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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14248.1877
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   90.5
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.169
   ET - UTC  (sec) :   68.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
   273/17:05:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.0  
   000/00:00:00.000           0.0               0.0              213.6  
   
   278/01:56:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.1  
   000/00:00:00.000           0.0               0.0              213.3  
   
 
 
    Coasting Arc #1 (Orbit 2028)
    ---------------------------------------
 
    Vector Time (GMT): 2016/267/13:52:19.901
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1924217.74                 A    =         6782802.06  meter
     Y    =        5059089.68  meter          E    =           .0013212
     Z    =        4085773.28                 I    =           51.28141
     XDOT =      -4593.369540                 Wp   =           46.87101
     YDOT =       4825.469298  meter/sec      RA   =          286.41567  deg
     ZDOT =      -3795.053593                 TA   =           82.57890
                                              MA   =           82.42879
                                              Ha   =            222.376  n.mi
                                              Hp   =            214.750
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6313050.33                 X    =         1847655.70
     Y    =       16598063.24  feet           Y    =         5080179.79  meter
     Z    =       13404767.98                 Z    =         4094934.35
     XDOT =     -15070.110040                 XDOT =       -4628.552971
     YDOT =      15831.592185  feet/sec       YDOT =        4773.906157  meter/sec
     ZDOT =     -12450.963230                 ZDOT =       -3817.452926
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13705556.72                 X    =        -4177453.69
     Y    =      -11245361.75  feet           Y    =        -3427586.26  meter
     Z    =       13443870.97                 Z    =         4097691.87
     XDOT =       4219.575863                 XDOT =        1286.126723
     YDOT =     -20211.028162  feet/sec       YDOT =       -6160.321384  meter/sec
     ZDOT =     -12549.626154                 ZDOT =       -3825.126052
  
  
    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   16267.61921095  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6396 287.0031 0006645 354.8215   5.2868 15.53926117 20294
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16267.61921095   =   yrday.fracday
    Element set:     900
    Inclination:       51.6396  deg
    RA of node:       287.0031  deg
    Eccentricity:     .0006645     
    Arg of perigee:   354.8215  deg
    Mean anomaly:       5.2868  deg
    Mean motion:   15.53926117  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2029
    Checksum:              310
 
 
    Coasting Arc #2 (Orbit 2043)
    ---------------------------------------
 
    Vector Time (GMT): 2016/268/13:52:19.901
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1136137.68                 A    =         6786433.43  meter
     Y    =       -6035734.29  meter          E    =           .0009572
     Z    =       -2879011.40                 I    =           51.28543
     XDOT =       4770.757465                 Wp   =           25.58052
     YDOT =      -3286.903520  meter/sec      RA   =          281.41002  deg
     ZDOT =       5022.933824                 TA   =          301.46530
                                              MA   =          301.55883
                                              Ha   =            222.515  n.mi
                                              Hp   =            214.568
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3727485.83                 X    =        -1054575.12
     Y    =      -19802277.85  feet           Y    =        -6047983.53  meter
     Z    =       -9445575.46                 Z    =        -2884331.88
     XDOT =      15652.091419                 XDOT =        4782.758622
     YDOT =     -10783.804198  feet/sec       YDOT =       -3233.486204  meter/sec
     ZDOT =      16479.441680                 ZDOT =        5046.138391
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13356821.20                 X    =         4071159.10
     Y    =       15073165.88  feet           Y    =         4594300.96  meter
     Z    =       -9467748.01                 Z    =        -2885769.59
     XDOT =      -6655.312574                 XDOT =       -2028.539273
     YDOT =      16282.241898  feet/sec       YDOT =        4962.827330  meter/sec
     ZDOT =      16581.343799                 ZDOT =        5053.993590
  
  
    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   16268.58387757  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6398 282.1968 0006602    .0430    .0722 15.53908413 20441
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16268.58387757   =   yrday.fracday
    Element set:     901
    Inclination:       51.6398  deg
    RA of node:       282.1968  deg
    Eccentricity:     .0006602     
    Arg of perigee:      .0430  deg
    Mean anomaly:        .0722  deg
    Mean motion:   15.53908413  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2044
    Checksum:              296
 
 
    Coasting Arc #3 (Orbit 2059)
    ---------------------------------------
 
    Vector Time (GMT): 2016/269/13:52:19.901
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         348142.30                 A    =         6789080.16  meter
     Y    =        6640728.39  meter          E    =           .0012314
     Z    =        1356903.35                 I    =           51.28948
     XDOT =      -4823.334090                 Wp   =           90.38480
     YDOT =       1443.105613  meter/sec      RA   =          276.41123  deg
     ZDOT =      -5779.540043                 TA   =           74.76946
                                              MA   =           74.63334
                                              Ha   =            222.643  n.mi
                                              Hp   =            214.366
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1142199.16                 X    =          267266.87
     Y    =       21787166.64  feet           Y    =         6644169.48  meter
     Z    =        4451782.66                 Z    =         1358397.49
     XDOT =     -15824.586908                 XDOT =       -4811.038315
     YDOT =       4734.598467  feet/sec       YDOT =        1389.236069  meter/sec
     ZDOT =     -18961.745548                 ZDOT =       -5802.940818
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12502950.26                 X    =        -3810899.24
     Y    =      -17877740.69  feet           Y    =        -5449135.36  meter
     Z    =        4457156.09                 Z    =         1358541.18
     XDOT =       9494.882998                 XDOT =        2894.040338
     YDOT =     -11430.480349  feet/sec       YDOT =       -3484.010410  meter/sec
     ZDOT =     -19064.180410                 ZDOT =       -5810.762189
  
  
    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   16269.61284809  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6401 277.0682 0006810   3.0117 357.1075 15.53944959 20608
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16269.61284809   =   yrday.fracday
    Element set:     902
    Inclination:       51.6401  deg
    RA of node:       277.0682  deg
    Eccentricity:     .0006810     
    Arg of perigee:     3.0117  deg
    Mean anomaly:     357.1075  deg
    Mean motion:   15.53944959  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2060
    Checksum:              303
 
 
    Coasting Arc #4 (Orbit 2075)
    ---------------------------------------
 
    Vector Time (GMT): 2016/270/13:52:19.901
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         376165.20                 A    =         6789791.75  meter
     Y    =       -6763853.53  meter          E    =           .0018080
     Z    =         260315.13                 I    =           51.28829
     XDOT =       4782.191169                 Wp   =           34.19815
     YDOT =        503.347868  meter/sec      RA   =          271.41826  deg
     ZDOT =       5980.366047                 TA   =          328.62250
                                              MA   =          328.73024
                                              Ha   =            222.612  n.mi
                                              Hp   =            214.224
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1234137.80                 X    =          450507.88
     Y    =      -22191120.50  feet           Y    =        -6759231.29  meter
     Z    =         854052.27                 Z    =          262323.74
     XDOT =      15689.603572                 XDOT =        4747.157206
     YDOT =       1651.403767  feet/sec       YDOT =         556.630299  meter/sec
     ZDOT =      19620.623513                 ZDOT =        6003.511528
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11065029.54                 X    =         3372621.01
     Y    =       19274776.02  feet           Y    =         5874951.73  meter
     Z    =         863979.61                 Z    =          263340.99
     XDOT =     -12543.041372                 XDOT =       -3823.119010
     YDOT =       6289.241703  feet/sec       YDOT =        1916.960871  meter/sec
     ZDOT =      19721.610056                 ZDOT =        6011.146745
  
  
    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   16270.64181344  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6390 271.9413 0006583   7.2994 352.8254 15.53961783 20768
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16270.64181344   =   yrday.fracday
    Element set:     903
    Inclination:       51.6390  deg
    RA of node:       271.9413  deg
    Eccentricity:     .0006583     
    Arg of perigee:     7.2994  deg
    Mean anomaly:     352.8254  deg
    Mean motion:   15.53961783  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2076
    Checksum:              319
 
 
    Coasting Arc #5 (Orbit 2090)
    ---------------------------------------
 
    Vector Time (GMT): 2016/271/13:52:19.901
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1117460.47                 A    =         6788338.15  meter
     Y    =        6425293.84  meter          E    =           .0005752
     Z    =       -1891397.43                 I    =           51.28389
     XDOT =      -4638.095121                 Wp   =           77.77030
     YDOT =      -2446.562277  meter/sec      RA   =          266.42290  deg
     ZDOT =      -5584.259479                 TA   =          123.14467
                                              MA   =          123.08947
                                              Ha   =            222.817  n.mi
                                              Hp   =            214.090
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3666208.88                 X    =        -1180039.10
     Y    =       21080360.35  feet           Y    =         6412447.51  meter
     Z    =       -6205372.16                 Z    =        -1896978.56
     XDOT =     -15216.847509                 XDOT =       -4583.266431
     YDOT =      -8026.779123  feet/sec       YDOT =       -2498.122694  meter/sec
     ZDOT =     -18321.061284                 ZDOT =       -5606.656676
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8786125.15                 X    =        -2678010.94
     Y    =      -19501541.52  feet           Y    =        -5944069.85  meter
     Z    =       -6230827.16                 Z    =        -1899156.12
     XDOT =      15583.706328                 XDOT =        4749.913689
     YDOT =      -1150.059145  feet/sec       YDOT =        -350.538027  meter/sec
     ZDOT =     -18418.456117                 ZDOT =       -5613.945425
  
  
    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   16271.60646641  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6394 267.1333 0006790   9.9757 350.1529 15.53941752 20913
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16271.60646641   =   yrday.fracday
    Element set:     904
    Inclination:       51.6394  deg
    RA of node:       267.1333  deg
    Eccentricity:     .0006790     
    Arg of perigee:     9.9757  deg
    Mean anomaly:     350.1529  deg
    Mean motion:   15.53941752  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2091
    Checksum:              318
 
 
    Coasting Arc #6 (Orbit 2106)
    ---------------------------------------
 
    Vector Time (GMT): 2016/272/13:52:19.901
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1834645.40                 A    =         6785082.56  meter
     Y    =       -5621156.28  meter          E    =           .0015620
     Z    =        3308201.60                 I    =           51.27714
     XDOT =       4418.091792                 Wp   =           64.18565
     YDOT =       4195.481065  meter/sec      RA   =          261.42214  deg
     ZDOT =       4668.087080                 TA   =          334.55731
                                              MA   =          334.63413
                                              Ha   =            222.706  n.mi
                                              Hp   =            213.975
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6019177.83                 X    =         1881296.41
     Y    =      -18442113.78  feet           Y    =        -5600378.75  meter
     Z    =       10853679.79                 Z    =         3317227.94
     XDOT =      14495.051812                 XDOT =        4348.172908
     YDOT =      13764.701656  feet/sec       YDOT =        4244.496831  meter/sec
     ZDOT =      15315.246324                 ZDOT =        4689.378684
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5704068.76                 X    =         1738600.16
     Y    =       18518317.80  feet           Y    =         5644383.27  meter
     Z    =       10894031.97                 Z    =         3320500.94
     XDOT =     -18337.654087                 XDOT =       -5589.316966
     YDOT =      -3435.841432  feet/sec       YDOT =       -1047.244468  meter/sec
     ZDOT =      15407.529897                 ZDOT =        4696.215113
  
  
    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   16272.63542080  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6402 262.0059 0006646  12.9506 347.1816 15.53979321 21074
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16272.63542080   =   yrday.fracday
    Element set:     905
    Inclination:       51.6402  deg
    RA of node:       262.0059  deg
    Eccentricity:     .0006646     
    Arg of perigee:    12.9506  deg
    Mean anomaly:     347.1816  deg
    Mean motion:   15.53979321  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2107
    Checksum:              296
 
 
    Coasting Arc #7 (Orbit 2121)
    ---------------------------------------
 
    Vector Time (GMT): 2016/273/13:52:19.901
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2580456.35                 A    =         6781458.97  meter
     Y    =        4452066.87  meter          E    =           .0014518
     Z    =       -4431745.73                 I    =           51.27028
     XDOT =      -4055.047434                 Wp   =           47.40417
     YDOT =      -5609.409134  meter/sec      RA   =          256.41075  deg
     ZDOT =      -3271.235659                 TA   =          189.37030
                                              MA   =          189.39742
                                              Ha   =            222.990  n.mi
                                              Hp   =            213.703
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8466064.14                 X    =        -2608521.10
     Y    =       14606518.62  feet           Y    =         4423052.92  meter
     Z    =      -14539848.20                 Z    =        -4444349.81
     XDOT =     -13303.961396                 XDOT =       -3976.129886
     YDOT =     -18403.573275  feet/sec       YDOT =       -5654.314617  meter/sec
     ZDOT =     -10732.400456                 ZDOT =       -3290.741649
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1807293.17                 X    =         -550862.96
     Y    =      -16737184.09  feet           Y    =        -5101493.71  meter
     Z    =      -14595621.73                 Z    =        -4448745.50
     XDOT =      20302.194129                 XDOT =        6188.108771
     YDOT =       7248.316144  feet/sec       YDOT =        2209.286761  meter/sec
     ZDOT =     -10816.664729                 ZDOT =       -3296.919410
  
  
    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   16273.60006292  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6399 257.1977 0006901  17.0339 343.1044 15.53958786 21225
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16273.60006292   =   yrday.fracday
    Element set:     906
    Inclination:       51.6399  deg
    RA of node:       257.1977  deg
    Eccentricity:     .0006901     
    Arg of perigee:    17.0339  deg
    Mean anomaly:     343.1044  deg
    Mean motion:   15.53958786  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2122
    Checksum:              316
 
 
    Coasting Arc #8 (Orbit 2123)
    ---------------------------------------
 
    Vector Time (GMT): 2016/273/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3980632.05                 A    =         6777886.51  meter
     Y    =        1537195.32  meter          E    =           .0018429
     Z    =       -5281180.56                 I    =           51.26196
     XDOT =      -2227.260139                 Wp   =           66.01140
     YDOT =      -7310.834900  meter/sec      RA   =          255.72228  deg
     ZDOT =       -443.070362                 TA   =          199.69772
                                              MA   =          199.76899
                                              Ha   =            222.971  n.mi
                                              Hp   =            213.590
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13059816.43                 X    =        -3971871.68
     Y    =        5043291.74  feet           Y    =         1492729.43  meter
     Z    =      -17326707.87                 Z    =        -5300496.51
     XDOT =      -7307.283922                 XDOT =       -2143.190731
     YDOT =     -23985.678806  feet/sec       YDOT =       -7335.271622  meter/sec
     ZDOT =      -1453.642921                 ZDOT =        -453.684620
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3727028.29                 X    =        -1135998.22
     Y    =      -13385207.94  feet           Y    =        -4079811.38  meter
     Z    =      -17411314.45                 Z    =        -5306968.64
     XDOT =      23617.368224                 XDOT =        7198.573835
     YDOT =      -4600.480875  feet/sec       YDOT =       -1402.226571  meter/sec
     ZDOT =      -1498.799167                 ZDOT =        -456.833986
  
  
    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   16273.72868167  .00016717  00000-0  10270-3 0  9078
    2 25544  51.6424 256.5580 0006928  17.5952 342.5439 15.53971620 21247
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16273.72868167   =   yrday.fracday
    Element set:     907
    Inclination:       51.6424  deg
    RA of node:       256.5580  deg
    Eccentricity:     .0006928     
    Arg of perigee:    17.5952  deg
    Mean anomaly:     342.5439  deg
    Mean motion:   15.53971620  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2124
    Checksum:              329
 
 
    Coasting Arc #9 (Orbit 2139)
    ---------------------------------------
 
    Vector Time (GMT): 2016/274/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4421557.65                 A    =         6778381.14  meter
     Y    =         175326.70  meter          E    =           .0010866
     Z    =        5131440.45                 I    =           51.27266
     XDOT =       1378.995700                 Wp   =           33.65895
     YDOT =       7409.357913  meter/sec      RA   =          250.69855  deg
     ZDOT =      -1431.027386                 TA   =           70.23416
                                              MA   =           70.11701
                                              Ha   =            222.830  n.mi
                                              Hp   =            213.637
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14506422.73                 X    =         4394341.93
     Y    =         575218.84  feet           Y    =          224620.11  meter
     Z    =       16835434.55                 Z    =         5152853.32
     XDOT =       4524.264107                 XDOT =        1302.991257
     YDOT =      24308.917036  feet/sec       YDOT =        7424.353589  meter/sec
     ZDOT =      -4694.971738                 ZDOT =       -1424.514218
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1762177.15                 X    =         -537111.60
     Y    =       14300538.99  feet           Y    =         4358804.28  meter
     Z    =       16928920.52                 Z    =         5159934.98
     XDOT =     -23558.521711                 XDOT =       -7180.637418
     YDOT =       2662.643836  feet/sec       YDOT =         811.573841  meter/sec
     ZDOT =      -4667.727360                 ZDOT =       -1422.723299
  
  
    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   16274.75762549  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6422 251.4305 0006855  19.6630 340.4786 15.54004819 21407
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16274.75762549   =   yrday.fracday
    Element set:     908
    Inclination:       51.6422  deg
    RA of node:       251.4305  deg
    Eccentricity:     .0006855     
    Arg of perigee:    19.6630  deg
    Mean anomaly:     340.4786  deg
    Mean motion:   15.54004819  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2140
    Checksum:              311
 
 
    Coasting Arc #10 (Orbit 2154)
    ---------------------------------------
 
    Vector Time (GMT): 2016/275/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4759201.96                 A    =         6781056.87  meter
     Y    =       -1764009.69  meter          E    =           .0012223
     Z    =       -4505540.43                 I    =           51.29419
     XDOT =       -384.653737                 Wp   =           76.31452
     YDOT =      -6973.612810  meter/sec      RA   =          245.67964  deg
     ZDOT =       3146.669964                 TA   =          225.39718
                                              MA   =          225.49697
                                              Ha   =            223.020  n.mi
                                              Hp   =            213.436
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15614179.67                 X    =        -4717236.40
     Y    =       -5787433.37  feet           Y    =        -1816996.29  meter
     Z    =      -14781956.81                 Z    =        -4528557.54
     XDOT =      -1261.987327                 XDOT =        -321.929789
     YDOT =     -22879.307120  feet/sec       YDOT =       -6977.563103  meter/sec
     ZDOT =      10323.720354                 ZDOT =        3144.954744
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6790059.68                 X    =         2069610.19
     Y    =      -15106903.48  feet           Y    =        -4604584.18  meter
     Z    =      -14882197.27                 Z    =        -4536093.73
     XDOT =      21814.722808                 XDOT =        6649.127512
     YDOT =       -326.613098  feet/sec       YDOT =         -99.551672  meter/sec
     ZDOT =      10317.347999                 ZDOT =        3144.727670
  
  
    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   16275.72225637  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6434 246.6229 0006881  23.1679 336.9782 15.53977200 21557
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16275.72225637   =   yrday.fracday
    Element set:     909
    Inclination:       51.6434  deg
    RA of node:       246.6229  deg
    Eccentricity:     .0006881     
    Arg of perigee:    23.1679  deg
    Mean anomaly:     336.9782  deg
    Mean motion:   15.53977200  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2155
    Checksum:              332
 
 
    Coasting Arc #11 (Orbit 2170)
    ---------------------------------------
 
    Vector Time (GMT): 2016/276/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4918569.99                 A    =         6784770.03  meter
     Y    =        3200866.33  meter          E    =           .0016854
     Z    =        3397915.09                 I    =           51.32070
     XDOT =       -783.996521                 Wp   =           68.54583
     YDOT =       6097.489537  meter/sec      RA   =          240.67072  deg
     ZDOT =      -4584.581974                 TA   =           71.52236
                                              MA   =           71.33925
                                              Ha   =            223.149  n.mi
                                              Hp   =            213.322
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16137040.64                 X    =         4865905.66
     Y    =       10501529.94  feet           Y    =         3255575.07  meter
     Z    =       11148015.39                 Z    =         3421680.28
     XDOT =      -2572.167063                 XDOT =        -829.851668
     YDOT =      20004.886933  feet/sec       YDOT =        6088.465352  meter/sec
     ZDOT =     -15041.279441                 ZDOT =       -4588.502690
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11263814.34                 X    =        -3433210.61
     Y    =       15540243.61  feet           Y    =         4736666.25  meter
     Z    =       11251300.98                 Z    =         3429396.54
     XDOT =     -18727.994325                 XDOT =       -5708.292670
     YDOT =      -2613.650662  feet/sec       YDOT =        -796.640722  meter/sec
     ZDOT =     -15059.373421                 ZDOT =       -4590.097019
  
  
    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   16276.75118932  .00016717  00000-0  10270-3 0  9106
    2 25544  51.6433 241.4952 0006976  28.2084 331.9445 15.53982768 21717
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16276.75118932   =   yrday.fracday
    Element set:     910
    Inclination:       51.6433  deg
    RA of node:       241.4952  deg
    Eccentricity:     .0006976     
    Arg of perigee:    28.2084  deg
    Mean anomaly:     331.9445  deg
    Mean motion:   15.53982768  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2171
    Checksum:              327
 
 
    Coasting Arc #12 (Orbit 2185)
    ---------------------------------------
 
    Vector Time (GMT): 2016/277/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4861487.92                 A    =         6787942.33  meter
     Y    =       -4288554.12  meter          E    =           .0013503
     Z    =       -1995978.51                 I    =           51.34830
     XDOT =       2040.728433                 Wp   =           35.62987
     YDOT =      -4882.593272  meter/sec      RA   =          235.67232  deg
     ZDOT =       5549.989234                 TA   =          302.23489
                                              MA   =          302.36571
                                              Ha   =            223.115  n.mi
                                              Hp   =            213.245
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15949763.52                 X    =        -4803475.13
     Y    =      -14070059.45  feet           Y    =        -4342594.42  meter
     Z    =       -6548485.94                 Z    =        -2019453.37
     XDOT =       6695.303259                 XDOT =        2068.215237
     YDOT =     -16019.006798  feet/sec       YDOT =       -4859.618108  meter/sec
     ZDOT =      18208.626097                 ZDOT =        5559.970114
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14556373.71                 X    =         4436782.71
     Y    =      -15463801.25  feet           Y    =        -4713366.62  meter
     Z    =       -6650340.81                 Z    =        -2027023.88
     XDOT =      14678.451363                 XDOT =        4473.991975
     YDOT =       6008.578575  feet/sec       YDOT =        1831.414750  meter/sec
     ZDOT =      18252.991806                 ZDOT =        5563.511902
  
  
    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   16277.71580787  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6435 236.6880 0006895  30.5146 329.6407 15.54004668 21863
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16277.71580787   =   yrday.fracday
    Element set:     911
    Inclination:       51.6435  deg
    RA of node:       236.6880  deg
    Eccentricity:     .0006895     
    Arg of perigee:    30.5146  deg
    Mean anomaly:     329.6407  deg
    Mean motion:   15.54004668  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2186
    Checksum:              332
 
 
    Coasting Arc #13 (Orbit 2191)
    ---------------------------------------
 
    Vector Time (GMT): 2016/278/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1174398.76                 A    =         6780402.15  meter
     Y    =        4764025.52  meter          E    =           .0016333
     Z    =       -4695582.46                 I    =           51.32907
     XDOT =      -5791.896516                 Wp   =           57.61180
     YDOT =      -4164.906449  meter/sec      RA   =          233.86166  deg
     ZDOT =      -2775.532792                 TA   =          184.70847
                                              MA   =          184.72385
                                              Ha   =            223.106  n.mi
                                              Hp   =            213.278
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3853014.32                 X    =        -1204774.50
     Y    =       15630004.97  feet           Y    =         4750722.21  meter
     Z    =      -15405454.26                 Z    =        -4701361.84
     XDOT =     -19002.285156                 XDOT =       -5731.410418
     YDOT =     -13664.391237  feet/sec       YDOT =       -4229.337451  meter/sec
     ZDOT =      -9106.078715                 ZDOT =       -2803.521465
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7505024.02                 X    =         2287531.32
     Y    =       14213225.84  feet           Y    =         4332191.24  meter
     Z    =      -15431449.10                 Z    =        -4703505.69
     XDOT =     -22212.231680                 XDOT =       -6770.288216
     YDOT =       1704.878388  feet/sec       YDOT =         519.646933  meter/sec
     ZDOT =      -9227.672835                 ZDOT =       -2812.594680
  
  
    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   16278.10165448  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6431 234.7608 0006366  34.4766 325.6798 15.53984405 21921
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16278.10165448   =   yrday.fracday
    Element set:     912
    Inclination:       51.6431  deg
    RA of node:       234.7608  deg
    Eccentricity:     .0006366     
    Arg of perigee:    34.4766  deg
    Mean anomaly:     325.6798  deg
    Mean motion:   15.53984405  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2192
    Checksum:              328
 
 
    Coasting Arc #14 (Orbit 2207)
    ---------------------------------------
 
    Vector Time (GMT): 2016/279/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2405845.94                 A    =         6777938.21  meter
     Y    =       -3588083.27  meter          E    =           .0007682
     Z    =        5216282.82                 I    =           51.34199
     XDOT =       5577.700018                 Wp   =           66.29507
     YDOT =       5177.276585  meter/sec      RA   =          228.84462  deg
     ZDOT =        990.590676                 TA   =           14.20131
                                              MA   =           14.17972
                                              Ha   =            222.990  n.mi
                                              Hp   =            213.146
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7893195.33                 X    =         2420451.06
     Y    =      -11771926.73  feet           Y    =        -3561097.28  meter
     Z    =       17113788.78                 Z    =         5228005.88
     XDOT =      18299.540743                 XDOT =        5514.579892
     YDOT =      16985.815566  feet/sec       YDOT =        5239.297345  meter/sec
     ZDOT =       3249.969409                 ZDOT =        1017.532389
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2171698.07                 X    =         -661933.57
     Y    =      -13942375.30  feet           Y    =        -4249635.99  meter
     Z    =       17165560.18                 Z    =         5232062.74
     XDOT =      23934.351617                 XDOT =        7295.190373
     YDOT =        409.559065  feet/sec       YDOT =         124.833603  meter/sec
     ZDOT =       3366.844658                 ZDOT =        1026.214252
  
  
    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   16279.13057100  .00016717  00000-0  10270-3 0  9133
    2 25544  51.6438 229.6325 0006434  37.8877 322.2727 15.54042426 22085
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16279.13057100   =   yrday.fracday
    Element set:     913
    Inclination:       51.6438  deg
    RA of node:       229.6325  deg
    Eccentricity:     .0006434     
    Arg of perigee:    37.8877  deg
    Mean anomaly:     322.2727  deg
    Mean motion:   15.54042426  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2208
    Checksum:              302
 
 
    Coasting Arc #15 (Orbit 2222)
    ---------------------------------------
 
    Vector Time (GMT): 2016/280/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3634144.52                 A    =         6777887.48  meter
     Y    =        2322519.72  meter          E    =           .0019044
     Z    =       -5244522.42                 I    =           51.36339
     XDOT =      -4964.129421                 Wp   =           80.40361
     YDOT =      -5757.713018  meter/sec      RA   =          223.82743  deg
     ZDOT =        895.963798                 TA   =          198.18010
                                              MA   =          198.24828
                                              Ha   =            223.206  n.mi
                                              Hp   =            212.871
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11923046.33                 X    =        -3634369.34
     Y    =        7619815.36  feet           Y    =         2281878.55  meter
     Z    =      -17206438.39                 Z    =        -5262177.26
     XDOT =     -16286.513847                 XDOT =       -4903.728544
     YDOT =     -18890.134574  feet/sec       YDOT =       -5812.887440  meter/sec
     ZDOT =       2939.513772                 ZDOT =         871.996101
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3368761.78                 X    =        -1026798.59
     Y    =       13645491.11  feet           Y    =         4159145.69  meter
     Z    =      -17283927.75                 Z    =        -5268141.18
     XDOT =     -23826.935435                 XDOT =       -7262.449920
     YDOT =      -2314.916357  feet/sec       YDOT =        -705.586506  meter/sec
     ZDOT =       2835.706141                 ZDOT =         864.323232
  
  
    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   16280.09517518  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6435 224.8264 0006611  41.3824 318.7828 15.54031173 22236
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16280.09517518   =   yrday.fracday
    Element set:     914
    Inclination:       51.6435  deg
    RA of node:       224.8264  deg
    Eccentricity:     .0006611     
    Arg of perigee:    41.3824  deg
    Mean anomaly:     318.7828  deg
    Mean motion:   15.54031173  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2223
    Checksum:              295
 
 
    Coasting Arc #16 (Orbit 2238)
    ---------------------------------------
 
    Vector Time (GMT): 2016/281/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4758087.64                 A    =         6779989.29  meter
     Y    =       -1006763.07  meter          E    =           .0014096
     Z    =        4717547.09                 I    =           51.39427
     XDOT =       3970.896255                 Wp   =           54.53853
     YDOT =       5976.995528  meter/sec      RA   =          218.81297  deg
     ZDOT =      -2715.715535                 TA   =           62.46549
                                              MA   =           62.32232
                                              Ha   =            223.124  n.mi
                                              Hp   =            212.889
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15610523.74                 X    =         4746075.69
     Y    =       -3303028.46  feet           Y    =         -953621.73  meter
     Z    =       15477516.71                 Z    =         4740631.98
     XDOT =      13027.874851                 XDOT =        3916.956836
     YDOT =      19609.565382  feet/sec       YDOT =        6021.098944  meter/sec
     ZDOT =      -8909.827871                 ZDOT =       -2696.557088
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8795366.51                 X    =         2680827.71
     Y    =      -13194803.10  feet           Y    =        -4021775.98  meter
     Z    =       15578532.38                 Z    =         4748336.67
     XDOT =      22097.601330                 XDOT =        6735.348885
     YDOT =       4255.086372  feet/sec       YDOT =        1296.950326  meter/sec
     ZDOT =      -8827.050276                 ZDOT =       -2690.484924
  
  
    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   16281.12407871  .00016717  00000-0  10270-3 0  9151
    2 25544  51.6432 219.6982 0006605  45.0863 315.0824 15.54047327 22390
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16281.12407871   =   yrday.fracday
    Element set:     915
    Inclination:       51.6432  deg
    RA of node:       219.6982  deg
    Eccentricity:     .0006605     
    Arg of perigee:    45.0863  deg
    Mean anomaly:     315.0824  deg
    Mean motion:   15.54047327  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2239
    Checksum:              305
 
 
    Coasting Arc #17 (Orbit 2253)
    ---------------------------------------
 
    Vector Time (GMT): 2016/282/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5653025.20                 A    =         6783468.34  meter
     Y    =        -185233.58  meter          E    =           .0011120
     Z    =       -3751755.28                 I    =           51.43139
     XDOT =      -2614.669039                 Wp   =           75.09463
     YDOT =      -5820.449086  meter/sec      RA   =          213.80951  deg
     ZDOT =       4240.413726                 TA   =          239.91515
                                              MA   =          240.02546
                                              Ha   =            223.189  n.mi
                                              Hp   =            212.744
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18546670.61                 X    =        -5632309.05
     Y    =        -607721.71  feet           Y    =         -248333.94  meter
     Z    =      -12308908.39                 Z    =        -3779166.32
     XDOT =      -8578.310494                 XDOT =       -2569.987365
     YDOT =     -19095.961568  feet/sec       YDOT =       -5849.437931  meter/sec
     ZDOT =      13912.118522                 ZDOT =        4227.821086
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13426102.89                 X    =        -4092276.16
     Y    =       12693535.86  feet           Y    =         3868989.73  meter
     Z    =      -12428654.42                 Z    =        -3788253.87
     XDOT =     -18741.741247                 XDOT =       -5712.482732
     YDOT =      -6297.002089  feet/sec       YDOT =       -1919.326237  meter/sec
     ZDOT =      13857.991507                 ZDOT =        4223.915811
  
  
    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   16282.08866842  .00016717  00000-0  10270-3 0  9165
    2 25544  51.6428 214.8917 0006508  48.5089 311.6622 15.54052537 22544
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16282.08866842   =   yrday.fracday
    Element set:     916
    Inclination:       51.6428  deg
    RA of node:       214.8917  deg
    Eccentricity:     .0006508     
    Arg of perigee:    48.5089  deg
    Mean anomaly:     311.6622  deg
    Mean motion:   15.54052537  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2254
    Checksum:              323
 
             

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