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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14929.5432
   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 
   ------------------------------------------------------------------------
    There are no maneuvers.
 
 
    Coasting Arc #1 (Orbit 113)
    ---------------------------------------
 
    Vector Time (GMT): 2016/144/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2928850.74                 A    =         6778101.44  meter
     Y    =        3802974.42  meter          E    =           .0012430
     Z    =       -4797201.54                 I    =           51.62149
     XDOT =      -6908.314125                 Wp   =           77.55902
     YDOT =       2048.185350  meter/sec      RA   =          180.07209  deg
     ZDOT =      -2597.131736                 TA   =          166.82817
                                              MA   =          166.79568
                                              Ha   =            220.707  n.mi
                                              Hp   =            213.355
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9609090.34                 X    =         2909410.32
     Y    =       12476950.21  feet           Y    =         3835618.54  meter
     Z    =      -15738850.18                 Z    =        -4783020.56
     XDOT =     -22665.072587                 XDOT =       -6918.088072
     YDOT =       6719.768210  feet/sec       YDOT =        1970.877584  meter/sec
     ZDOT =      -8520.773413                 ZDOT =       -2630.714638
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15632308.98                 X    =         4764727.78
     Y    =       -2357462.78  feet           Y    =         -718554.66  meter
     Z    =      -15677805.78                 Z    =        -4778595.20
     XDOT =      -5385.072754                 XDOT =       -1641.370176
     YDOT =      21863.703734  feet/sec       YDOT =        6664.056898  meter/sec
     ZDOT =      -8667.198092                 ZDOT =       -2641.761978
  
  
    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   16144.52075979  .00016717  00000-0  10270-3 0  9007
    2 25544  51.6405 181.0912 0001653 119.2160 240.9158 15.54665633  1149
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16144.52075979   =   yrday.fracday
    Element set:     900
    Inclination:       51.6405  deg
    RA of node:       181.0912  deg
    Eccentricity:     .0001653     
    Arg of perigee:   119.2160  deg
    Mean anomaly:     240.9158  deg
    Mean motion:   15.54665633  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             114
    Checksum:              290
 
 
    Coasting Arc #2 (Orbit 129)
    ---------------------------------------
 
    Vector Time (GMT): 2016/145/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -962322.05                 A    =         6775825.80  meter
     Y    =       -4118628.90  meter          E    =           .0004563
     Z    =        5290230.03                 I    =           51.64577
     XDOT =       7577.665287                 Wp   =          115.33295
     YDOT =      -1079.383206  meter/sec      RA   =          175.06854  deg
     ZDOT =        535.810606                 TA   =          329.54488
                                              MA   =          329.57137
                                              Ha   =            220.721  n.mi
                                              Hp   =            213.228
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3157224.58                 X    =         -941892.94
     Y    =      -13512562.02  feet           Y    =        -4129276.54  meter
     Z    =       17356397.74                 Z    =         5285604.46
     XDOT =      24861.106584                 XDOT =        7586.569263
     YDOT =      -3541.283484  feet/sec       YDOT =        -994.594980  meter/sec
     ZDOT =       1757.908813                 ZDOT =         572.642953
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13443766.42                 X    =        -4097660.01
     Y    =       -3535050.49  feet           Y    =        -1077483.39  meter
     Z    =       17336969.29                 Z    =         5284308.24
     XDOT =       8418.961136                 XDOT =        2566.099354
     YDOT =     -22572.578436  feet/sec       YDOT =       -6880.121907  meter/sec
     ZDOT =       1918.329701                 ZDOT =         584.706893
  
  
    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   16145.54922732  .00016717  00000-0  10270-3 0  9019
    2 25544  51.6400 175.9601 0001690 116.7792 243.3534 15.54689208  1302
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16145.54922732   =   yrday.fracday
    Element set:     901
    Inclination:       51.6400  deg
    RA of node:       175.9601  deg
    Eccentricity:     .0001690     
    Arg of perigee:   116.7792  deg
    Mean anomaly:     243.3534  deg
    Mean motion:   15.54689208  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             130
    Checksum:              295
 
 
    Coasting Arc #3 (Orbit 144)
    ---------------------------------------
 
    Vector Time (GMT): 2016/146/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1083793.09                 A    =         6776575.83  meter
     Y    =        4307084.29  meter          E    =           .0015066
     Z    =       -5131747.35                 I    =           51.68148
     XDOT =      -7488.169277                 Wp   =          104.00787
     YDOT =         25.395187  meter/sec      RA   =          170.06488  deg
     ZDOT =       1603.159791                 TA   =          181.46555
                                              MA   =          181.46997
                                              Ha   =            220.638  n.mi
                                              Hp   =            213.284
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3555751.60                 X    =        -1106947.41
     Y    =       14130853.98  feet           Y    =         4294835.65  meter
     Z    =      -16836441.42                 Z    =        -5137067.99
     XDOT =     -24567.484504                 XDOT =       -7495.684237
     YDOT =         83.317544  feet/sec       YDOT =         -58.384683  meter/sec
     ZDOT =       5259.710602                 ZDOT =        1566.765587
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10966429.80                 X    =         3342567.80
     Y    =        9552862.19  feet           Y    =         2911712.40  meter
     Z    =      -16860320.43                 Z    =        -5139025.67
     XDOT =     -10530.480700                 XDOT =       -3209.690517
     YDOT =      21090.074481  feet/sec       YDOT =        6428.254702  meter/sec
     ZDOT =       5101.349483                 ZDOT =        1554.891323
  
  
    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   16146.51341058  .00016717  00000-0  10270-3 0  9024
    2 25544  51.6413 171.1498 0001509 119.6802 240.4501 15.54672133  1458
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16146.51341058   =   yrday.fracday
    Element set:     902
    Inclination:       51.6413  deg
    RA of node:       171.1498  deg
    Eccentricity:     .0001509     
    Arg of perigee:   119.6802  deg
    Mean anomaly:     240.4501  deg
    Mean motion:   15.54672133  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             145
    Checksum:              276
 
 
    Coasting Arc #4 (Orbit 160)
    ---------------------------------------
 
    Vector Time (GMT): 2016/147/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 924109.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2990169.34                 A    =         6779700.58  meter
     Y    =       -4303705.70  meter          E    =           .0010900
     Z    =        4293395.84                 I    =           51.72212
     XDOT =       6711.007600                 Wp   =           78.95341
     YDOT =       1110.625593  meter/sec      RA   =          165.06992  deg
     ZDOT =      -3550.963073                 TA   =           47.21378
                                              MA   =           47.12217
                                              Ha   =            220.538  n.mi
                                              Hp   =            213.207
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9810266.88                 X    =         3017216.65
     Y    =      -14119769.37  feet           Y    =        -4270116.81  meter
     Z    =       14085944.35                 Z    =         4307986.70
     XDOT =      22017.741471                 XDOT =        6715.338668
     YDOT =       3643.784754  feet/sec       YDOT =        1185.697093  meter/sec
     ZDOT =     -11650.141316                 ZDOT =       -3518.351879
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8334310.05                 X    =        -2540297.70
     Y    =      -14977818.20  feet           Y    =        -4565238.99  meter
     Z    =       14150169.24                 Z    =         4312971.58
     XDOT =      11981.742135                 XDOT =        3652.035003
     YDOT =     -17569.502006  feet/sec       YDOT =       -5355.184211  meter/sec
     ZDOT =     -11508.411880                 ZDOT =       -3507.763941
  
  
    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   16147.54186817  .00016717  00000-0  10270-3 0  9039
    2 25544  51.6395 166.0189 0001619 119.9961 240.1353 15.54721576  1614
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16147.54186817   =   yrday.fracday
    Element set:     903
    Inclination:       51.6395  deg
    RA of node:       166.0189  deg
    Eccentricity:     .0001619     
    Arg of perigee:   119.9961  deg
    Mean anomaly:     240.1353  deg
    Mean motion:   15.54721576  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             161
    Checksum:              317
 
 
    Coasting Arc #5 (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    =       -4543306.00                 A    =         6783888.84  meter
     Y    =        4100745.12  meter          E    =           .0005601
     Z    =       -2930057.26                 I    =           51.76826
     XDOT =      -5307.506419                 Wp   =           81.72990
     YDOT =      -2292.494868  meter/sec      RA   =          160.08912  deg
     ZDOT =       5030.301971                 TA   =          244.92239
                                              MA   =          244.98053
                                              Ha   =            220.557  n.mi
                                              Hp   =            213.194
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14905859.57                 X    =        -4574590.88
     Y    =       13453888.20  feet           Y    =         4049764.17  meter
     Z    =       -9613048.75                 Z    =        -2952203.23
     XDOT =     -17413.078803                 XDOT =       -5305.911826
     YDOT =      -7521.308621  feet/sec       YDOT =       -2351.838433  meter/sec
     ZDOT =      16503.615390                 ZDOT =        5004.523025
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5793341.10                 X    =         1765810.37
     Y    =       19176887.24  feet           Y    =         5845115.23  meter
     Z    =       -9710131.72                 Z    =        -2959648.15
     XDOT =     -12903.916899                 XDOT =       -3933.113871
     YDOT =      12183.383177  feet/sec       YDOT =        3713.495192  meter/sec
     ZDOT =      16391.803435                 ZDOT =        4996.221687
  
  
    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   16148.50604291  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6408 161.2089 0001607 123.9822 236.1484 15.54721117  1760
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16148.50604291   =   yrday.fracday
    Element set:     904
    Inclination:       51.6408  deg
    RA of node:       161.2089  deg
    Eccentricity:     .0001607     
    Arg of perigee:   123.9822  deg
    Mean anomaly:     236.1484  deg
    Mean motion:   15.54721117  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             176
    Checksum:              292
 
 
    Coasting Arc #6 (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    =        5623314.42                 A    =         6787012.29  meter
     Y    =       -3607389.39  meter          E    =           .0015298
     Z    =        1152811.79                 I    =           51.80754
     XDOT =       3460.992045                 Wp   =          122.46133
     YDOT =       3498.727898  meter/sec      RA   =          155.12150  deg
     ZDOT =      -5885.371010                 TA   =           45.04379
                                              MA   =           44.91983
                                              Ha   =            220.571  n.mi
                                              Hp   =            213.216
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18449194.28                 X    =         5657635.33
     Y    =      -11835267.02  feet           Y    =        -3544313.92  meter
     Z    =        3782190.92                 Z    =         1180211.66
     XDOT =      11354.960779                 XDOT =        3450.199858
     YDOT =      11478.766071  feet/sec       YDOT =        3537.371077  meter/sec
     ZDOT =     -19308.960007                 ZDOT =       -5868.584291
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3169937.95                 X    =         -966197.09
     Y    =      -21667408.73  feet           Y    =        -6604226.18  meter
     Z    =        3902073.25                 Z    =         1189351.93
     XDOT =      13613.075974                 XDOT =        4149.265557
     YDOT =      -5483.821916  feet/sec       YDOT =       -1671.468920  meter/sec
     ZDOT =     -19236.482008                 ZDOT =       -5863.279716
  
  
    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   16149.53449022  .00016717  00000-0  10270-3 0  9052
    2 25544  51.6399 156.0773 0001584 122.6648 237.4658 15.54720513  1921
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16149.53449022   =   yrday.fracday
    Element set:     905
    Inclination:       51.6399  deg
    RA of node:       156.0773  deg
    Eccentricity:     .0001584     
    Arg of perigee:   122.6648  deg
    Mean anomaly:     237.4658  deg
    Mean motion:   15.54720513  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             192
    Checksum:              317
 
 
    Coasting Arc #7 (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    =       -6114572.52                 A    =         6787282.53  meter
     Y    =        2838426.26  meter          E    =           .0013526
     Z    =         738166.95                 I    =           51.83660
     XDOT =      -1406.908855                 Wp   =           59.45648
     YDOT =      -4603.118033  meter/sec      RA   =          150.16228  deg
     ZDOT =       5971.482694                 TA   =          308.50114
                                              MA   =          308.62237
                                              Ha   =            220.447  n.mi
                                              Hp   =            213.290
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20060933.45                 X    =        -6149443.78
     Y    =        9312422.11  feet           Y    =         2769854.02  meter
     Z    =        2421807.58                 Z    =          708379.20
     XDOT =      -4615.842699                 XDOT =       -1384.338107
     YDOT =     -15102.093285  feet/sec       YDOT =       -4618.725163  meter/sec
     ZDOT =      19591.478655                 ZDOT =        5964.702808
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         571346.85                 X    =          174146.52
     Y    =       22123501.78  feet           Y    =         6743243.34  meter
     Z    =        2291645.73                 Z    =          698493.62
     XDOT =     -14128.165529                 XDOT =       -4306.264853
     YDOT =      -1688.293475  feet/sec       YDOT =        -514.591851  meter/sec
     ZDOT =      19562.746208                 ZDOT =        5962.725044
  
  
    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   16150.56293079  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6390 150.9470 0001560 135.0261 225.1019 15.54762471  2084
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16150.56293079   =   yrday.fracday
    Element set:     906
    Inclination:       51.6390  deg
    RA of node:       150.9470  deg
    Eccentricity:     .0001560     
    Arg of perigee:   135.0261  deg
    Mean anomaly:     225.1019  deg
    Mean motion:   15.54762471  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             208
    Checksum:              285
 
 
    Coasting Arc #8 (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    =        6032923.73                 A    =         6784871.98  meter
     Y    =       -1729174.51  meter          E    =           .0006727
     Z    =       -2576070.48                 I    =           51.85507
     XDOT =       -668.496688                 Wp   =          130.13331
     YDOT =       5515.830646  meter/sec      RA   =          145.20000  deg
     ZDOT =      -5281.349631                 TA   =           78.73763
                                              MA   =           78.66204
                                              Ha   =            220.561  n.mi
                                              Hp   =            213.373
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19793056.86                 X    =         6064324.95
     Y    =       -5673144.71  feet           Y    =        -1661534.63  meter
     Z    =       -8451674.81                 Z    =        -2546687.63
     XDOT =      -2193.230604                 XDOT =        -704.471679
     YDOT =      18096.557237  feet/sec       YDOT =        5508.154187  meter/sec
     ZDOT =     -17327.262568                 ZDOT =       -5284.684150
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2324509.83                 X    =          708510.60
     Y    =      -20510906.90  feet           Y    =        -6251724.42  meter
     Z    =       -8323450.59                 Z    =        -2536987.74
     XDOT =      14437.620668                 XDOT =        4400.586780
     YDOT =       8656.001050  feet/sec       YDOT =        2638.349120  meter/sec
     ZDOT =     -17342.723610                 ZDOT =       -5286.062156
  
  
    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   16151.52709334  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6385 146.1356 0001497 130.3957 229.7327 15.54721445  2232
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16151.52709334   =   yrday.fracday
    Element set:     907
    Inclination:       51.6385  deg
    RA of node:       146.1356  deg
    Eccentricity:     .0001497     
    Arg of perigee:   130.3957  deg
    Mean anomaly:     229.7327  deg
    Mean motion:   15.54721445  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             223
    Checksum:              307
 
 
    Coasting Arc #9 (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    =       -5420953.29                 A    =         6780661.07  meter
     Y    =         377246.06  meter          E    =           .0011920
     Z    =        4048122.13                 I    =           51.86719
     XDOT =       2513.380054                 Wp   =          105.63309
     YDOT =      -6096.743529  meter/sec      RA   =          140.22984  deg
     ZDOT =       3921.181102                 TA   =          303.78680
                                              MA   =          303.90027
                                              Ha   =            220.478  n.mi
                                              Hp   =            213.373
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17785279.81                 X    =        -5444433.11
     Y    =        1237683.91  feet           Y    =          316493.85  meter
     Z    =       13281240.58                 Z    =         4021731.18
     XDOT =       8245.997552                 XDOT =        2562.320941
     YDOT =     -20002.439401  feet/sec       YDOT =       -6068.363798  meter/sec
     ZDOT =      12864.767395                 ZDOT =        3933.509171
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5377290.36                 X    =        -1638998.10
     Y    =       17087236.56  feet           Y    =         5208189.70  meter
     Z    =       13166263.17                 Z    =         4013077.02
     XDOT =     -14388.821546                 XDOT =       -4385.712807
     YDOT =     -14515.416986  feet/sec       YDOT =       -4424.299097  meter/sec
     ZDOT =      12919.496581                 ZDOT =        3937.862558
  
  
    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   16152.55552381  .00016717  00000-0  10270-3 0  9084
    2 25544  51.6386 141.0047 0001327 138.5232 221.6022 15.54757905  2392
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16152.55552381   =   yrday.fracday
    Element set:     908
    Inclination:       51.6386  deg
    RA of node:       141.0047  deg
    Eccentricity:     .0001327     
    Arg of perigee:   138.5232  deg
    Mean anomaly:     221.6022  deg
    Mean motion:   15.54757905  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             239
    Checksum:              290
 
 
    Coasting Arc #10 (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    =        4400474.45                 A    =         6776993.09  meter
     Y    =        1191574.98  meter          E    =           .0013417
     Z    =       -5026443.44                 I    =           51.87807
     XDOT =      -3998.585794                 Wp   =           80.10801
     YDOT =       6208.633209  meter/sec      RA   =          135.24738  deg
     ZDOT =      -2031.158297                 TA   =          170.20478
                                              MA   =          170.17860
                                              Ha   =            220.436  n.mi
                                              Hp   =            213.479
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14437252.15                 X    =         4411239.56
     Y    =        3909366.74  feet           Y    =         1240844.52  meter
     Z    =      -16490956.18                 Z    =        -5005040.50
     XDOT =     -13118.719796                 XDOT =       -4057.848465
     YDOT =      20369.531525  feet/sec       YDOT =        6163.587130  meter/sec
     ZDOT =      -6663.905174                 ZDOT =       -2050.726266
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8742542.79                 X    =         2664727.04
     Y    =      -12261477.37  feet           Y    =        -3737298.30  meter
     Z    =      -16397961.82                 Z    =        -4998098.76
     XDOT =      13623.030291                 XDOT =        4152.299633
     YDOT =      18730.328992  feet/sec       YDOT =        5709.004277  meter/sec
     ZDOT =      -6750.195703                 ZDOT =       -2057.459650
  
  
    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   16153.51967469  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6378 136.1933 0001352 134.2807 225.8457 15.54734768  2548
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16153.51967469   =   yrday.fracday
    Element set:     909
    Inclination:       51.6378  deg
    RA of node:       136.1933  deg
    Eccentricity:     .0001352     
    Arg of perigee:   134.2807  deg
    Mean anomaly:     225.8457  deg
    Mean motion:   15.54734768  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             254
    Checksum:              331
 
 
    Coasting Arc #11 (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    =       -3109523.94                 A    =         6775566.57  meter
     Y    =       -2794887.74  meter          E    =           .0003312
     Z    =        5329001.99                 I    =           51.89546
     XDOT =       5023.561288                 Wp   =          105.01476
     YDOT =      -5798.153742  meter/sec      RA   =          130.25911  deg
     ZDOT =       -110.425681                 TA   =          346.02868
                                              MA   =          346.03784
                                              Ha   =            220.475  n.mi
                                              Hp   =            213.407
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10201850.19                 X    =        -3103926.11
     Y    =       -9169579.20  feet           Y    =        -2829629.64  meter
     Z    =       17483602.32                 Z    =         5313909.82
     XDOT =      16481.500289                 XDOT =        5088.560741
     YDOT =     -19022.814113  feet/sec       YDOT =       -5741.613493  meter/sec
     ZDOT =       -362.288980                 ZDOT =         -85.864666
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12080783.91                 X    =        -3682222.93
     Y    =        6670113.59  feet           Y    =         2033050.62  meter
     Z    =       17418367.45                 Z    =         5309118.40
     XDOT =     -11957.078428                 XDOT =       -3644.517505
     YDOT =     -20999.044481  feet/sec       YDOT =       -6400.508758  meter/sec
     ZDOT =       -254.305191                 ZDOT =         -77.512222
  
  
    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   16154.54809701  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6376 131.0619 0001273 141.6179 218.5065 15.54740267  2700
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16154.54809701   =   yrday.fracday
    Element set:     910
    Inclination:       51.6376  deg
    RA of node:       131.0619  deg
    Eccentricity:     .0001273     
    Arg of perigee:   141.6179  deg
    Mean anomaly:     218.5065  deg
    Mean motion:   15.54740267  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             270
    Checksum:              293
 
 
    Coasting Arc #12 (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    =        1713288.63                 A    =         6777184.25  meter
     Y    =        4304963.07  meter          E    =           .0013336
     Z    =       -4958290.42                 I    =           51.92205
     XDOT =      -5540.230097                 Wp   =          109.48807
     YDOT =       4788.519350  meter/sec      RA   =          125.27231  deg
     ZDOT =       2243.765646                 TA   =          182.35832
                                              MA   =          182.36462
                                              Ha   =            220.330  n.mi
                                              Hp   =            213.479
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5621025.68                 X    =         1689107.74
     Y    =       14123894.58  feet           Y    =         4323987.51  meter
     Z    =      -16267357.02                 Z    =        -4950025.84
     XDOT =     -18176.607929                 XDOT =       -5604.264179
     YDOT =      15710.365320  feet/sec       YDOT =        4726.206541  meter/sec
     ZDOT =       7361.435845                 ZDOT =        2216.697117
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15209003.61                 X    =         4635704.30
     Y    =        -954699.05  feet           Y    =         -290992.27  meter
     Z    =      -16232128.36                 Z    =        -4947552.72
     XDOT =       9055.796861                 XDOT =        2760.206883
     YDOT =      21154.492754  feet/sec       YDOT =        6447.889391  meter/sec
     ZDOT =       7242.686343                 ZDOT =        2207.570797
  
  
    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   16155.51223639  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6387 126.2510 0001205 142.3829 217.7408 15.54742432  2857
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16155.51223639   =   yrday.fracday
    Element set:     911
    Inclination:       51.6387  deg
    RA of node:       126.2510  deg
    Eccentricity:     .0001205     
    Arg of perigee:   142.3829  deg
    Mean anomaly:     217.7408  deg
    Mean motion:   15.54742432  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             285
    Checksum:              289
 
 
    Coasting Arc #13 (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    =        -324508.94                 A    =         6780941.11  meter
     Y    =       -5519775.65  meter          E    =           .0011658
     Z    =        3915996.76                 I    =           51.95274
     XDOT =       5613.962444                 Wp   =           85.60035
     YDOT =      -3247.237938  meter/sec      RA   =          120.29575  deg
     ZDOT =      -4100.570286                 TA   =           47.18416
                                              MA   =           47.08622
                                              Ha   =            220.265  n.mi
                                              Hp   =            213.416
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1064661.87                 X    =         -281783.79
     Y    =      -18109500.17  feet           Y    =        -5523166.12  meter
     Z    =       12847758.39                 Z    =         3914523.44
     XDOT =      18418.511956                 XDOT =        5669.775700
     YDOT =     -10653.667775  feet/sec       YDOT =       -3184.146293  meter/sec
     ZDOT =     -13453.314588                 ZDOT =       -4073.163527
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17615831.18                 X    =        -5369305.34
     Y    =       -4348477.43  feet           Y    =        -1325415.92  meter
     Z    =       12842337.51                 Z    =         3914344.47
     XDOT =      -4917.292884                 XDOT =       -1498.790871
     YDOT =     -19567.147318  feet/sec       YDOT =       -5964.066503  meter/sec
     ZDOT =     -13333.345581                 ZDOT =       -4064.003733
  
  
    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   16156.54064653  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6387 121.1194 0001089 144.6315 215.4911 15.54775174  3016
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16156.54064653   =   yrday.fracday
    Element set:     912
    Inclination:       51.6387  deg
    RA of node:       121.1194  deg
    Eccentricity:     .0001089     
    Arg of perigee:   144.6315  deg
    Mean anomaly:     215.4911  deg
    Mean motion:   15.54775174  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             301
    Checksum:              292
 
 
    Coasting Arc #14 (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    =        -912296.10                 A    =         6785053.15  meter
     Y    =        6285634.66  meter          E    =           .0005466
     Z    =       -2385515.41                 I    =           51.98210
     XDOT =      -5281.627813                 Wp   =           58.07974
     YDOT =       1280.362778  meter/sec      RA   =          115.33345  deg
     ZDOT =       5405.371731                 TA   =          275.41382
                                              MA   =          275.47617
                                              Ha   =            220.234  n.mi
                                              Hp   =            213.463
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2993097.44                 X    =         -970927.93
     Y    =       20622160.96  feet           Y    =         6275105.26  meter
     Z    =       -7826494.11                 Z    =        -2390088.69
     XDOT =     -17328.175238                 XDOT =       -5321.809809
     YDOT =       4200.665282  feet/sec       YDOT =        1221.074679  meter/sec
     ZDOT =      17734.159224                 ZDOT =        5379.617248
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18935518.27                 X    =         5771545.97
     Y    =        8680323.49  feet           Y    =         2645762.60  meter
     Z    =       -7847566.33                 Z    =        -2391938.22
     XDOT =       -293.557884                 XDOT =         -89.476443
     YDOT =      16536.452616  feet/sec       YDOT =        5040.310757  meter/sec
     ZDOT =      17621.726486                 ZDOT =        5371.102233
  
  
    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   16157.50477706  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6390 116.3091 0001104 149.0756 211.0462 15.54763208  3162
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16157.50477706   =   yrday.fracday
    Element set:     913
    Inclination:       51.6390  deg
    RA of node:       116.3091  deg
    Eccentricity:     .0001104     
    Arg of perigee:   149.0756  deg
    Mean anomaly:     211.0462  deg
    Mean motion:   15.54763208  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             316
    Checksum:              283
 
 
    Coasting Arc #15 (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    =        1980815.28                 A    =         6787316.83  meter
     Y    =       -6464880.36  meter          E    =           .0013944
     Z    =         505385.83                 I    =           52.00466
     XDOT =       4661.684257                 Wp   =          131.53978
     YDOT =        950.244829  meter/sec      RA   =          110.38209  deg
     ZDOT =      -6017.720552                 TA   =           43.03296
                                              MA   =           42.92400
                                              Ha   =            220.174  n.mi
                                              Hp   =            213.474
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6498737.80                 X    =         2050505.02
     Y    =      -21210237.42  feet           Y    =        -6442339.98  meter
     Z    =        1658089.98                 Z    =          515176.51
     XDOT =      15294.239687                 XDOT =        4679.943522
     YDOT =       3117.601145  feet/sec       YDOT =        1002.477844  meter/sec
     ZDOT =     -19743.177664                 ZDOT =       -5995.030675
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18700538.05                 X    =        -5699924.00
     Y    =      -11926872.91  feet           Y    =        -3635310.86  meter
     Z    =        1701941.77                 Z    =          518751.85
     XDOT =       6258.911724                 XDOT =        1907.716293
     YDOT =     -12661.410115  feet/sec       YDOT =       -3859.197803  meter/sec
     ZDOT =     -19644.493743                 ZDOT =       -5987.641693
  
  
    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   16158.53317707  .00016717  00000-0  10270-3 0  9146
    2 25544  51.6410 111.1773 0001061 156.1162 204.0041 15.54782537  3326
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16158.53317707   =   yrday.fracday
    Element set:     914
    Inclination:       51.6410  deg
    RA of node:       111.1773  deg
    Eccentricity:     .0001061     
    Arg of perigee:   156.1162  deg
    Mean anomaly:     204.0041  deg
    Mean motion:   15.54782537  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             332
    Checksum:              266
 
             

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