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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  18029.55
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   132.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.186
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 660)
    ---------------------------------------
 
    Vector Time (GMT): 2015/030/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5346411.11                 A    =         6783777.10  meter
     Y    =        2089635.42  meter          E    =           .0003259
     Z    =       -3612443.83                 I    =           51.93264
     XDOT =        570.588465                 Wp   =            7.66098
     YDOT =       6220.055379  meter/sec      RA   =           50.87723  deg
     ZDOT =       4446.096580                 TA   =          309.76591
                                              MA   =          309.79462
                                              Ha   =            220.422  n.mi
                                              Hp   =            216.409
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17540718.87                 X    =         5340194.59
     Y    =        6855759.24  feet           Y    =         2149387.76  meter
     Z    =      -11851849.83                 Z    =        -3586487.47
     XDOT =       1872.009400                 XDOT =         479.394801
     YDOT =      20407.005838  feet/sec       YDOT =        6225.926111  meter/sec
     ZDOT =      14586.931036                 ZDOT =        4448.646941
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5624124.54                 X    =         1714233.16
     Y    =       18046026.94  feet           Y    =         5500429.01  meter
     Z    =      -11741155.51                 Z    =        -3578704.20
     XDOT =     -13530.138898                 XDOT =       -4123.986336
     YDOT =      13705.865053  feet/sec       YDOT =        4177.547668  meter/sec
     ZDOT =      14596.640872                 ZDOT =        4449.056138
  
  
    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   15030.50755452  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6463  51.5213 0006168 308.7781  51.2820 15.54169192  6613
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15030.50755452   =   yrday.fracday
    Element set:     900
    Inclination:       51.6463  deg
    RA of node:        51.5213  deg
    Eccentricity:     .0006168     
    Arg of perigee:   308.7781  deg
    Mean anomaly:      51.2820  deg
    Mean motion:   15.54169192  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             661
    Checksum:              286
 
 
    Coasting Arc #2 (Orbit 676)
    ---------------------------------------
 
    Vector Time (GMT): 2015/031/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5530510.07                 A    =         6787209.53  meter
     Y    =       -3289996.96  meter          E    =           .0008576
     Z    =        2149272.51                 I    =           51.92233
     XDOT =        958.001481                 Wp   =           93.51648
     YDOT =      -5230.312818  meter/sec      RA   =           45.91696  deg
     ZDOT =      -5522.722969                 TA   =           62.75281
                                              MA   =           62.66548
                                              Ha   =            220.428  n.mi
                                              Hp   =            216.159
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18144718.08                 X    =        -5503749.68
     Y    =      -10793953.29  feet           Y    =        -3351693.12  meter
     Z    =        7051418.99                 Z    =         2122471.83
     XDOT =       3143.049479                 XDOT =        1043.243679
     YDOT =     -17159.818958  feet/sec       YDOT =       -5219.123139  meter/sec
     ZDOT =     -18119.169847                 ZDOT =       -5517.862295
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3262398.16                 X    =         -994378.96
     Y    =      -20897194.13  feet           Y    =        -6369464.77  meter
     Z    =        6937345.85                 Z    =         2114503.01
     XDOT =      13782.017259                 XDOT =        4200.758861
     YDOT =      -8179.885171  feet/sec       YDOT =       -2493.229000  meter/sec
     ZDOT =     -18097.345033                 ZDOT =       -5516.070766
  
  
    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   15031.53635540  .00016717  00000-0  10270-3 0  9019
    2 25544  51.6448  46.3919 0006172 313.2491  46.8146 15.54205838  6771
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15031.53635540   =   yrday.fracday
    Element set:     901
    Inclination:       51.6448  deg
    RA of node:        46.3919  deg
    Eccentricity:     .0006172     
    Arg of perigee:   313.2491  deg
    Mean anomaly:      46.8146  deg
    Mean motion:   15.54205838  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             677
    Checksum:              304
 
 
    Coasting Arc #3 (Orbit 691)
    ---------------------------------------
 
    Vector Time (GMT): 2015/032/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5340409.66                 A    =         6788854.75  meter
     Y    =        4151731.02  meter          E    =           .0013059
     Z    =        -466825.60                 I    =           51.90616
     XDOT =      -2586.851631                 Wp   =           13.96278
     YDOT =       3998.501168  meter/sec      RA   =           40.96339  deg
     ZDOT =       6014.929301                 TA   =          341.01845
                                              MA   =          341.06708
                                              Ha   =            220.454  n.mi
                                              Hp   =            215.892
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17521029.08                 X    =         5295854.74
     Y    =       13621164.76  feet           Y    =         4211201.84  meter
     Z    =       -1531580.04                 Z    =         -440991.70
     XDOT =      -8487.046032                 XDOT =       -2660.589185
     YDOT =      13118.442153  feet/sec       YDOT =        3969.161000  meter/sec
     ZDOT =      19734.020017                 ZDOT =        6002.184069
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1044435.55                 X    =          318343.96
     Y    =       22175570.37  feet           Y    =         6759113.85  meter
     Z    =       -1421815.71                 Z    =         -433369.43
     XDOT =     -13951.077574                 XDOT =       -4252.288445
     YDOT =       1908.086861  feet/sec       YDOT =         581.584875  meter/sec
     ZDOT =      19678.684383                 ZDOT =        5998.063000
  
  
    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   15032.50083726  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6451  41.5837 0006082 315.5266  44.5398 15.54264888  6927
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15032.50083726   =   yrday.fracday
    Element set:     902
    Inclination:       51.6451  deg
    RA of node:        41.5837  deg
    Eccentricity:     .0006082     
    Arg of perigee:   315.5266  deg
    Mean anomaly:      44.5398  deg
    Mean motion:   15.54264888  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             692
    Checksum:              312
 
 
    Coasting Arc #4 (Orbit 707)
    ---------------------------------------
 
    Vector Time (GMT): 2015/033/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4730235.09                 A    =         6788237.55  meter
     Y    =       -4692192.88  meter          E    =           .0002650
     Z    =       -1293079.45                 I    =           51.87842
     XDOT =       4199.207003                 Wp   =          145.92099
     YDOT =      -2623.219030  meter/sec      RA   =           36.00880  deg
     ZDOT =      -5850.255737                 TA   =           48.09413
                                              MA   =           48.07153
                                              Ha   =            220.648  n.mi
                                              Hp   =            215.741
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15519143.99                 X    =        -4671133.18
     Y    =      -15394333.59  feet           Y    =        -4744759.00  meter
     Z    =       -4242386.64                 Z    =        -1315913.86
     XDOT =      13776.925863                 XDOT =        4256.646031
     YDOT =      -8606.361646  feet/sec       YDOT =       -2575.939667  meter/sec
     ZDOT =     -19193.752417                 ZDOT =       -5829.717756
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1253558.39                 X    =          382084.60
     Y    =      -21804290.49  feet           Y    =        -6645947.74  meter
     Z    =       -4339203.71                 Z    =        -1322589.29
     XDOT =      14068.719026                 XDOT =        4288.145559
     YDOT =       4605.857600  feet/sec       YDOT =        1403.865396  meter/sec
     ZDOT =     -19105.330529                 ZDOT =       -5823.304745
  
  
    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   15033.52959780  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6439  36.4535 0006177 320.7075  39.3629 15.54247463  7089
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15033.52959780   =   yrday.fracday
    Element set:     903
    Inclination:       51.6439  deg
    RA of node:        36.4535  deg
    Eccentricity:     .0006177     
    Arg of perigee:   320.7075  deg
    Mean anomaly:      39.3629  deg
    Mean motion:   15.54247463  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             708
    Checksum:              320
 
 
    Coasting Arc #5 (Orbit 723)
    ---------------------------------------
 
    Vector Time (GMT): 2015/034/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3691893.24                 A    =         6785177.16  meter
     Y    =        4886057.21  meter          E    =           .0011615
     Z    =        2904261.31                 I    =           51.84250
     XDOT =      -5633.993702                 Wp   =           53.31749
     YDOT =       1246.596877  meter/sec      RA   =           31.04800  deg
     ZDOT =       5057.475285                 TA   =          339.70329
                                              MA   =          339.74942
                                              Ha   =            220.639  n.mi
                                              Hp   =            215.536
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12112510.62                 X    =         3622874.35
     Y    =       16030371.43  feet           Y    =         4926956.54  meter
     Z    =        9528416.38                 Z    =         2922027.59
     XDOT =     -18484.231305                 XDOT =       -5672.081419
     YDOT =       4089.884768  feet/sec       YDOT =        1183.381073  meter/sec
     ZDOT =      16592.766684                 ZDOT =        5030.014580
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3672203.91                 X    =        -1119287.75
     Y    =       19717102.89  feet           Y    =         6009772.96  meter
     Z    =        9603500.01                 Z    =         2927146.80
     XDOT =     -14140.033512                 XDOT =       -4309.882214
     YDOT =     -10669.311072  feet/sec       YDOT =       -3252.006015  meter/sec
     ZDOT =      16474.986343                 ZDOT =        5021.575837
  
  
    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   15034.55833549  .00016717  00000-0  10270-3 0  9046
    2 25544  51.6437  31.3240 0006264 323.4166  36.6558 15.54306250  7241
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15034.55833549   =   yrday.fracday
    Element set:     904
    Inclination:       51.6437  deg
    RA of node:        31.3240  deg
    Eccentricity:     .0006264     
    Arg of perigee:   323.4166  deg
    Mean anomaly:      36.6558  deg
    Mean motion:   15.54306250  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             724
    Checksum:              291
 
 
    Coasting Arc #6 (Orbit 738)
    ---------------------------------------
 
    Vector Time (GMT): 2015/035/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2278121.84                 A    =         6781243.46  meter
     Y    =       -4807051.17  meter          E    =           .0009143
     Z    =       -4214749.36                 I    =           51.80151
     XDOT =       6714.314897                 Wp   =           27.53842
     YDOT =         55.225176  meter/sec      RA   =           26.07423  deg
     ZDOT =      -3687.441825                 TA   =          204.66788
                                              MA   =          204.71163
                                              Ha   =            220.849  n.mi
                                              Hp   =            215.292
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7474153.01                 X    =        -2203725.78
     Y    =      -15771165.27  feet           Y    =        -4832110.84  meter
     Z    =      -13827917.86                 Z    =        -4225634.85
     XDOT =      22028.592181                 XDOT =        6731.110104
     YDOT =        181.184962  feet/sec       YDOT =         130.402755  meter/sec
     ZDOT =     -12097.906251                 ZDOT =       -3654.785008
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6356302.79                 X    =         1937401.09
     Y    =      -16214979.32  feet           Y    =        -4942325.70  meter
     Z    =      -13873564.44                 Z    =        -4228662.44
     XDOT =      13902.994246                 XDOT =        4237.632646
     YDOT =      15694.591125  feet/sec       YDOT =        4783.711375  meter/sec
     ZDOT =     -11958.146559                 ZDOT =       -3644.843071
  
  
    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   15035.52275965  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6434  26.5141 0006254 328.4106  31.6670 15.54306110  7393
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15035.52275965   =   yrday.fracday
    Element set:     905
    Inclination:       51.6434  deg
    RA of node:        26.5141  deg
    Eccentricity:     .0006254     
    Arg of perigee:   328.4106  deg
    Mean anomaly:      31.6670  deg
    Mean motion:   15.54306110  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             739
    Checksum:              284
 
 
    Coasting Arc #7 (Orbit 754)
    ---------------------------------------
 
    Vector Time (GMT): 2015/036/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         567918.67                 A    =         6777857.70  meter
     Y    =        4483449.43  meter          E    =           .0002913
     Z    =        5049259.42                 I    =           51.76176
     XDOT =      -7329.487504                 Wp   =           31.50759
     YDOT =      -1216.408851  meter/sec      RA   =           21.08839  deg
     ZDOT =       1906.418309                 TA   =           40.05573
                                              MA   =           40.03425
                                              Ha   =            220.955  n.mi
                                              Hp   =            215.129
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1863250.23                 X    =          493214.64
     Y    =       14709479.75  feet           Y    =         4489382.89  meter
     Z    =       16565811.74                 Z    =         5051836.47
     XDOT =     -24046.875012                 XDOT =       -7324.601044
     YDOT =      -3990.842686  feet/sec       YDOT =       -1298.344513  meter/sec
     ZDOT =       6254.653246                 ZDOT =        1870.825859
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9263021.51                 X    =        -2823368.96
     Y    =       11562895.03  feet           Y    =         3524370.40  meter
     Z    =       16575961.68                 Z    =         5052353.12
     XDOT =     -13187.992156                 XDOT =       -4019.700009
     YDOT =     -19304.135255  feet/sec       YDOT =       -5883.900426  meter/sec
     ZDOT =       6102.564633                 ZDOT =        1860.061700
  
  
    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   15036.55145634  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6434  21.3842 0006383 331.7444  28.3361 15.54344994  7559
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15036.55145634   =   yrday.fracday
    Element set:     906
    Inclination:       51.6434  deg
    RA of node:        21.3842  deg
    Eccentricity:     .0006383     
    Arg of perigee:   331.7444  deg
    Mean anomaly:      28.3361  deg
    Mean motion:   15.54344994  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             755
    Checksum:              304
 
 
    Coasting Arc #8 (Orbit 769)
    ---------------------------------------
 
    Vector Time (GMT): 2015/037/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1265301.12                 A    =         6776664.75  meter
     Y    =       -4008332.14  meter          E    =           .0013456
     Z    =       -5326079.09                 I    =           51.72841
     XDOT =       7337.910574                 Wp   =           65.45123
     YDOT =       2196.057752  meter/sec      RA   =           16.09359  deg
     ZDOT =         96.169450                 TA   =          205.43191
                                              MA   =          205.49818
                                              Ha   =            221.038  n.mi
                                              Hp   =            214.953
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4151250.40                 X    =         1335900.76
     Y    =      -13150696.00  feet           Y    =        -3993788.37  meter
     Z    =      -17474012.75                 Z    =        -5319760.85
     XDOT =      24074.509758                 XDOT =        7312.341228
     YDOT =       7204.913886  feet/sec       YDOT =        2277.972089  meter/sec
     ZDOT =        315.516567                 ZDOT =         131.752581
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12261468.99                 X    =         3737295.75
     Y    =       -6387621.01  feet           Y    =        -1946946.88  meter
     Z    =      -17446188.20                 Z    =        -5317598.16
     XDOT =      11642.691509                 XDOT =        3548.692372
     YDOT =      21123.112279  feet/sec       YDOT =        6438.324623  meter/sec
     ZDOT =        467.363959                 ZDOT =         142.452535
  
  
    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   15037.51583950  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6437  16.5749 0006331 335.9396  24.1461 15.54367501  7700
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15037.51583950   =   yrday.fracday
    Element set:     907
    Inclination:       51.6437  deg
    RA of node:        16.5749  deg
    Eccentricity:     .0006331     
    Arg of perigee:   335.9396  deg
    Mean anomaly:      24.1461  deg
    Mean motion:   15.54367501  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             770
    Checksum:              310
 
 
    Coasting Arc #9 (Orbit 785)
    ---------------------------------------
 
    Vector Time (GMT): 2015/038/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3096241.08                 A    =         6778061.92  meter
     Y    =        3400127.16  meter          E    =           .0009850
     Z    =        4979935.49                 I    =           51.70305
     XDOT =      -6725.839374                 Wp   =           17.23601
     YDOT =      -3017.898832  meter/sec      RA   =           11.09691  deg
     ZDOT =      -2110.964481                 TA   =           93.35489
                                              MA   =           93.24221
                                              Ha   =            221.159  n.mi
                                              Hp   =            214.716
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10158271.26                 X    =        -3158222.22
     Y    =       11155272.85  feet           Y    =         3365156.83  meter
     Z    =       16338371.03                 Z    =         4964744.00
     XDOT =     -22066.402145                 XDOT =       -6681.338549
     YDOT =      -9901.242886  feet/sec       YDOT =       -3092.862903  meter/sec
     ZDOT =      -6925.736487                 ZDOT =       -2143.528385
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15124023.33                 X    =        -4609802.31
     Y    =        1017938.05  feet           Y    =          310267.52  meter
     Z    =       16272697.25                 Z    =         4959918.12
     XDOT =      -9067.373142                 XDOT =       -2763.735334
     YDOT =     -21245.530047  feet/sec       YDOT =       -6475.637558  meter/sec
     ZDOT =      -7064.492579                 ZDOT =       -2153.257338
  
  
    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   15038.54449300  .00016717  00000-0  10270-3 0  9081
    2 25544  51.6439  11.4449 0006416 339.1014  20.9876 15.54413612  7866
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15038.54449300   =   yrday.fracday
    Element set:     908
    Inclination:       51.6439  deg
    RA of node:        11.4449  deg
    Eccentricity:     .0006416     
    Arg of perigee:   339.1014  deg
    Mean anomaly:      20.9876  deg
    Mean motion:   15.54413612  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             786
    Checksum:              301
 
 
    Coasting Arc #10 (Orbit 800)
    ---------------------------------------
 
    Vector Time (GMT): 2015/039/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4683225.43                 A    =         6781532.29  meter
     Y    =       -2735451.64  meter          E    =           .0006294
     Z    =       -4072424.96                 I    =           51.68392
     XDOT =       5504.545388                 Wp   =           50.81412
     YDOT =       3667.836894  meter/sec      RA   =            6.10579  deg
     ZDOT =       3874.348058                 TA   =          259.25328
                                              MA   =          259.32415
                                              Ha   =            221.280  n.mi
                                              Hp   =            214.582
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15364912.82                 X    =         4733247.85
     Y    =       -8974578.88  feet           Y    =        -2682801.42  meter
     Z    =      -13360974.27                 Z    =        -4049553.37
     XDOT =      18059.532114                 XDOT =        5444.301808
     YDOT =      12033.585610  feet/sec       YDOT =        3729.055791  meter/sec
     ZDOT =      12711.115675                 ZDOT =        3900.941044
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17450499.10                 X    =         5318912.13
     Y    =        3837119.37  feet           Y    =         1169553.98  meter
     Z    =      -13262572.96                 Z    =        -4042432.24
     XDOT =       5383.563508                 XDOT =        1640.910157
     YDOT =      19751.720364  feet/sec       YDOT =        6020.324367  meter/sec
     ZDOT =      12824.185461                 ZDOT =        3908.811729
  
  
    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   15039.50883525  .00016717  00000-0  10270-3 0  9090
    2 25544  51.6442   6.6357 0006445 343.1728  16.9210 15.54425606  8014
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15039.50883525   =   yrday.fracday
    Element set:     909
    Inclination:       51.6442  deg
    RA of node:         6.6357  deg
    Eccentricity:     .0006445     
    Arg of perigee:   343.1728  deg
    Mean anomaly:      16.9210  deg
    Mean motion:   15.54425606  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             801
    Checksum:              298
 
 
    Coasting Arc #11 (Orbit 816)
    ---------------------------------------
 
    Vector Time (GMT): 2015/040/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5918557.10                 A    =         6785389.07  meter
     Y    =        1983753.61  meter          E    =           .0012203
     Z    =        2655114.24                 I    =           51.66631
     XDOT =      -3752.014195                 Wp   =           74.04905
     YDOT =      -4192.464812  meter/sec      RA   =            1.12349  deg
     ZDOT =      -5208.109848                 TA   =           76.01766
                                              MA   =           75.88199
                                              Ha   =            221.256  n.mi
                                              Hp   =            214.318
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19417838.24                 X    =        -5953197.42
     Y    =        6508377.97  feet           Y    =         1917374.97  meter
     Z    =        8711004.74                 Z    =         2626279.09
     XDOT =     -12309.757858                 XDOT =       -3679.555462
     YDOT =     -13754.805814  feet/sec       YDOT =       -4234.017561  meter/sec
     ZDOT =     -17086.974566                 ZDOT =       -5226.159853
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18887198.03                 X    =        -5756817.96
     Y    =       -8051463.25  feet           Y    =        -2454086.00  meter
     Z    =        8587241.67                 Z    =         2617391.26
     XDOT =       -587.165965                 XDOT =        -178.968186
     YDOT =     -17010.433326  feet/sec       YDOT =       -5184.780078  meter/sec
     ZDOT =     -17163.381329                 ZDOT =       -5231.398629
  
  
    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   15040.53744482  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6447   1.5054 0006473 346.7166  13.3815 15.54485466  8172
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15040.53744482   =   yrday.fracday
    Element set:     910
    Inclination:       51.6447  deg
    RA of node:         1.5054  deg
    Eccentricity:     .0006473     
    Arg of perigee:   346.7166  deg
    Mean anomaly:      13.3815  deg
    Mean motion:   15.54485466  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             817
    Checksum:              301
 
 
    Coasting Arc #12 (Orbit 831)
    ---------------------------------------
 
    Vector Time (GMT): 2015/041/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6606128.39                 A    =         6787858.13  meter
     Y    =       -1193195.21  meter          E    =           .0015031
     Z    =        -943734.94                 I    =           51.64333
     XDOT =       1668.197906                 Wp   =           19.93107
     YDOT =       4584.855535  meter/sec      RA   =          356.14912  deg
     ZDOT =       5922.137330                 TA   =          329.84291
                                              MA   =          329.92935
                                              Ha   =            221.314  n.mi
                                              Hp   =            214.057
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21673649.56                 X    =         6623564.26
     Y    =       -3914682.46  feet           Y    =        -1119223.76  meter
     Z    =       -3096243.24                 Z    =         -911601.53
     XDOT =       5473.090244                 XDOT =        1588.037747
     YDOT =      15042.176952  feet/sec       YDOT =        4603.062646  meter/sec
     ZDOT =      19429.584416                 ZDOT =        5930.045993
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19021237.15                 X    =         5797673.08
     Y    =       11139935.94  feet           Y    =         3395452.48  meter
     Z    =       -2958531.80                 Z    =         -901760.49
     XDOT =      -4912.157111                 XDOT =       -1497.225488
     YDOT =      13518.351238  feet/sec       YDOT =        4120.393457  meter/sec
     ZDOT =      19462.520934                 ZDOT =        5932.176381
  
  
    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   15041.50174519  .00016717  00000-0  10270-3 0  9112
    2 25544  51.6446 356.6961 0006406 350.3340   9.7689 15.54516345  8329
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15041.50174519   =   yrday.fracday
    Element set:     911
    Inclination:       51.6446  deg
    RA of node:       356.6961  deg
    Eccentricity:     .0006406     
    Arg of perigee:   350.3340  deg
    Mean anomaly:       9.7689  deg
    Mean motion:   15.54516345  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             832
    Checksum:              305
 
 
    Coasting Arc #13 (Orbit 847)
    ---------------------------------------
 
    Vector Time (GMT): 2015/042/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6717739.55                 A    =         6787696.11  meter
     Y    =         303450.98  meter          E    =           .0005580
     Z    =        -922215.63                 I    =           51.61273
     XDOT =        589.497702                 Wp   =          102.43545
     YDOT =      -4834.802414  meter/sec      RA   =          351.17630  deg
     ZDOT =      -5916.419197                 TA   =           87.54660
                                              MA   =           87.48272
                                              Ha   =            221.326  n.mi
                                              Hp   =            213.857
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22039827.94                 X    =        -6716153.80
     Y    =         995574.08  feet           Y    =          228337.65  meter
     Z    =       -3025641.83                 Z    =         -954844.97
     XDOT =       1934.047579                 XDOT =         672.257274
     YDOT =     -15862.212643  feet/sec       YDOT =       -4827.747905  meter/sec
     ZDOT =     -19410.824136                 ZDOT =       -5913.354239
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17601232.54                 X    =        -5364855.68
     Y    =      -13269409.34  feet           Y    =        -4044515.97  meter
     Z    =       -3165293.14                 Z    =         -964781.35
     XDOT =      10729.417209                 XDOT =        3270.326365
     YDOT =      -9628.660955  feet/sec       YDOT =       -2934.815859  meter/sec
     ZDOT =     -19396.763297                 ZDOT =       -5912.133453
  
  
    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   15042.53030992  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6455 351.5654 0006468 353.6536   6.4534 15.54552437  8485
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15042.53030992   =   yrday.fracday
    Element set:     912
    Inclination:       51.6455  deg
    RA of node:       351.5654  deg
    Eccentricity:     .0006468     
    Arg of perigee:   353.6536  deg
    Mean anomaly:       6.4534  deg
    Mean motion:   15.54552437  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             848
    Checksum:              312
 
 
    Coasting Arc #14 (Orbit 863)
    ---------------------------------------
 
    Vector Time (GMT): 2015/043/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6199223.43                 A    =         6784911.11  meter
     Y    =         646726.14  meter          E    =           .0015826
     Z    =        2655863.39                 I    =           51.57271
     XDOT =      -2749.070657                 Wp   =           54.28955
     YDOT =       4927.062827  meter/sec      RA   =          346.19715  deg
     ZDOT =       5204.285005                 TA   =          335.73610
                                              MA   =          335.81055
                                              Ha   =            221.262  n.mi
                                              Hp   =            213.651
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20338659.55                 X    =         6178629.79
     Y    =        2121804.93  feet           Y    =          715934.89  meter
     Z    =        8713462.57                 Z    =         2685927.66
     XDOT =      -9019.260687                 XDOT =       -2829.242135
     YDOT =      16164.904289  feet/sec       YDOT =        4895.872930  meter/sec
     ZDOT =      17074.425870                 ZDOT =        5190.735708
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14523714.79                 X    =         4426828.27
     Y    =       14316745.83  feet           Y    =         4363744.13  meter
     Z    =        8841948.64                 Z    =         2695025.95
     XDOT =     -16176.817391                 XDOT =       -4930.693941
     YDOT =       5876.601287  feet/sec       YDOT =        1791.188072  meter/sec
     ZDOT =      17015.496575                 ZDOT =        5186.323356
  
  
    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   15043.55885118  .00016717  00000-0  10270-3 0  9135
    2 25544  51.6455 346.4350 0006407 357.3360   2.7758 15.54588414  8649
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15043.55885118   =   yrday.fracday
    Element set:     913
    Inclination:       51.6455  deg
    RA of node:       346.4350  deg
    Eccentricity:     .0006407     
    Arg of perigee:   357.3360  deg
    Mean anomaly:       2.7758  deg
    Mean motion:   15.54588414  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             864
    Checksum:              318
 
 
    Coasting Arc #15 (Orbit 878)
    ---------------------------------------
 
    Vector Time (GMT): 2015/044/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950073.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5146706.24                 A    =         6780663.07  meter
     Y    =       -1684227.87  meter          E    =           .0011495
     Z    =       -4093366.72                 I    =           51.52894
     XDOT =       4606.318462                 Wp   =           38.42846
     YDOT =      -4776.796523  meter/sec      RA   =          341.20455  deg
     ZDOT =      -3823.203336                 TA   =          191.94308
                                              MA   =          191.97036
                                              Ha   =            221.411  n.mi
                                              Hp   =            213.320
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16885519.15                 X    =        -5107606.49
     Y    =       -5525681.97  feet           Y    =        -1741563.23  meter
     Z    =      -13429680.83                 Z    =        -4118273.08
     XDOT =      15112.593379                 XDOT =        4677.962842
     YDOT =     -15671.904603  feet/sec       YDOT =       -4724.885236  meter/sec
     ZDOT =     -12543.318033                 ZDOT =       -3800.652800
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9930919.76                 X    =        -3026944.34
     Y    =      -14634432.08  feet           Y    =        -4460574.90  meter
     Z    =      -13535895.83                 Z    =        -4125741.05
     XDOT =      20533.523348                 XDOT =        6258.617916
     YDOT =      -2413.273586  feet/sec       YDOT =        -735.565789  meter/sec
     ZDOT =     -12445.915649                 ZDOT =       -3793.515090
  
  
    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   15044.52308755  .00016717  00000-0  10270-3 0  9141
    2 25544  51.6459 341.6246 0006482   1.0278 359.0888 15.54631601  8793
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15044.52308755   =   yrday.fracday
    Element set:     914
    Inclination:       51.6459  deg
    RA of node:       341.6246  deg
    Eccentricity:     .0006482     
    Arg of perigee:     1.0278  deg
    Mean anomaly:     359.0888  deg
    Mean motion:   15.54631601  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             879
    Checksum:              318
 
             

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