4339631.78  meter
     Z    =      -13261024.88                 Z    =        -4041960.38
     XDOT =      20199.779356                 XDOT =        6156.892748
     YDOT =       3364.556091  feet/sec       YDOT =        1025.516697  meter/sec
     ZDOT =      12809.452926                 ZDOT =        3904.321252
  
  
    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   15107.56011412  .00016717  00000-0  10270-3 0  9001
    2 25544  51.6478  26.9199 0005741 232.3396 127.7237 15.55831869 18609
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15107.56011412   =   yrday.fracday
    Element set:     900
    Inclination:       51.6478  deg
    RA of node:        26.9199  deg
    Eccentricity:     .0005741     
    Arg of perigee:   232.3396  deg
    Mean anomaly:     127.7237  deg
    Mean motion:   15.55831869  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1860
    Checksum:              314
 
 
    Coasting Arc #2 (Orbit 1875)
    ---------------------------------------
 
    Vector Time (GMT): 2015/108/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6361368.77                 A    =         6782217.83  meter
     Y    =        -582389.96  meter          E    =           .0011459
     Z    =        2257196.20                 I    =           51.79743
     XDOT =      -1466.169837                 Wp   =          132.39829
     YDOT =      -5189.030865  meter/sec      RA   =           21.37688  deg
     ZDOT =      -5460.798390                 TA   =           22.51657
                                              MA   =           22.46632
                                              Ha   =            217.539  n.mi
                                              Hp   =            213.714
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20870632.44                 X    =        -6365348.36
     Y    =       -1910728.21  feet           Y    =         -653548.98  meter
     Z    =        7405499.35                 Z    =         2226283.76
     XDOT =      -4810.268494                 XDOT =       -1381.508913
     YDOT =     -17024.379477  feet/sec       YDOT =       -5204.953681  meter/sec
     ZDOT =     -17916.005216                 ZDOT =       -5467.714757
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16382798.95                 X    =        -4993477.12
     Y    =       13144656.31  feet           Y    =         4006491.24  meter
     Z    =        7273067.47                 Z    =         2216830.97
     XDOT =     -14240.670681                 XDOT =       -4340.556423
     YDOT =      -7801.193704  feet/sec       YDOT =       -2377.803841  meter/sec
     ZDOT =     -17944.655735                 ZDOT =       -5469.531068
  
  
    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   15108.58780479  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6478  21.7842 0005806 235.0205 125.0404 15.55858500 18763
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15108.58780479   =   yrday.fracday
    Element set:     901
    Inclination:       51.6478  deg
    RA of node:        21.7842  deg
    Eccentricity:     .0005806     
    Arg of perigee:   235.0205  deg
    Mean anomaly:     125.0404  deg
    Mean motion:   15.55858500  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1876
    Checksum:              308
 
 
    Coasting Arc #3 (Orbit 1891)
    ---------------------------------------
 
    Vector Time (GMT): 2015/109/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6507775.06                 A    =         6784051.09  meter
     Y    =        1902735.95  meter          E    =           .0006633
     Z    =         -16317.96                 I    =           51.77509
     XDOT =      -1320.434268                 Wp   =           32.23849
     YDOT =       4558.134215  meter/sec      RA   =           16.40641  deg
     ZDOT =       6025.053596                 TA   =          327.58598
                                              MA   =          327.62671
                                              Ha   =            217.081  n.mi
                                              Hp   =            213.729
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21350968.06                 X    =         6486093.81
     Y    =        6242572.03  feet           Y    =         1975388.92  meter
     Z    =         -53536.61                 Z    =           15243.35
     XDOT =      -4332.133425                 XDOT =       -1400.574284
     YDOT =      14954.508580  feet/sec       YDOT =        4542.920606  meter/sec
     ZDOT =      19767.236208                 ZDOT =        6018.444073
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19521801.25                 X    =         5950245.02
     Y    =      -10664382.63  feet           Y    =        -3250503.82  meter
     Z    =          81411.17                 Z    =           24814.12
     XDOT =       6632.868807                 XDOT =        2021.698412
     YDOT =      12311.200903  feet/sec       YDOT =        3752.454035  meter/sec
     ZDOT =      19738.008192                 ZDOT =        6016.144897
  
  
    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   15109.61545573  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6482  16.6474 0005904 240.7579 119.2985 15.55945702 18926
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15109.61545573   =   yrday.fracday
    Element set:     902
    Inclination:       51.6482  deg
    RA of node:        16.6474  deg
    Eccentricity:     .0005904     
    Arg of perigee:   240.7579  deg
    Mean anomaly:     119.2985  deg
    Mean motion:   15.55945702  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1892
    Checksum:              331
 
 
    Coasting Arc #4 (Orbit 1906)
    ---------------------------------------
 
    Vector Time (GMT): 2015/110/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5663319.74                 A    =         6781769.30  meter
     Y    =       -2960855.41  meter          E    =           .0007033
     Z    =       -2256058.41                 I    =           51.73700
     XDOT =       4039.952096                 Wp   =          191.05055
     YDOT =      -3573.128313  meter/sec      RA   =           11.43437  deg
     ZDOT =      -5455.925030                 TA   =           14.03502
                                              MA   =           14.01549
                                              Ha   =            216.848  n.mi
                                              Hp   =            213.849
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18580445.33                 X    =        -5618830.54
     Y    =       -9714092.56  feet           Y    =        -3023937.71  meter
     Z    =       -7401766.44                 Z    =        -2283462.02
     XDOT =      13254.436011                 XDOT =        4106.110738
     YDOT =     -11722.861919  feet/sec       YDOT =       -3527.581285  meter/sec
     ZDOT =     -17900.016502                 ZDOT =       -5436.138491
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19870365.97                 X    =        -6056487.55
     Y    =        6559025.20  feet           Y    =         1999190.88  meter
     Z    =       -7518672.34                 Z    =        -2291691.33
     XDOT =       1352.025217                 XDOT =         412.097286
     YDOT =     -16310.448347  feet/sec       YDOT =       -4971.424656  meter/sec
     ZDOT =     -17814.483073                 ZDOT =       -5429.854441
  
  
    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   15110.57884637  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6481  11.8322 0006131 244.0290 116.0233 15.55962619 19078
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15110.57884637   =   yrday.fracday
    Element set:     903
    Inclination:       51.6481  deg
    RA of node:        11.8322  deg
    Eccentricity:     .0006131     
    Arg of perigee:   244.0290  deg
    Mean anomaly:     116.0233  deg
    Mean motion:   15.55962619  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1907
    Checksum:              288
 
 
    Coasting Arc #5 (Orbit 1922)
    ---------------------------------------
 
    Vector Time (GMT): 2015/111/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3930631.68                 A    =         6776597.15  meter
     Y    =        3700332.30  meter          E    =           .0006550
     Z    =        4095554.41                 I    =           51.68880
     XDOT =      -6213.965591                 Wp   =          134.33001
     YDOT =       2347.150846  meter/sec      RA   =            6.44448  deg
     ZDOT =       3834.822265                 TA   =          276.04963
                                              MA   =          276.12426
                                              Ha   =            216.534  n.mi
                                              Hp   =            213.796
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12895773.23                 X    =         3869066.56
     Y    =       12140197.85  feet           Y    =         3743943.09  meter
     Z    =       13436858.29                 Z    =         4114499.32
     XDOT =     -20387.026218                 XDOT =       -6258.378585
     YDOT =       7700.626134  feet/sec       YDOT =        2277.414009  meter/sec
     ZDOT =      12581.437878                 ZDOT =        3804.527590
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17617797.99                 X    =         5369904.83
     Y    =       -1062569.64  feet           Y    =         -323871.23  meter
     Z    =       13517347.06                 Z    =         4120087.38
     XDOT =      -8432.506034                 XDOT =       -2570.227839
     YDOT =      18923.874361  feet/sec       YDOT =        5767.996905  meter/sec
     ZDOT =      12451.095409                 ZDOT =        3795.093881
  
  
    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   15111.60642723  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6478   6.6948 0005934 249.0783 110.9736 15.56028953 19236
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15111.60642723   =   yrday.fracday
    Element set:     904
    Inclination:       51.6478  deg
    RA of node:         6.6948  deg
    Eccentricity:     .0005934     
    Arg of perigee:   249.0783  deg
    Mean anomaly:     110.9736  deg
    Mean motion:   15.56028953  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1923
    Checksum:              320
 
 
    Coasting Arc #6 (Orbit 1937)
    ---------------------------------------
 
    Vector Time (GMT): 2015/112/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1532672.39                 A    =         6772209.43  meter
     Y    =       -4121211.50  meter          E    =           .0007792
     Z    =       -5157542.52                 I    =           51.64258
     XDOT =       7465.705594                 Wp   =           83.51412
     YDOT =       -961.856473  meter/sec      RA   =            1.43345  deg
     ZDOT =      -1451.028043                 TA   =          172.52355
                                              MA   =          172.51192
                                              Ha   =            216.203  n.mi
                                              Hp   =            213.753
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5028452.73                 X    =        -1461420.38
     Y    =      -13521035.09  feet           Y    =        -4137952.54  meter
     Z    =      -16921071.27                 Z    =        -5164814.91
     XDOT =      24493.784756                 XDOT =        7482.955074
     YDOT =      -3155.697089  feet/sec       YDOT =        -878.273653  meter/sec
     ZDOT =      -4760.590692                 ZDOT =       -1414.718704
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13332703.30                 X    =        -4063807.97
     Y    =       -5414276.47  feet           Y    =        -1650271.47  meter
     Z    =      -16951430.99                 Z    =        -5166796.17
     XDOT =      13704.053624                 XDOT =        4176.995544
     YDOT =     -19339.962461  feet/sec       YDOT =       -5894.820558  meter/sec
     ZDOT =      -4604.739502                 ZDOT =       -1403.524600
  
  
    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   15112.56974901  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6471   1.8782 0006144 253.4608 106.5871 15.56119742 19385
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15112.56974901   =   yrday.fracday
    Element set:     905
    Inclination:       51.6471  deg
    RA of node:         1.8782  deg
    Eccentricity:     .0006144     
    Arg of perigee:   253.4608  deg
    Mean anomaly:     106.5871  deg
    Mean motion:   15.56119742  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1938
    Checksum:              312
 
 
    Coasting Arc #7 (Orbit 1953)
    ---------------------------------------
 
    Vector Time (GMT): 2015/113/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1123661.20                 A    =         6771939.78  meter
     Y    =        4196374.25  meter          E    =           .0002805
     Z    =        5197355.63                 I    =           51.61056
     XDOT =      -7554.352757                 Wp   =          289.33036
     YDOT =       -501.222096  meter/sec      RA   =          356.41143  deg
     ZDOT =      -1228.183178                 TA   =          172.46009
                                              MA   =          172.45587
                                              Ha   =            215.952  n.mi
                                              Hp   =            213.791
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3686552.49                 X    =        -1195749.60
     Y    =       13767632.06  feet           Y    =         4183405.74  meter
     Z    =       17051691.69                 Z    =         5191721.88
     XDOT =     -24784.621907                 XDOT =       -7542.220401
     YDOT =      -1644.429448  feet/sec       YDOT =        -585.631986  meter/sec
     ZDOT =      -4029.472368                 ZDOT =       -1264.851644
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7878738.24                 X    =         2401439.42
     Y    =       11912820.79  feet           Y    =         3631027.78  meter
     Z    =       17026706.54                 Z    =         5189740.15
     XDOT =     -16650.330208                 XDOT =       -5075.020647
     YDOT =      16997.457269  feet/sec       YDOT =        5180.824975  meter/sec
     ZDOT =      -4186.568866                 ZDOT =       -1276.066190
  
  
    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   15113.59725819  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6473 356.7408 0006256 256.9593 103.0862 15.56172900 19544
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15113.59725819   =   yrday.fracday
    Element set:     906
    Inclination:       51.6473  deg
    RA of node:       356.7408  deg
    Eccentricity:     .0006256     
    Arg of perigee:   256.9593  deg
    Mean anomaly:     103.0862  deg
    Mean motion:   15.56172900  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1954
    Checksum:              328
 
 
    Coasting Arc #8 (Orbit 1968)
    ---------------------------------------
 
    Vector Time (GMT): 2015/114/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3607142.32                 A    =         6775860.27  meter
     Y    =       -3912242.33  meter          E    =           .0003800
     Z    =       -4198059.53                 I    =           51.59136
     XDOT =       6429.805073                 Wp   =          162.91644
     YDOT =       1977.222290  meter/sec      RA   =          351.39327  deg
     ZDOT =       3679.432676                 TA   =          144.85929
                                              MA   =          144.83422
                                              Ha   =            215.665  n.mi
                                              Hp   =            213.838
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11834456.44                 X    =         3671014.60
     Y    =      -12835440.72  feet           Y    =        -3871547.86  meter
     Z    =      -13773161.18                 Z    =        -4180381.38
     XDOT =      21095.161000                 XDOT =        6389.343990
     YDOT =       6486.949769  feet/sec       YDOT =        2048.898416  meter/sec
     ZDOT =      12071.629513                 ZDOT =        3710.569327
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2131799.24                 X    =         -649772.41
     Y    =      -17388542.60  feet           Y    =        -5300027.78  meter
     Z    =      -13696601.21                 Z    =        -4174724.05
     XDOT =      17238.743907                 XDOT =        5254.369143
     YDOT =     -11733.879026  feet/sec       YDOT =       -3576.486327  meter/sec
     ZDOT =      12204.714568                 ZDOT =        3719.997000
  
  
    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   15114.56051567  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6463 351.9231 0006351 260.8410  99.2026 15.56216787 19698
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15114.56051567   =   yrday.fracday
    Element set:     907
    Inclination:       51.6463  deg
    RA of node:       351.9231  deg
    Eccentricity:     .0006351     
    Arg of perigee:   260.8410  deg
    Mean anomaly:      99.2026  deg
    Mean motion:   15.56216787  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1969
    Checksum:              313
 
 
    Coasting Arc #9 (Orbit 1984)
    ---------------------------------------
 
    Vector Time (GMT): 2015/115/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5483208.47                 A    =         6780816.02  meter
     Y    =        3228300.71  meter          E    =           .0008277
     Z    =        2329419.18                 I    =           51.57777
     XDOT =      -4282.740169                 Wp   =          123.76393
     YDOT =      -3370.757473  meter/sec      RA   =          346.39339  deg
     ZDOT =      -5400.359997                 TA   =           30.20890
                                              MA   =           30.16120
                                              Ha   =            215.393  n.mi
                                              Hp   =            213.661
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17989529.10                 X    =        -5530216.08
     Y    =       10591537.78  feet           Y    =         3166721.13  meter
     Z    =        7642451.39                 Z    =         2302668.39
     XDOT =     -14050.984806                 XDOT =       -4218.496182
     YDOT =     -11058.915593  feet/sec       YDOT =       -3418.290834  meter/sec
     ZDOT =     -17717.716526                 ZDOT =       -5421.008682
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3170860.09                 X    =         -966478.16
     Y    =       20676041.88  feet           Y    =         6302057.56  meter
     Z    =        7527139.65                 Z    =         2294272.17
     XDOT =     -15869.035087                 XDOT =       -4836.881895
     YDOT =       4059.740291  feet/sec       YDOT =        1237.408841  meter/sec
     ZDOT =     -17805.563066                 ZDOT =       -5427.135622
  
  
    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   15115.58795479  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6466 346.7855 0006377 265.9461  94.0964 15.56289987 19859
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15115.58795479   =   yrday.fracday
    Element set:     908
    Inclination:       51.6466  deg
    RA of node:       346.7855  deg
    Eccentricity:     .0006377     
    Arg of perigee:   265.9461  deg
    Mean anomaly:      94.0964  deg
    Mean motion:   15.56289987  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1985
    Checksum:              385
 
 
    Coasting Arc #10 (Orbit 2000)
    ---------------------------------------
 
    Vector Time (GMT): 2015/116/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6430094.49                 A    =         6782989.88  meter
     Y    =       -2141314.31  meter          E    =           .0008660
     Z    =          26289.38                 I    =           51.55344
     XDOT =       1483.515851                 Wp   =           15.35763
     YDOT =       4534.044091  meter/sec      RA   =          341.40505  deg
     ZDOT =       6008.721374                 TA   =          344.92615
                                              MA   =          344.95194
                                              Ha   =            215.221  n.mi
                                              Hp   =            213.592
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21096110.52                 X    =         6453433.57
     Y    =       -7025309.43  feet           Y    =        -2069278.30  meter
     Z    =          86251.26                 Z    =           57582.48
     XDOT =       4867.177990                 XDOT =        1403.516564
     YDOT =      14875.472740  feet/sec       YDOT =        4550.186696  meter/sec
     ZDOT =      19713.652802                 ZDOT =        6015.733533
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7508431.88                 X    =         2288570.04
     Y    =      -20928043.00  feet           Y    =        -6378867.51  meter
     Z    =         220811.93                 Z    =           67303.48
     XDOT =      13101.949544                 XDOT =        3993.474221
     YDOT =       4914.959873  feet/sec       YDOT =        1498.079769  meter/sec
     ZDOT =      19742.815087                 ZDOT =        6017.610038
  
  
    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   15116.61535894  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6453 341.6461 0006481 268.8575  91.1836 15.56311767 20014
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15116.61535894   =   yrday.fracday
    Element set:     909
    Inclination:       51.6453  deg
    RA of node:       341.6461  deg
    Eccentricity:     .0006481     
    Arg of perigee:   268.8575  deg
    Mean anomaly:      91.1836  deg
    Mean motion:   15.56311767  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2001
    Checksum:              319
 
 
    Coasting Arc #11 (Orbit 2015)
    ---------------------------------------
 
    Vector Time (GMT): 2015/117/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6303285.85                 A    =         6780321.98  meter
     Y    =         671237.62  meter          E    =           .0004231
     Z    =       -2398409.56                 I    =           51.51470
     XDOT =       1475.000514                 Wp   =          215.77623
     YDOT =      -5289.662401  meter/sec      RA   =          336.41555  deg
     ZDOT =      -5355.452879                 TA   =          351.10141
                                              MA   =          351.10891
                                              Ha   =            215.114  n.mi
                                              Hp   =            213.526
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20680071.68                 X    =        -6298672.67
     Y    =        2202223.17  feet           Y    =          600775.83  meter
     Z    =       -7868797.76                 Z    =        -2429018.71
     XDOT =       4839.240531                 XDOT =        1560.056095
     YDOT =     -17354.535437  feet/sec       YDOT =       -5272.692696  meter/sec
     ZDOT =     -17570.383461                 ZDOT =       -5348.080692
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10709920.99                 X    =        -3264383.92
     Y    =       17768754.96  feet           Y    =         5415916.51  meter
     Z    =       -8000129.33                 Z    =        -2438439.42
     XDOT =      -9543.247537                 XDOT =       -2908.781849
     YDOT =     -13650.267212  feet/sec       YDOT =       -4160.601446  meter/sec
     ZDOT =     -17537.743845                 ZDOT =       -5345.504324
  
  
    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   15117.57851747  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6447 336.8292 0006549 272.4631  87.5773 15.56359687 20162
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15117.57851747   =   yrday.fracday
    Element set:     910
    Inclination:       51.6447  deg
    RA of node:       336.8292  deg
    Eccentricity:     .0006549     
    Arg of perigee:   272.4631  deg
    Mean anomaly:      87.5773  deg
    Mean motion:   15.56359687  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2016
    Checksum:              343
 
 
    Coasting Arc #12 (Orbit 2031)
    ---------------------------------------
 
    Vector Time (GMT): 2015/118/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5155311.60                 A    =         6774867.58  meter
     Y    =        1058389.88  meter          E    =           .0003537
     Z    =        4265283.48                 I    =           51.46778
     XDOT =      -4066.081599                 Wp   =          127.96331
     YDOT =       5444.669937  meter/sec      RA   =          331.40536  deg
     ZDOT =       3559.350225                 TA   =          285.63668
                                              MA   =          285.67571
                                              Ha   =            215.052  n.mi
                                              Hp   =            213.563
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16913751.96                 X    =         5122373.96
     Y    =        3472407.73  feet           Y    =         1115856.04  meter
     Z    =       13993712.19                 Z    =         4290247.11
     XDOT =     -13340.162728                 XDOT =       -4143.953124
     YDOT =      17863.090346  feet/sec       YDOT =        5398.765165  meter/sec
     ZDOT =      11677.658220                 ZDOT =        3539.408359
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12736721.03                 X    =         3882152.57
     Y    =      -11528591.96  feet           Y    =        -3513914.83  meter
     Z    =       14100500.21                 Z    =         4297832.46
     XDOT =       5658.281823                 XDOT =        1724.644300
     YDOT =      20444.737323  feet/sec       YDOT =        6231.555936  meter/sec
     ZDOT =      11591.120357                 ZDOT =        3532.973485
  
  
    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   15118.60585253  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6442 331.6893 0006630 276.7525  83.2875 15.56403721 20320
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15118.60585253   =   yrday.fracday
    Element set:     911
    Inclination:       51.6442  deg
    RA of node:       331.6893  deg
    Eccentricity:     .0006630     
    Arg of perigee:   276.7525  deg
    Mean anomaly:      83.2875  deg
    Mean motion:   15.56403721  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2032
    Checksum:              303
 
 
    Coasting Arc #13 (Orbit 2046)
    ---------------------------------------
 
    Vector Time (GMT): 2015/119/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3234459.05                 A    =         6770832.57  meter
     Y    =       -2854357.69  meter          E    =           .0008403
     Z    =       -5225965.40                 I    =           51.42640
     XDOT =       5862.892490                 Wp   =           69.40116
     YDOT =      -4840.799325  meter/sec      RA   =          326.37348  deg
     ZDOT =       -983.065124                 TA   =          191.14931
                                              MA   =          191.16794
                                              Ha   =            215.231  n.mi
                                              Hp   =            213.325
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10611742.29                 X    =        -3176914.49
     Y    =       -9364690.57  feet           Y    =        -2890206.10  meter
     Z    =      -17145555.79                 Z    =        -5241537.99
     XDOT =      19235.211581                 XDOT =        5921.363129
     YDOT =     -15881.887548  feet/sec       YDOT =       -4774.909761  meter/sec
     ZDOT =      -3225.279279                 ZDOT =        -954.441697
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13707603.22                 X    =        -4178077.46
     Y    =        3183426.10  feet           Y    =          970308.28  meter
     Z    =      -17211740.16                 Z    =        -5246138.40
     XDOT =      -1646.922173                 XDOT =        -501.981878
     YDOT =     -23889.760215  feet/sec       YDOT =       -7281.598913  meter/sec
     ZDOT =      -3101.661441                 ZDOT =        -945.386407
  
  
    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   15119.56894604  .00016717  00000-0  10270-3 0  9129
    2 25544  51.6432 326.8710 0006521 279.5190  80.5226 15.56472077 20477
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15119.56894604   =   yrday.fracday
    Element set:     912
    Inclination:       51.6432  deg
    RA of node:       326.8710  deg
    Eccentricity:     .0006521     
    Arg of perigee:   279.5190  deg
    Mean anomaly:      80.5226  deg
    Mean motion:   15.56472077  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2047
    Checksum:              310
 
 
    Coasting Arc #14 (Orbit 2062)
    ---------------------------------------
 
    Vector Time (GMT): 2015/120/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         903914.47                 A    =         6771607.91  meter
     Y    =        4431663.46  meter          E    =           .0004995
     Z    =        5042552.90                 I    =           51.40323
     XDOT =      -6614.085299                 Wp   =          337.84435
     YDOT =       3428.467291  meter/sec      RA   =          321.33277  deg
     ZDOT =      -1823.546025                 TA   =          129.88823
                                              MA   =          129.84430
                                              Ha   =            215.428  n.mi
                                              Hp   =            213.496
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2965598.64                 X    =          829796.19
     Y    =       14539578.28  feet           Y    =         4441357.51  meter
     Z    =       16543808.72                 Z    =         5046763.70
     XDOT =     -21699.754919                 XDOT =       -6643.073433
     YDOT =      11248.252268  feet/sec       YDOT =        3354.342070  meter/sec
     ZDOT =      -5982.762550                 ZDOT =       -1855.747036
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13633114.19                 X    =         4155373.21
     Y    =        5810628.63  feet           Y    =         1771079.61  meter
     Z    =       16560993.66                 Z    =         5047790.87
     XDOT =      -2454.692379                 XDOT =        -748.190237
     YDOT =      23242.995980  feet/sec       YDOT =        7084.465175  meter/sec
     ZDOT =      -6121.427078                 ZDOT =       -1865.810973
  
  
    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   15120.59621173  .00016717  00000-0  10270-3 0  9134
    2 25544  51.6432 321.7315 0006627 283.1206  76.9208 15.56500126 20632
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15120.59621173   =   yrday.fracday
    Element set:     913
    Inclination:       51.6432  deg
    RA of node:       321.7315  deg
    Eccentricity:     .0006627     
    Arg of perigee:   283.1206  deg
    Mean anomaly:      76.9208  deg
    Mean motion:   15.56500126  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2063
    Checksum:              280
 
 
    Coasting Arc #15 (Orbit 2077)
    ---------------------------------------
 
    Vector Time (GMT): 2015/121/13:13:50.043
    Vector Time (MET): N/A
    Weight (LBS)     : 923717.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1399401.62                 A    =         6776293.27  meter
     Y    =       -5471498.92  meter          E    =           .0000879
     Z    =       -3743589.25                 I    =           51.39504
     XDOT =       6258.978537                 Wp   =          317.91713
     YDOT =      -1299.504826  meter/sec      RA   =          316.30128  deg
     ZDOT =       4239.059042                 TA   =          357.09094
                                              MA   =          357.09145
                                              Ha   =            215.511  n.mi
                                              Hp   =            213.321
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4591212.66                 X    =         1478666.48
     Y    =      -17951111.94  feet           Y    =        -5455406.90  meter
     Z    =      -12282116.96                 Z    =        -3736598.28
     XDOT =      20534.706485                 XDOT =        6252.452609
     YDOT =      -4263.467277  feet/sec       YDOT =       -1229.549094  meter/sec
     ZDOT =      13907.674023                 ZDOT =        4269.448686
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12458471.78                 X    =        -3797342.20
     Y    =      -13742965.09  feet           Y    =        -4188855.76  meter
     Z    =      -12251099.63                 Z    =        -3734135.17
     XDOT =       6636.308358                 XDOT =        2022.746788
     YDOT =     -18530.105599  feet/sec       YDOT =       -5647.976187  meter/sec
     ZDOT =      14038.154558                 ZDOT =        4278.829509
  
  
    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   15121.55924038  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6428 316.9120 0006565 286.5726  73.4706 15.56575503 20784
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15121.55924038   =   yrday.fracday
    Element set:     914
    Inclination:       51.6428  deg
    RA of node:       316.9120  deg
    Eccentricity:     .0006565     
    Arg of perigee:   286.5726  deg
    Mean anomaly:      73.4706  deg
    Mean motion:   15.56575503  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2078
    Checksum:              316
 
             

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