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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  13813.3257
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   98.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.869
   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 
   ------------------------------------------------------------------------
   160/13:47:39.077          -0.2               1.9              2.0    
   N/A                        1.9              -0.2              220.2  
   000/00:05:18.153           0.2              -0.0              214.9  
   
   161/01:18:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.3  
   000/00:00:00.000           0.0               0.0              214.8  
   
 
 
    Coasting Arc #1 (Orbit 175)
    ---------------------------------------
 
    Vector Time (GMT): 2016/148/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4534160.59                 A    =         6783916.95  meter
     Y    =        4104747.54  meter          E    =           .0005594
     Z    =       -2938749.84                 I    =           51.76823
     XDOT =      -5317.486063                 Wp   =           82.21237
     YDOT =      -2283.418774  meter/sec      RA   =          160.08885  deg
     ZDOT =       5023.804118                 TA   =          244.32833
                                              MA   =          244.38612
                                              Ha   =            220.583  n.mi
                                              Hp   =            213.223
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14875854.94                 X    =        -4565448.68
     Y    =       13467019.50  feet           Y    =         4053868.84  meter
     Z    =       -9641567.70                 Z    =        -2960851.39
     XDOT =     -17445.820418                 XDOT =       -5315.960655
     YDOT =      -7491.531410  feet/sec       YDOT =       -2342.874325  meter/sec
     ZDOT =      16482.296976                 ZDOT =        4997.976526
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5818140.50                 X    =         1773369.23
     Y    =       19155238.93  feet           Y    =         5838516.83  meter
     Z    =       -9738458.03                 Z    =        -2968282.01
     XDOT =     -12892.566322                 XDOT =       -3929.654215
     YDOT =      12223.793173  feet/sec       YDOT =        3725.812159  meter/sec
     ZDOT =      16370.271755                 ZDOT =        4989.658831
  
  
    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   16148.50606296  .00016717  00000-0  10270-3 0  9001
    2 25544  51.6409 161.2087 0001609 124.5472 235.5834 15.54704009  1762
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16148.50606296   =   yrday.fracday
    Element set:     900
    Inclination:       51.6409  deg
    RA of node:       161.2087  deg
    Eccentricity:     .0001609     
    Arg of perigee:   124.5472  deg
    Mean anomaly:     235.5834  deg
    Mean motion:   15.54704009  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             176
    Checksum:              297
 
 
    Coasting Arc #2 (Orbit 191)
    ---------------------------------------
 
    Vector Time (GMT): 2016/149/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5613646.66                 A    =         6787057.59  meter
     Y    =       -3617200.68  meter          E    =           .0015310
     Z    =        1169261.02                 I    =           51.80753
     XDOT =       3481.091814                 Wp   =          122.33618
     YDOT =       3485.773462  meter/sec      RA   =          155.12127  deg
     ZDOT =      -5881.187280                 TA   =           44.98778
                                              MA   =           44.86385
                                              Ha   =            220.602  n.mi
                                              Hp   =            213.252
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18417475.90                 X    =         5647998.10
     Y    =      -11867456.30  feet           Y    =        -3554233.16  meter
     Z    =        3836158.20                 Z    =         1196613.99
     XDOT =      11420.904900                 XDOT =        3470.422669
     YDOT =      11436.264638  feet/sec       YDOT =        3524.642097  meter/sec
     ZDOT =     -19295.233858                 ZDOT =       -5864.302623
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3212491.55                 X    =         -979167.43
     Y    =      -21651496.27  feet           Y    =        -6599376.06  meter
     Z    =        3955838.08                 Z    =         1205739.45
     XDOT =      13602.725058                 XDOT =        4146.110598
     YDOT =      -5558.246545  feet/sec       YDOT =       -1694.153547  meter/sec
     ZDOT =     -19222.327342                 ZDOT =       -5858.965374
  
  
    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   16149.53452301  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6399 156.0773 0001584 123.1384 236.9921 15.54699194  1921
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16149.53452301   =   yrday.fracday
    Element set:     901
    Inclination:       51.6399  deg
    RA of node:       156.0773  deg
    Eccentricity:     .0001584     
    Arg of perigee:   123.1384  deg
    Mean anomaly:     236.9921  deg
    Mean motion:   15.54699194  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             192
    Checksum:              317
 
 
    Coasting Arc #3 (Orbit 207)
    ---------------------------------------
 
    Vector Time (GMT): 2016/150/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6108789.65                 A    =         6787371.00  meter
     Y    =        2857365.28  meter          E    =           .0013478
     Z    =         713623.96                 I    =           51.83669
     XDOT =      -1439.060440                 Wp   =           59.23670
     YDOT =      -4588.097841  meter/sec      RA   =          150.16214  deg
     ZDOT =       5975.276953                 TA   =          308.45457
                                              MA   =          308.57544
                                              Ha   =            220.484  n.mi
                                              Hp   =            213.332
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20041960.79                 X    =        -6143753.90
     Y    =        9374558.01  feet           Y    =         2788857.19  meter
     Z    =        2341285.95                 Z    =          683864.07
     XDOT =      -4721.326902                 XDOT =       -1416.673693
     YDOT =     -15052.814439  feet/sec       YDOT =       -4604.065540  meter/sec
     ZDOT =      19603.927010                 ZDOT =        5968.340436
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         636105.61                 X    =          193884.99
     Y    =       22130294.34  feet           Y    =         6745313.72  meter
     Z    =        2211242.19                 Z    =          673986.62
     XDOT =     -14124.378593                 XDOT =       -4305.110595
     YDOT =      -1576.563799  feet/sec       YDOT =        -480.536646  meter/sec
     ZDOT =      19574.510124                 ZDOT =        5966.310686
  
  
    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   16150.56297941  .00016717  00000-0  10270-3 0  9025
    2 25544  51.6390 150.9470 0001562 135.4428 224.6851 15.54736909  2080
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16150.56297941   =   yrday.fracday
    Element set:     902
    Inclination:       51.6390  deg
    RA of node:       150.9470  deg
    Eccentricity:     .0001562     
    Arg of perigee:   135.4428  deg
    Mean anomaly:     224.6851  deg
    Mean motion:   15.54736909  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             208
    Checksum:              309
 
 
    Coasting Arc #4 (Orbit 222)
    ---------------------------------------
 
    Vector Time (GMT): 2016/151/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6036673.71                 A    =         6785024.65  meter
     Y    =       -1760526.89  meter          E    =           .0006796
     Z    =       -2546020.75                 I    =           51.85532
     XDOT =       -624.669885                 Wp   =          130.88222
     YDOT =       5503.123801  meter/sec      RA   =          145.20013  deg
     ZDOT =      -5299.972172                 TA   =           77.62050
                                              MA   =           77.54445
                                              Ha   =            220.606  n.mi
                                              Hp   =            213.423
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19805359.94                 X    =         6068279.27
     Y    =       -5776006.87  feet           Y    =        -1692843.94  meter
     Z    =       -8353086.44                 Z    =        -2516619.18
     XDOT =      -2049.441881                 XDOT =        -660.415582
     YDOT =      18054.868115  feet/sec       YDOT =        5495.938726  meter/sec
     ZDOT =     -17388.360145                 ZDOT =       -5303.093233
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2233881.24                 X    =          680887.00
     Y    =      -20560920.10  feet           Y    =        -6266968.45  meter
     Z    =       -8224775.40                 Z    =        -2506911.54
     XDOT =      14450.419586                 XDOT =        4404.487890
     YDOT =       8513.426440  feet/sec       YDOT =        2594.892379  meter/sec
     ZDOT =     -17402.889650                 ZDOT =       -5304.400765
  
  
    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   16151.52715967  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6386 146.1358 0001493 130.6539 229.4744 15.54691068  2237
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16151.52715967   =   yrday.fracday
    Element set:     903
    Inclination:       51.6386  deg
    RA of node:       146.1358  deg
    Eccentricity:     .0001493     
    Arg of perigee:   130.6539  deg
    Mean anomaly:     229.4744  deg
    Mean motion:   15.54691068  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             223
    Checksum:              317
 
 
    Coasting Arc #5 (Orbit 238)
    ---------------------------------------
 
    Vector Time (GMT): 2016/152/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5439723.66                 A    =         6780863.13  meter
     Y    =         423033.47  meter          E    =           .0012000
     Z    =        4018581.46                 I    =           51.86758
     XDOT =       2461.164552                 Wp   =          105.07194
     YDOT =      -6092.837906  meter/sec      RA   =          140.23047  deg
     ZDOT =       3960.043353                 TA   =          303.86026
                                              MA   =          303.97440
                                              Ha   =            220.528  n.mi
                                              Hp   =            213.431
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17846862.40                 X    =        -5463570.59
     Y    =        1387905.07  feet           Y    =          362069.31  meter
     Z    =       13184322.37                 Z    =         3992098.44
     XDOT =       8074.686849                 XDOT =        2509.876868
     YDOT =     -19989.625676  feet/sec       YDOT =       -6065.043363  meter/sec
     ZDOT =      12992.268219                 ZDOT =        3972.117215
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5259743.34                 X    =        -1603169.77
     Y    =       17198870.37  feet           Y    =         5242215.69  meter
     Z    =       13068936.17                 Z    =         3983411.75
     XDOT =     -14431.644599                 XDOT =       -4398.765274
     YDOT =     -14359.078159  feet/sec       YDOT =       -4376.647023  meter/sec
     ZDOT =      13045.889850                 ZDOT =        3976.387226
  
  
    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   16152.55561201  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6386 141.0051 0001323 138.8136 221.3117 15.54723209  2391
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16152.55561201   =   yrday.fracday
    Element set:     904
    Inclination:       51.6386  deg
    RA of node:       141.0051  deg
    Eccentricity:     .0001323     
    Arg of perigee:   138.8136  deg
    Mean anomaly:     221.3117  deg
    Mean motion:   15.54723209  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             239
    Checksum:              266
 
 
    Coasting Arc #6 (Orbit 253)
    ---------------------------------------
 
    Vector Time (GMT): 2016/153/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4438668.84                 A    =         6777193.61  meter
     Y    =        1131939.37  meter          E    =           .0013272
     Z    =       -5006735.63                 I    =           51.87840
     XDOT =      -3944.601527                 Wp   =           79.75818
     YDOT =       6222.752570  meter/sec      RA   =          135.24863  deg
     ZDOT =      -2092.595997                 TA   =          169.93318
                                              MA   =          169.90657
                                              Ha   =            220.496  n.mi
                                              Hp   =            213.545
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14562561.82                 X    =         4450002.24
     Y    =        3713711.84  feet           Y    =         1181639.20  meter
     Z    =      -16426297.99                 Z    =        -4985145.77
     XDOT =     -12941.606060                 XDOT =       -4003.727655
     YDOT =      20415.854889  feet/sec       YDOT =        6178.310947  meter/sec
     ZDOT =      -6865.472432                 ZDOT =       -2111.901388
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8602855.92                 X    =         2622150.48
     Y    =      -12446851.73  feet           Y    =        -3793800.41  meter
     Z    =      -16332479.30                 Z    =        -4978139.69
     XDOT =      13715.230014                 XDOT =        4180.402108
     YDOT =      18589.526316  feet/sec       YDOT =        5666.087621  meter/sec
     ZDOT =      -6950.621984                 ZDOT =       -2118.549581
  
  
    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   16153.51978629  .00016717  00000-0  10270-3 0  9055
    2 25544  51.6379 136.1938 0001343 134.2772 225.8491 15.54694839  2547
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16153.51978629   =   yrday.fracday
    Element set:     905
    Inclination:       51.6379  deg
    RA of node:       136.1938  deg
    Eccentricity:     .0001343     
    Arg of perigee:   134.2772  deg
    Mean anomaly:     225.8491  deg
    Mean motion:   15.54694839  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             254
    Checksum:              336
 
 
    Coasting Arc #7 (Orbit 269)
    ---------------------------------------
 
    Vector Time (GMT): 2016/154/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3169257.39                 A    =         6775694.56  meter
     Y    =       -2725479.99  meter          E    =           .0003346
     Z    =        5329940.87                 I    =           51.89549
     XDOT =       4975.618300                 Wp   =          107.54234
     YDOT =      -5840.206345  meter/sec      RA   =          130.26097  deg
     ZDOT =        -28.801929                 TA   =          342.72531
                                              MA   =          342.73669
                                              Ha   =            220.545  n.mi
                                              Hp   =            213.479
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10397826.07                 X    =        -3164435.82
     Y    =       -8941863.50  feet           Y    =        -2760894.21  meter
     Z    =       17486682.64                 Z    =         5314556.64
     XDOT =      16324.207020                 XDOT =        5040.695059
     YDOT =     -19160.781973  feet/sec       YDOT =       -5784.201801  meter/sec
     ZDOT =        -94.494517                 ZDOT =          -4.473628
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11931385.37                 X    =        -3636686.26
     Y    =        6930780.67  feet           Y    =         2112501.95  meter
     Z    =       17420163.66                 Z    =         5309665.88
     XDOT =     -12121.114629                 XDOT =       -3694.515739
     YDOT =     -20905.972912  feet/sec       YDOT =       -6372.140544  meter/sec
     ZDOT =         12.483190                 ZDOT =           3.804876
  
  
    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   16154.54823663  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6377 131.0626 0001261 141.3673 218.7571 15.54695616  2703
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16154.54823663   =   yrday.fracday
    Element set:     906
    Inclination:       51.6377  deg
    RA of node:       131.0626  deg
    Eccentricity:     .0001261     
    Arg of perigee:   141.3673  deg
    Mean anomaly:     218.7571  deg
    Mean motion:   15.54695616  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             270
    Checksum:              304
 
 
    Coasting Arc #8 (Orbit 284)
    ---------------------------------------
 
    Vector Time (GMT): 2016/155/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1793657.42                 A    =         6777196.25  meter
     Y    =        4234809.02  meter          E    =           .0013527
     Z    =       -4990374.77                 I    =           51.92166
     XDOT =      -5507.770374                 Wp   =          108.85474
     YDOT =       4867.460399  meter/sec      RA   =          125.27445  deg
     ZDOT =       2151.387550                 TA   =          182.04978
                                              MA   =          182.05533
                                              Ha   =            220.405  n.mi
                                              Hp   =            213.560
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5884702.82                 X    =         1770410.90
     Y    =       13893730.39  feet           Y    =         4254737.43  meter
     Z    =      -16372620.65                 Z    =        -4981717.52
     XDOT =     -18070.112776                 XDOT =       -5572.240867
     YDOT =      15969.358265  feet/sec       YDOT =        4805.508146  meter/sec
     ZDOT =       7058.358105                 ZDOT =        2124.475654
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15074477.05                 X    =         4594700.60
     Y    =       -1278370.99  feet           Y    =         -389647.48  meter
     Z    =      -16335669.18                 Z    =        -4979111.97
     XDOT =       9312.178757                 XDOT =        2838.352085
     YDOT =      21143.521970  feet/sec       YDOT =        6444.545496  meter/sec
     ZDOT =       6940.276742                 ZDOT =        2115.396351
  
  
    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   16155.51240519  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6388 126.2519 0001191 142.0853 218.0384 15.54693003  2851
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16155.51240519   =   yrday.fracday
    Element set:     907
    Inclination:       51.6388  deg
    RA of node:       126.2519  deg
    Eccentricity:     .0001191     
    Arg of perigee:   142.0853  deg
    Mean anomaly:     218.0384  deg
    Mean motion:   15.54693003  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             285
    Checksum:              294
 
 
    Coasting Arc #9 (Orbit 300)
    ---------------------------------------
 
    Vector Time (GMT): 2016/156/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -422155.92                 A    =         6780862.63  meter
     Y    =       -5462278.76  meter          E    =           .0011419
     Z    =        3986763.22                 I    =           51.95201
     XDOT =       5605.613431                 Wp   =           84.24949
     YDOT =      -3369.575168  meter/sec      RA   =          120.29776  deg
     ZDOT =      -4012.138563                 TA   =           47.40402
                                              MA   =           47.30775
                                              Ha   =            220.351  n.mi
                                              Hp   =            213.502
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1385025.99                 X    =         -380410.21
     Y    =      -17920862.08  feet           Y    =        -5466766.67  meter
     Z    =       13079931.83                 Z    =         3984813.18
     XDOT =      18391.120180                 XDOT =        5662.365744
     YDOT =     -11055.036642  feet/sec       YDOT =       -3306.571648  meter/sec
     ZDOT =     -13163.184262                 ZDOT =       -3984.770096
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17532635.43                 X    =        -5343947.28
     Y    =       -3984800.80  feet           Y    =        -1214567.28  meter
     Z    =       13072423.98                 Z    =         3984474.83
     XDOT =      -5282.351276                 XDOT =       -1610.060669
     YDOT =     -19665.938428  feet/sec       YDOT =       -5994.178033  meter/sec
     ZDOT =     -13043.359967                 ZDOT =       -3975.616118
  
  
    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   16156.54084961  .00016717  00000-0  10270-3 0  9081
    2 25544  51.6387 121.1205 0001071 144.0155 216.1070 15.54721197  3016
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16156.54084961   =   yrday.fracday
    Element set:     908
    Inclination:       51.6387  deg
    RA of node:       121.1205  deg
    Eccentricity:     .0001071     
    Arg of perigee:   144.0155  deg
    Mean anomaly:     216.1070  deg
    Mean motion:   15.54721197  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             301
    Checksum:              271
 
 
    Coasting Arc #10 (Orbit 315)
    ---------------------------------------
 
    Vector Time (GMT): 2016/157/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -803566.21                 A    =         6785001.39  meter
     Y    =        6257729.56  meter          E    =           .0005261
     Z    =       -2496103.50                 I    =           51.98139
     XDOT =      -5304.131732                 Wp   =           61.22996
     YDOT =       1444.963889  meter/sec      RA   =          115.33510  deg
     ZDOT =       5341.031973                 TA   =          270.93186
                                              MA   =          270.99213
                                              Ha   =            220.328  n.mi
                                              Hp   =            213.559
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2636372.07                 X    =         -861356.88
     Y    =       20530608.81  feet           Y    =         6248420.77  meter
     Z    =       -8189315.94                 Z    =        -2500146.56
     XDOT =     -17402.006994                 XDOT =       -5345.840129
     YDOT =       4740.695175  feet/sec       YDOT =        1385.415610  meter/sec
     ZDOT =      17523.070779                 ZDOT =        5315.164486
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18949722.17                 X    =         5775875.32
     Y    =        8310043.10  feet           Y    =         2532901.14  meter
     Z    =       -8208073.14                 Z    =        -2501820.69
     XDOT =        176.605713                 XDOT =          53.829421
     YDOT =      16758.328712  feet/sec       YDOT =        5107.938591  meter/sec
     ZDOT =      17410.115662                 ZDOT =        5306.603254
  
  
    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   16157.50501532  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6390 116.3104 0001075 148.1513 211.9705 15.54702660  3169
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16157.50501532   =   yrday.fracday
    Element set:     909
    Inclination:       51.6390  deg
    RA of node:       116.3104  deg
    Eccentricity:     .0001075     
    Arg of perigee:   148.1513  deg
    Mean anomaly:     211.9705  deg
    Mean motion:   15.54702660  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             316
    Checksum:              270
 
 
    Coasting Arc #11 (Orbit 331)
    ---------------------------------------
 
    Vector Time (GMT): 2016/158/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1868526.65                 A    =         6787430.88  meter
     Y    =       -6485436.25  meter          E    =           .0014114
     Z    =         649512.74                 I    =           52.00445
     XDOT =       4720.690321                 Wp   =          129.97376
     YDOT =        751.485067  meter/sec      RA   =          110.38355  deg
     ZDOT =      -5999.835757                 TA   =           43.04440
                                              MA   =           42.93409
                                              Ha   =            220.276  n.mi
                                              Hp   =            213.570
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6130336.76                 X    =         1937754.48
     Y    =      -21277677.98  feet           Y    =        -6464154.16  meter
     Z    =        2130947.30                 Z    =          658756.82
     XDOT =      15487.829137                 XDOT =        4741.080905
     YDOT =       2465.502188  feet/sec       YDOT =         804.389841  meter/sec
     ZDOT =     -19684.500516                 ZDOT =       -5976.854094
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18864869.34                 X    =        -5750012.17
     Y    =      -11587011.50  feet           Y    =        -3531721.11  meter
     Z    =        2172421.36                 Z    =          662154.03
     XDOT =       5707.080803                 XDOT =        1739.518229
     YDOT =     -13010.080464  feet/sec       YDOT =       -3965.472525  meter/sec
     ZDOT =     -19584.508583                 ZDOT =       -5969.358216
  
  
    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   16158.53345608  .00016717  00000-0  10270-3 0  9103
    2 25544  51.6410 111.1789 0001035 154.7855 205.3349 15.54718635  3320
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16158.53345608   =   yrday.fracday
    Element set:     910
    Inclination:       51.6410  deg
    RA of node:       111.1789  deg
    Eccentricity:     .0001035     
    Arg of perigee:   154.7855  deg
    Mean anomaly:     205.3349  deg
    Mean motion:   15.54718635  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             332
    Checksum:              297
 
 
    Coasting Arc #12 (Orbit 347)
    ---------------------------------------
 
    Vector Time (GMT): 2016/159/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2693776.94                 A    =         6786940.20  meter
     Y    =        6096629.61  meter          E    =           .0013659
     Z    =        1247088.45                 I    =           52.01302
     XDOT =      -3945.511931                 Wp   =           62.86363
     YDOT =      -2954.327431  meter/sec      RA   =          105.43636  deg
     ZDOT =       5877.083806                 TA   =          310.63053
                                              MA   =          310.74924
                                              Ha   =            220.249  n.mi
                                              Hp   =            213.583
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8837850.85                 X    =        -2767808.59
     Y    =       20002065.63  feet           Y    =         6066091.89  meter
     Z    =        4091497.55                 Z    =         1233823.79
     XDOT =     -12944.592949                 XDOT =       -3940.730990
     YDOT =      -9692.675298  feet/sec       YDOT =       -2998.422851  meter/sec
     ZDOT =      19281.771017                 ZDOT =        5857.928704
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17137606.72                 X    =         5223542.53
     Y    =       13600421.75  feet           Y    =         4145408.55  meter
     Z    =        4032561.65                 Z    =         1229124.79
     XDOT =     -11668.811882                 XDOT =       -3556.653862
     YDOT =       8968.480635  feet/sec       YDOT =        2733.592897  meter/sec
     ZDOT =      19198.854164                 ZDOT =        5851.810749
  
  
    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   16159.56189338  .00016717  00000-0  10270-3 0  9114
    2 25544  51.6408 106.0482 0001015 155.6402 204.4799 15.54731231  3489
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16159.56189338   =   yrday.fracday
    Element set:     911
    Inclination:       51.6408  deg
    RA of node:       106.0482  deg
    Eccentricity:     .0001015     
    Arg of perigee:   155.6402  deg
    Mean anomaly:     204.4799  deg
    Mean motion:   15.54731231  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             348
    Checksum:              297
 
 
    Coasting Arc #13 (Orbit 362)
    ---------------------------------------
 
    Vector Time (GMT): 2016/160/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3337260.72                 A    =         6783743.07  meter
     Y    =       -5076702.00  meter          E    =           .0005193
     Z    =       -3018963.91                 I    =           52.01054
     XDOT =       3043.296080                 Wp   =          118.11908
     YDOT =       4961.245354  meter/sec      RA   =          100.48408  deg
     ZDOT =      -4987.583506                 TA   =           96.25803
                                              MA   =           96.19887
                                              Ha   =            220.220  n.mi
                                              Hp   =            213.632
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10949018.11                 X    =         3408446.42
     Y    =      -16655846.45  feet           Y    =        -5038984.13  meter
     Z    =       -9904737.23                 Z    =        -3002580.11
     XDOT =       9984.567191                 XDOT =        3011.819457
     YDOT =      16277.051685  feet/sec       YDOT =        4995.102139  meter/sec
     ZDOT =     -16363.462947                 ZDOT =       -4972.875818
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13613076.23                 X    =        -4149265.64
     Y    =      -14608571.86  feet           Y    =        -4452692.70  meter
     Z    =       -9832386.38                 Z    =        -2996911.37
     XDOT =      17121.160700                 XDOT =        5218.529781
     YDOT =      -5003.209420  feet/sec       YDOT =       -1524.978231  meter/sec
     ZDOT =     -16300.300799                 ZDOT =       -4968.331683
  
  
    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   16160.52605253  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6412 101.2381 0000908 157.7699 202.3493 15.54738844  3632
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16160.52605253   =   yrday.fracday
    Element set:     912
    Inclination:       51.6412  deg
    RA of node:       101.2381  deg
    Eccentricity:     .0000908     
    Arg of perigee:   157.7699  deg
    Mean anomaly:     202.3493  deg
    Mean motion:   15.54738844  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             363
    Checksum:              298
 
 
    Coasting Arc #14 (Orbit 363)
    ---------------------------------------
 
    Vector Time (GMT): 2016/160/13:50:18.153
    Vector Time (MET): N/A
    Weight (LBS)     : 923904.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3731545.55                 A    =         6777282.89  meter
     Y    =        2247720.82  meter          E    =           .0012884
     Z    =       -5203197.38                 I    =           51.98723
     XDOT =      -2371.124978                 Wp   =          105.04620
     YDOT =       7149.490631  meter/sec      RA   =          100.06905  deg
     ZDOT =       1387.618037                 TA   =          178.25012
                                              MA   =          178.24561
                                              Ha   =            220.201  n.mi
                                              Hp   =            214.854
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12242603.50                 X    =         3731408.44
     Y    =        7374412.14  feet           Y    =         2289449.32  meter
     Z    =      -17070857.55                 Z    =        -5185070.58
     XDOT =      -7779.281423                 XDOT =       -2457.636574
     YDOT =      23456.334092  feet/sec       YDOT =        7122.491248  meter/sec
     ZDOT =       4552.552614                 ZDOT =        1375.890496
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4141068.05                 X    =         1262197.54
     Y    =      -13776474.39  feet           Y    =        -4199069.39  meter
     Z    =      -16992285.94                 Z    =        -5179248.76
     XDOT =      23647.768797                 XDOT =        7207.839929
     YDOT =       1556.127373  feet/sec       YDOT =         474.307623  meter/sec
     ZDOT =       4500.102659                 ZDOT =        1371.631291
  
  
    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   16160.59033051  .00016717  00000-0  10270-3 0  9131
    2 25544  51.6426 100.9178 0001462 236.7783 123.3230 15.54367558  3647
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16160.59033051   =   yrday.fracday
    Element set:     913
    Inclination:       51.6426  deg
    RA of node:       100.9178  deg
    Eccentricity:     .0001462     
    Arg of perigee:   236.7783  deg
    Mean anomaly:     123.3230  deg
    Mean motion:   15.54367558  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             364
    Checksum:              292
 
 
    Coasting Arc #15 (Orbit 371)
    ---------------------------------------
 
    Vector Time (GMT): 2016/161/01:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923904.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4232008.88                 A    =         6776977.95  meter
     Y    =         695583.89  meter          E    =           .0003880
     Z    =        5246259.31                 I    =           51.98990
     XDOT =        145.062017                 Wp   =          152.26473
     YDOT =      -7586.603895  meter/sec      RA   =           97.71525  deg
     ZDOT =       1119.224770                 TA   =          287.04113
                                              MA   =          287.08364
                                              Ha   =            220.278  n.mi
                                              Hp   =            214.751
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13884543.55                 X    =        -4264956.50
     Y    =        2282099.38  feet           Y    =          648073.93  meter
     Z    =       17212136.86                 Z    =         5225621.41
     XDOT =        475.925251                 XDOT =         224.449853
     YDOT =     -24890.432725  feet/sec       YDOT =       -7584.537959  meter/sec
     ZDOT =       3671.997276                 ZDOT =        1120.121397
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3882387.55                 X    =        -1183351.72
     Y    =      -13638479.11  feet           Y    =        -4157008.43  meter
     Z    =       17122065.79                 Z    =         5218805.65
     XDOT =      23781.651700                 XDOT =        7248.647438
     YDOT =      -2137.957882  feet/sec       YDOT =        -651.649563  meter/sec
     ZDOT =       3677.334794                 ZDOT =        1120.851645
  
  
    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   16161.10466597  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6434  98.3498 0001920 227.4374 132.6617 15.54398239  3724
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16161.10466597   =   yrday.fracday
    Element set:     914
    Inclination:       51.6434  deg
    RA of node:        98.3498  deg
    Eccentricity:     .0001920     
    Arg of perigee:   227.4374  deg
    Mean anomaly:     132.6617  deg
    Mean motion:   15.54398239  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             372
    Checksum:              323
 
 
    Coasting Arc #16 (Orbit 386)
    ---------------------------------------
 
    Vector Time (GMT): 2016/162/01:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923904.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4075718.27                 A    =         6776885.80  meter
     Y    =        1228831.20  meter          E    =           .0013200
     Z    =       -5284483.75                 I    =           51.99284
     XDOT =      -1078.128246                 Wp   =          102.31427
     YDOT =       7527.137852  meter/sec      RA   =           92.73745  deg
     ZDOT =        918.002472                 TA   =          176.43995
                                              MA   =          176.43055
                                              Ha   =            220.115  n.mi
                                              Hp   =            214.921
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13371779.11                 X    =         4087343.89
     Y    =        4031598.44  feet           Y    =         1274474.11  meter
     Z    =      -17337545.12                 Z    =        -5264656.66
     XDOT =      -3537.166160                 XDOT =       -1166.677700
     YDOT =      24695.334160  feet/sec       YDOT =        7514.586306  meter/sec
     ZDOT =       3011.819135                 ZDOT =         912.550869
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2209476.11                 X    =         -673448.32
     Y    =       13898103.50  feet           Y    =         4236141.95  meter
     Z    =      -17251367.13                 Z    =        -5258216.70
     XDOT =     -23935.617146                 XDOT =       -7295.576106
     YDOT =        -94.674385  feet/sec       YDOT =         -28.856753  meter/sec
     ZDOT =       2986.630767                 ZDOT =         910.325058
  
  
    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   16162.06904674  .00016717  00000-0  10270-3 0  9155
    2 25544  51.6434  93.5415 0001780 234.2112 125.8875 15.54384173  3878
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16162.06904674   =   yrday.fracday
    Element set:     915
    Inclination:       51.6434  deg
    RA of node:        93.5415  deg
    Eccentricity:     .0001780     
    Arg of perigee:   234.2112  deg
    Mean anomaly:     125.8875  deg
    Mean motion:   15.54384173  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             387
    Checksum:              307
 
 
    Coasting Arc #17 (Orbit 402)
    ---------------------------------------
 
    Vector Time (GMT): 2016/163/01:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923904.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3798577.74                 A    =         6779229.52  meter
     Y    =       -3057900.87  meter          E    =           .0006317
     Z    =        4705683.32                 I    =           52.00144
     XDOT =       1964.900383                 Wp   =           64.70222
     YDOT =      -6843.156614  meter/sec      RA   =           87.76244  deg
     ZDOT =      -2855.159143                 TA   =           53.51266
                                              MA   =           53.45447
                                              Ha   =            220.182  n.mi
                                              Hp   =            214.788
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12462525.40                 X    =        -3786959.32
     Y    =      -10032483.16  feet           Y    =        -3100314.52  meter
     Z    =       15438593.58                 Z    =         4687258.81
     XDOT =       6446.523566                 XDOT =        2055.145327
     YDOT =     -22451.301227  feet/sec       YDOT =       -6820.678965  meter/sec
     ZDOT =      -9367.320022                 ZDOT =       -2845.395549
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8041465.21                 X    =         2451038.60
     Y    =      -13919596.39  feet           Y    =        -4242692.98  meter
     Z    =       15358877.01                 Z    =         4681385.71
     XDOT =      22157.330851                 XDOT =        6753.554443
     YDOT =       2492.563529  feet/sec       YDOT =         759.733364  meter/sec
     ZDOT =      -9323.457420                 ZDOT =       -2841.789822
  
  
    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   16163.09771581  .00016717  00000-0  10270-3 0  9169
    2 25544  51.6434  88.4118 0001720 240.3326 119.7655 15.54401192  4038
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16163.09771581   =   yrday.fracday
    Element set:     916
    Inclination:       51.6434  deg
    RA of node:        88.4118  deg
    Eccentricity:     .0001720     
    Arg of perigee:   240.3326  deg
    Mean anomaly:     119.7655  deg
    Mean motion:   15.54401192  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             403
    Checksum:              291
 
             

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