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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  17659.2707
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   101.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.975
   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 
   ------------------------------------------------------------------------
   132/13:26:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.9  
   000/00:00:00.000           0.0               0.0              213.5  
   
   135/07:32:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.9  
   000/00:00:00.000           0.0               0.0              213.1  
   
 
 
    Coasting Arc #1 (Orbit 3818)
    ---------------------------------------
 
    Vector Time (GMT): 2016/125/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3200427.03                 A    =         6783341.74  meter
     Y    =       -4894661.40  meter          E    =           .0014021
     Z    =        3425030.34                 I    =           51.27632
     XDOT =       3189.857169                 Wp   =           90.69731
     YDOT =       5285.277919  meter/sec      RA   =          275.17058  deg
     ZDOT =       4556.069982                 TA   =          309.67626
                                              MA   =          309.79983
                                              Ha   =            221.034  n.mi
                                              Hp   =            213.518
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10500088.67                 X    =         3238284.87
     Y    =      -16058600.41  feet           Y    =        -4858660.28  meter
     Z    =       11236976.18                 Z    =         3440669.65
     XDOT =      10465.410659                 XDOT =        3108.386970
     YDOT =      17340.150653  feet/sec       YDOT =        5320.493686  meter/sec
     ZDOT =      14947.736163                 ZDOT =        4571.367684
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2980257.87                 X    =         -908382.60
     Y    =      -18912889.99  feet           Y    =        -5764648.87  meter
     Z    =       11305786.04                 Z    =         3446003.59
     XDOT =      17925.483889                 XDOT =        5463.687489
     YDOT =       6181.858850  feet/sec       YDOT =        1884.230577  meter/sec
     ZDOT =      15013.191026                 ZDOT =        4576.020625
  
  
    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   16125.55707577  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6400 275.6799 0001678  91.6122 268.5223 15.54454875 38193
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16125.55707577   =   yrday.fracday
    Element set:     900
    Inclination:       51.6400  deg
    RA of node:       275.6799  deg
    Eccentricity:     .0001678     
    Arg of perigee:    91.6122  deg
    Mean anomaly:     268.5223  deg
    Mean motion:   15.54454875  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3819
    Checksum:              332
 
 
    Coasting Arc #2 (Orbit 3833)
    ---------------------------------------
 
    Vector Time (GMT): 2016/126/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3697559.82                 A    =         6779333.04  meter
     Y    =        3354948.98  meter          E    =           .0011985
     Z    =       -4597747.33                 I    =           51.26203
     XDOT =      -2359.185362                 Wp   =           72.90077
     YDOT =      -6656.818664  meter/sec      RA   =          270.15456  deg
     ZDOT =      -2963.122084                 TA   =          167.37878
                                              MA   =          167.34875
                                              Ha   =            221.124  n.mi
                                              Hp   =            213.374
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12131101.78                 X    =        -3712466.53
     Y    =       11007050.45  feet           Y    =         3313516.94  meter
     Z    =      -15084472.86                 Z    =        -4615745.83
     XDOT =      -7740.109454                 XDOT =       -2270.177933
     YDOT =     -21839.956246  feet/sec       YDOT =       -6682.703051  meter/sec
     ZDOT =      -9721.529146                 ZDOT =       -2974.366297
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1312220.35                 X    =         -399964.76
     Y    =       16254670.47  feet           Y    =         4954423.56  meter
     Z    =      -15163240.99                 Z    =        -4621755.85
     XDOT =     -19313.680317                 XDOT =       -5886.809760
     YDOT =     -10663.329506  feet/sec       YDOT =       -3250.182833  meter/sec
     ZDOT =      -9769.138464                 ZDOT =       -2977.633404
  
  
    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   16126.52141115  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6410 270.8707 0001788  89.4782 270.6576 15.54457258 38349
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16126.52141115   =   yrday.fracday
    Element set:     901
    Inclination:       51.6410  deg
    RA of node:       270.8707  deg
    Eccentricity:     .0001788     
    Arg of perigee:    89.4782  deg
    Mean anomaly:     270.6576  deg
    Mean motion:   15.54457258  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3834
    Checksum:              317
 
 
    Coasting Arc #3 (Orbit 3849)
    ---------------------------------------
 
    Vector Time (GMT): 2016/127/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4060236.60                 A    =         6776683.63  meter
     Y    =       -1525659.13  meter          E    =           .0005233
     Z    =        5202896.91                 I    =           51.25417
     XDOT =       1470.652960                 Wp   =          113.35670
     YDOT =       7458.785611  meter/sec      RA   =          265.12789  deg
     ZDOT =       1036.618801                 TA   =          326.65138
                                              MA   =          326.68434
                                              Ha   =            220.921  n.mi
                                              Hp   =            213.492
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13320986.21                 X    =         4051721.12
     Y    =       -5005443.33  feet           Y    =        -1480302.46  meter
     Z    =       17069871.74                 Z    =         5222600.29
     XDOT =       4824.976902                 XDOT =        1382.102090
     YDOT =      24471.081400  feet/sec       YDOT =        7474.736315  meter/sec
     ZDOT =       3400.980319                 ZDOT =        1043.547930
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6043772.05                 X    =         1842141.72
     Y    =      -12768636.82  feet           Y    =        -3891880.50  meter
     Z    =       17155710.15                 Z    =         5229060.45
     XDOT =      19504.513104                 XDOT =        5944.975594
     YDOT =      13852.759697  feet/sec       YDOT =        4222.321156  meter/sec
     ZDOT =       3429.713103                 ZDOT =        1045.376554
  
  
    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   16127.55002544  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6410 265.7402 0001693  92.5824 267.5523 15.54479914 38509
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16127.55002544   =   yrday.fracday
    Element set:     902
    Inclination:       51.6410  deg
    RA of node:       265.7402  deg
    Eccentricity:     .0001693     
    Arg of perigee:    92.5824  deg
    Mean anomaly:     267.5523  deg
    Mean motion:   15.54479914  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3850
    Checksum:              304
 
 
    Coasting Arc #4 (Orbit 3864)
    ---------------------------------------
 
    Vector Time (GMT): 2016/128/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4322583.39                 A    =         6776645.79  meter
     Y    =        -426807.87  meter          E    =           .0016100
     Z    =       -5215738.85                 I    =           51.25844
     XDOT =       -487.539063                 Wp   =           97.82102
     YDOT =      -7572.575700  meter/sec      RA   =          260.09871  deg
     ZDOT =       1024.296452                 TA   =          182.05111
                                              MA   =          182.05772
                                              Ha   =            221.067  n.mi
                                              Hp   =            213.284
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14181704.05                 X    =        -4292153.09
     Y    =       -1400288.27  feet           Y    =         -474975.60  meter
     Z    =      -17112004.12                 Z    =        -5236663.44
     XDOT =      -1599.537608                 XDOT =        -407.800094
     YDOT =     -24844.408463  feet/sec       YDOT =       -7577.581863  meter/sec
     ZDOT =       3360.552663                 ZDOT =        1022.121555
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10955089.56                 X    =        -3339111.30
     Y    =        8941590.81  feet           Y    =         2725396.88  meter
     Z    =      -17202795.94                 Z    =        -5243412.20
     XDOT =     -18036.151236                 XDOT =       -5497.418897
     YDOT =     -15651.345672  feet/sec       YDOT =       -4770.530161  meter/sec
     ZDOT =       3352.478968                 ZDOT =        1021.835590
  
  
    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   16128.51434377  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6416 260.9319 0001764  96.8588 263.2766 15.54491937 38659
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16128.51434377   =   yrday.fracday
    Element set:     903
    Inclination:       51.6416  deg
    RA of node:       260.9319  deg
    Eccentricity:     .0001764     
    Arg of perigee:    96.8588  deg
    Mean anomaly:     263.2766  deg
    Mean motion:   15.54491937  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3865
    Checksum:              345
 
 
    Coasting Arc #5 (Orbit 3880)
    ---------------------------------------
 
    Vector Time (GMT): 2016/129/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4420431.91                 A    =         6779297.71  meter
     Y    =        2312838.82  meter          E    =           .0009964
     Z    =        4583532.87                 I    =           51.27456
     XDOT =       -591.687879                 Wp   =           71.31977
     YDOT =       7047.162534  meter/sec      RA   =          255.07199  deg
     ZDOT =      -2976.883443                 TA   =           48.54455
                                              MA   =           48.45902
                                              Ha   =            220.996  n.mi
                                              Hp   =            213.455
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14502729.36                 X    =         4371975.39
     Y    =        7588053.89  feet           Y    =         2361999.89  meter
     Z    =       15037837.49                 Z    =         4604889.02
     XDOT =      -1941.233199                 XDOT =        -655.986352
     YDOT =      23120.611988  feet/sec       YDOT =        7040.186508  meter/sec
     ZDOT =      -9766.677961                 ZDOT =       -2979.913622
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15475562.62                 X    =         4716951.49
     Y    =       -5062523.88  feet           Y    =        -1543057.28  meter
     Z    =       15130171.52                 Z    =         4611676.28
     XDOT =      14925.485348                 XDOT =        4549.287934
     YDOT =      16310.617789  feet/sec       YDOT =        4971.476302  meter/sec
     ZDOT =      -9781.107688                 ZDOT =       -2981.281623
  
  
    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   16129.54293949  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6426 255.8011 0001827  99.2241 260.9119 15.54470518 38811
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16129.54293949   =   yrday.fracday
    Element set:     904
    Inclination:       51.6426  deg
    RA of node:       255.8011  deg
    Eccentricity:     .0001827     
    Arg of perigee:    99.2241  deg
    Mean anomaly:     260.9119  deg
    Mean motion:   15.54470518  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3881
    Checksum:              320
 
 
    Coasting Arc #6 (Orbit 3895)
    ---------------------------------------
 
    Vector Time (GMT): 2016/130/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4345417.67                 A    =         6783208.50  meter
     Y    =       -3928836.43  meter          E    =           .0006637
     Z    =       -3425725.28                 I    =           51.29697
     XDOT =       1746.539910                 Wp   =           93.26540
     YDOT =      -5903.145990  meter/sec      RA   =          250.05761  deg
     ZDOT =       4561.973190                 TA   =          226.43013
                                              MA   =          226.48526
                                              Ha   =            221.011  n.mi
                                              Hp   =            213.395
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14256619.65                 X    =        -4284520.55
     Y    =      -12889883.31  feet           Y    =        -3977089.09  meter
     Z    =      -11239256.16                 Z    =        -3446686.84
     XDOT =       5730.117815                 XDOT =        1790.260146
     YDOT =     -19367.276870  feet/sec       YDOT =       -5883.370827  meter/sec
     ZDOT =      14967.103643                 ZDOT =        4570.563417
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19104495.31                 X    =        -5823050.17
     Y    =        1542604.09  feet           Y    =          470185.73  meter
     Z    =      -11329598.67                 Z    =        -3453261.68
     XDOT =     -10173.005336                 XDOT =       -3100.732026
     YDOT =     -15955.777352  feet/sec       YDOT =       -4863.320937  meter/sec
     ZDOT =      15005.471354                 ZDOT =        4573.667669
  
  
    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   16130.50723514  .00016717  00000-0  10270-3 0  9050
    2 25544  51.6425 250.9927 0001684  97.0628 263.0717 15.54494649 38963
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16130.50723514   =   yrday.fracday
    Element set:     905
    Inclination:       51.6425  deg
    RA of node:       250.9927  deg
    Eccentricity:     .0001684     
    Arg of perigee:    97.0628  deg
    Mean anomaly:     263.0717  deg
    Mean motion:   15.54494649  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3896
    Checksum:              327
 
 
    Coasting Arc #7 (Orbit 3911)
    ---------------------------------------
 
    Vector Time (GMT): 2016/131/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4004341.90                 A    =         6786763.52  meter
     Y    =        5159954.67  meter          E    =           .0015704
     Z    =        1816937.29                 I    =           51.32021
     XDOT =      -2967.182512                 Wp   =          113.07394
     YDOT =       4294.087407  meter/sec      RA   =          245.05501  deg
     ZDOT =      -5622.736180                 TA   =           46.84734
                                              MA   =           46.71616
                                              Ha   =            220.979  n.mi
                                              Hp   =            213.402
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13137604.66                 X    =         3937518.40
     Y    =       16928985.15  feet           Y    =         5204360.15  meter
     Z    =        5961080.35                 Z    =         1836227.56
     XDOT =      -9734.850762                 XDOT =       -2987.666445
     YDOT =      14088.213277  feet/sec       YDOT =        4260.792193  meter/sec
     ZDOT =     -18447.297177                 ZDOT =       -5637.199656
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21342282.08                 X    =         6505127.58
     Y    =        1642930.68  feet           Y    =          500765.27  meter
     Z    =        6043959.60                 Z    =         1842198.89
     XDOT =       4115.551695                 XDOT =        1254.420157
     YDOT =      15024.676347  feet/sec       YDOT =        4579.521351  meter/sec
     ZDOT =     -18510.887263                 ZDOT =       -5642.118438
  
  
    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   16131.53580776  .00016717  00000-0  10270-3 0  9066
    2 25544  51.6418 245.8626 0001763 105.6797 254.4551 15.54517237 39123
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16131.53580776   =   yrday.fracday
    Element set:     906
    Inclination:       51.6418  deg
    RA of node:       245.8626  deg
    Eccentricity:     .0001763     
    Arg of perigee:   105.6797  deg
    Mean anomaly:     254.4551  deg
    Mean motion:   15.54517237  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3912
    Checksum:              323
 
 
    Coasting Arc #8 (Orbit 3926)
    ---------------------------------------
 
    Vector Time (GMT): 2016/132/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 945238.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3399084.35                 A    =         6788119.81  meter
     Y    =       -5869421.19  meter          E    =           .0013073
     Z    =         -20242.22                 I    =           51.34052
     XDOT =       4140.805687                 Wp   =           51.75809
     YDOT =      -2409.546249  meter/sec      RA   =          240.06091  deg
     ZDOT =       5988.565849                 TA   =          308.02293
                                              MA   =          308.14088
                                              Ha   =            220.951  n.mi
                                              Hp   =            213.389
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11151851.54                 X    =        -3333100.06
     Y    =      -19256631.21  feet           Y    =        -5907063.07  meter
     Z    =         -66411.50                 Z    =          -36594.26
     XDOT =      13585.320496                 XDOT =        4138.352016
     YDOT =      -7905.335463  feet/sec       YDOT =       -2363.255022  meter/sec
     ZDOT =      19647.525750                 ZDOT =        6008.674902
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21838146.67                 X    =        -6656267.10
     Y    =       -4273498.44  feet           Y    =        -1302562.32  meter
     Z    =        -136418.67                 Z    =          -41580.41
     XDOT =       2592.388827                 XDOT =         790.160114
     YDOT =     -13742.619480  feet/sec       YDOT =       -4188.750417  meter/sec
     ZDOT =      19735.310109                 ZDOT =        6015.322521
  
  
    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   16132.50008290  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6430 241.0533 0001731 101.5264 258.6084 15.54543881 39278
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16132.50008290   =   yrday.fracday
    Element set:     907
    Inclination:       51.6430  deg
    RA of node:       241.0533  deg
    Eccentricity:     .0001731     
    Arg of perigee:   101.5264  deg
    Mean anomaly:     258.6084  deg
    Mean motion:   15.54543881  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3927
    Checksum:              283
 
 
    Coasting Arc #9 (Orbit 3927)
    ---------------------------------------
 
    Vector Time (GMT): 2016/132/13:26:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4669916.63                 A    =         6785874.69  meter
     Y    =       -4351618.69  meter          E    =           .0006792
     Z    =       -2300827.09                 I    =           51.33367
     XDOT =       2052.327495                 Wp   =           55.48497
     YDOT =      -5045.687692  meter/sec      RA   =          239.74329  deg
     ZDOT =       5392.677698                 TA   =          278.77459
                                              MA   =          278.85151
                                              Ha   =            220.894  n.mi
                                              Hp   =            213.450
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15321248.80                 X    =        -4609732.17
     Y    =      -14276964.20  feet           Y    =        -4403504.18  meter
     Z    =       -7548645.30                 Z    =        -2323366.55
     XDOT =       6733.357923                 XDOT =        2082.401628
     YDOT =     -16554.093478  feet/sec       YDOT =       -5022.569310  meter/sec
     ZDOT =      17692.512132                 ZDOT =        5402.720257
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18571473.11                 X    =        -5660585.01
     Y    =        9601902.64  feet           Y    =         2926659.93  meter
     Z    =       -7645800.77                 Z    =        -2330440.07
     XDOT =     -12675.225638                 XDOT =       -3863.408774
     YDOT =     -10431.222833  feet/sec       YDOT =       -3179.436719  meter/sec
     ZDOT =      17737.027256                 ZDOT =        5406.245908
  
  
    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   16132.56436680  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6428 240.7341 0001506  97.5082 262.6242 15.54522903 39284
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16132.56436680   =   yrday.fracday
    Element set:     908
    Inclination:       51.6428  deg
    RA of node:       240.7341  deg
    Eccentricity:     .0001506     
    Arg of perigee:    97.5082  deg
    Mean anomaly:     262.6242  deg
    Mean motion:   15.54522903  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3928
    Checksum:              304
 
 
    Coasting Arc #10 (Orbit 3943)
    ---------------------------------------
 
    Vector Time (GMT): 2016/133/13:26:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4220226.97                 A    =         6787961.94  meter
     Y    =        5285006.95  meter          E    =           .0014509
     Z    =         495424.78                 I    =           51.35709
     XDOT =      -3475.221395                 Wp   =          126.53858
     YDOT =       3344.768885  meter/sec      RA   =          234.74918  deg
     ZDOT =      -5964.152346                 TA   =           48.09435
                                              MA   =           47.97069
                                              Ha   =            220.921  n.mi
                                              Hp   =            213.356
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13845889.00                 X    =         4158408.47
     Y    =       17339261.65  feet           Y    =         5331854.67  meter
     Z    =        1625409.40                 Z    =          515775.73
     XDOT =     -11401.644998                 XDOT =       -3483.393730
     YDOT =      10973.651196  feet/sec       YDOT =        3305.861163  meter/sec
     ZDOT =     -19567.428956                 ZDOT =       -5981.053915
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20846890.67                 X    =         6354132.28
     Y    =       -7581139.55  feet           Y    =        -2310731.34  meter
     Z    =        1712911.29                 Z    =          522095.36
     XDOT =       6248.984323                 XDOT =        1904.690422
     YDOT =      12666.146651  feet/sec       YDOT =        3860.641499  meter/sec
     ZDOT =     -19641.444604                 ZDOT =       -5986.712315
  
  
    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   16133.59291549  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6420 235.6040 0001691 101.7776 258.3567 15.54559884 39446
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16133.59291549   =   yrday.fracday
    Element set:     909
    Inclination:       51.6420  deg
    RA of node:       235.6040  deg
    Eccentricity:     .0001691     
    Arg of perigee:   101.7776  deg
    Mean anomaly:     258.3567  deg
    Mean motion:   15.54559884  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3944
    Checksum:              334
 
 
    Coasting Arc #11 (Orbit 3959)
    ---------------------------------------
 
    Vector Time (GMT): 2016/134/13:26:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3423870.87                 A    =         6787319.80  meter
     Y    =       -5698175.64  meter          E    =           .0015086
     Z    =        1336111.27                 I    =           51.37401
     XDOT =       4791.290974                 Wp   =           64.07147
     YDOT =      -1509.139685  meter/sec      RA   =          229.75805  deg
     ZDOT =       5797.302560                 TA   =          310.53774
                                              MA   =          310.66903
                                              Ha   =            220.908  n.mi
                                              Hp   =            213.383
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11233172.13                 X    =        -3366388.25
     Y    =      -18694801.98  feet           Y    =        -5736142.27  meter
     Z    =        4383567.17                 Z    =         1319618.39
     XDOT =      15719.458576                 XDOT =        4779.649524
     YDOT =      -4951.245685  feet/sec       YDOT =       -1455.625495  meter/sec
     ZDOT =      19020.021523                 ZDOT =        5820.549253
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21225836.28                 X    =        -6469634.90
     Y    =        5075268.71  feet           Y    =         1546941.90  meter
     Z    =        4312883.04                 Z    =         1314566.75
     XDOT =        372.999491                 XDOT =         113.690245
     YDOT =     -14815.365014  feet/sec       YDOT =       -4515.723256  meter/sec
     ZDOT =      19121.293006                 ZDOT =        5828.170108
  
  
    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   16134.62145309  .00016717  00000-0  10270-3 0  9103
    2 25544  51.6418 230.4736 0001674 101.5870 258.5471 15.54569157 39600
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16134.62145309   =   yrday.fracday
    Element set:     910
    Inclination:       51.6418  deg
    RA of node:       230.4736  deg
    Eccentricity:     .0001674     
    Arg of perigee:   101.5870  deg
    Mean anomaly:     258.5471  deg
    Mean motion:   15.54569157  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3960
    Checksum:              307
 
 
    Coasting Arc #12 (Orbit 3970)
    ---------------------------------------
 
    Vector Time (GMT): 2016/135/07:32:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3692751.09                 A    =         6776211.22  meter
     Y    =        2216119.63  meter          E    =           .0016361
     Z    =       -5245932.65                 I    =           51.35110
     XDOT =      -4774.457135                 Wp   =           97.74030
     YDOT =      -5924.469208  meter/sec      RA   =          225.95989  deg
     ZDOT =        858.247341                 TA   =          180.51027
                                              MA   =          180.51194
                                              Ha   =            220.917  n.mi
                                              Hp   =            213.120
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12115325.08                 X    =        -3691775.22
     Y    =        7270733.70  feet           Y    =         2174830.35  meter
     Z    =      -17211065.13                 Z    =        -5263868.81
     XDOT =     -15664.229444                 XDOT =       -4712.022409
     YDOT =     -19437.234936  feet/sec       YDOT =       -5977.511283  meter/sec
     ZDOT =       2815.772117                 ZDOT =         835.205669
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13501831.06                 X    =        -4115358.11
     Y    =        3826635.52  feet           Y    =         1166358.51  meter
     Z    =      -17289385.53                 Z    =        -5269804.71
     XDOT =      -9689.011355                 XDOT =       -2953.210661
     YDOT =     -21914.348618  feet/sec       YDOT =       -6679.493459  meter/sec
     ZDOT =       2716.657222                 ZDOT =         828.037121
  
  
    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   16135.32856668  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6396 226.9442 0001859 105.4885 254.6474 15.54600814 39711
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16135.32856668   =   yrday.fracday
    Element set:     911
    Inclination:       51.6396  deg
    RA of node:       226.9442  deg
    Eccentricity:     .0001859     
    Arg of perigee:   105.4885  deg
    Mean anomaly:     254.6474  deg
    Mean motion:   15.54600814  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3971
    Checksum:              334
 
 
    Coasting Arc #13 (Orbit 3986)
    ---------------------------------------
 
    Vector Time (GMT): 2016/136/07:32:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4883760.60                 A    =         6778726.13  meter
     Y    =        -676323.21  meter          E    =           .0009514
     Z    =        4645666.51                 I    =           51.38216
     XDOT =       3587.818902                 Wp   =           72.28428
     YDOT =       6146.057136  meter/sec      RA   =          220.93805  deg
     ZDOT =      -2869.247645                 TA   =           46.34789
                                              MA   =           46.26904
                                              Ha   =            220.833  n.mi
                                              Hp   =            213.279
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16022836.60                 X    =         4868393.62
     Y    =       -2218908.17  feet           Y    =         -621795.70  meter
     Z    =       15241688.01                 Z    =         4669353.45
     XDOT =      11771.059391                 XDOT =        3532.763174
     YDOT =      20164.229448  feet/sec       YDOT =        6185.870696  meter/sec
     ZDOT =      -9413.542141                 ZDOT =       -2851.952475
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15975932.39                 X    =         4869464.19
     Y    =        1808963.18  feet           Y    =          551371.98  meter
     Z    =       15344742.95                 Z    =         4677077.65
     XDOT =       6582.050050                 XDOT =        2006.208855
     YDOT =      21305.879620  feet/sec       YDOT =        6494.032108  meter/sec
     ZDOT =      -9339.421546                 ZDOT =       -2846.655687
  
  
    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   16136.35708658  .00016717  00000-0  10270-3 0  9129
    2 25544  51.6394 221.8122 0001921 108.3839 251.7523 15.54577632 39870
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16136.35708658   =   yrday.fracday
    Element set:     912
    Inclination:       51.6394  deg
    RA of node:       221.8122  deg
    Eccentricity:     .0001921     
    Arg of perigee:   108.3839  deg
    Mean anomaly:     251.7523  deg
    Mean motion:   15.54577632  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3987
    Checksum:              323
 
 
    Coasting Arc #14 (Orbit 4001)
    ---------------------------------------
 
    Vector Time (GMT): 2016/137/07:32:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5771887.52                 A    =         6782630.96  meter
     Y    =        -743989.76  meter          E    =           .0006968
     Z    =       -3490753.99                 I    =           51.42126
     XDOT =      -1968.095691                 Wp   =           99.37942
     YDOT =      -5871.261922  meter/sec      RA   =          215.93027  deg
     ZDOT =       4512.157676                 TA   =          219.47389
                                              MA   =          219.52468
                                              Ha   =            220.858  n.mi
                                              Hp   =            213.149
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18936638.84                 X    =        -5746182.30
     Y    =       -2440911.28  feet           Y    =         -808391.10  meter
     Z    =      -11452604.95                 Z    =        -3518730.23
     XDOT =      -6457.006859                 XDOT =       -1924.213845
     YDOT =     -19262.670347  feet/sec       YDOT =       -5893.025141  meter/sec
     ZDOT =      14803.666916                 ZDOT =        4502.703617
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17782826.03                 X    =        -5420205.37
     Y    =       -6747479.63  feet           Y    =        -2056631.79  meter
     Z    =      -11574070.84                 Z    =        -3527776.79
     XDOT =      -2401.359480                 XDOT =        -731.934370
     YDOT =     -18958.713124  feet/sec       YDOT =       -5778.615760  meter/sec
     ZDOT =      14763.566216                 ZDOT =        4499.934983
  
  
    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   16137.32131455  .00016717  00000-0  10270-3 0  9133
    2 25544  51.6402 217.0030 0001874 110.5063 249.6292 15.54617627 40023
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16137.32131455   =   yrday.fracday
    Element set:     913
    Inclination:       51.6402  deg
    RA of node:       217.0030  deg
    Eccentricity:     .0001874     
    Arg of perigee:   110.5063  deg
    Mean anomaly:     249.6292  deg
    Mean motion:   15.54617627  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4002
    Checksum:              270
 
 
    Coasting Arc #15 (Orbit 4017)
    ---------------------------------------
 
    Vector Time (GMT): 2016/138/07:32:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6206723.32                 A    =         6786349.10  meter
     Y    =        1990126.31  meter          E    =           .0015733
     Z    =        1862573.14                 I    =           51.46008
     XDOT =         18.814497                 Wp   =          113.77097
     YDOT =       5227.035396  meter/sec      RA   =          210.93545  deg
     ZDOT =      -5616.302575                 TA   =           45.66348
                                              MA   =           45.53464
                                              Ha   =            220.771  n.mi
                                              Hp   =            213.256
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20363265.48                 X    =         6174960.23
     Y    =        6529285.81  feet           Y    =         2059356.41  meter
     Z    =        6110804.25                 Z    =         1892647.12
     XDOT =         61.727354                 XDOT =         -12.354973
     YDOT =      17149.066260  feet/sec       YDOT =        5227.071566  meter/sec
     ZDOT =     -18426.189550                 ZDOT =       -5616.286837
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18444122.94                 X    =         5621768.67
     Y    =       10746997.50  feet           Y    =         3275684.84  meter
     Z    =        6241190.32                 Z    =         1902314.81
     XDOT =      -2727.109952                 XDOT =        -831.223114
     YDOT =      15440.111264  feet/sec       YDOT =        4706.145913  meter/sec
     ZDOT =     -18426.997404                 ZDOT =       -5616.548809
  
  
    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   16138.34981742  .00016717  00000-0  10270-3 0  9149
    2 25544  51.6400 211.8718 0001779 116.3505 243.7831 15.54626937 40180
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16138.34981742   =   yrday.fracday
    Element set:     914
    Inclination:       51.6400  deg
    RA of node:       211.8718  deg
    Eccentricity:     .0001779     
    Arg of perigee:   116.3505  deg
    Mean anomaly:     243.7831  deg
    Mean motion:   15.54626937  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4018
    Checksum:              313
 
 
    Coasting Arc #16 (Orbit 4032)
    ---------------------------------------
 
    Vector Time (GMT): 2016/139/07:32:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6110252.20                 A    =         6787822.56  meter
     Y    =       -2944221.37  meter          E    =           .0012695
     Z    =         -33345.88                 I    =           51.49482
     XDOT =       2053.037114                 Wp   =           53.05011
     YDOT =      -4310.718696  meter/sec      RA   =          205.95117  deg
     ZDOT =       6001.225716                 TA   =          306.58993
                                              MA   =          306.70667
                                              Ha   =            220.780  n.mi
                                              Hp   =            213.261
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20046759.17                 X    =        -6076713.06
     Y    =       -9659518.92  feet           Y    =        -3012362.74  meter
     Z    =        -109402.48                 Z    =          -62947.02
     XDOT =       6735.686069                 XDOT =        2071.936222
     YDOT =     -14142.777875  feet/sec       YDOT =       -4287.654712  meter/sec
     ZDOT =      19689.060748                 ZDOT =        6011.244840
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17733657.21                 X    =        -5405218.72
     Y    =      -13440676.41  feet           Y    =        -4096718.17  meter
     Z    =        -237586.55                 Z    =          -72416.38
     XDOT =       8300.088587                 XDOT =        2529.867001
     YDOT =     -11257.545234  feet/sec       YDOT =       -3431.299787  meter/sec
     ZDOT =      19733.334697                 ZDOT =        6014.720416
  
  
    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   16139.31403110  .00016717  00000-0  10270-3 0  9156
    2 25544  51.6417 207.0620 0001806 115.2861 244.8480 15.54645538 40338
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16139.31403110   =   yrday.fracday
    Element set:     915
    Inclination:       51.6417  deg
    RA of node:       207.0620  deg
    Eccentricity:     .0001806     
    Arg of perigee:   115.2861  deg
    Mean anomaly:     244.8480  deg
    Mean motion:   15.54645538  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4033
    Checksum:              278
 
 
    Coasting Arc #17 (Orbit 4048)
    ---------------------------------------
 
    Vector Time (GMT): 2016/140/07:32:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926503.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5414592.29                 A    =         6786369.84  meter
     Y    =        3646104.99  meter          E    =           .0009010
     Z    =       -1845386.33                 I    =           51.51853
     XDOT =      -4083.955989                 Wp   =          137.13662
     YDOT =       3227.084273  meter/sec      RA   =          200.96941  deg
     ZDOT =      -5629.433720                 TA   =           63.19863
                                              MA   =           63.10650
                                              Ha   =            220.792  n.mi
                                              Hp   =            213.248
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17764410.39                 X    =         5382382.46
     Y    =       11962286.71  feet           Y    =         3706474.53  meter
     Z    =       -6054417.10                 Z    =        -1819161.23
     XDOT =     -13398.805737                 XDOT =       -4092.392662
     YDOT =      10587.546827  feet/sec       YDOT =        3181.367771  meter/sec
     ZDOT =     -18469.270734                 ZDOT =       -5649.293304
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15339405.97                 X    =         4675450.94
     Y    =       14991114.80  feet           Y    =         4569291.79  meter
     Z    =       -5941014.05                 Z    =        -1810821.08
     XDOT =     -13885.529266                 XDOT =       -4232.309320
     YDOT =       6884.310410  feet/sec       YDOT =        2098.337813  meter/sec
     ZDOT =     -18556.148386                 ZDOT =       -5655.914028
  
  
    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   16140.34251866  .00016717  00000-0  10270-3 0  9161
    2 25544  51.6409 201.9315 0001810 117.3825 242.7513 15.54666808 40495
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16140.34251866   =   yrday.fracday
    Element set:     916
    Inclination:       51.6409  deg
    RA of node:       201.9315  deg
    Eccentricity:     .0001810     
    Arg of perigee:   117.3825  deg
    Mean anomaly:     242.7513  deg
    Mean motion:   15.54666808  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4049
    Checksum:              300
 
             

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