Return to Human Space Flight home page

    
   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14262.1813
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   71.2
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.940
   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 
   ------------------------------------------------------------------------
   146/12:07:22.200           0.0               0.0              0.0    
   N/A                       -0.0              -0.0              228.5  
   000/00:12:03.600           0.0               0.0              222.2  
   
   148/20:33:33.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.5  
   000/00:00:00.000           0.0               0.0              222.2  
   
   149/04:45:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.6  
   000/00:00:00.000           0.0               0.0              222.2  
   
   149/15:39:55.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.5  
   000/00:00:00.000           0.0               0.0              222.2  
   
   152/12:36:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.7  
   000/00:00:00.000           0.0               0.0              222.0  
   
   160/04:50:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.1  
   000/00:00:00.000           0.0               0.0              221.7  
   
 
 
    Coasting Arc #1 (Orbit 2848)
    ---------------------------------------
 
    Vector Time (GMT): 2020/146/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 918884.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2889874.51                 A    =         6794559.08  meter
     Y    =        4146263.08  meter          E    =           .0008863
     Z    =       -4549652.35                 I    =           52.01546
     XDOT =      -3558.870999                 Wp   =          100.43334
     YDOT =       5977.020061  meter/sec      RA   =           99.78665  deg
     ZDOT =       3190.246072                 TA   =          201.47895
                                              MA   =          201.51616
                                              Ha   =            228.508  n.mi
                                              Hp   =            222.348
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9481215.58                 X    =         2865394.76
     Y    =       13603225.32  feet           Y    =         4178443.61  meter
     Z    =      -14926680.95                 Z    =        -4535673.11
     XDOT =     -11676.085955                 XDOT =       -3640.939819
     YDOT =      19609.645868  feet/sec       YDOT =        5936.762816  meter/sec
     ZDOT =      10466.686589                 ZDOT =        3172.760012
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16485077.08                 X    =         5024651.49
     Y    =       -2256772.27  feet           Y    =         -687864.19  meter
     Z    =      -14862577.33                 Z    =        -4530113.57
     XDOT =      11850.386685                 XDOT =        3611.997862
     YDOT =      18245.111353  feet/sec       YDOT =        5561.109940  meter/sec
     ZDOT =      10385.912307                 ZDOT =        3165.626071
  
  
    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   20146.51043290  .00016717  00000-0  10270-3 0  9004
    2 25544  51.6406 100.7144 0001800 349.1600  10.9511 15.49370393 28497
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20146.51043290   =   yrday.fracday
    Element set:     900
    Inclination:       51.6406  deg
    RA of node:       100.7144  deg
    Eccentricity:     .0001800     
    Arg of perigee:   349.1600  deg
    Mean anomaly:      10.9511  deg
    Mean motion:   15.49370393  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2849
    Checksum:              265
 
 
    Coasting Arc #2 (Orbit 2848)
    ---------------------------------------
 
    Vector Time (GMT): 2020/146/12:13:24.000
    Vector Time (MET): N/A
    Weight (LBS)     : 953907.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -701260.56                 A    =         6802998.96  meter
     Y    =        6735841.02  meter          E    =           .0011985
     Z    =        -577568.87                 I    =           52.04380
     XDOT =      -4756.359817                 Wp   =           34.69622
     YDOT =         13.772283  meter/sec      RA   =           99.75811  deg
     ZDOT =       6006.255110                 TA   =          319.11688
                                              MA   =          319.20671
                                              Ha   =            228.479  n.mi
                                              Hp   =            222.228
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2300723.61                 X    =         -773725.09
     Y    =       22099215.96  feet           Y    =         6727593.95  meter
     Z    =       -1894911.00                 Z    =         -581150.21
     XDOT =     -15604.855044                 XDOT =       -4785.335498
     YDOT =         45.184656  feet/sec       YDOT =         -39.579749  meter/sec
     ZDOT =      19705.561386                 ZDOT =        5983.080014
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19256206.59                 X    =         5869291.77
     Y    =       11081655.95  feet           Y    =         3377688.73  meter
     Z    =       -1911745.70                 Z    =         -582700.09
     XDOT =      -5553.452079                 XDOT =       -1692.692194
     YDOT =      12991.496985  feet/sec       YDOT =        3959.808281  meter/sec
     ZDOT =      19598.924930                 ZDOT =        5973.752319
  
  
    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   20146.51043288  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6406 100.7145 0001739 350.4977   9.6140 15.49388265 28491
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20146.51043288   =   yrday.fracday
    Element set:     901
    Inclination:       51.6406  deg
    RA of node:       100.7145  deg
    Eccentricity:     .0001739     
    Arg of perigee:   350.4977  deg
    Mean anomaly:       9.6140  deg
    Mean motion:   15.49388265  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2849
    Checksum:              307
 
 
    Coasting Arc #3 (Orbit 2864)
    ---------------------------------------
 
    Vector Time (GMT): 2020/147/12:13:24.000
    Vector Time (MET): N/A
    Weight (LBS)     : 953907.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         240217.86                 A    =         6803092.67  meter
     Y    =       -6780518.15  meter          E    =           .0011549
     Z    =         426130.12                 I    =           52.04946
     XDOT =       4730.741475                 Wp   =          124.45933
     YDOT =       -217.667071  meter/sec      RA   =           94.83664  deg
     ZDOT =      -6020.727335                 TA   =           50.98127
                                              MA   =           50.87850
                                              Ha   =            228.508  n.mi
                                              Hp   =            222.226
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         788116.33                 X    =          313951.87
     Y    =      -22245794.47  feet           Y    =        -6777419.67  meter
     Z    =        1398064.69                 Z    =          427474.94
     XDOT =      15520.805365                 XDOT =        4762.069237
     YDOT =       -714.130811  feet/sec       YDOT =        -164.588367  meter/sec
     ZDOT =     -19753.042439                 ZDOT =       -5997.671111
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20169169.59                 X    =        -6147562.89
     Y    =       -9417149.50  feet           Y    =        -2870347.17  meter
     Z    =        1404626.96                 Z    =          428130.30
     XDOT =       4777.859810                 XDOT =        1456.291670
     YDOT =     -13216.807430  feet/sec       YDOT =       -4028.482905  meter/sec
     ZDOT =     -19646.932111                 ZDOT =       -5988.384907
  
  
    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   20147.54241826  .00016717  00000-0  10270-3 0  9025
    2 25544  51.6415  95.6070 0001774 352.3114   7.8008 15.49379051 28657
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20147.54241826   =   yrday.fracday
    Element set:     902
    Inclination:       51.6415  deg
    RA of node:        95.6070  deg
    Eccentricity:     .0001774     
    Arg of perigee:   352.3114  deg
    Mean anomaly:       7.8008  deg
    Mean motion:   15.49379051  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2865
    Checksum:              296
 
 
    Coasting Arc #4 (Orbit 2879)
    ---------------------------------------
 
    Vector Time (GMT): 2020/148/12:13:24.000
    Vector Time (MET): N/A
    Weight (LBS)     : 953907.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         251524.14                 A    =         6803096.90  meter
     Y    =        6784787.01  meter          E    =           .0012691
     Z    =        -309656.41                 I    =           52.05143
     XDOT =      -4703.414238                 Wp   =           36.96813
     YDOT =        443.375401  meter/sec      RA   =           89.91521  deg
     ZDOT =       6032.082295                 TA   =          319.71962
                                              MA   =          319.81358
                                              Ha   =            228.529  n.mi
                                              Hp   =            222.181
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         825210.44                 X    =          177140.08
     Y    =       22259799.89  feet           Y    =         6787183.87  meter
     Z    =       -1015933.11                 Z    =         -308614.18
     XDOT =     -15431.149076                 XDOT =       -4737.323010
     YDOT =       1454.643705  feet/sec       YDOT =         390.587913  meter/sec
     ZDOT =      19790.296244                 ZDOT =        6009.152672
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20945544.48                 X    =         6384201.96
     Y    =        7581079.66  feet           Y    =         2310713.08  meter
     Z    =       -1011524.16                 Z    =         -308312.57
     XDOT =      -3938.345258                 XDOT =       -1200.407635
     YDOT =      13447.015885  feet/sec       YDOT =        4098.650442  meter/sec
     ZDOT =      19684.747180                 ZDOT =        5999.910941
  
  
    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   20148.50990252  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6417  90.8191 0001788 354.3512   5.7618 15.49390270 28806
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20148.50990252   =   yrday.fracday
    Element set:     903
    Inclination:       51.6417  deg
    RA of node:        90.8191  deg
    Eccentricity:     .0001788     
    Arg of perigee:   354.3512  deg
    Mean anomaly:       5.7618  deg
    Mean motion:   15.49390270  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2880
    Checksum:              307
 
 
    Coasting Arc #5 (Orbit 2885)
    ---------------------------------------
 
    Vector Time (GMT): 2020/148/20:33:33.000
    Vector Time (MET): N/A
    Weight (LBS)     : 953907.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3083515.96                 A    =         6797274.51  meter
     Y    =       -4746944.28  meter          E    =           .0011636
     Z    =        3755767.29                 I    =           52.03018
     XDOT =       3184.651135                 Wp   =           76.55949
     YDOT =      -5483.136797  meter/sec      RA   =           88.17932  deg
     ZDOT =      -4301.754022                 TA   =           58.90773
                                              MA   =           58.79359
                                              Ha   =            228.524  n.mi
                                              Hp   =            222.241
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10116522.17                 X    =        -3048448.38
     Y    =      -15573964.18  feet           Y    =        -4781230.86  meter
     Z    =       12322071.15                 Z    =         3740873.23
     XDOT =      10448.330497                 XDOT =        3266.623933
     YDOT =     -17989.293953  feet/sec       YDOT =       -5447.064755  meter/sec
     ZDOT =     -14113.366215                 ZDOT =       -4286.086011
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13518508.89                 X    =         4120441.51
     Y    =       12799223.14  feet           Y    =         3901203.21  meter
     Z    =       12253800.35                 Z    =         3734958.35
     XDOT =      -5174.880094                 XDOT =       -1577.303453
     YDOT =      18951.894138  feet/sec       YDOT =        5776.537333  meter/sec
     ZDOT =     -14040.942766                 ZDOT =       -4279.679355
  
  
    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   20148.89689468  .00016717  00000-0  10270-3 0  9044
    2 25544  51.6400  88.9000 0001552 350.3688   9.7432 15.49384063 28861
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20148.89689468   =   yrday.fracday
    Element set:     904
    Inclination:       51.6400  deg
    RA of node:        88.9000  deg
    Eccentricity:     .0001552     
    Arg of perigee:   350.3688  deg
    Mean anomaly:       9.7432  deg
    Mean motion:   15.49384063  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2886
    Checksum:              329
 
 
    Coasting Arc #6 (Orbit 2890)
    ---------------------------------------
 
    Vector Time (GMT): 2020/149/04:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 953907.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3424456.97                 A    =         6794135.53  meter
     Y    =       -3586466.27  meter          E    =           .0010891
     Z    =       -4655231.62                 I    =           52.02236
     XDOT =       2731.266477                 Wp   =           62.15332
     YDOT =       6490.755674  meter/sec      RA   =           86.54889  deg
     ZDOT =      -2991.826359                 TA   =          178.10843
                                              MA   =          178.10431
                                              Ha   =            228.556  n.mi
                                              Hp   =            222.235
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11235095.06                 X    =         3486919.79
     Y    =      -11766621.63  feet           Y    =        -3547821.61  meter
     Z    =      -15273069.62                 Z    =        -4638445.81
     XDOT =       8960.848023                 XDOT =        2673.014472
     YDOT =      21295.130164  feet/sec       YDOT =        6520.973378  meter/sec
     ZDOT =      -9815.703276                 ZDOT =       -2978.699479
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16324519.36                 X    =         4975713.50
     Y    =        -742272.37  feet           Y    =         -226244.62  meter
     Z    =      -15195607.94                 Z    =        -4631621.30
     XDOT =      -8148.749160                 XDOT =       -2483.738744
     YDOT =      20475.963468  feet/sec       YDOT =        6241.073665  meter/sec
     ZDOT =      -9755.668588                 ZDOT =       -2973.527786
  
  
    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   20149.21938957  .00016717  00000-0  10270-3 0  9052
    2 25544  51.6431  87.3066 0001595 359.6128    .5021 15.49383675 28915
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20149.21938957   =   yrday.fracday
    Element set:     905
    Inclination:       51.6431  deg
    RA of node:        87.3066  deg
    Eccentricity:     .0001595     
    Arg of perigee:   359.6128  deg
    Mean anomaly:        .5021  deg
    Mean motion:   15.49383675  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2891
    Checksum:              321
 
 
    Coasting Arc #7 (Orbit 2897)
    ---------------------------------------
 
    Vector Time (GMT): 2020/149/15:39:55.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3952090.34                 A    =         6791572.19  meter
     Y    =       -1734265.44  meter          E    =           .0014449
     Z    =       -5256571.32                 I    =           52.01410
     XDOT =       1662.795802                 Wp   =           73.23091
     YDOT =       7373.070355  meter/sec      RA   =           84.29978  deg
     ZDOT =      -1181.030567                 TA   =          185.46516
                                              MA   =          185.48094
                                              Ha   =            228.516  n.mi
                                              Hp   =            222.244
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12966175.67                 X    =         3996723.02
     Y    =       -5689847.24  feet           Y    =        -1689820.06  meter
     Z    =      -17245968.90                 Z    =        -5237265.51
     XDOT =       5455.366804                 XDOT =        1585.961111
     YDOT =      24189.863369  feet/sec       YDOT =        7391.235476  meter/sec
     ZDOT =      -3874.772201                 ZDOT =       -1173.138962
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11575416.21                 X    =        -3528186.86
     Y    =       -8340630.30  feet           Y    =        -2542224.11  meter
     Z    =      -17157014.37                 Z    =        -5229457.98
     XDOT =      17387.365052                 XDOT =        5299.668868
     YDOT =     -16224.786995  feet/sec       YDOT =       -4945.315076  meter/sec
     ZDOT =      -3838.887915                 ZDOT =       -1170.093037
  
  
    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   20149.67088053  .00016717  00000-0  10270-3 0  9066
    2 25544  51.6442  85.0740 0001957 356.7746   3.3392 15.49414510 28989
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20149.67088053   =   yrday.fracday
    Element set:     906
    Inclination:       51.6442  deg
    RA of node:        85.0740  deg
    Eccentricity:     .0001957     
    Arg of perigee:   356.7746  deg
    Mean anomaly:       3.3392  deg
    Mean motion:   15.49414510  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2898
    Checksum:              319
 
 
    Coasting Arc #8 (Orbit 2913)
    ---------------------------------------
 
    Vector Time (GMT): 2020/150/15:39:55.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3833331.39                 A    =         6791512.11  meter
     Y    =        1899084.64  meter          E    =           .0003154
     Z    =        5272106.00                 I    =           52.00853
     XDOT =      -2183.876654                 Wp   =           90.85231
     YDOT =      -7272.857605  meter/sec      RA   =           79.37532  deg
     ZDOT =       1031.315979                 TA   =          349.31227
                                              MA   =          349.31897
                                              Ha   =            228.761  n.mi
                                              Hp   =            222.074
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12576546.55                 X    =        -3879891.42
     Y    =        6230592.64  feet           Y    =         1855956.64  meter
     Z    =       17296935.71                 Z    =         5253372.37
     XDOT =      -7164.949653                 XDOT =       -2107.396620
     YDOT =     -23861.081382  feet/sec       YDOT =       -7296.851764  meter/sec
     ZDOT =       3383.582607                 ZDOT =        1020.892477
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11972657.45                 X    =         3649265.99
     Y    =        7524927.84  feet           Y    =         2293598.01  meter
     Z    =       17210599.27                 Z    =         5245790.66
     XDOT =     -15974.229044                 XDOT =       -4868.945013
     YDOT =      17781.672720  feet/sec       YDOT =        5419.853845  meter/sec
     ZDOT =       3336.050235                 ZDOT =        1016.828112
  
  
    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   20150.70286133  .00016717  00000-0  10270-3 0  9072
    2 25544  51.6435  79.9662 0001894   2.3710 357.7449 15.49392457 29144
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20150.70286133   =   yrday.fracday
    Element set:     907
    Inclination:       51.6435  deg
    RA of node:        79.9662  deg
    Eccentricity:     .0001894     
    Arg of perigee:     2.3710  deg
    Mean anomaly:     357.7449  deg
    Mean motion:   15.49392457  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2914
    Checksum:              320
 
 
    Coasting Arc #9 (Orbit 2928)
    ---------------------------------------
 
    Vector Time (GMT): 2020/151/15:39:55.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3725093.87                 A    =         6791367.59  meter
     Y    =       -2065957.70  meter          E    =           .0014870
     Z    =       -5302329.77                 I    =           52.00036
     XDOT =       2689.744462                 Wp   =           75.69881
     YDOT =       7107.262304  meter/sec      RA   =           74.45019  deg
     ZDOT =       -878.060369                 TA   =          185.91686
                                              MA   =          185.93444
                                              Ha   =            228.581  n.mi
                                              Hp   =            222.174
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12221436.60                 X    =         3773674.85
     Y    =       -6778076.44  feet           Y    =        -2024028.87  meter
     Z    =      -17396095.05                 Z    =        -5284116.94
     XDOT =       8824.620939                 XDOT =        2614.334151
     YDOT =      23317.789711  feet/sec       YDOT =        7136.919385  meter/sec
     ZDOT =      -2880.775488                 ZDOT =        -865.177081
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12369678.90                 X    =        -3770278.13
     Y    =       -6723894.36  feet           Y    =        -2049443.00  meter
     Z    =      -17312141.52                 Z    =        -5276740.74
     XDOT =      14357.603851                 XDOT =        4376.197654
     YDOT =     -19134.660074  feet/sec       YDOT =       -5832.244391  meter/sec
     ZDOT =      -2821.923849                 ZDOT =        -860.122389
  
  
    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   20151.67034205  .00016717  00000-0  10270-3 0  9081
    2 25544  51.6430  75.1776 0001969   1.9303 358.1854 15.49413342 29297
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20151.67034205   =   yrday.fracday
    Element set:     908
    Inclination:       51.6430  deg
    RA of node:        75.1776  deg
    Eccentricity:     .0001969     
    Arg of perigee:     1.9303  deg
    Mean anomaly:     358.1854  deg
    Mean motion:   15.49413342  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2929
    Checksum:              302
 
 
    Coasting Arc #10 (Orbit 2942)
    ---------------------------------------
 
    Vector Time (GMT): 2020/152/12:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3942327.12                 A    =         6791047.42  meter
     Y    =        1391871.96  meter          E    =           .0003231
     Z    =        5349372.14                 I    =           51.99118
     XDOT =      -2583.917138                 Wp   =           51.65637
     YDOT =      -7214.389109  meter/sec      RA   =           70.14733  deg
     ZDOT =        -25.172616                 TA   =           38.59405
                                              MA   =           38.57096
                                              Ha   =            228.716  n.mi
                                              Hp   =            221.987
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12934144.10                 X    =        -3983582.72
     Y    =        4566509.06  feet           Y    =         1347554.88  meter
     Z    =       17550433.52                 Z    =         5330121.72
     XDOT =      -8477.418432                 XDOT =       -2502.929379
     YDOT =     -23669.255606  feet/sec       YDOT =       -7242.831477  meter/sec
     ZDOT =        -82.587323                 ZDOT =         -37.528286
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1650666.96                 X    =          503123.29
     Y    =       13730460.88  feet           Y    =         4185044.48  meter
     Z    =       17461745.26                 Z    =         5322339.96
     XDOT =     -23937.793464                 XDOT =       -7296.239448
     YDOT =       3062.766006  feet/sec       YDOT =         933.531079  meter/sec
     ZDOT =       -138.991037                 ZDOT =         -42.364468
  
  
    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   20152.57332332  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6434  70.7082 0001915   3.9610 356.1555 15.49434558 29430
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20152.57332332   =   yrday.fracday
    Element set:     909
    Inclination:       51.6434  deg
    RA of node:        70.7082  deg
    Eccentricity:     .0001915     
    Arg of perigee:     3.9610  deg
    Mean anomaly:     356.1555  deg
    Mean motion:   15.49434558  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2943
    Checksum:              298
 
 
    Coasting Arc #11 (Orbit 2957)
    ---------------------------------------
 
    Vector Time (GMT): 2020/153/12:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3885946.87                 A    =         6791126.99  meter
     Y    =       -1572988.27  meter          E    =           .0015324
     Z    =       -5355806.04                 I    =           51.97990
     XDOT =       3077.685885                 Wp   =           83.84458
     YDOT =       7000.873640  meter/sec      RA   =           65.22082  deg
     ZDOT =        178.933036                 TA   =          187.84489
                                              MA   =          187.86889
                                              Ha   =            228.711  n.mi
                                              Hp   =            222.038
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12749169.53                 X    =         3929263.33
     Y    =       -5160722.67  feet           Y    =        -1529290.13  meter
     Z    =      -17571542.11                 Z    =        -5336824.42
     XDOT =      10097.394637                 XDOT =        2998.302135
     YDOT =      22968.745538  feet/sec       YDOT =        7034.846636  meter/sec
     ZDOT =        587.050644                 ZDOT =         193.691209
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2505678.05                 X    =         -763730.67
     Y    =      -13636790.95  feet           Y    =        -4156493.88  meter
     Z    =      -17484078.02                 Z    =        -5329146.98
     XDOT =      23520.373777                 XDOT =        7169.009927
     YDOT =      -5152.285385  feet/sec       YDOT =       -1570.416585  meter/sec
     ZDOT =        654.508009                 ZDOT =         199.494041
  
  
    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   20153.54080201  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6446  65.9195 0002034  12.2919 347.8281 15.49415880 29588
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20153.54080201   =   yrday.fracday
    Element set:     910
    Inclination:       51.6446  deg
    RA of node:        65.9195  deg
    Eccentricity:     .0002034     
    Arg of perigee:    12.2919  deg
    Mean anomaly:     347.8281  deg
    Mean motion:   15.49415880  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2958
    Checksum:              301
 
 
    Coasting Arc #12 (Orbit 2973)
    ---------------------------------------
 
    Vector Time (GMT): 2020/154/12:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3817524.40                 A    =         6791078.99  meter
     Y    =        1736794.88  meter          E    =           .0003967
     Z    =        5338849.60                 I    =           51.96452
     XDOT =      -3561.240704                 Wp   =           47.38391
     YDOT =      -6777.156614  meter/sec      RA   =           60.29411  deg
     ZDOT =       -338.984404                 TA   =           45.85191
                                              MA   =           45.81929
                                              Ha   =            228.816  n.mi
                                              Hp   =            221.868
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12524686.34                 X    =        -3862595.40
     Y    =        5698145.94  feet           Y    =         1693852.01  meter
     Z    =       17515910.77                 Z    =         5320196.06
     XDOT =     -11683.860576                 XDOT =       -3483.545234
     YDOT =     -22234.765795  feet/sec       YDOT =       -6816.546483  meter/sec
     ZDOT =      -1112.153556                 ZDOT =        -356.095762
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3309189.57                 X    =         1008640.98
     Y    =       13468113.97  feet           Y    =         4105081.14  meter
     Z    =       17429943.65                 Z    =         5312646.82
     XDOT =     -23002.860688                 XDOT =       -7011.271938
     YDOT =       7204.381325  feet/sec       YDOT =        2195.895428  meter/sec
     ZDOT =      -1190.436204                 ZDOT =        -362.844955
  
  
    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   20154.57277630  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6443  60.8122 0001995  12.6931 347.4269 15.49438452 29742
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20154.57277630   =   yrday.fracday
    Element set:     911
    Inclination:       51.6443  deg
    RA of node:        60.8122  deg
    Eccentricity:     .0001995     
    Arg of perigee:    12.6931  deg
    Mean anomaly:     347.4269  deg
    Mean motion:   15.49438452  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2974
    Checksum:              314
 
 
    Coasting Arc #13 (Orbit 2988)
    ---------------------------------------
 
    Vector Time (GMT): 2020/155/12:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3752880.36                 A    =         6791189.45  meter
     Y    =       -1918724.59  meter          E    =           .0015220
     Z    =       -5337941.63                 I    =           51.94747
     XDOT =       4016.024688                 Wp   =           86.26773
     YDOT =       6492.048964  meter/sec      RA   =           55.36645  deg
     ZDOT =        492.099615                 TA   =          188.40545
                                              MA   =          188.43097
                                              Ha   =            228.735  n.mi
                                              Hp   =            221.989
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12312599.60                 X    =         3799986.21
     Y    =       -6295028.17  feet           Y    =        -1876493.10  meter
     Z    =      -17512931.84                 Z    =        -5319597.19
     XDOT =      13175.934017                 XDOT =        3940.739817
     YDOT =      21299.373240  feet/sec       YDOT =        6536.538000  meter/sec
     ZDOT =       1614.500048                 ZDOT =         511.426182
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4164024.01                 X    =        -1269194.52
     Y    =      -13298234.84  feet           Y    =        -4053301.98  meter
     Z    =      -17428371.24                 Z    =        -5312167.56
     XDOT =      22206.027415                 XDOT =        6768.397156
     YDOT =      -9175.786450  feet/sec       YDOT =       -2796.779710  meter/sec
     ZDOT =       1702.977018                 ZDOT =         519.067395
  
  
    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   20155.54025356  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6448  56.0244 0002017  15.3179 344.8032 15.49420344 29895
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20155.54025356   =   yrday.fracday
    Element set:     912
    Inclination:       51.6448  deg
    RA of node:        56.0244  deg
    Eccentricity:     .0002017     
    Arg of perigee:    15.3179  deg
    Mean anomaly:     344.8032  deg
    Mean motion:   15.49420344  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2989
    Checksum:              292
 
 
    Coasting Arc #14 (Orbit 3004)
    ---------------------------------------
 
    Vector Time (GMT): 2020/156/12:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3679011.95                 A    =         6791177.98  meter
     Y    =        2080987.82  meter          E    =           .0004608
     Z    =        5313011.36                 I    =           51.92842
     XDOT =      -4456.970395                 Wp   =           44.58426
     YDOT =      -6199.559359  meter/sec      RA   =           50.43717  deg
     ZDOT =       -654.476607                 TA   =           51.66437
                                              MA   =           51.62297
                                              Ha   =            228.833  n.mi
                                              Hp   =            221.825
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12070249.18                 X    =        -3727816.65
     Y    =        6827387.87  feet           Y    =         2039572.75  meter
     Z    =       17431139.63                 Z    =         5295021.72
     XDOT =     -14622.606284                 XDOT =       -4384.134714
     YDOT =     -20339.761677  feet/sec       YDOT =       -6248.993018  meter/sec
     ZDOT =      -2147.232961                 ZDOT =        -675.951216
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4954534.95                 X    =         1510142.25
     Y    =       13062981.02  feet           Y    =         3981596.61  meter
     Z    =       17348195.29                 Z    =         5287729.92
     XDOT =     -21320.609679                 XDOT =       -6498.521830
     YDOT =      11084.232419  feet/sec       YDOT =        3378.474041  meter/sec
     ZDOT =      -2245.597850                 ZDOT =        -684.458225
  
  
    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   20156.57222510  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6456  50.9169 0001990  15.7573 344.3639 15.49442796 30057
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20156.57222510   =   yrday.fracday
    Element set:     913
    Inclination:       51.6456  deg
    RA of node:        50.9169  deg
    Eccentricity:     .0001990     
    Arg of perigee:    15.7573  deg
    Mean anomaly:     344.3639  deg
    Mean motion:   15.49442796  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3005
    Checksum:              310
 
 
    Coasting Arc #15 (Orbit 3019)
    ---------------------------------------
 
    Vector Time (GMT): 2020/157/12:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3605128.07                 A    =         6791315.14  meter
     Y    =       -2264003.83  meter          E    =           .0015131
     Z    =       -5304440.68                 I    =           51.90597
     XDOT =       4860.536062                 Wp   =           88.27934
     YDOT =       5851.447704  meter/sec      RA   =           45.50628  deg
     ZDOT =        808.391358                 TA   =          189.42330
                                              MA   =          189.45172
                                              Ha   =            228.808  n.mi
                                              Hp   =            221.889
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11827847.99                 X    =         3655943.08
     Y    =       -7427834.07  feet           Y    =        -2223403.60  meter
     Z    =      -17403020.60                 Z    =        -5286805.20
     XDOT =      15946.640624                 XDOT =        4790.815448
     YDOT =      19197.663071  feet/sec       YDOT =        5905.411694  meter/sec
     ZDOT =       2652.202618                 ZDOT =         831.833936
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5805483.09                 X    =        -1769511.24
     Y    =      -12813717.94  feet           Y    =        -3905621.23  meter
     Z    =      -17321686.74                 Z    =        -5279650.12
     XDOT =      20178.737011                 XDOT =        6150.479041
     YDOT =     -12861.988900  feet/sec       YDOT =       -3920.334217  meter/sec
     ZDOT =       2759.635004                 ZDOT =         841.136749
  
  
    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   20157.53969837  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6453  46.1285 0002133  20.6040 339.5196 15.49426741 30207
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20157.53969837   =   yrday.fracday
    Element set:     914
    Inclination:       51.6453  deg
    RA of node:        46.1285  deg
    Eccentricity:     .0002133     
    Arg of perigee:    20.6040  deg
    Mean anomaly:     339.5196  deg
    Mean motion:   15.49426741  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3020
    Checksum:              298
 
 
    Coasting Arc #16 (Orbit 3035)
    ---------------------------------------
 
    Vector Time (GMT): 2020/158/12:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3524345.89                 A    =         6791375.54  meter
     Y    =        2426894.50  meter          E    =           .0005472
     Z    =        5270911.24                 I    =           51.88111
     XDOT =      -5248.194455                 Wp   =           44.97962
     YDOT =      -5499.066676  meter/sec      RA   =           40.57412  deg
     ZDOT =       -972.825434                 TA   =           54.33134
                                              MA   =           54.28041
                                              Ha   =            228.933  n.mi
                                              Hp   =            221.729
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11562814.60                 X    =        -3576825.40
     Y    =        7962252.28  feet           Y    =         2387188.25  meter
     Z    =       17293015.87                 Z    =         5253664.28
     XDOT =     -17218.485745                 XDOT =       -5181.586749
     YDOT =     -18041.557336  feet/sec       YDOT =       -5557.383097  meter/sec
     ZDOT =      -3191.684495                 ZDOT =        -998.158578
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6586160.78                 X    =         2007461.81
     Y    =       12508561.02  feet           Y    =         3812609.40  meter
     Z    =       17213451.95                 Z    =         5246660.16
     XDOT =     -18964.656344                 XDOT =       -5780.427254
     YDOT =      14557.420570  feet/sec       YDOT =        4437.101790  meter/sec
     ZDOT =      -3307.833379                 ZDOT =       -1008.227614
  
  
    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   20158.57166748  .00016717  00000-0  10270-3 0  9153
    2 25544  51.6445  41.0211 0002083  23.3917 336.7327 15.49437661 30363
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20158.57166748   =   yrday.fracday
    Element set:     915
    Inclination:       51.6445  deg
    RA of node:        41.0211  deg
    Eccentricity:     .0002083     
    Arg of perigee:    23.3917  deg
    Mean anomaly:     336.7327  deg
    Mean motion:   15.49437661  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3036
    Checksum:              300
 
 
    Coasting Arc #17 (Orbit 3050)
    ---------------------------------------
 
    Vector Time (GMT): 2020/159/12:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3437294.31                 A    =         6791528.11  meter
     Y    =       -2613757.43  meter          E    =           .0014880
     Z    =       -5254844.43                 I    =           51.85456
     XDOT =       5592.244878                 Wp   =           90.72103
     YDOT =       5097.019119  meter/sec      RA   =           35.63977  deg
     ZDOT =       1125.312688                 TA   =          190.04471
                                              MA   =          190.07448
                                              Ha   =            228.854  n.mi
                                              Hp   =            221.822
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11277212.31                 X    =         3491791.67
     Y    =       -8575319.64  feet           Y    =        -2575013.36  meter
     Z    =      -17240303.25                 Z    =        -5238015.58
     XDOT =      18347.260099                 XDOT =        5529.366749
     YDOT =      16722.503672  feet/sec       YDOT =        5159.203776  meter/sec
     ZDOT =       3691.970762                 ZDOT =        1152.325946
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7438121.30                 X    =        -2267139.37
     Y    =      -12167895.01  feet           Y    =        -3708774.40  meter
     Z    =      -17162644.41                 Z    =        -5231174.02
     XDOT =      17523.468607                 XDOT =        5341.153231
     YDOT =     -16082.209945  feet/sec       YDOT =       -4901.857591  meter/sec
     ZDOT =       3815.875793                 ZDOT =        1163.078942
  
  
    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   20159.53913921  .00016717  00000-0  10270-3 0  9164
    2 25544  51.6439  36.2325 0002106  25.7314 334.3941 15.49426941 30513
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20159.53913921   =   yrday.fracday
    Element set:     916
    Inclination:       51.6439  deg
    RA of node:        36.2325  deg
    Eccentricity:     .0002106     
    Arg of perigee:    25.7314  deg
    Mean anomaly:     334.3941  deg
    Mean motion:   15.49426941  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3051
    Checksum:              291
 
 
    Coasting Arc #18 (Orbit 3061)
    ---------------------------------------
 
    Vector Time (GMT): 2020/160/04:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2842517.57                 A    =         6791281.17  meter
     Y    =        3137908.83  meter          E    =           .0004951
     Z    =        5306871.95                 I    =           51.83185
     XDOT =      -6171.099180                 Wp   =           51.01506
     YDOT =      -4498.843242  meter/sec      RA   =           32.30485  deg
     ZDOT =       -641.856605                 TA   =           45.12019
                                              MA   =           45.08000
                                              Ha   =            229.058  n.mi
                                              Hp   =            221.658
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9325845.04                 X    =        -2903172.98
     Y    =       10294976.46  feet           Y    =         3105781.56  meter
     Z    =       17410997.20                 Z    =         5292917.47
     XDOT =     -20246.388385                 XDOT =       -6117.215371
     YDOT =     -14759.984389  feet/sec       YDOT =       -4567.551452  meter/sec
     ZDOT =      -2105.828757                 ZDOT =        -671.703309
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13422958.21                 X    =        -4091317.66
     Y    =        3875966.42  feet           Y    =         1181394.56  meter
     Z    =       17346522.04                 Z    =         5287219.92
     XDOT =      -9310.304367                 XDOT =       -2837.780771
     YDOT =     -22154.558397  feet/sec       YDOT =       -6752.709399  meter/sec
     ZDOT =      -2242.818002                 ZDOT =        -683.610927
  
  
    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   20160.24861767  .00016717  00000-0  10270-3 0  9175
    2 25544  51.6409  32.7196 0002088  33.6699 326.4584 15.49407739 30621
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20160.24861767   =   yrday.fracday
    Element set:     917
    Inclination:       51.6409  deg
    RA of node:        32.7196  deg
    Eccentricity:     .0002088     
    Arg of perigee:    33.6699  deg
    Mean anomaly:     326.4584  deg
    Mean motion:   15.49407739  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3062
    Checksum:              330
 
 
    Coasting Arc #19 (Orbit 3076)
    ---------------------------------------
 
    Vector Time (GMT): 2020/161/04:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 980162.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2718185.57                 A    =         6791403.09  meter
     Y    =       -3287201.38  meter          E    =           .0015683
     Z    =       -5298311.04                 I    =           51.80358
     XDOT =       6443.644369                 Wp   =           89.07041
     YDOT =       4043.601805  meter/sec      RA   =           27.36740  deg
     ZDOT =        799.320456                 TA   =          188.55721
                                              MA   =          188.58398
                                              Ha   =            229.023  n.mi
                                              Hp   =            221.700
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8917931.66                 X    =         2780477.97
     Y    =      -10784781.43  feet           Y    =        -3256455.41  meter
     Z    =      -17382910.24                 Z    =        -5284956.57
     XDOT =      21140.565514                 XDOT =        6394.066098
     YDOT =      13266.410123  feet/sec       YDOT =        4115.381865  meter/sec
     ZDOT =       2622.442442                 ZDOT =         830.501260
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13249941.89                 X    =         4038582.29
     Y    =       -4735212.94  feet           Y    =        -1443292.90  meter
     Z    =      -17321183.05                 Z    =        -5279496.59
     XDOT =      11167.812292                 XDOT =        3403.949187
     YDOT =      21160.662797  feet/sec       YDOT =        6449.770021  meter/sec
     ZDOT =       2765.603024                 ZDOT =         842.955802
  
  
    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   20161.21608553  .00016717  00000-0  10270-3 0  9186
    2 25544  51.6415  27.9310 0002203  36.5304 323.5996 15.49397635 30770
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20161.21608553   =   yrday.fracday
    Element set:     918
    Inclination:       51.6415  deg
    RA of node:        27.9310  deg
    Eccentricity:     .0002203     
    Arg of perigee:    36.5304  deg
    Mean anomaly:     323.5996  deg
    Mean motion:   15.49397635  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3077
    Checksum:              300
 
             

Curator: Kim Dismukes | Responsible NASA Official: Amiko Kauderer | Updated: 06/08/2009
Privacy Policy and Important Notices