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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14538.8138
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   72.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.475
   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 
   ------------------------------------------------------------------------
   231/17:35:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.2  
   000/00:00:00.000           0.0               0.0              222.2  
   
   234/09:30:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.1  
   000/00:00:00.000           0.0               0.0              222.1  
   
   238/20:27:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.4  
   000/00:00:00.000           0.0               0.0              221.8  
   
 
 
    Coasting Arc #1 (Orbit 73)
    ---------------------------------------
 
    Vector Time (GMT): 2020/225/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 958140.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1832476.05                 A    =         6795687.70  meter
     Y    =       -4842973.89  meter          E    =           .0009644
     Z    =       -4411058.15                 I    =           52.00064
     XDOT =       4755.114894                 Wp   =           62.52374
     YDOT =       4918.602475  meter/sec      RA   =           69.00169  deg
     ZDOT =      -3426.225266                 TA   =          172.85451
                                              MA   =          172.84075
                                              Ha   =            228.976  n.mi
                                              Hp   =            222.465
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6012060.52                 X    =         1907921.69
     Y    =      -15889021.94  feet           Y    =        -4822059.75  meter
     Z    =      -14471975.57                 Z    =        -4401973.78
     XDOT =      15600.770651                 XDOT =        4716.402734
     YDOT =      16137.147228  feet/sec       YDOT =        4971.561299  meter/sec
     ZDOT =     -11240.896541                 ZDOT =       -3403.220686
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14823078.98                 X    =        -4518074.47
     Y    =        8372665.02  feet           Y    =         2551988.30  meter
     Z    =      -14429787.82                 Z    =        -4398199.33
     XDOT =      -1220.187247                 XDOT =        -371.913073
     YDOT =     -21342.545455  feet/sec       YDOT =       -6505.207855  meter/sec
     ZDOT =     -11134.905445                 ZDOT =       -3393.919180
  
  
    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   20225.52232684  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6415  69.6636 0001326  10.2223 349.8954 15.49155900   744
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20225.52232684   =   yrday.fracday
    Element set:     900
    Inclination:       51.6415  deg
    RA of node:        69.6636  deg
    Eccentricity:     .0001326     
    Arg of perigee:    10.2223  deg
    Mean anomaly:     349.8954  deg
    Mean motion:   15.49155900  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              74
    Checksum:              288
 
 
    Coasting Arc #2 (Orbit 89)
    ---------------------------------------
 
    Vector Time (GMT): 2020/226/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 958140.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1450632.06                 A    =         6795636.71  meter
     Y    =        4937960.33  meter          E    =           .0009237
     Z    =        4430877.18                 I    =           51.98767
     XDOT =      -5152.699905                 Wp   =          101.02129
     YDOT =      -4554.880347  meter/sec      RA   =           64.07775  deg
     ZDOT =       3381.521681                 TA   =          314.88296
                                              MA   =          314.95791
                                              Ha   =            229.105  n.mi
                                              Hp   =            222.413
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4759291.54                 X    =        -1527264.49
     Y    =       16200657.25  feet           Y    =         4921309.54  meter
     Z    =       14536998.63                 Z    =         4423644.85
     XDOT =     -16905.183414                 XDOT =       -5117.808277
     YDOT =     -14943.833160  feet/sec       YDOT =       -4612.306662  meter/sec
     ZDOT =      11094.231238                 ZDOT =        3356.576510
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13891161.25                 X    =         4234025.95
     Y    =       -9650132.47  feet           Y    =        -2941360.38  meter
     Z    =       14503346.60                 Z    =         4420620.04
     XDOT =       3275.407159                 XDOT =         998.344102
     YDOT =      21253.779344  feet/sec       YDOT =        6478.151944  meter/sec
     ZDOT =      10979.271423                 ZDOT =        3346.481930
  
  
    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   20226.55446480  .00016717  00000-0  10270-3 0  9016
    2 25544  51.6422  64.5564 0001409  12.5879 347.5306 15.49135563   907
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20226.55446480   =   yrday.fracday
    Element set:     901
    Inclination:       51.6422  deg
    RA of node:        64.5564  deg
    Eccentricity:     .0001409     
    Arg of perigee:    12.5879  deg
    Mean anomaly:     347.5306  deg
    Mean motion:   15.49135563  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              90
    Checksum:              297
 
 
    Coasting Arc #3 (Orbit 104)
    ---------------------------------------
 
    Vector Time (GMT): 2020/227/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 958140.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1085447.80                 A    =         6795410.69  meter
     Y    =       -5007410.73  meter          E    =           .0010274
     Z    =       -4474316.24                 I    =           51.97025
     XDOT =       5502.534459                 Wp   =           63.47168
     YDOT =       4154.753049  meter/sec      RA   =           59.15260  deg
     ZDOT =      -3316.311390                 TA   =          173.14933
                                              MA   =          173.13528
                                              Ha   =            229.063  n.mi
                                              Hp   =            222.330
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3561180.45                 X    =         1163094.92
     Y    =      -16428512.89  feet           Y    =        -4994837.97  meter
     Z    =      -14679515.22                 Z    =        -4468855.42
     XDOT =      18052.934577                 XDOT =        5471.774374
     YDOT =      13631.079556  feet/sec       YDOT =        4216.114592  meter/sec
     ZDOT =     -10880.286711                 ZDOT =       -3289.656905
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12912637.44                 X    =        -3935771.89
     Y    =       10797658.42  feet           Y    =         3291126.28  meter
     Z    =      -14654029.34                 Z    =        -4466548.14
     XDOT =      -5282.902412                 XDOT =       -1610.228655
     YDOT =     -20910.741207  feet/sec       YDOT =       -6373.593920  meter/sec
     ZDOT =     -10757.421021                 ZDOT =       -3278.861927
  
  
    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   20227.52209074  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6411  59.7683 0001396  21.7448 338.3761 15.49163833  1053
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20227.52209074   =   yrday.fracday
    Element set:     902
    Inclination:       51.6411  deg
    RA of node:        59.7683  deg
    Eccentricity:     .0001396     
    Arg of perigee:    21.7448  deg
    Mean anomaly:     338.3761  deg
    Mean motion:   15.49163833  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             105
    Checksum:              298
 
 
    Coasting Arc #4 (Orbit 120)
    ---------------------------------------
 
    Vector Time (GMT): 2020/228/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 958140.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -700693.76                 A    =         6795347.53  meter
     Y    =        5043447.55  meter          E    =           .0009128
     Z    =        4493342.17                 I    =           51.95095
     XDOT =      -5841.771641                 Wp   =          102.48831
     YDOT =      -3730.887155  meter/sec      RA   =           54.22689  deg
     ZDOT =       3269.166012                 TA   =          314.67554
                                              MA   =          314.74988
                                              Ha   =            229.132  n.mi
                                              Hp   =            222.318
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2298864.06                 X    =         -778864.78
     Y    =       16546743.93  feet           Y    =         5035174.45  meter
     Z    =       14741936.26                 Z    =         4489749.07
     XDOT =     -19165.917456                 XDOT =       -5815.497071
     YDOT =     -12240.443423  feet/sec       YDOT =       -3796.067371  meter/sec
     ZDOT =      10725.610275                 ZDOT =        3240.852914
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11781684.12                 X    =         3591057.32
     Y    =      -11864594.05  feet           Y    =        -3616328.27  meter
     Z    =       14725064.44                 Z    =         4488199.64
     XDOT =       7301.465191                 XDOT =        2225.486590
     YDOT =      20430.534833  feet/sec       YDOT =        6227.227017  meter/sec
     ZDOT =      10595.068365                 ZDOT =        3229.376838
  
  
    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   20228.55422589  .00016717  00000-0  10270-3 0  9034
    2 25544  51.6405  54.6614 0001379  21.9435 338.1774 15.49147344  1212
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20228.55422589   =   yrday.fracday
    Element set:     903
    Inclination:       51.6405  deg
    RA of node:        54.6614  deg
    Eccentricity:     .0001379     
    Arg of perigee:    21.9435  deg
    Mean anomaly:     338.1774  deg
    Mean motion:   15.49147344  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             121
    Checksum:              300
 
 
    Coasting Arc #5 (Orbit 135)
    ---------------------------------------
 
    Vector Time (GMT): 2020/229/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 958140.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         335502.27                 A    =         6795139.97  meter
     Y    =       -5058253.91  meter          E    =           .0010799
     Z    =       -4535901.80                 I    =           51.92924
     XDOT =       6127.127438                 Wp   =           65.15529
     YDOT =       3276.716641  meter/sec      RA   =           49.29952  deg
     ZDOT =      -3202.431887                 TA   =          172.73248
                                              MA   =          172.71682
                                              Ha   =            229.125  n.mi
                                              Hp   =            222.212
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1100729.25                 X    =          414072.64
     Y    =      -16595321.21  feet           Y    =        -5054062.45  meter
     Z    =      -14881567.58                 Z    =        -4534081.62
     XDOT =      20102.124140                 XDOT =        6105.586114
     YDOT =      10750.382681  feet/sec       YDOT =        3345.114340  meter/sec
     ZDOT =     -10506.666295                 ZDOT =       -3172.721361
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10630255.01                 X    =        -3240101.73
     Y    =       12801273.06  feet           Y    =         3901828.03  meter
     Z    =      -14872875.69                 Z    =        -4533252.51
     XDOT =      -9225.120536                 XDOT =       -2811.816739
     YDOT =     -19702.360533  feet/sec       YDOT =       -6005.279490  meter/sec
     ZDOT =     -10369.650302                 ZDOT =       -3160.669412
  
  
    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   20229.52185183  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6400  49.8735 0001352  34.1830 325.9407 15.49170345  1363
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20229.52185183   =   yrday.fracday
    Element set:     904
    Inclination:       51.6400  deg
    RA of node:        49.8735  deg
    Eccentricity:     .0001352     
    Arg of perigee:    34.1830  deg
    Mean anomaly:     325.9407  deg
    Mean motion:   15.49170345  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             136
    Checksum:              286
 
 
    Coasting Arc #6 (Orbit 151)
    ---------------------------------------
 
    Vector Time (GMT): 2020/230/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 958140.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =          43907.60                 A    =         6795036.27  meter
     Y    =        5037200.10  meter          E    =           .0008949
     Z    =        4554107.17                 I    =           51.90629
     XDOT =      -6398.612420                 Wp   =          104.55421
     YDOT =      -2801.608401  meter/sec      RA   =           44.37022  deg
     ZDOT =       3153.124258                 TA   =          313.88969
                                              MA   =          313.96356
                                              Ha   =            229.106  n.mi
                                              Hp   =            222.243
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         144053.80                 X    =          -34543.88
     Y    =       16526247.06  feet           Y    =         5037252.22  meter
     Z    =       14941296.49                 Z    =         4554130.18
     XDOT =     -20992.822899                 XDOT =       -6382.124162
     YDOT =      -9191.628613  feet/sec       YDOT =       -2873.070232  meter/sec
     ZDOT =      10344.895858                 ZDOT =        3122.082915
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9344738.53                 X    =         2848276.30
     Y    =      -13631541.55  feet           Y    =        -4154893.86  meter
     Z    =       14941113.45                 Z    =         4554051.38
     XDOT =      11132.368963                 XDOT =        3393.146060
     YDOT =      18839.767272  feet/sec       YDOT =        5742.361064  meter/sec
     ZDOT =      10201.711447                 ZDOT =        3109.481649
  
  
    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   20230.55398432  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6404  44.7659 0001266  30.0257 330.0965 15.49167681  1521
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20230.55398432   =   yrday.fracday
    Element set:     905
    Inclination:       51.6404  deg
    RA of node:        44.7659  deg
    Eccentricity:     .0001266     
    Arg of perigee:    30.0257  deg
    Mean anomaly:     330.0965  deg
    Mean motion:   15.49167681  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             152
    Checksum:              293
 
 
    Coasting Arc #7 (Orbit 166)
    ---------------------------------------
 
    Vector Time (GMT): 2020/231/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 958140.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -399451.71                 A    =         6794855.07  meter
     Y    =       -4998589.66  meter          E    =           .0011414
     Z    =       -4596651.37                 I    =           51.88164
     XDOT =       6611.110065                 Wp   =           66.46294
     YDOT =       2305.583424  meter/sec      RA   =           39.43982  deg
     ZDOT =      -3083.333788                 TA   =          172.72983
                                              MA   =          172.71326
                                              Ha   =            229.206  n.mi
                                              Hp   =            222.066
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1310537.11                 X    =         -321198.95
     Y    =      -16399572.37  feet           Y    =        -5002618.95  meter
     Z    =      -15080877.21                 Z    =        -4598401.79
     XDOT =      21689.993651                 XDOT =        6599.813693
     YDOT =       7564.250079  feet/sec       YDOT =        2379.450507  meter/sec
     ZDOT =     -10115.924500                 ZDOT =       -3051.247772
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8067927.93                 X    =        -2459104.43
     Y    =       14329580.69  feet           Y    =         4367656.19  meter
     Z    =      -15088671.09                 Z    =        -4599026.95
     XDOT =     -12895.263527                 XDOT =       -3930.476323
     YDOT =     -17750.645690  feet/sec       YDOT =       -5410.396806  meter/sec
     ZDOT =      -9967.893072                 ZDOT =       -3038.213808
  
  
    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   20231.52160768  .00016717  00000-0  10270-3 0  9066
    2 25544  51.6412  39.9781 0001475  45.4072 314.7198 15.49181743  1677
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20231.52160768   =   yrday.fracday
    Element set:     906
    Inclination:       51.6412  deg
    RA of node:        39.9781  deg
    Eccentricity:     .0001475     
    Arg of perigee:    45.4072  deg
    Mean anomaly:     314.7198  deg
    Mean motion:   15.49181743  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             167
    Checksum:              307
 
 
    Coasting Arc #8 (Orbit 170)
    ---------------------------------------
 
    Vector Time (GMT): 2020/231/17:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3267133.25                 A    =         6791938.26  meter
     Y    =        2717303.64  meter          E    =           .0004342
     Z    =        5295610.23                 I    =           51.86955
     XDOT =      -5586.051496                 Wp   =           53.92148
     YDOT =      -5187.429519  meter/sec      RA   =           38.26485  deg
     ZDOT =       -781.589715                 TA   =           43.54571
                                              MA   =           43.51144
                                              Ha   =            229.154  n.mi
                                              Hp   =            222.167
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10718941.10                 X    =        -3322998.54
     Y    =        8915038.19  feet           Y    =         2680455.74  meter
     Z    =       17374049.30                 Z    =         5279604.54
     XDOT =     -18326.940604                 XDOT =       -5523.832520
     YDOT =     -17019.125718  feet/sec       YDOT =       -5249.548837  meter/sec
     ZDOT =      -2564.270719                 ZDOT =        -808.572887
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =          41184.13                 X    =           12552.92
     Y    =      -14033534.55  feet           Y    =        -4277421.33  meter
     Z    =       17299982.80                 Z    =         5273034.76
     XDOT =      23761.508952                 XDOT =        7242.507929
     YDOT =      -3256.563521  feet/sec       YDOT =        -992.600561  meter/sec
     ZDOT =      -2688.570210                 ZDOT =        -819.476200
  
  
    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   20231.77963806  .00016717  00000-0  10270-3 0  9078
    2 25544  51.6448  38.7024 0001156  36.0254 324.0974 15.49206016  1719
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20231.77963806   =   yrday.fracday
    Element set:     907
    Inclination:       51.6448  deg
    RA of node:        38.7024  deg
    Eccentricity:     .0001156     
    Arg of perigee:    36.0254  deg
    Mean anomaly:     324.0974  deg
    Mean motion:   15.49206016  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             171
    Checksum:              291
 
 
    Coasting Arc #9 (Orbit 185)
    ---------------------------------------
 
    Vector Time (GMT): 2020/232/17:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3085491.77                 A    =         6792112.41  meter
     Y    =       -2951017.51  meter          E    =           .0015150
     Z    =       -5295588.27                 I    =           51.84128
     XDOT =       5961.697552                 Wp   =           92.50841
     YDOT =       4717.080639  meter/sec      RA   =           33.33321  deg
     ZDOT =        846.411810                 TA   =          185.57312
                                              MA   =          185.59000
                                              Ha   =            229.145  n.mi
                                              Hp   =            222.285
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10123004.49                 X    =         3143983.95
     Y    =       -9681815.96  feet           Y    =        -2916186.31  meter
     Z    =      -17373977.25                 Z    =        -5280458.43
     XDOT =      19559.375171                 XDOT =        5904.395373
     YDOT =      15475.986348  feet/sec       YDOT =        4783.428214  meter/sec
     ZDOT =       2776.941634                 ZDOT =         875.231523
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1171241.58                 X    =          356994.43
     Y    =       14045267.25  feet           Y    =         4280997.46  meter
     Z    =      -17303945.41                 Z    =        -5274242.56
     XDOT =     -23263.893034                 XDOT =       -7090.834597
     YDOT =       5518.947745  feet/sec       YDOT =        1682.175273  meter/sec
     ZDOT =       2909.740268                 ZDOT =         886.888834
  
  
    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   20232.74726153  .00016717  00000-0  10270-3 0  9089
    2 25544  51.6437  33.9158 0001243  40.5850 319.5393 15.49163676  1865
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20232.74726153   =   yrday.fracday
    Element set:     908
    Inclination:       51.6437  deg
    RA of node:        33.9158  deg
    Eccentricity:     .0001243     
    Arg of perigee:    40.5850  deg
    Mean anomaly:     319.5393  deg
    Mean motion:   15.49163676  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             186
    Checksum:              308
 
 
    Coasting Arc #10 (Orbit 201)
    ---------------------------------------
 
    Vector Time (GMT): 2020/233/17:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2887336.44                 A    =         6792036.06  meter
     Y    =        3154531.52  meter          E    =           .0004637
     Z    =        5273863.38                 I    =           51.81327
     XDOT =      -6317.631131                 Wp   =           53.95520
     YDOT =      -4238.602431  meter/sec      RA   =           28.39876  deg
     ZDOT =       -920.256905                 TA   =           44.85176
                                              MA   =           44.81429
                                              Ha   =            229.169  n.mi
                                              Hp   =            222.147
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9472888.60                 X    =        -2948013.68
     Y    =       10349512.85  feet           Y    =         3121904.13  meter
     Z    =       17302701.38                 Z    =         5259690.65
     XDOT =     -20727.136257                 XDOT =       -6265.294277
     YDOT =     -13906.175956  feet/sec       YDOT =       -4308.958095  meter/sec
     ZDOT =      -3019.215568                 ZDOT =        -950.817650
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2338697.15                 X    =         -712834.89
     Y    =      -13915639.17  feet           Y    =        -4241486.82  meter
     Z    =       17237081.89                 Z    =         5253862.56
     XDOT =      22642.437343                 XDOT =        6901.414902
     YDOT =      -7732.831269  feet/sec       YDOT =       -2356.966971  meter/sec
     ZDOT =      -3160.068845                 ZDOT =        -963.188984
  
  
    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   20233.77939013  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6444  28.8091 0001136  41.8897 318.2340 15.49201700  2026
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20233.77939013   =   yrday.fracday
    Element set:     909
    Inclination:       51.6444  deg
    RA of node:        28.8091  deg
    Eccentricity:     .0001136     
    Arg of perigee:    41.8897  deg
    Mean anomaly:     318.2340  deg
    Mean motion:   15.49201700  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             202
    Checksum:              285
 
 
    Coasting Arc #11 (Orbit 211)
    ---------------------------------------
 
    Vector Time (GMT): 2020/234/09:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5177415.44                 A    =         6802284.42  meter
     Y    =       -4014824.39  meter          E    =           .0006956
     Z    =       -1823815.88                 I    =           51.82488
     XDOT =       4251.005408                 Wp   =          128.31405
     YDOT =      -2919.672810  meter/sec      RA   =           25.14951  deg
     ZDOT =      -5659.352038                 TA   =           71.63215
                                              MA   =           71.55652
                                              Ha   =            229.147  n.mi
                                              Hp   =            222.095
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16986271.12                 X    =        -5123276.76
     Y    =      -13171996.02  feet           Y    =        -4072419.31  meter
     Z    =       -5983647.92                 Z    =        -1848833.70
     XDOT =      13946.868138                 XDOT =        4310.827578
     YDOT =      -9578.979037  feet/sec       YDOT =       -2871.800749  meter/sec
     ZDOT =     -18567.427946                 ZDOT =       -5638.557248
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5950894.75                 X    =        -1813832.72
     Y    =       20621082.03  feet           Y    =         6285305.80  meter
     Z    =       -6098914.29                 Z    =        -1858949.08
     XDOT =     -12611.266712                 XDOT =       -3843.914094
     YDOT =      -9084.536308  feet/sec       YDOT =       -2768.966667  meter/sec
     ZDOT =     -18471.253068                 ZDOT =       -5630.037935
  
  
    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   20234.42447094  .00016717  00000-0  10270-3 0  9103
    2 25544  51.6418  25.6170 0001522  36.9132 323.2122 15.49182509  2126
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20234.42447094   =   yrday.fracday
    Element set:     910
    Inclination:       51.6418  deg
    RA of node:        25.6170  deg
    Eccentricity:     .0001522     
    Arg of perigee:    36.9132  deg
    Mean anomaly:     323.2122  deg
    Mean motion:   15.49182509  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             212
    Checksum:              263
 
 
    Coasting Arc #12 (Orbit 227)
    ---------------------------------------
 
    Vector Time (GMT): 2020/235/09:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5467594.20                 A    =         6802242.32  meter
     Y    =        3577191.07  meter          E    =           .0015282
     Z    =        1864917.92                 I    =           51.79325
     XDOT =      -4052.859399                 Wp   =           64.48838
     YDOT =       3238.720844  meter/sec      RA   =           20.21185  deg
     ZDOT =       5640.252146                 TA   =          315.95532
                                              MA   =          316.07696
                                              Ha   =            229.188  n.mi
                                              Hp   =            222.048
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17938301.17                 X    =         5418128.00
     Y    =       11736191.19  feet           Y    =         3638057.12  meter
     Z    =        6118497.11                 Z    =         1891356.78
     XDOT =     -13296.782805                 XDOT =       -4116.171364
     YDOT =      10625.724554  feet/sec       YDOT =        3193.045100  meter/sec
     ZDOT =      18504.764260                 ZDOT =        5620.411246
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3903423.42                 X    =         1189763.46
     Y    =      -21042298.75  feet           Y    =        -6413692.66  meter
     Z    =        6240335.59                 Z    =         1902054.29
     XDOT =      13455.974193                 XDOT =        4101.380934
     YDOT =       7984.981422  feet/sec       YDOT =        2433.822337  meter/sec
     ZDOT =      18412.981952                 ZDOT =        5612.276899
  
  
    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   20235.45659778  .00016717  00000-0  10270-3 0  9112
    2 25544  51.6415  20.5095 0001463  45.6958 314.4312 15.49176374  2283
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20235.45659778   =   yrday.fracday
    Element set:     911
    Inclination:       51.6415  deg
    RA of node:        20.5095  deg
    Eccentricity:     .0001463     
    Arg of perigee:    45.6958  deg
    Mean anomaly:     314.4312  deg
    Mean motion:   15.49176374  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             228
    Checksum:              309
 
 
    Coasting Arc #13 (Orbit 242)
    ---------------------------------------
 
    Vector Time (GMT): 2020/236/09:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5707077.73                 A    =         6802039.31  meter
     Y    =       -3146603.12  meter          E    =           .0006956
     Z    =       -1944173.73                 I    =           51.76040
     XDOT =       3846.664517                 Wp   =          125.77407
     YDOT =      -3526.312771  meter/sec      RA   =           15.27327  deg
     ZDOT =      -5602.573394                 TA   =           75.57008
                                              MA   =           75.49290
                                              Ha   =            229.230  n.mi
                                              Hp   =            221.942
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18724008.29                 X    =        -5662023.68
     Y    =      -10323501.04  feet           Y    =        -3210171.89  meter
     Z    =       -6378522.74                 Z    =        -1971786.79
     XDOT =      12620.290411                 XDOT =        3913.024852
     YDOT =     -11569.267621  feet/sec       YDOT =       -3482.925747  meter/sec
     ZDOT =     -18381.146306                 ZDOT =       -5583.726628
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1932174.50                 X    =         -588926.79
     Y    =       21255354.18  feet           Y    =         6478631.95  meter
     Z    =       -6505792.24                 Z    =        -1982965.48
     XDOT =     -14171.592028                 XDOT =       -4319.501250
     YDOT =      -6869.849770  feet/sec       YDOT =       -2093.930210  meter/sec
     ZDOT =     -18293.941862                 ZDOT =       -5575.993480
  
  
    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   20236.42421585  .00016717  00000-0  10270-3 0  9124
    2 25544  51.6412  15.7222 0001653  48.9219 311.2074 15.49197688  2433
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20236.42421585   =   yrday.fracday
    Element set:     912
    Inclination:       51.6412  deg
    RA of node:        15.7222  deg
    Eccentricity:     .0001653     
    Arg of perigee:    48.9219  deg
    Mean anomaly:     311.2074  deg
    Mean motion:   15.49197688  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             243
    Checksum:              291
 
 
    Coasting Arc #14 (Orbit 258)
    ---------------------------------------
 
    Vector Time (GMT): 2020/237/09:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5923414.22                 A    =         6802042.27  meter
     Y    =        2672038.98  meter          E    =           .0015336
     Z    =        1985257.13                 I    =           51.72668
     XDOT =      -3603.263464                 Wp   =           67.13232
     YDOT =       3819.561941  meter/sec      RA   =           10.33178  deg
     ZDOT =       5581.605467                 TA   =          314.71719
                                              MA   =          314.84196
                                              Ha   =            229.239  n.mi
                                              Hp   =            221.976
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19433773.70                 X    =         5883451.23
     Y    =        8766532.08  feet           Y    =         2738055.41  meter
     Z    =        6513310.79                 Z    =         2013933.56
     XDOT =     -11821.730525                 XDOT =       -3672.819308
     YDOT =      12531.371197  feet/sec       YDOT =        3778.878830  meter/sec
     ZDOT =      18312.353894                 ZDOT =        5563.933295
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -144437.26                 X    =          -44024.48
     Y    =      -21278235.03  feet           Y    =        -6485606.04  meter
     Z    =        6645503.32                 Z    =         2025549.41
     XDOT =      14828.005895                 XDOT =        4519.576197
     YDOT =       5621.689391  feet/sec       YDOT =        1713.490926  meter/sec
     ZDOT =      18230.557235                 ZDOT =        5556.673845
  
  
    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   20237.45634175  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6406  10.6151 0001462  58.3153 301.8139 15.49174851  2592
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20237.45634175   =   yrday.fracday
    Element set:     913
    Inclination:       51.6406  deg
    RA of node:        10.6151  deg
    Eccentricity:     .0001462     
    Arg of perigee:    58.3153  deg
    Mean anomaly:     301.8139  deg
    Mean motion:   15.49174851  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             259
    Checksum:              286
 
 
    Coasting Arc #15 (Orbit 273)
    ---------------------------------------
 
    Vector Time (GMT): 2020/238/09:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6089701.76                 A    =         6801793.78  meter
     Y    =       -2213473.13  meter          E    =           .0006839
     Z    =       -2065832.32                 I    =           51.69415
     XDOT =       3356.949598                 Wp   =          124.40992
     YDOT =      -4079.844051  meter/sec      RA   =            5.38830  deg
     ZDOT =      -5541.143118                 TA   =           78.36412
                                              MA   =           78.28736
                                              Ha   =            229.243  n.mi
                                              Hp   =            221.873
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19979336.50                 X    =        -6054462.85
     Y    =       -7262050.94  feet           Y    =        -2281375.48  meter
     Z    =       -6777665.08                 Z    =        -2095328.04
     XDOT =      11013.614168                 XDOT =        3429.237762
     YDOT =     -13385.315127  feet/sec       YDOT =       -4041.900002  meter/sec
     ZDOT =     -18179.603404                 ZDOT =       -5524.660884
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2101855.14                 X    =          640645.45
     Y    =       21109987.87  feet           Y    =         6434324.30  meter
     Z    =       -6913655.46                 Z    =        -2107282.18
     XDOT =     -15352.907774                 XDOT =       -4679.566289
     YDOT =      -4382.517370  feet/sec       YDOT =       -1335.791294  meter/sec
     ZDOT =     -18103.285211                 ZDOT =       -5517.881332
  
  
    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   20238.42395688  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6420   5.8274 0001634  56.8302 303.3005 15.49208435  2742
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20238.42395688   =   yrday.fracday
    Element set:     914
    Inclination:       51.6420  deg
    RA of node:         5.8274  deg
    Eccentricity:     .0001634     
    Arg of perigee:    56.8302  deg
    Mean anomaly:     303.3005  deg
    Mean motion:   15.49208435  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             274
    Checksum:              288
 
 
    Coasting Arc #16 (Orbit 280)
    ---------------------------------------
 
    Vector Time (GMT): 2020/238/20:27:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4105587.38                 A    =         6796466.75  meter
     Y    =       -3504278.12  meter          E    =           .0009425
     Z    =       -4139984.40                 I    =           51.66117
     XDOT =       6090.550816                 Wp   =           67.82110
     YDOT =      -2665.494761  meter/sec      RA   =            3.14012  deg
     ZDOT =      -3787.201236                 TA   =          163.06643
                                              MA   =          163.03495
                                              Ha   =            229.375  n.mi
                                              Hp   =            221.819
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13469774.88                 X    =        -4045986.76
     Y    =      -11496975.44  feet           Y    =        -3549856.41  meter
     Z    =      -13582625.99                 Z    =        -4159782.96
     XDOT =      19982.122100                 XDOT =        6138.300502
     YDOT =      -8745.061552  feet/sec       YDOT =       -2597.118812  meter/sec
     ZDOT =     -12425.200905                 ZDOT =       -3757.499912
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8859382.04                 X    =         2700339.65
     Y    =      -15252609.46  feet           Y    =        -4648995.36  meter
     Z    =      -13673780.13                 Z    =        -4167768.18
     XDOT =      11153.351529                 XDOT =        3399.541546
     YDOT =      17484.274118  feet/sec       YDOT =        5329.206751  meter/sec
     ZDOT =     -12287.964956                 ZDOT =       -3745.371718
  
  
    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   20238.87551000  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6424   3.5966 0001782  58.6086 301.5239 15.49172892  2816
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20238.87551000   =   yrday.fracday
    Element set:     915
    Inclination:       51.6424  deg
    RA of node:         3.5966  deg
    Eccentricity:     .0001782     
    Arg of perigee:    58.6086  deg
    Mean anomaly:     301.5239  deg
    Mean motion:   15.49172892  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             281
    Checksum:              304
 
 
    Coasting Arc #17 (Orbit 296)
    ---------------------------------------
 
    Vector Time (GMT): 2020/239/20:27:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928399.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4329105.01                 A    =         6796293.17  meter
     Y    =        3164539.04  meter          E    =           .0011389
     Z    =        4166753.32                 I    =           51.62599
     XDOT =      -5906.098667                 Wp   =           98.11148
     YDOT =       3146.369682  meter/sec      RA   =          358.19332  deg
     ZDOT =       3736.307430                 TA   =          313.39171
                                              MA   =          313.48649
                                              Ha   =            229.224  n.mi
                                              Hp   =            221.909
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14203100.41                 X    =         4273156.87
     Y    =       10382345.94  feet           Y    =         3212637.23  meter
     Z    =       13670450.53                 Z    =         4187646.49
     XDOT =     -19376.964131                 XDOT =       -5958.992083
     YDOT =      10322.735176  feet/sec       YDOT =        3080.027597  meter/sec
     ZDOT =      12258.226475                 ZDOT =        3707.489744
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7357244.38                 X    =        -2242488.09
     Y    =       15898179.09  feet           Y    =         4845764.99  meter
     Z    =       13766671.47                 Z    =         4196081.46
     XDOT =     -12841.198054                 XDOT =       -3913.997167
     YDOT =     -16471.107811  feet/sec       YDOT =       -5020.393661  meter/sec
     ZDOT =      12125.044822                 ZDOT =        3695.713662
  
  
    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   20239.90763003  .00016717  00000-0  10270-3 0  9168
    2 25544  51.6414 358.4903 0001692  56.4205 303.7107 15.49190309  2975
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20239.90763003   =   yrday.fracday
    Element set:     916
    Inclination:       51.6414  deg
    RA of node:       358.4903  deg
    Eccentricity:     .0001692     
    Arg of perigee:    56.4205  deg
    Mean anomaly:     303.7107  deg
    Mean motion:   15.49190309  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             297
    Checksum:              297
 
             

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