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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  22604.21
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   104.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   3.055
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
   048/10:49:56.644           1.5               2.9              2.9    
   N/A                       -2.3              -0.4              222.1  
   000/00:09:53.288           0.8               0.2              213.2  
   
 
 
    Coasting Arc #1 (Orbit 2513)
    ---------------------------------------
 
    Vector Time (GMT): 2016/041/14:38:11.336
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2027945.68                 A    =         6780106.38  meter
     Y    =        4823852.93  meter          E    =           .0016014
     Z    =        4299108.40                 I    =           51.47912
     XDOT =      -6824.073699                 Wp   =           81.44731
     YDOT =        266.986515  meter/sec      RA   =          333.64541  deg
     ZDOT =      -3505.064923                 TA   =           44.32215
                                              MA   =           44.19404
                                              Ha   =            222.643  n.mi
                                              Hp   =            211.542
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6653365.09                 X    =        -2102619.25
     Y    =       15826289.13  feet           Y    =         4800757.95  meter
     Z    =       14104686.36                 Z    =         4289075.57
     XDOT =     -22388.693239                 XDOT =       -6809.526299
     YDOT =        875.940009  feet/sec       YDOT =         190.756226  meter/sec
     ZDOT =     -11499.556833                 ZDOT =       -3538.178544
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7068822.29                 X    =        -2154577.03
     Y    =       15685106.87  feet           Y    =         4780820.57  meter
     Z    =       14060229.22                 Z    =         4285557.87
     XDOT =     -21183.915022                 XDOT =       -6456.857299
     YDOT =        929.896344  feet/sec       YDOT =         283.432405  meter/sec
     ZDOT =     -11643.157754                 ZDOT =       -3548.834483
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16041.65165517  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6446 334.0449 0006483  95.9362 264.2530 15.54614707 25144
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16041.65165517   =   yrday.fracday
    Element set:     900
    Inclination:       51.6446  deg
    RA of node:       334.0449  deg
    Eccentricity:     .0006483     
    Arg of perigee:    95.9362  deg
    Mean anomaly:     264.2530  deg
    Mean motion:   15.54614707  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2514
    Checksum:              303
 
 
    Coasting Arc #2 (Orbit 2528)
    ---------------------------------------
 
    Vector Time (GMT): 2016/042/14:38:11.336
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3563215.47                 A    =         6784163.57  meter
     Y    =       -4949791.75  meter          E    =           .0010526
     Z    =       -2979338.17                 I    =           51.46478
     XDOT =       5723.053989                 Wp   =           85.96356
     YDOT =       1141.905555  meter/sec      RA   =          328.64522  deg
     ZDOT =       4963.404421                 TA   =          239.90252
                                              MA   =          240.00691
                                              Ha   =            222.554  n.mi
                                              Hp   =            211.595
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11690339.45                 X    =         3632772.53
     Y    =      -16239474.26  feet           Y    =        -4909556.88  meter
     Z    =       -9774731.53                 Z    =        -2961859.85
     XDOT =      18776.423848                 XDOT =        5685.749907
     YDOT =       3746.409300  feet/sec       YDOT =        1205.696439  meter/sec
     ZDOT =      16284.135240                 ZDOT =        4991.114384
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11808424.87                 X    =         3599207.90
     Y    =      -16200004.03  feet           Y    =        -4937761.23  meter
     Z    =       -9697984.78                 Z    =        -2955945.76
     XDOT =      17477.204091                 XDOT =        5327.051807
     YDOT =       2950.757650  feet/sec       YDOT =         899.390932  meter/sec
     ZDOT =      16404.022926                 ZDOT =        4999.946188
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16042.61588738  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6448 329.2344 0006399  99.8869 260.3007 15.54629789 25295
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16042.61588738   =   yrday.fracday
    Element set:     901
    Inclination:       51.6448  deg
    RA of node:       329.2344  deg
    Eccentricity:     .0006399     
    Arg of perigee:    99.8869  deg
    Mean anomaly:     260.3007  deg
    Mean motion:   15.54629789  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2529
    Checksum:              356
 
 
    Coasting Arc #3 (Orbit 2544)
    ---------------------------------------
 
    Vector Time (GMT): 2016/043/14:38:11.336
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4731371.94                 A    =         6787284.99  meter
     Y    =        4696345.73  meter          E    =           .0020026
     Z    =        1228058.35                 I    =           51.44793
     XDOT =      -4197.039265                 Wp   =          116.12992
     YDOT =      -2685.352767  meter/sec      RA   =          323.65466  deg
     ZDOT =      -5835.362806                 TA   =           50.47536
                                              MA   =           50.29852
                                              Ha   =            222.560  n.mi
                                              Hp   =            211.587
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15522873.83                 X    =        -4789501.30
     Y    =       15407958.43  feet           Y    =         4643111.49  meter
     Z    =        4029062.84                 Z    =         1204933.22
     XDOT =     -13769.813863                 XDOT =       -4138.353757
     YDOT =      -8810.212489  feet/sec       YDOT =       -2731.959264  meter/sec
     ZDOT =     -19144.891097                 ZDOT =       -5855.607904
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15334680.61                 X    =        -4674010.65
     Y    =       15621053.36  feet           Y    =         4761297.07  meter
     Z    =        3927900.80                 Z    =         1197224.16
     XDOT =     -12627.593267                 XDOT =       -3848.890428
     YDOT =      -7504.907253  feet/sec       YDOT =       -2287.495731  meter/sec
     ZDOT =     -19232.111650                 ZDOT =       -5861.947631
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16043.64438105  .00016717  00000-0  10270-3 0  9024
    2 25544  51.6444 324.1032 0006492 105.2555 254.9316 15.54624581 25452
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16043.64438105   =   yrday.fracday
    Element set:     902
    Inclination:       51.6444  deg
    RA of node:       324.1032  deg
    Eccentricity:     .0006492     
    Arg of perigee:   105.2555  deg
    Mean anomaly:     254.9316  deg
    Mean motion:   15.54624581  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2545
    Checksum:              290
 
 
    Coasting Arc #4 (Orbit 2560)
    ---------------------------------------
 
    Vector Time (GMT): 2016/044/14:38:11.336
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5388695.18                 A    =         6787457.73  meter
     Y    =       -4069115.06  meter          E    =           .0017499
     Z    =         631219.22                 I    =           51.42383
     XDOT =       2440.951260                 Wp   =           69.02812
     YDOT =       4175.626072  meter/sec      RA   =          318.66683  deg
     ZDOT =       5952.160090                 TA   =          297.80940
                                              MA   =          297.98666
                                              Ha   =            222.333  n.mi
                                              Hp   =            211.510
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17679446.13                 X    =         5430730.37
     Y    =      -13350115.02  feet           Y    =        -4008620.01  meter
     Z    =        2070929.20                 Z    =          657498.31
     XDOT =       8008.370275                 XDOT =        2365.164240
     YDOT =      13699.560605  feet/sec       YDOT =        4202.499157  meter/sec
     ZDOT =      19528.084284                 ZDOT =        5963.833066
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17243808.23                 X    =         5255912.75
     Y    =      -13890689.01  feet           Y    =        -4233882.01  meter
     Z    =        2185628.19                 Z    =          666179.47
     XDOT =       7290.487021                 XDOT =        2222.140444
     YDOT =      12193.171577  feet/sec       YDOT =        3716.478697  meter/sec
     ZDOT =      19577.856669                 ZDOT =        5967.330713
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16044.67284911  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6441 318.9713 0006270 108.1838 251.9998 15.54708667 25615
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16044.67284911   =   yrday.fracday
    Element set:     903
    Inclination:       51.6441  deg
    RA of node:       318.9713  deg
    Eccentricity:     .0006270     
    Arg of perigee:   108.1838  deg
    Mean anomaly:     251.9998  deg
    Mean motion:   15.54708667  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2561
    Checksum:              332
 
 
    Coasting Arc #5 (Orbit 2575)
    ---------------------------------------
 
    Vector Time (GMT): 2016/045/14:38:11.336
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5572957.52                 A    =         6784987.69  meter
     Y    =        2973194.15  meter          E    =           .0011327
     Z    =       -2476544.66                 I    =           51.39164
     XDOT =       -593.304048                 Wp   =          120.55595
     YDOT =      -5506.347419  meter/sec      RA   =          313.67466  deg
     ZDOT =      -5299.245706                 TA   =           87.29174
                                              MA   =           87.16209
                                              Ha   =            222.233  n.mi
                                              Hp   =            211.586
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18283981.36                 X    =        -5593760.45
     Y    =        9754574.00  feet           Y    =         2910757.16  meter
     Z    =       -8125146.53                 Z    =        -2503667.16
     XDOT =      -1946.535591                 XDOT =        -505.945413
     YDOT =     -18065.444287  feet/sec       YDOT =       -5512.494050  meter/sec
     ZDOT =     -17385.976725                 ZDOT =       -5301.915241
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17740504.18                 X    =        -5407305.67
     Y    =       10620572.43  feet           Y    =         3237150.48  meter
     Z    =       -8243278.91                 Z    =        -2512551.41
     XDOT =      -1928.410221                 XDOT =        -587.779435
     YDOT =     -16664.036238  feet/sec       YDOT =       -5079.198245  meter/sec
     ZDOT =     -17396.469517                 ZDOT =       -5302.443909
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16045.63702037  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6435 314.1602 0006169 112.9276 247.2528 15.54699111 25765
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16045.63702037   =   yrday.fracday
    Element set:     904
    Inclination:       51.6435  deg
    RA of node:       314.1602  deg
    Eccentricity:     .0006169     
    Arg of perigee:   112.9276  deg
    Mean anomaly:     247.2528  deg
    Mean motion:   15.54699111  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2576
    Checksum:              304
 
 
    Coasting Arc #6 (Orbit 2591)
    ---------------------------------------
 
    Vector Time (GMT): 2016/046/14:38:11.336
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5280936.65                 A    =         6780816.36  meter
     Y    =       -1538367.73  meter          E    =           .0016986
     Z    =        3954714.98                 I    =           51.35617
     XDOT =      -1106.519475                 Wp   =          105.53687
     YDOT =       6470.069062  meter/sec      RA   =          308.66928  deg
     ZDOT =       3975.676641                 TA   =          302.82970
                                              MA   =          302.99315
                                              Ha   =            222.126  n.mi
                                              Hp   =            211.573
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17325907.64                 X    =         5278536.48
     Y    =       -5047138.22  feet           Y    =        -1479326.00  meter
     Z    =       12974786.68                 Z    =         3980362.42
     XDOT =      -3630.313237                 XDOT =       -1198.099064
     YDOT =      21227.260701  feet/sec       YDOT =        6457.183389  meter/sec
     ZDOT =      13043.558532                 ZDOT =        3970.078724
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16875702.98                 X    =         5143714.27
     Y    =       -6161711.19  feet           Y    =        -1878089.57  meter
     Z    =       13086242.14                 Z    =         3988686.60
     XDOT =      -2768.387831                 XDOT =        -843.804611
     YDOT =      20195.154904  feet/sec       YDOT =        6155.483215  meter/sec
     ZDOT =      13018.038320                 ZDOT =        3967.898080
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16046.66544835  .00016717  00000-0  10270-3 0  9050
    2 25544  51.6431 309.0277 0006189 114.6582 245.5216 15.54732406 25921
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16046.66544835   =   yrday.fracday
    Element set:     905
    Inclination:       51.6431  deg
    RA of node:       309.0277  deg
    Eccentricity:     .0006189     
    Arg of perigee:   114.6582  deg
    Mean anomaly:     245.5216  deg
    Mean motion:   15.54732406  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2592
    Checksum:              315
 
 
    Coasting Arc #7 (Orbit 2606)
    ---------------------------------------
 
    Vector Time (GMT): 2016/047/14:38:11.336
    Vector Time (MET): N/A
    Weight (LBS)     : 922504.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4624266.09                 A    =         6776861.13  meter
     Y    =        -224394.59  meter          E    =           .0017466
     Z    =       -4964212.24                 I    =           51.32318
     XDOT =       2577.406119                 Wp   =           88.55198
     YDOT =      -6898.680347  meter/sec      RA   =          303.64922  deg
     ZDOT =      -2095.043938                 TA   =          160.96319
                                              MA   =          160.89782
                                              Ha   =            222.033  n.mi
                                              Hp   =            211.470
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15171476.68                 X    =        -4597299.49
     Y    =        -736202.72  feet           Y    =         -275955.64  meter
     Z    =      -16286785.57                 Z    =        -4986609.95
     XDOT =       8456.056822                 XDOT =        2664.533995
     YDOT =     -22633.465705  feet/sec       YDOT =       -6869.371015  meter/sec
     ZDOT =      -6873.503734                 ZDOT =       -2082.311789
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15076072.97                 X    =        -4595187.04
     Y    =         507679.83  feet           Y    =          154740.81  meter
     Z    =      -16383814.22                 Z    =        -4993786.57
     XDOT =       6640.953395                 XDOT =        2024.162595
     YDOT =     -22158.761916  feet/sec       YDOT =       -6753.990632  meter/sec
     ZDOT =      -6816.989286                 ZDOT =       -2077.818335
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16047.62957767  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6421 304.2158 0006058 119.5797 240.5961 15.54788978 26076
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16047.62957767   =   yrday.fracday
    Element set:     906
    Inclination:       51.6421  deg
    RA of node:       304.2158  deg
    Eccentricity:     .0006058     
    Arg of perigee:   119.5797  deg
    Mean anomaly:     240.5961  deg
    Mean motion:   15.54788978  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2607
    Checksum:              350
 
 
    Coasting Arc #8 (Orbit 2619)
    ---------------------------------------
 
    Vector Time (GMT): 2016/048/10:54:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1382189.49                 A    =         6780333.80  meter
     Y    =       -4891509.63  meter          E    =           .0013487
     Z    =       -4501016.20                 I    =           51.31670
     XDOT =       5391.818777                 Wp   =          116.46941
     YDOT =      -4426.662050  meter/sec      RA   =          299.37439  deg
     ZDOT =       3156.431849                 TA   =          185.39920
                                              MA   =          185.41375
                                              Ha   =            222.068  n.mi
                                              Hp   =            213.216
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4534742.42                 X    =        -1305525.05
     Y    =      -16048259.94  feet           Y    =        -4906537.72  meter
     Z    =      -14767113.50                 Z    =        -4507544.00
     XDOT =      17689.694151                 XDOT =        5425.585745
     YDOT =     -14523.169455  feet/sec       YDOT =       -4366.178221  meter/sec
     ZDOT =      10355.747536                 ZDOT =        3182.705722
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9503162.46                 X    =         2896563.92
     Y    =      -13674495.66  feet           Y    =        -4167986.28  meter
     Z    =      -14794466.83                 Z    =        -4509353.49
     XDOT =      21436.052937                 XDOT =        6533.708935
     YDOT =       3574.273535  feet/sec       YDOT =        1089.438573  meter/sec
     ZDOT =      10470.469424                 ZDOT =        3191.399080
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16048.46514428  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6437 300.0457 0004077 131.6664 228.4839 15.54264459 26203
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16048.46514428   =   yrday.fracday
    Element set:     907
    Inclination:       51.6437  deg
    RA of node:       300.0457  deg
    Eccentricity:     .0004077     
    Arg of perigee:   131.6664  deg
    Mean anomaly:     228.4839  deg
    Mean motion:   15.54264459  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2620
    Checksum:              314
 
 
    Coasting Arc #9 (Orbit 2635)
    ---------------------------------------
 
    Vector Time (GMT): 2016/049/10:54:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         243496.28                 A    =         6784210.74  meter
     Y    =        5902869.04  meter          E    =           .0015831
     Z    =        3318091.34                 I    =           51.31455
     XDOT =      -5388.754009                 Wp   =          101.74826
     YDOT =       2851.397957  meter/sec      RA   =          294.36372  deg
     ZDOT =      -4661.445129                 TA   =           39.39807
                                              MA   =           39.28304
                                              Ha   =            221.990  n.mi
                                              Hp   =            213.293
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         798872.31                 X    =          161353.31
     Y    =       19366368.25  feet           Y    =         5905132.85  meter
     Z    =       10886126.45                 Z    =         3319074.37
     XDOT =     -17679.639138                 XDOT =       -5397.595708
     YDOT =       9354.980174  feet/sec       YDOT =        2791.087679  meter/sec
     ZDOT =     -15293.455147                 ZDOT =       -4687.643428
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14201974.11                 X    =        -4328761.71
     Y    =       13188251.87  feet           Y    =         4019779.17  meter
     Z    =       10889265.78                 Z    =         3319048.21
     XDOT =     -17597.288011                 XDOT =       -5363.653386
     YDOT =      -6185.630857  feet/sec       YDOT =       -1885.380285  meter/sec
     ZDOT =     -15407.543901                 ZDOT =       -4696.219381
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16049.49387811  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6434 294.9163 0004122 135.5551 224.5933 15.54280719 26360
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16049.49387811   =   yrday.fracday
    Element set:     908
    Inclination:       51.6434  deg
    RA of node:       294.9163  deg
    Eccentricity:     .0004122     
    Arg of perigee:   135.5551  deg
    Mean anomaly:     224.5933  deg
    Mean motion:   15.54280719  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2636
    Checksum:              320
 
 
    Coasting Arc #10 (Orbit 2650)
    ---------------------------------------
 
    Vector Time (GMT): 2016/050/10:58:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1946561.51                 A    =         6788678.09  meter
     Y    =       -6488478.29  meter          E    =           .0011477
     Z    =        -392868.46                 I    =           51.31813
     XDOT =       4694.076059                 Wp   =           62.20087
     YDOT =       1055.290305  meter/sec      RA   =          289.36074  deg
     ZDOT =       5968.375801                 TA   =          293.54570
                                              MA   =          293.66623
                                              Ha   =            221.833  n.mi
                                              Hp   =            213.330
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6386356.66                 X    =         2020880.95
     Y    =      -21287658.44  feet           Y    =        -6466295.03  meter
     Z    =       -1288938.53                 Z    =         -383231.88
     XDOT =      15400.512006                 XDOT =        4652.935535
     YDOT =       3462.238535  feet/sec       YDOT =        1107.552896  meter/sec
     ZDOT =      19581.285435                 ZDOT =        5991.077939
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19978922.79                 X    =         6089575.67
     Y    =       -9741743.18  feet           Y    =        -2969283.32  meter
     Z    =       -1245953.38                 Z    =         -379766.59
     XDOT =       7105.510268                 XDOT =        2165.759530
     YDOT =      12115.858712  feet/sec       YDOT =        3692.913736  meter/sec
     ZDOT =      19679.483667                 ZDOT =        5998.306622
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16050.45829562  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6439 290.1070 0003949 140.0714 220.0729 15.54329850 26519
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16050.45829562   =   yrday.fracday
    Element set:     909
    Inclination:       51.6439  deg
    RA of node:       290.1070  deg
    Eccentricity:     .0003949     
    Arg of perigee:   140.0714  deg
    Mean anomaly:     220.0729  deg
    Mean motion:   15.54329850  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2651
    Checksum:              302
 
 
    Coasting Arc #11 (Orbit 2666)
    ---------------------------------------
 
    Vector Time (GMT): 2016/051/10:58:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2711441.49                 A    =         6787908.58  meter
     Y    =        6056741.35  meter          E    =           .0012497
     Z    =       -1403050.36                 I    =           51.30571
     XDOT =      -3977.030545                 Wp   =          143.47137
     YDOT =      -3109.309130  meter/sec      RA   =          284.36654  deg
     ZDOT =      -5773.069430                 TA   =           51.89768
                                              MA   =           51.78506
                                              Ha   =            221.734  n.mi
                                              Hp   =            213.443
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8895805.40                 X    =        -2772152.70
     Y    =       19871198.65  feet           Y    =         6026080.65  meter
     Z    =       -4603183.61                 Z    =        -1416369.45
     XDOT =     -13048.000477                 XDOT =       -3913.923500
     YDOT =     -10201.145439  feet/sec       YDOT =       -3153.430500  meter/sec
     ZDOT =     -18940.516502                 ZDOT =       -5792.234869
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20491453.46                 X    =        -6245795.01
     Y    =        7318125.18  feet           Y    =         2230564.56  meter
     Z    =       -4662034.72                 Z    =        -1420988.18
     XDOT =      -1020.103928                 XDOT =        -310.927677
     YDOT =     -14899.879363  feet/sec       YDOT =       -4541.483230  meter/sec
     ZDOT =     -19023.009565                 ZDOT =       -5798.213315
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16051.48698873  .00016717  00000-0  10270-3 0  9104
    2 25544  51.6438 284.9771 0003977 146.3115 213.8292 15.54321807 26678
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16051.48698873   =   yrday.fracday
    Element set:     910
    Inclination:       51.6438  deg
    RA of node:       284.9771  deg
    Eccentricity:     .0003977     
    Arg of perigee:   146.3115  deg
    Mean anomaly:     213.8292  deg
    Mean motion:   15.54321807  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2667
    Checksum:              336
 
 
    Coasting Arc #12 (Orbit 2682)
    ---------------------------------------
 
    Vector Time (GMT): 2016/052/10:58:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3283721.21                 A    =         6784747.22  meter
     Y    =       -5114632.49  meter          E    =           .0015186
     Z    =        3003987.32                 I    =           51.28806
     XDOT =       3182.375141                 Wp   =           96.23335
     YDOT =       4947.676597  meter/sec      RA   =          279.36510  deg
     ZDOT =       4922.148902                 TA   =          298.36557
                                              MA   =          298.51861
                                              Ha   =            221.591  n.mi
                                              Hp   =            213.416
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10773363.57                 X    =         3326078.53
     Y    =      -16780290.31  feet           Y    =        -5077674.62  meter
     Z    =        9855601.45                 Z    =         3020041.78
     XDOT =      10440.863323                 XDOT =        3102.903382
     YDOT =      16232.534766  feet/sec       YDOT =        4982.820130  meter/sec
     ZDOT =      16148.782487                 ZDOT =        4937.414223
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19461151.18                 X    =         5931758.88
     Y    =       -4184744.48  feet           Y    =        -1275510.12  meter
     Z    =        9926121.79                 Z    =         3025481.92
     XDOT =      -4578.404396                 XDOT =       -1395.497660
     YDOT =      17346.106942  feet/sec       YDOT =        5287.093396  meter/sec
     ZDOT =      16214.044481                 ZDOT =        4942.040758
  
  
    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   16052.51566066  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6433 279.8467 0003772 146.9540 213.1850 15.54370259 26835
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16052.51566066   =   yrday.fracday
    Element set:     911
    Inclination:       51.6433  deg
    RA of node:       279.8467  deg
    Eccentricity:     .0003772     
    Arg of perigee:   146.9540  deg
    Mean anomaly:     213.1850  deg
    Mean motion:   15.54370259  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2683
    Checksum:              317
 
 
    Coasting Arc #13 (Orbit 2697)
    ---------------------------------------
 
    Vector Time (GMT): 2016/053/10:58:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3742520.48                 A    =         6780560.20  meter
     Y    =        3675038.11  meter          E    =           .0009660
     Z    =       -4305160.84                 I    =           51.26970
     XDOT =      -2310.673023                 Wp   =           91.58459
     YDOT =      -6422.046297  meter/sec      RA   =          274.35244  deg
     ZDOT =      -3480.447607                 TA   =          142.83298
                                              MA   =          142.76607
                                              Ha   =            221.380  n.mi
                                              Hp   =            213.442
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12278610.51                 X    =        -3762425.39
     Y    =       12057211.66  feet           Y    =         3633074.99  meter
     Z    =      -14124543.44                 Z    =        -4323389.40
     XDOT =      -7580.948237                 XDOT =       -2221.782254
     YDOT =     -21069.705699  feet/sec       YDOT =       -6447.389145  meter/sec
     ZDOT =     -11418.791363                 ZDOT =       -3491.455403
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17142697.70                 X    =        -5225094.26
     Y    =         107389.38  feet           Y    =           32732.28  meter
     Z    =      -14204215.55                 Z    =        -4329444.90
     XDOT =       9361.518567                 XDOT =        2853.390859
     YDOT =     -19068.556874  feet/sec       YDOT =       -5812.096135  meter/sec
     ZDOT =     -11465.347507                 ZDOT =       -3494.637920
  
  
    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   16053.48002022  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6427 275.0369 0003648 154.1270 206.0066 15.54413454 26981
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16053.48002022   =   yrday.fracday
    Element set:     912
    Inclination:       51.6427  deg
    RA of node:       275.0369  deg
    Eccentricity:     .0003648     
    Arg of perigee:   154.1270  deg
    Mean anomaly:     206.0066  deg
    Mean motion:   15.54413454  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2698
    Checksum:              288
 
 
    Coasting Arc #14 (Orbit 2713)
    ---------------------------------------
 
    Vector Time (GMT): 2016/054/10:58:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4052613.63                 A    =         6777358.38  meter
     Y    =       -1919227.88  meter          E    =           .0008448
     Z    =        5078509.21                 I    =           51.25758
     XDOT =       1409.215318                 Wp   =          137.83860
     YDOT =       7358.891436  meter/sec      RA   =          269.32845  deg
     ZDOT =       1648.707664                 TA   =          296.12444
                                              MA   =          296.21133
                                              Ha   =            221.248  n.mi
                                              Hp   =            213.525
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13295976.48                 X    =         4049105.02
     Y    =       -6296679.41  feet           Y    =        -1873927.84  meter
     Z    =       16661775.63                 Z    =         5098187.10
     XDOT =       4623.409835                 XDOT =        1318.813090
     YDOT =      24143.344605  feet/sec       YDOT =        7374.144956  meter/sec
     ZDOT =       5409.145878                 ZDOT =        1655.332634
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13912248.73                 X    =         4240453.41
     Y    =        4474319.76  feet           Y    =         1363772.66  meter
     Z    =       16747409.57                 Z    =         5104610.44
     XDOT =     -12908.564119                 XDOT =       -3934.530343
     YDOT =      19693.444179  feet/sec       YDOT =        6002.561786  meter/sec
     ZDOT =       5436.554856                 ZDOT =        1657.061920
  
  
    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   16054.50865212  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6426 269.9063 0003675 155.8755 204.2570 15.54437776 27141
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16054.50865212   =   yrday.fracday
    Element set:     913
    Inclination:       51.6426  deg
    RA of node:       269.9063  deg
    Eccentricity:     .0003675     
    Arg of perigee:   155.8755  deg
    Mean anomaly:     204.2570  deg
    Mean motion:   15.54437776  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2714
    Checksum:              321
 
 
    Coasting Arc #15 (Orbit 2728)
    ---------------------------------------
 
    Vector Time (GMT): 2016/055/10:58:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4262864.83                 A    =         6776344.72  meter
     Y    =         -37281.80  meter          E    =           .0016430
     Z    =       -5281454.72                 I    =           51.25500
     XDOT =       -436.991426                 Wp   =          104.70195
     YDOT =      -7634.068281  meter/sec      RA   =          264.29660  deg
     ZDOT =        403.564365                 TA   =          169.19040
                                              MA   =          169.15505
                                              Ha   =            221.142  n.mi
                                              Hp   =            213.416
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13985777.01                 X    =        -4236476.53
     Y    =        -122315.63  feet           Y    =          -84805.16  meter
     Z    =      -17327607.36                 Z    =        -5302098.19
     XDOT =      -1433.698903                 XDOT =        -353.553213
     YDOT =     -25046.155776  feet/sec       YDOT =       -7638.488423  meter/sec
     ZDOT =       1324.030069                 ZDOT =         401.645303
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10168748.52                 X    =        -3099434.55
     Y    =       -9439532.45  feet           Y    =        -2877169.49  meter
     Z    =      -17417080.03                 Z    =        -5308725.99
     XDOT =      15121.211095                 XDOT =        4608.945142
     YDOT =     -18737.751392  feet/sec       YDOT =       -5711.266624  meter/sec
     ZDOT =       1317.049876                 ZDOT =         401.436802
  
  
    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   16055.47297366  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6415 265.0951 0003535 161.5553 198.5728 15.54495194 27291
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16055.47297366   =   yrday.fracday
    Element set:     914
    Inclination:       51.6415  deg
    RA of node:       265.0951  deg
    Eccentricity:     .0003535     
    Arg of perigee:   161.5553  deg
    Mean anomaly:     198.5728  deg
    Mean motion:   15.54495194  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2729
    Checksum:              338
 
 
    Coasting Arc #16 (Orbit 2744)
    ---------------------------------------
 
    Vector Time (GMT): 2016/056/10:58:53.288
    Vector Time (MET): N/A
    Weight (LBS)     : 922176.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4319203.43                 A    =         6778090.94  meter
     Y    =        1964662.32  meter          E    =           .0006759
     Z    =        4834346.97                 I    =           51.26574
     XDOT =       -595.625337                 Wp   =           88.62263
     YDOT =       7259.009703  meter/sec      RA   =          259.26769  deg
     ZDOT =      -2414.790254                 TA   =           25.18686
                                              MA   =           25.15392
                                              Ha   =            220.828  n.mi
                                              Hp   =            213.646
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14170614.93                 X    =         4273430.23
     Y    =        6445742.51  feet           Y    =         2012707.25  meter
     Z    =       15860718.42                 Z    =         4855216.84
     XDOT =      -1954.151367                 XDOT =        -665.023267
     YDOT =      23815.648633  feet/sec       YDOT =        7251.960664  meter/sec
     ZDOT =      -7922.540202                 ZDOT =       -2417.853173
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6295958.10                 X    =         1919008.03
     Y    =       14136758.14  feet           Y    =         4308883.88  meter
     Z    =       15950839.90                 Z    =         4861816.00
     XDOT =     -16138.026556                 XDOT =       -4918.870494
     YDOT =      16154.210422  feet/sec       YDOT =        4923.803337  meter/sec
     ZDOT =      -7937.073823                 ZDOT =       -2419.220101
  
  
    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   16056.50156298  .00016717  00000-0  10270-3 0  9157
    2 25544  51.6418 259.9643 0003451 167.2179 192.9062 15.54537691 27454
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16056.50156298   =   yrday.fracday
    Element set:     915
    Inclination:       51.6418  deg
    RA of node:       259.9643  deg
    Eccentricity:     .0003451     
    Arg of perigee:   167.2179  deg
    Mean anomaly:     192.9062  deg
    Mean motion:   15.54537691  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2745
    Checksum:              335
 
             

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