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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  12916.69
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   72.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.25
   ET - UTC  (sec) :   66.18
   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 3121)
    ---------------------------------------
 
    Vector Time (GMT): 2009/328/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1243135.65                 A    =         6714572.23  meter
     Y    =       -3998519.93  meter          E    =           .0008004
     Z    =        5245240.93                 I    =           51.49757
     XDOT =       7228.621248                 Wp   =           30.04315
     YDOT =       2657.190528  meter/sec      RA   =          202.07147  deg
     ZDOT =        319.026735                 TA   =           56.96367
                                              MA   =           56.88680
                                              Ha   =            188.917  n.mi
                                              Hp   =            179.682
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4078529.05                 X    =         1262274.63
     Y    =      -13118503.71  feet           Y    =        -3984511.72  meter
     Z    =       17208795.70                 Z    =         5251326.44
     XDOT =      23715.948978                 XDOT =        7196.821033
     YDOT =       8717.816692  feet/sec       YDOT =        2737.847414  meter/sec
     ZDOT =       1046.675641                 ZDOT =         354.066756
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10312196.25                 X    =         3143157.42
     Y    =        9031429.02  feet           Y    =         2752779.56  meter
     Z    =       17232645.95                 Z    =         5252510.49
     XDOT =     -17057.160045                 XDOT =       -5199.022382
     YDOT =      17256.076295  feet/sec       YDOT =        5259.652055  meter/sec
     ZDOT =       1185.149240                 ZDOT =         361.233488
  
  
    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   09328.55608418  .00016717  00000-0  10270-3 0  9006
    2 25544  51.6457 202.8335 0007833  11.2964 348.8375 15.75951685 31225
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09328.55608418   =   yrday.fracday
    Element set:     900
    Inclination:       51.6457  deg
    RA of node:       202.8335  deg
    Eccentricity:     .0007833     
    Arg of perigee:    11.2964  deg
    Mean anomaly:     348.8375  deg
    Mean motion:   15.75951685  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3122
    Checksum:              325
 
 
    Coasting Arc #2 (Orbit 3137)
    ---------------------------------------
 
    Vector Time (GMT): 2009/329/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6321397.76                 A    =         6726479.55  meter
     Y    =       -2234164.38  meter          E    =           .0019868
     Z    =         376061.70                 I    =           51.56599
     XDOT =       1925.981027                 Wp   =           36.03877
     YDOT =      -4411.073900  meter/sec      RA   =          196.91376  deg
     ZDOT =       6024.263692                 TA   =          328.06096
                                              MA   =          328.18126
                                              Ha   =            188.969  n.mi
                                              Hp   =            179.509
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20739493.95                 X    =        -6297771.99
     Y    =       -7329935.64  feet           Y    =        -2304721.90  meter
     Z    =        1233798.22                 Z    =          345409.14
     XDOT =       6318.835392                 XDOT =        1945.898026
     YDOT =     -14472.027232  feet/sec       YDOT =       -4389.425338  meter/sec
     ZDOT =      19764.644658                 ZDOT =        6033.668451
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14954416.06                 X    =         4558106.02
     Y    =      -16140144.36  feet           Y    =        -4919516.00  meter
     Z    =        1112656.40                 Z    =          339137.67
     XDOT =       9649.355576                 XDOT =        2941.123580
     YDOT =      10341.770796  feet/sec       YDOT =        3152.171739  meter/sec
     ZDOT =      19801.583439                 ZDOT =        6035.522632
  
  
    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   09329.57065440  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6453 197.6080 0007850  14.2944 345.8441 15.75990185 31385
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09329.57065440   =   yrday.fracday
    Element set:     901
    Inclination:       51.6453  deg
    RA of node:       197.6080  deg
    Eccentricity:     .0007850     
    Arg of perigee:    14.2944  deg
    Mean anomaly:     345.8441  deg
    Mean motion:   15.75990185  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3138
    Checksum:              321
 
 
    Coasting Arc #3 (Orbit 3152)
    ---------------------------------------
 
    Vector Time (GMT): 2009/330/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2146998.88                 A    =         6714809.23  meter
     Y    =        3738631.18  meter          E    =           .0017382
     Z    =       -5161303.72                 I    =           51.55533
     XDOT =      -7184.398136                 Wp   =           72.67483
     YDOT =      -2471.785127  meter/sec      RA   =          191.74343  deg
     ZDOT =       1206.522498                 TA   =          208.82850
                                              MA   =          208.92465
                                              Ha   =            189.028  n.mi
                                              Hp   =            179.233
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7043959.59                 X    =        -2163572.17
     Y    =       12265850.32  feet           Y    =         3714529.69  meter
     Z    =      -16933411.15                 Z    =        -5171774.16
     XDOT =     -23570.860025                 XDOT =       -7162.085420
     YDOT =      -8109.531258  feet/sec       YDOT =       -2552.000595  meter/sec
     ZDOT =       3958.407145                 ZDOT =        1171.674113
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8699004.14                 X    =        -2651456.46
     Y    =      -11090511.52  feet           Y    =        -3380387.91  meter
     Z    =      -16974591.17                 Z    =        -5173855.39
     XDOT =      15670.404971                 XDOT =        4776.339435
     YDOT =     -18096.899436  feet/sec       YDOT =       -5515.934948  meter/sec
     ZDOT =       3820.675263                 ZDOT =        1164.541820
  
  
    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   09330.52179795  .00016717  00000-0  10270-3 0  9029
    2 25544  51.6445 192.7089 0007885  17.4480 342.6953 15.76014395 31530
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09330.52179795   =   yrday.fracday
    Element set:     902
    Inclination:       51.6445  deg
    RA of node:       192.7089  deg
    Eccentricity:     .0007885     
    Arg of perigee:    17.4480  deg
    Mean anomaly:     342.6953  deg
    Mean motion:   15.76014395  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3153
    Checksum:              333
 
 
    Coasting Arc #4 (Orbit 3168)
    ---------------------------------------
 
    Vector Time (GMT): 2009/331/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6153370.17                 A    =         6725214.82  meter
     Y    =        2095697.08  meter          E    =           .0007568
     Z    =       -1733261.65                 I    =           51.61960
     XDOT =      -3027.699885                 Wp   =           81.67071
     YDOT =       4192.993400  meter/sec      RA   =          186.61584  deg
     ZDOT =      -5699.126147                 TA   =          117.51655
                                              MA   =          117.43962
                                              Ha   =            189.104  n.mi
                                              Hp   =            179.266
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20188222.33                 X    =         6137898.45
     Y    =        6875646.60  feet           Y    =         2164421.26  meter
     Z    =       -5686553.96                 Z    =        -1703405.37
     XDOT =      -9933.398574                 XDOT =       -3046.675669
     YDOT =      13756.540026  feet/sec       YDOT =        4159.030000  meter/sec
     ZDOT =     -18697.920430                 ZDOT =       -5713.880986
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13775759.82                 X    =        -4198851.59
     Y    =       16321626.12  feet           Y    =         4974831.64  meter
     Z    =       -5568545.14                 Z    =        -1697292.56
     XDOT =      -8036.449224                 XDOT =       -2449.509723
     YDOT =     -13159.085399  feet/sec       YDOT =       -4010.889230  meter/sec
     ZDOT =     -18756.004898                 ZDOT =       -5716.830293
  
  
    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   09331.53633312  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6442 187.4842 0007776  20.9157 339.2324 15.76004948 31698
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09331.53633312   =   yrday.fracday
    Element set:     903
    Inclination:       51.6442  deg
    RA of node:       187.4842  deg
    Eccentricity:     .0007776     
    Arg of perigee:    20.9157  deg
    Mean anomaly:     339.2324  deg
    Mean motion:   15.76004948  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3169
    Checksum:              314
 
 
    Coasting Arc #5 (Orbit 3184)
    ---------------------------------------
 
    Vector Time (GMT): 2009/332/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3121788.53                 A    =         6716564.79  meter
     Y    =       -3643085.61  meter          E    =           .0014678
     Z    =        4696566.04                 I    =           51.62110
     XDOT =       6826.365477                 Wp   =           42.91885
     YDOT =       2324.108888  meter/sec      RA   =          181.42583  deg
     ZDOT =      -2719.135624                 TA   =           73.91042
                                              MA   =           73.74886
                                              Ha   =            189.006  n.mi
                                              Hp   =            178.976
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10242088.37                 X    =         3139478.45
     Y    =      -11952380.60  feet           Y    =        -3608077.26  meter
     Z    =       15408681.22                 Z    =         4711774.87
     XDOT =      22396.212194                 XDOT =        6813.078954
     YDOT =       7625.029161  feet/sec       YDOT =        2400.371190  meter/sec
     ZDOT =      -8921.048635                 ZDOT =       -2686.004394
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7663669.01                 X    =         2335886.31
     Y    =       13681305.04  feet           Y    =         4170061.78  meter
     Z    =       15468590.84                 Z    =         4714826.49
     XDOT =     -13973.864673                 XDOT =       -4259.233952
     YDOT =      17823.333502  feet/sec       YDOT =        5432.552051  meter/sec
     ZDOT =      -8790.086377                 ZDOT =       -2679.218328
  
  
    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   09332.55084798  .00016717  00000-0  10270-3 0  9044
    2 25544  51.6439 182.2579 0007849  23.9849 336.1680 15.76078380 31856
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09332.55084798   =   yrday.fracday
    Element set:     904
    Inclination:       51.6439  deg
    RA of node:       182.2579  deg
    Eccentricity:     .0007849     
    Arg of perigee:    23.9849  deg
    Mean anomaly:     336.1680  deg
    Mean motion:   15.76078380  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3185
    Checksum:              354
 
 
    Coasting Arc #6 (Orbit 3200)
    ---------------------------------------
 
    Vector Time (GMT): 2009/333/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5684121.00                 A    =         6722453.08  meter
     Y    =       -1984034.79  meter          E    =           .0018941
     Z    =        2965792.47                 I    =           51.66953
     XDOT =       4088.374491                 Wp   =           63.18587
     YDOT =      -4221.000562  meter/sec      RA   =          176.31969  deg
     ZDOT =       4995.932816                 TA   =          331.10123
                                              MA   =          331.20599
                                              Ha   =            189.167  n.mi
                                              Hp   =            178.855
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18648690.94                 X    =        -5675920.42
     Y    =       -6509300.48  feet           Y    =        -2047552.36  meter
     Z    =        9730290.26                 Z    =         2938197.97
     XDOT =      13413.302135                 XDOT =        4111.000546
     YDOT =     -13848.427040  feet/sec       YDOT =       -4175.155816  meter/sec
     ZDOT =      16390.855696                 ZDOT =        5015.849365
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12356699.40                 X    =         3766321.98
     Y    =      -15477972.62  feet           Y    =        -4717686.05  meter
     Z    =        9621203.60                 Z    =         2932542.86
     XDOT =       7505.202015                 XDOT =        2287.585574
     YDOT =      16262.053742  feet/sec       YDOT =        4956.673981  meter/sec
     ZDOT =      16469.345658                 ZDOT =        5019.856557
  
  
    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   09333.56534573  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6424 177.0316 0007788  27.6842 332.4735 15.76101164 32013
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09333.56534573   =   yrday.fracday
    Element set:     905
    Inclination:       51.6424  deg
    RA of node:       177.0316  deg
    Eccentricity:     .0007788     
    Arg of perigee:    27.6842  deg
    Mean anomaly:     332.4735  deg
    Mean motion:   15.76101164  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3201
    Checksum:              305
 
 
    Coasting Arc #7 (Orbit 3215)
    ---------------------------------------
 
    Vector Time (GMT): 2009/334/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3967609.50                 A    =         6719388.88  meter
     Y    =        3753999.17  meter          E    =           .0011647
     Z    =       -3919271.68                 I    =           51.68838
     XDOT =      -6139.397187                 Wp   =           67.36319
     YDOT =      -2277.498180  meter/sec      RA   =          171.12005  deg
     ZDOT =       4047.563653                 TA   =          244.65003
                                              MA   =          244.77068
                                              Ha   =            189.127  n.mi
                                              Hp   =            178.587
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13017091.54                 X    =        -3990252.81
     Y    =       12316270.23  feet           Y    =         3709504.82  meter
     Z    =      -12858502.88                 Z    =        -3938601.51
     XDOT =     -20142.379224                 XDOT =       -6133.136419
     YDOT =      -7472.106890  feet/sec       YDOT =       -2346.117962  meter/sec
     ZDOT =      13279.408309                 ZDOT =        4017.752542
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7593041.99                 X    =        -2314359.20
     Y    =      -16171434.69  feet           Y    =        -4929053.29  meter
     Z    =      -12934708.90                 Z    =        -3942499.27
     XDOT =      12301.497377                 XDOT =        3749.496401
     YDOT =     -16266.949400  feet/sec       YDOT =       -4958.166177  meter/sec
     ZDOT =      13161.542984                 ZDOT =        4011.638302
  
  
    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   09334.51642119  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6412 172.1315 0007818  32.0982 328.0656 15.76114502 32163
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09334.51642119   =   yrday.fracday
    Element set:     906
    Inclination:       51.6412  deg
    RA of node:       172.1315  deg
    Eccentricity:     .0007818     
    Arg of perigee:    32.0982  deg
    Mean anomaly:     328.0656  deg
    Mean motion:   15.76114502  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3216
    Checksum:              288
 
 
    Coasting Arc #8 (Orbit 3231)
    ---------------------------------------
 
    Vector Time (GMT): 2009/335/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4962994.20                 A    =         6719038.73  meter
     Y    =        2059204.01  meter          E    =           .0014437
     Z    =       -4050195.49                 I    =           51.71589
     XDOT =      -4984.155612                 Wp   =           53.33313
     YDOT =       4392.464119  meter/sec      RA   =          166.02476  deg
     ZDOT =      -3875.273155                 TA   =          176.73744
                                              MA   =          176.72802
                                              Ha   =            189.218  n.mi
                                              Hp   =            178.552
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16282789.37                 X    =         4959274.60
     Y    =        6755918.67  feet           Y    =         2114682.89  meter
     Z    =      -13288042.94                 Z    =        -4026093.36
     XDOT =     -16352.216574                 XDOT =       -5014.076590
     YDOT =      14410.971520  feet/sec       YDOT =        4336.561577  meter/sec
     ZDOT =     -12714.150772                 ZDOT =       -3899.558933
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11349203.53                 X    =        -3459237.24
     Y    =       13582753.42  feet           Y    =         4140023.24  meter
     Z    =      -13192730.60                 Z    =        -4021144.29
     XDOT =      -7877.990373                 XDOT =       -2401.211466
     YDOT =     -19021.254016  feet/sec       YDOT =       -5797.678224  meter/sec
     ZDOT =     -12809.927436                 ZDOT =       -3904.465882
  
  
    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   09335.53088319  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6403 166.9055 0007913  36.1173 324.0524 15.76148530 32324
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09335.53088319   =   yrday.fracday
    Element set:     907
    Inclination:       51.6403  deg
    RA of node:       166.9055  deg
    Eccentricity:     .0007913     
    Arg of perigee:    36.1173  deg
    Mean anomaly:     324.0524  deg
    Mean motion:   15.76148530  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3232
    Checksum:              299
 
 
    Coasting Arc #9 (Orbit 3247)
    ---------------------------------------
 
    Vector Time (GMT): 2009/336/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4673664.09                 A    =         6722493.38  meter
     Y    =       -3944688.60  meter          E    =           .0018576
     Z    =        2780318.42                 I    =           51.75751
     XDOT =       5175.380893                 Wp   =           78.33379
     YDOT =       2487.683574  meter/sec      RA   =          160.82987  deg
     ZDOT =      -5137.768176                 TA   =           69.86791
                                              MA   =           69.66815
                                              Ha   =            189.106  n.mi
                                              Hp   =            178.315
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15333543.60                 X    =         4703920.35
     Y    =      -12941891.75  feet           Y    =        -3892256.20  meter
     Z    =        9121779.58                 Z    =         2803096.46
     XDOT =      16979.596106                 XDOT =        5172.137425
     YDOT =       8161.691516  feet/sec       YDOT =        2545.540401  meter/sec
     ZDOT =     -16856.194802                 ZDOT =       -5112.633108
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8082413.45                 X    =         2463519.62
     Y    =       18320407.85  feet           Y    =         5584060.31  meter
     Z    =        9211635.74                 Z    =         2807706.57
     XDOT =     -11329.353935                 XDOT =       -3453.187079
     YDOT =      13476.608088  feet/sec       YDOT =        4107.670145  meter/sec
     ZDOT =     -16756.771844                 ZDOT =       -5107.464058
  
  
    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   09336.54532513  .00016717  00000-0  10270-3 0  9084
    2 25544  51.6406 161.6784 0007809  38.2115 321.9602 15.76198983 32488
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09336.54532513   =   yrday.fracday
    Element set:     908
    Inclination:       51.6406  deg
    RA of node:       161.6784  deg
    Eccentricity:     .0007809     
    Arg of perigee:    38.2115  deg
    Mean anomaly:     321.9602  deg
    Mean motion:   15.76198983  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3248
    Checksum:              326
 
 
    Coasting Arc #10 (Orbit 3263)
    ---------------------------------------
 
    Vector Time (GMT): 2009/337/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4039308.68                 A    =         6715933.48  meter
     Y    =       -2342056.02  meter          E    =           .0011764
     Z    =        4816594.00                 I    =           51.76221
     XDOT =       5633.164797                 Wp   =           80.01476
     YDOT =      -4661.624003  meter/sec      RA   =          155.72864  deg
     ZDOT =       2454.363029                 TA   =          346.06889
                                              MA   =          346.10132
                                              Ha   =            189.387  n.mi
                                              Hp   =            178.210
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13252325.08                 X    =        -4036217.69
     Y    =       -7683910.83  feet           Y    =        -2387209.46  meter
     Z    =       15802473.77                 Z    =         4796977.86
     XDOT =      18481.511801                 XDOT =        5672.950187
     YDOT =     -15294.042005  feet/sec       YDOT =       -4598.408583  meter/sec
     ZDOT =       8052.372144                 ZDOT =        2481.825244
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10965060.94                 X    =         3342150.57
     Y    =      -10811158.83  feet           Y    =        -3295241.21  meter
     Z    =       15724855.04                 Z    =         4792935.82
     XDOT =       9033.467955                 XDOT =        2753.401033
     YDOT =      21046.439943  feet/sec       YDOT =        6414.954894  meter/sec
     ZDOT =       8160.732182                 ZDOT =        2487.391169
  
  
    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   09337.55975235  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6398 156.4513 0007882  43.4696 316.7089 15.76178130 32644
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09337.55975235   =   yrday.fracday
    Element set:     909
    Inclination:       51.6398  deg
    RA of node:       156.4513  deg
    Eccentricity:     .0007882     
    Arg of perigee:    43.4696  deg
    Mean anomaly:     316.7089  deg
    Mean motion:   15.76178130  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3264
    Checksum:              347
 
 
    Coasting Arc #11 (Orbit 3278)
    ---------------------------------------
 
    Vector Time (GMT): 2009/338/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5068277.99                 A    =         6724905.10  meter
     Y    =        4167523.39  meter          E    =           .0016188
     Z    =       -1446590.80                 I    =           51.82059
     XDOT =      -4081.612409                 Wp   =           42.88503
     YDOT =      -2958.129364  meter/sec      RA   =          150.55341  deg
     ZDOT =       5827.691800                 TA   =          301.21975
                                              MA   =          301.37829
                                              Ha   =            189.226  n.mi
                                              Hp   =            178.016
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16628208.62                 X    =        -5107475.94
     Y    =       13672976.99  feet           Y    =         4110627.97  meter
     Z    =       -4746032.80                 Z    =        -1471307.27
     XDOT =     -13391.116829                 XDOT =       -4076.540848
     YDOT =      -9705.148833  feet/sec       YDOT =       -3003.744914  meter/sec
     ZDOT =      19119.723752                 ZDOT =        5807.875009
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9085482.83                 X    =        -2769255.17
     Y    =      -19492721.88  feet           Y    =        -5941381.63  meter
     Z    =       -4843577.67                 Z    =        -1476322.47
     XDOT =      11352.512697                 XDOT =        3460.245870
     YDOT =      -9983.220238  feet/sec       YDOT =       -3042.885529  meter/sec
     ZDOT =      19041.277175                 ZDOT =        5803.781283
  
  
    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   09338.51075874  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6404 151.5510 0007838  48.2358 311.9475 15.76221975 32792
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09338.51075874   =   yrday.fracday
    Element set:     910
    Inclination:       51.6404  deg
    RA of node:       151.5510  deg
    Eccentricity:     .0007838     
    Arg of perigee:    48.2358  deg
    Mean anomaly:     311.9475  deg
    Mean motion:   15.76221975  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3279
    Checksum:              324
 
 
    Coasting Arc #12 (Orbit 3294)
    ---------------------------------------
 
    Vector Time (GMT): 2009/339/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3061761.45                 A    =         6713896.85  meter
     Y    =        2899259.49  meter          E    =           .0021923
     Z    =       -5243240.44                 I    =           51.80990
     XDOT =      -5927.345313                 Wp   =           73.22142
     YDOT =       4833.581988  meter/sec      RA   =          145.43476  deg
     ZDOT =       -785.001743                 TA   =          189.29415
                                              MA   =          189.33479
                                              Ha   =            189.300  n.mi
                                              Hp   =            177.903
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10045149.12                 X    =         3054584.68
     Y    =        9512006.21  feet           Y    =         2933458.50  meter
     Z    =      -17202232.42                 Z    =        -5228383.38
     XDOT =     -19446.670973                 XDOT =       -5977.141326
     YDOT =      15858.208621  feet/sec       YDOT =        4767.020598  meter/sec
     ZDOT =      -2575.465036                 ZDOT =        -813.917201
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11617401.14                 X    =        -3540983.87
     Y    =        7644632.45  feet           Y    =         2330083.97  meter
     Z    =      -17143385.57                 Z    =        -5225303.92
     XDOT =     -10325.909111                 XDOT =       -3147.337097
     YDOT =     -21749.465790  feet/sec       YDOT =       -6629.237173  meter/sec
     ZDOT =      -2689.600642                 ZDOT =        -819.790276
  
  
    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   09339.52514853  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6410 146.3250 0007955  52.7034 307.4855 15.76260136 32955
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09339.52514853   =   yrday.fracday
    Element set:     911
    Inclination:       51.6410  deg
    RA of node:       146.3250  deg
    Eccentricity:     .0007955     
    Arg of perigee:    52.7034  deg
    Mean anomaly:     307.4855  deg
    Mean motion:   15.76260136  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3295
    Checksum:              305
 
 
    Coasting Arc #13 (Orbit 3310)
    ---------------------------------------
 
    Vector Time (GMT): 2009/340/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5221838.09                 A    =         6725572.76  meter
     Y    =       -4233334.25  meter          E    =           .0015532
     Z    =        -101492.93                 I    =           51.87400
     XDOT =       2932.628094                 Wp   =          105.15222
     YDOT =       3744.214164  meter/sec      RA   =          140.28944  deg
     ZDOT =      -6057.389181                 TA   =           75.94738
                                              MA   =           75.77478
                                              Ha   =            189.244  n.mi
                                              Hp   =            177.692
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17132014.75                 X    =         5269280.91
     Y    =      -13888891.91  feet           Y    =        -4174675.30  meter
     Z    =        -332982.04                 Z    =          -76010.41
     XDOT =       9621.483248                 XDOT =        2919.967429
     YDOT =      12284.167204  feet/sec       YDOT =        3776.938416  meter/sec
     ZDOT =     -19873.324085                 ZDOT =       -6043.172788
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9845896.82                 X    =         3001029.35
     Y    =       19736322.82  feet           Y    =         6015631.20  meter
     Z    =        -232383.35                 Z    =          -70830.44
     XDOT =     -12662.795178                 XDOT =       -3859.619970
     YDOT =       6126.309551  feet/sec       YDOT =        1867.299151  meter/sec
     ZDOT =     -19816.971438                 ZDOT =       -6040.212894
  
  
    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   09340.53951804  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6410 141.0973 0007982  54.3943 305.7964 15.76321506 33116
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09340.53951804   =   yrday.fracday
    Element set:     912
    Inclination:       51.6410  deg
    RA of node:       141.0973  deg
    Eccentricity:     .0007982     
    Arg of perigee:    54.3943  deg
    Mean anomaly:     305.7964  deg
    Mean motion:   15.76321506  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3311
    Checksum:              301
 
 
    Coasting Arc #14 (Orbit 3326)
    ---------------------------------------
 
    Vector Time (GMT): 2009/341/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2099529.10                 A    =         6713943.88  meter
     Y    =       -3675733.71  meter          E    =           .0011552
     Z    =        5203651.12                 I    =           51.85692
     XDOT =       5943.534611                 Wp   =           59.66735
     YDOT =      -4812.566546  meter/sec      RA   =          135.14346  deg
     ZDOT =       -994.083506                 TA   =           39.80823
                                              MA   =           39.72354
                                              Ha   =            189.467  n.mi
                                              Hp   =            177.648
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6888218.84                 X    =        -2083548.82
     Y    =      -12059493.81  feet           Y    =        -3699122.98  meter
     Z    =       17072346.20                 Z    =         5193490.08
     XDOT =      19499.785470                 XDOT =        6001.736925
     YDOT =     -15789.260320  feet/sec       YDOT =       -4745.776923  meter/sec
     ZDOT =      -3261.428827                 ZDOT =        -965.068773
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13212508.56                 X    =         4027172.61
     Y    =       -4436620.62  feet           Y    =        -1352281.96  meter
     Z    =       17032027.76                 Z    =         5191362.06
     XDOT =      11245.805542                 XDOT =        3427.721529
     YDOT =      21317.172851  feet/sec       YDOT =        6497.474285  meter/sec
     ZDOT =      -3146.873566                 ZDOT =        -959.167063
  
  
    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   09341.55387333  .00016717  00000-0  10270-3 0  9135
    2 25544  51.6412 135.8705 0008038  60.2666 299.9298 15.76265361 33270
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09341.55387333   =   yrday.fracday
    Element set:     913
    Inclination:       51.6412  deg
    RA of node:       135.8705  deg
    Eccentricity:     .0008038     
    Arg of perigee:    60.2666  deg
    Mean anomaly:     299.9298  deg
    Mean motion:   15.76265361  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3327
    Checksum:              329
 
 
    Coasting Arc #15 (Orbit 3342)
    ---------------------------------------
 
    Vector Time (GMT): 2009/342/12:11:21.825
    Vector Time (MET): N/A
    Weight (LBS)     : 731798.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5081294.35                 A    =         6724384.53  meter
     Y    =        4080220.04  meter          E    =           .0022008
     Z    =        1615760.09                 I    =           51.91457
     XDOT =      -1941.880777                 Wp   =           63.58589
     YDOT =      -4725.462120  meter/sec      RA   =          130.03162  deg
     ZDOT =       5775.684920                 TA   =          314.21743
                                              MA   =          314.39797
                                              Ha   =            189.272  n.mi
                                              Hp   =            177.510
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16670913.23                 X    =        -5134391.55
     Y    =       13386548.69  feet           Y    =         4023101.01  meter
     Z    =        5301050.15                 Z    =         1590946.32
     XDOT =      -6370.999923                 XDOT =       -1916.952894
     YDOT =     -15503.484646  feet/sec       YDOT =       -4747.038394  meter/sec
     ZDOT =      18949.097507                 ZDOT =        5766.311437
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10104265.30                 X    =        -3079780.06
     Y    =      -18869341.46  feet           Y    =        -5751375.28  meter
     Z    =        5203070.47                 Z    =         1585895.88
     XDOT =      15051.417894                 XDOT =        4587.672174
     YDOT =      -2798.516573  feet/sec       YDOT =        -852.987851  meter/sec
     ZDOT =      18911.853364                 ZDOT =        5764.332905
  
  
    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   09342.56820488  .00016717  00000-0  10270-3 0  9141
    2 25544  51.6424 130.6440 0007895  64.2128 295.9850 15.76359037 33431
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      09342.56820488   =   yrday.fracday
    Element set:     914
    Inclination:       51.6424  deg
    RA of node:       130.6440  deg
    Eccentricity:     .0007895     
    Arg of perigee:    64.2128  deg
    Mean anomaly:     295.9850  deg
    Mean motion:   15.76359037  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3343
    Checksum:              326
 
             

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