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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  16466.6302
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   69.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.708
   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 
   ------------------------------------------------------------------------
   023/14:19:41.994           1.2               1.8              1.8    
   N/A                       -0.9               0.0              229.5  
   000/00:09:23.988          -0.9              -0.0              221.9  
   
   023/17:25:20.976           0.6               0.9              0.9    
   N/A                       -0.5              -0.0              229.6  
   000/00:04:41.953          -0.4              -0.0              222.4  
   
   024/09:05:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.8  
   000/00:00:00.000           0.0               0.0              222.5  
   
   031/14:35:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.7  
   000/00:00:00.000           0.0               0.0              223.5  
   
   031/19:42:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.8  
   000/00:00:00.000           0.0               0.0              223.4  
   
   035/03:40:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.3  
   000/00:00:00.000           0.0               0.0              223.8  
   
   037/05:49:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.8  
   000/00:00:00.000           0.0               0.0              224.2  
   
 
 
    Coasting Arc #1 (Orbit 926)
    ---------------------------------------
 
    Vector Time (GMT): 2020/022/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936369.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4703983.85                 A    =         6795473.57  meter
     Y    =       -2732871.00  meter          E    =           .0008954
     Z    =       -4078549.10                 I    =           51.59691
     XDOT =       5483.868307                 Wp   =          100.82609
     YDOT =      -3686.897726  meter/sec      RA   =          353.69449  deg
     ZDOT =      -3863.233649                 TA   =          129.12039
                                              MA   =          129.04075
                                              Ha   =            229.208  n.mi
                                              Hp   =            220.931
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15433017.89                 X    =        -4653263.63
     Y    =       -8966112.20  feet           Y    =        -2785190.27  meter
     Z    =      -13381066.59                 Z    =        -4101275.84
     XDOT =      17991.693921                 XDOT =        5543.453707
     YDOT =     -12096.121149  feet/sec       YDOT =       -3625.239681  meter/sec
     ZDOT =     -12674.651080                 ZDOT =       -3836.451347
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         -34301.97                 X    =          -10455.24
     Y    =      -17770238.59  feet           Y    =        -5416368.72  meter
     Z    =      -13484791.29                 Z    =        -4110164.39
     XDOT =      18288.106346                 XDOT =        5574.214814
     YDOT =       9467.563818  feet/sec       YDOT =        2885.713452  meter/sec
     ZDOT =     -12551.739042                 ZDOT =       -3825.770060
  
  
    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   20022.52325217  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6411 354.1460 0004516 156.9070 203.2284 15.49577808  9270
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20022.52325217   =   yrday.fracday
    Element set:     900
    Inclination:       51.6411  deg
    RA of node:       354.1460  deg
    Eccentricity:     .0004516     
    Arg of perigee:   156.9070  deg
    Mean anomaly:     203.2284  deg
    Mean motion:   15.49577808  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             927
    Checksum:              284
 
 
    Coasting Arc #2 (Orbit 942)
    ---------------------------------------
 
    Vector Time (GMT): 2020/023/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936369.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4757795.86                 A    =         6794961.09  meter
     Y    =        2441193.88  meter          E    =           .0013123
     Z    =        4187324.95                 I    =           51.56336
     XDOT =      -5347.844040                 Wp   =          121.82260
     YDOT =       4055.939436  meter/sec      RA   =          348.74031  deg
     ZDOT =       3696.514312                 TA   =          290.09109
                                              MA   =          290.23227
                                              Ha   =            228.999  n.mi
                                              Hp   =            221.089
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15609566.47                 X    =         4709804.98
     Y    =        8009166.27  feet           Y    =         2494130.20  meter
     Z    =       13737942.75                 Z    =         4210319.57
     XDOT =     -17545.420080                 XDOT =       -5410.756397
     YDOT =      13306.887913  feet/sec       YDOT =        3995.783948  meter/sec
     ZDOT =      12127.671627                 ZDOT =        3670.384789
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1247465.39                 X    =          380227.45
     Y    =       17417053.49  feet           Y    =         5308717.90  meter
     Z    =       13842920.88                 Z    =         4219322.28
     XDOT =     -19272.741108                 XDOT =       -5874.331490
     YDOT =      -8202.872560  feet/sec       YDOT =       -2500.235556  meter/sec
     ZDOT =      12007.717474                 ZDOT =        3659.952286
  
  
    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   20023.55510441  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6420 349.0382 0004510 162.9638 197.1665 15.49618959  9432
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20023.55510441   =   yrday.fracday
    Element set:     901
    Inclination:       51.6420  deg
    RA of node:       349.0382  deg
    Eccentricity:     .0004510     
    Arg of perigee:   162.9638  deg
    Mean anomaly:     197.1665  deg
    Mean motion:   15.49618959  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             943
    Checksum:              306
 
 
    Coasting Arc #3 (Orbit 943)
    ---------------------------------------
 
    Vector Time (GMT): 2020/023/14:24:23.988
    Vector Time (MET): N/A
    Weight (LBS)     : 936187.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2890793.86                 A    =         6792675.05  meter
     Y    =       -3503158.75  meter          E    =           .0013180
     Z    =       -5061744.86                 I    =           51.55019
     XDOT =       6815.099155                 Wp   =           97.56650
     YDOT =      -2934.143108  meter/sec      RA   =          348.23319  deg
     ZDOT =      -1867.349090                 TA   =          154.30850
                                              MA   =          154.24296
                                              Ha   =            229.479  n.mi
                                              Hp   =            221.907
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9484231.83                 X    =        -2826819.22
     Y    =      -11493302.99  feet           Y    =        -3535127.49  meter
     Z    =      -16606774.46                 Z    =        -5075631.80
     XDOT =      22359.249196                 XDOT =        6856.473384
     YDOT =      -9626.453765  feet/sec       YDOT =       -2857.700334  meter/sec
     ZDOT =      -6126.473393                 ZDOT =       -1834.144604
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4284220.24                 X    =        -1305830.33
     Y    =      -14198203.54  feet           Y    =        -4327612.44  meter
     Z    =      -16669975.96                 Z    =        -5081008.67
     XDOT =      23343.203462                 XDOT =        7115.008415
     YDOT =        -51.916417  feet/sec       YDOT =         -15.824124  meter/sec
     ZDOT =      -5974.256585                 ZDOT =       -1820.953407
  
  
    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   20023.61959959  .00016717  00000-0  10270-3 0  9029
    2 25544  51.6434 348.7186 0004945 176.5909 183.5275 15.49255423  9449
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20023.61959959   =   yrday.fracday
    Element set:     902
    Inclination:       51.6434  deg
    RA of node:       348.7186  deg
    Eccentricity:     .0004945     
    Arg of perigee:   176.5909  deg
    Mean anomaly:     183.5275  deg
    Mean motion:   15.49255423  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             944
    Checksum:              342
 
 
    Coasting Arc #4 (Orbit 945)
    ---------------------------------------
 
    Vector Time (GMT): 2020/023/17:27:41.953
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3890844.39                 A    =         6794556.59  meter
     Y    =       -2978034.12  meter          E    =           .0009974
     Z    =       -4715057.43                 I    =           51.55218
     XDOT =       6140.752164                 Wp   =           99.73074
     YDOT =      -3616.717484  meter/sec      RA   =          347.60988  deg
     ZDOT =      -2789.696791                 TA   =          142.56602
                                              MA   =          142.49650
                                              Ha   =            229.607  n.mi
                                              Hp   =            222.415
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12765237.49                 X    =        -3834351.49
     Y    =       -9770453.16  feet           Y    =        -3021228.00  meter
     Z    =      -15469348.52                 Z    =        -4733820.22
     XDOT =      20146.824686                 XDOT =        6194.289378
     YDOT =     -11865.871012  feet/sec       YDOT =       -3547.747648  meter/sec
     ZDOT =      -9152.548526                 ZDOT =       -2759.738469
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15509846.52                 X    =        -4727401.22
     Y    =       -3899126.12  feet           Y    =        -1188453.64  meter
     Z    =      -15554911.23                 Z    =        -4741136.94
     XDOT =      13499.636674                 XDOT =        4114.689258
     YDOT =     -17821.378550  feet/sec       YDOT =       -5431.956182  meter/sec
     ZDOT =      -9015.119802                 ZDOT =       -2747.808516
  
  
    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   20023.74860950  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6449 348.0816 0005356 185.6375 174.4715 15.49089858  9460
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20023.74860950   =   yrday.fracday
    Element set:     903
    Inclination:       51.6449  deg
    RA of node:       348.0816  deg
    Eccentricity:     .0005356     
    Arg of perigee:   185.6375  deg
    Mean anomaly:     174.4715  deg
    Mean motion:   15.49089858  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             946
    Checksum:              340
 
 
    Coasting Arc #5 (Orbit 955)
    ---------------------------------------
 
    Vector Time (GMT): 2020/024/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -617868.42                 A    =         6792258.06  meter
     Y    =       -4208551.60  meter          E    =           .0015614
     Z    =       -5308173.62                 I    =           51.51992
     XDOT =       7444.327363                 Wp   =          114.37769
     YDOT =      -1694.631494  meter/sec      RA   =          344.35982  deg
     ZDOT =        471.863014                 TA   =          160.17231
                                              MA   =          160.11155
                                              Ha   =            229.772  n.mi
                                              Hp   =            222.495
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2027127.38                 X    =         -544977.88
     Y    =      -13807583.98  feet           Y    =        -4215053.05  meter
     Z    =      -17415267.79                 Z    =        -5310998.21
     XDOT =      24423.646203                 XDOT =        7460.431979
     YDOT =      -5559.814613  feet/sec       YDOT =       -1611.293745  meter/sec
     ZDOT =       1548.107002                 ZDOT =         508.062632
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13912271.07                 X    =         4240460.22
     Y    =         878127.46  feet           Y    =          267653.25  meter
     Z    =      -17427787.55                 Z    =        -5311989.64
     XDOT =        652.463245                 XDOT =         198.870797
     YDOT =      24016.261436  feet/sec       YDOT =        7320.156486  meter/sec
     ZDOT =       1713.901822                 ZDOT =         522.397275
  
  
    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   20024.39372918  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6420 344.8891 0005543 185.0551 175.0544 15.49056594  9563
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20024.39372918   =   yrday.fracday
    Element set:     904
    Inclination:       51.6420  deg
    RA of node:       344.8891  deg
    Eccentricity:     .0005543     
    Arg of perigee:   185.0551  deg
    Mean anomaly:     175.0544  deg
    Mean motion:   15.49056594  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             956
    Checksum:              318
 
 
    Coasting Arc #6 (Orbit 971)
    ---------------------------------------
 
    Vector Time (GMT): 2020/025/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         948843.55                 A    =         6792200.04  meter
     Y    =        4144823.74  meter          E    =           .0004654
     Z    =        5294813.62                 I    =           51.48670
     XDOT =      -7288.476504                 Wp   =          158.48324
     YDOT =       2309.077790  meter/sec      RA   =          339.40473  deg
     ZDOT =       -505.550876                 TA   =          296.32998
                                              MA   =          296.37777
                                              Ha   =            229.551  n.mi
                                              Hp   =            222.693
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3113003.76                 X    =          876705.98
     Y    =       13598503.09  feet           Y    =         4155030.72  meter
     Z    =       17371435.77                 Z    =         5299247.65
     XDOT =     -23912.324487                 XDOT =       -7311.299996
     YDOT =       7575.714534  feet/sec       YDOT =        2227.445299  meter/sec
     ZDOT =      -1658.631483                 ZDOT =        -541.009685
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13917614.72                 X    =        -4242088.97
     Y    =         467369.32  feet           Y    =          142454.17  meter
     Z    =       17391331.92                 Z    =         5300877.97
     XDOT =      -3060.270447                 XDOT =        -932.770432
     YDOT =     -23865.835154  feet/sec       YDOT =       -7274.306555  meter/sec
     ZDOT =      -1821.085059                 ZDOT =        -555.066726
  
  
    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   20025.42591973  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6407 339.7829 0005520 189.9921 170.1120 15.49075404  9726
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20025.42591973   =   yrday.fracday
    Element set:     905
    Inclination:       51.6407  deg
    RA of node:       339.7829  deg
    Eccentricity:     .0005520     
    Arg of perigee:   189.9921  deg
    Mean anomaly:     170.1120  deg
    Mean motion:   15.49075404  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             972
    Checksum:              311
 
 
    Coasting Arc #7 (Orbit 986)
    ---------------------------------------
 
    Vector Time (GMT): 2020/026/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1252718.08                 A    =         6792274.35  meter
     Y    =       -4078667.34  meter          E    =           .0014875
     Z    =       -5297073.24                 I    =           51.45633
     XDOT =       7061.513082                 Wp   =          115.56527
     YDOT =      -2890.167181  meter/sec      RA   =          334.44738  deg
     ZDOT =        550.324465                 TA   =          159.74167
                                              MA   =          159.68259
                                              Ha   =            229.527  n.mi
                                              Hp   =            222.757
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4109967.44                 X    =        -1181286.75
     Y    =      -13381454.53  feet           Y    =        -4092276.52  meter
     Z    =      -17378849.22                 Z    =        -5302984.94
     XDOT =      23167.693837                 XDOT =        7090.633878
     YDOT =      -9482.175790  feet/sec       YDOT =       -2811.037535  meter/sec
     ZDOT =       1805.526459                 ZDOT =         584.696105
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13858183.39                 X    =         4223974.30
     Y    =       -1725749.55  feet           Y    =         -526008.46  meter
     Z    =      -17405519.22                 Z    =        -5305202.26
     XDOT =       5399.486940                 XDOT =        1645.763619
     YDOT =      23392.944850  feet/sec       YDOT =        7130.169590  meter/sec
     ZDOT =       1963.046954                 ZDOT =         598.336712
  
  
    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   20026.39359684  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6412 334.9961 0005477 193.0075 167.0935 15.49060609  9879
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20026.39359684   =   yrday.fracday
    Element set:     906
    Inclination:       51.6412  deg
    RA of node:       334.9961  deg
    Eccentricity:     .0005477     
    Arg of perigee:   193.0075  deg
    Mean anomaly:     167.0935  deg
    Mean motion:   15.49060609  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             987
    Checksum:              333
 
 
    Coasting Arc #8 (Orbit 1002)
    ---------------------------------------
 
    Vector Time (GMT): 2020/027/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1567283.75                 A    =         6792210.61  meter
     Y    =        3967839.50  meter          E    =           .0004053
     Z    =        5283990.59                 I    =           51.42671
     XDOT =      -6807.016421                 Wp   =          164.57242
     YDOT =       3467.078072  meter/sec      RA   =          329.48793  deg
     ZDOT =       -588.185030                 TA   =          291.04110
                                              MA   =          291.08444
                                              Ha   =            229.276  n.mi
                                              Hp   =            222.964
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5142007.06                 X    =         1497131.88
     Y    =       13017846.11  feet           Y    =         3984973.63  meter
     Z    =       17335927.14                 Z    =         5291433.31
     XDOT =     -22332.731041                 XDOT =       -6842.423417
     YDOT =      11374.928058  feet/sec       YDOT =        3390.759228  meter/sec
     ZDOT =      -1929.740912                 ZDOT =        -621.335807
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13619901.52                 X    =        -4151345.98
     Y    =        3038677.64  feet           Y    =          926188.94  meter
     Z    =       17369618.44                 Z    =         5294259.70
     XDOT =      -7718.444360                 XDOT =       -2352.581841
     YDOT =     -22765.739173  feet/sec       YDOT =       -6938.997300  meter/sec
     ZDOT =      -2081.712682                 ZDOT =        -634.506025
  
  
    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   20027.42578189  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6413 329.8898 0005412 197.6504 162.4458 15.49082565 10032
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20027.42578189   =   yrday.fracday
    Element set:     907
    Inclination:       51.6413  deg
    RA of node:       329.8898  deg
    Eccentricity:     .0005412     
    Arg of perigee:   197.6504  deg
    Mean anomaly:     162.4458  deg
    Mean motion:   15.49082565  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1003
    Checksum:              325
 
 
    Coasting Arc #9 (Orbit 1017)
    ---------------------------------------
 
    Vector Time (GMT): 2020/028/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1856244.79                 A    =         6792280.94  meter
     Y    =       -3857890.37  meter          E    =           .0014110
     Z    =       -5284745.17                 I    =           51.39818
     XDOT =       6489.802470                 Wp   =          116.12055
     YDOT =      -4000.810845  meter/sec      RA   =          324.52642  deg
     ZDOT =        636.341793                 TA   =          160.01684
                                              MA   =          159.96153
                                              Ha   =            229.237  n.mi
                                              Hp   =            223.012
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6090041.95                 X    =        -1787297.20
     Y    =      -12657120.64  feet           Y    =        -3878262.69  meter
     Z    =      -17338402.77                 Z    =        -5293594.38
     XDOT =      21292.002854                 XDOT =        6530.967480
     YDOT =     -13126.019833  feet/sec       YDOT =       -3928.007107  meter/sec
     ZDOT =       2087.735540                 ZDOT =         667.965824
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13332410.69                 X    =         4063718.78
     Y    =       -4259641.78  feet           Y    =        -1298338.81  meter
     Z    =      -17378544.29                 Z    =        -5296980.30
     XDOT =       9909.571342                 XDOT =        3020.437345
     YDOT =      21843.634303  feet/sec       YDOT =        6657.939736  meter/sec
     ZDOT =       2232.752675                 ZDOT =         680.543015
  
  
    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   20028.39345345  .00016717  00000-0  10270-3 0  9083
    2 25544  51.6409 325.1030 0005312 201.0402 159.0530 15.49070131 10185
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20028.39345345   =   yrday.fracday
    Element set:     908
    Inclination:       51.6409  deg
    RA of node:       325.1030  deg
    Eccentricity:     .0005312     
    Arg of perigee:   201.0402  deg
    Mean anomaly:     159.0530  deg
    Mean motion:   15.49070131  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1018
    Checksum:              252
 
 
    Coasting Arc #10 (Orbit 1033)
    ---------------------------------------
 
    Vector Time (GMT): 2020/029/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2149267.12                 A    =         6792252.98  meter
     Y    =        3703434.72  meter          E    =           .0003437
     Z    =        5271811.81                 I    =           51.37102
     XDOT =      -6144.698694                 Wp   =          172.02931
     YDOT =       4525.346720  meter/sec      RA   =          319.56325  deg
     ZDOT =       -677.194978                 TA   =          284.44847
                                              MA   =          284.48661
                                              Ha   =            229.002  n.mi
                                              Hp   =            223.256
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7051401.32                 X    =         2082087.67
     Y    =       12150376.39  feet           Y    =         3727093.78  meter
     Z    =       17295970.52                 Z    =         5282088.67
     XDOT =     -20159.772619                 XDOT =       -6191.556420
     YDOT =      14846.938058  feet/sec       YDOT =        4456.370339  meter/sec
     ZDOT =      -2221.768302                 ZDOT =        -707.156644
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12863504.70                 X    =        -3920796.23
     Y    =        5501531.86  feet           Y    =         1676866.91  meter
     Z    =       17342661.19                 Z    =         5286043.13
     XDOT =     -12048.975483                 XDOT =       -3672.527727
     YDOT =     -20769.398130  feet/sec       YDOT =       -6330.512550  meter/sec
     ZDOT =      -2359.208166                 ZDOT =        -719.086649
  
  
    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   20029.42563530  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6403 319.9970 0005333 205.6654 154.4232 15.49081311 10343
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20029.42563530   =   yrday.fracday
    Element set:     909
    Inclination:       51.6403  deg
    RA of node:       319.9970  deg
    Eccentricity:     .0005333     
    Arg of perigee:   205.6654  deg
    Mean anomaly:     154.4232  deg
    Mean motion:   15.49081311  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1034
    Checksum:              284
 
 
    Coasting Arc #11 (Orbit 1048)
    ---------------------------------------
 
    Vector Time (GMT): 2020/030/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2418448.41                 A    =         6792284.71  meter
     Y    =       -3551929.81  meter          E    =           .0013317
     Z    =       -5271197.16                 I    =           51.34680
     XDOT =       5746.280800                 Wp   =          117.06765
     YDOT =      -4998.870699  meter/sec      RA   =          314.59752  deg
     ZDOT =        727.495122                 TA   =          159.95206
                                              MA   =          159.89970
                                              Ha   =            228.950  n.mi
                                              Hp   =            223.278
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7934542.02                 X    =        -2352946.01
     Y    =      -11653313.01  feet           Y    =        -3578608.44  meter
     Z    =      -17293953.93                 Z    =        -5282785.65
     XDOT =      18852.627296                 XDOT =        5798.218884
     YDOT =     -16400.494420  feet/sec       YDOT =       -4934.321299  meter/sec
     ZDOT =       2386.795021                 ZDOT =         755.533943
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12357957.12                 X    =         3766705.33
     Y    =       -6649191.15  feet           Y    =        -2026673.46  meter
     Z    =      -17346661.26                 Z    =        -5287262.35
     XDOT =      14010.020111                 XDOT =        4270.254130
     YDOT =      19437.606380  feet/sec       YDOT =        5924.582425  meter/sec
     ZDOT =       2515.461535                 ZDOT =         766.712676
  
  
    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   20030.39330295  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6408 315.2097 0005323 209.6041 150.4808 15.49082812 10498
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20030.39330295   =   yrday.fracday
    Element set:     910
    Inclination:       51.6408  deg
    RA of node:       315.2097  deg
    Eccentricity:     .0005323     
    Arg of perigee:   209.6041  deg
    Mean anomaly:     150.4808  deg
    Mean motion:   15.49082812  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1049
    Checksum:              279
 
 
    Coasting Arc #12 (Orbit 1064)
    ---------------------------------------
 
    Vector Time (GMT): 2020/031/09:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 936097.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2683120.50                 A    =         6792267.85  meter
     Y    =        3359031.86  meter          E    =           .0002777
     Z    =        5258326.53                 I    =           51.32482
     XDOT =      -5321.721985                 Wp   =          181.43260
     YDOT =       5456.197159  meter/sec      RA   =          309.63054  deg
     ZDOT =       -772.696240                 TA   =          275.97473
                                              MA   =          276.00638
                                              Ha   =            228.685  n.mi
                                              Hp   =            223.528
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8802888.77                 X    =         2619817.90
     Y    =       11020445.73  feet           Y    =         3388682.53  meter
     Z    =       17251727.45                 Z    =         5271206.06
     XDOT =     -17459.717798                 XDOT =       -5378.586012
     YDOT =      17900.909313  feet/sec       YDOT =        5396.367934  meter/sec
     ZDOT =      -2535.092652                 ZDOT =        -798.684815
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11680323.28                 X    =        -3560162.54
     Y    =        7777190.04  feet           Y    =         2370487.52  meter
     Z    =       17310359.26                 Z    =         5276197.50
     XDOT =     -15882.476013                 XDOT =       -4840.978689
     YDOT =     -17965.161437  feet/sec       YDOT =       -5475.781206  meter/sec
     ZDOT =      -2654.402526                 ZDOT =        -809.061890
  
  
    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   20031.42547902  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6414 310.1034 0005240 214.0776 146.0039 15.49091845 10654
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20031.42547902   =   yrday.fracday
    Element set:     911
    Inclination:       51.6414  deg
    RA of node:       310.1034  deg
    Eccentricity:     .0005240     
    Arg of perigee:   214.0776  deg
    Mean anomaly:     146.0039  deg
    Mean motion:   15.49091845  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1065
    Checksum:              266
 
 
    Coasting Arc #13 (Orbit 1067)
    ---------------------------------------
 
    Vector Time (GMT): 2020/031/14:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920821.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1104300.53                 A    =         6794391.10  meter
     Y    =       -4731634.24  meter          E    =           .0010709
     Z    =       -4759078.36                 I    =           51.32989
     XDOT =       5926.859939                 Wp   =          136.38143
     YDOT =      -4050.716795  meter/sec      RA   =          308.47949  deg
     ZDOT =       2648.065403                 TA   =          159.95154
                                              MA   =          159.90944
                                              Ha   =            228.675  n.mi
                                              Hp   =            223.522
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3623033.24                 X    =        -1028191.43
     Y    =      -15523734.39  feet           Y    =        -4743557.81  meter
     Z    =      -15613774.14                 Z    =        -4764257.63
     XDOT =      19445.078540                 XDOT =        5958.853173
     YDOT =     -13289.753263  feet/sec       YDOT =       -3984.259530  meter/sec
     ZDOT =       8687.878620                 ZDOT =        2676.933044
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -251997.37                 X    =          -76808.80
     Y    =      -15916060.05  feet           Y    =        -4851215.10  meter
     Z    =      -15637076.84                 Z    =        -4766181.02
     XDOT =      20542.180187                 XDOT =        6261.256521
     YDOT =      -9003.809639  feet/sec       YDOT =       -2744.361178  meter/sec
     ZDOT =       8820.238053                 ZDOT =        2688.408559
  
  
    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   20031.61901044  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6441 309.1472 0005272 216.6802 143.3988 15.49114788 10689
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20031.61901044   =   yrday.fracday
    Element set:     912
    Inclination:       51.6441  deg
    RA of node:       309.1472  deg
    Eccentricity:     .0005272     
    Arg of perigee:   216.6802  deg
    Mean anomaly:     143.3988  deg
    Mean motion:   15.49114788  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1068
    Checksum:              294
 
 
    Coasting Arc #14 (Orbit 1071)
    ---------------------------------------
 
    Vector Time (GMT): 2020/031/19:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920821.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5296967.66                 A    =         6797684.32  meter
     Y    =       -1895718.87  meter          E    =           .0010300
     Z    =        3813433.29                 I    =           51.33279
     XDOT =       -712.074435                 Wp   =          127.16120
     YDOT =       6394.725464  meter/sec      RA   =          307.46088  deg
     ZDOT =       4154.119124                 TA   =          278.77829
                                              MA   =          278.89493
                                              Ha   =            228.794  n.mi
                                              Hp   =            223.436
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17378502.82                 X    =         5299249.28
     Y    =       -6219550.10  feet           Y    =        -1836471.63  meter
     Z    =       12511264.07                 Z    =         3839169.04
     XDOT =      -2336.202214                 XDOT =        -803.707225
     YDOT =      20980.070420  feet/sec       YDOT =        6386.250230  meter/sec
     ZDOT =      13628.999751                 ZDOT =        4150.437586
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1639632.89                 X    =          499760.11
     Y    =      -18304200.92  feet           Y    =        -5579120.44  meter
     Z    =       12629122.09                 Z    =         3849356.41
     XDOT =      16673.735958                 XDOT =        5082.154720
     YDOT =      10916.193335  feet/sec       YDOT =        3327.255728  meter/sec
     ZDOT =      13611.643628                 ZDOT =        4148.828978
  
  
    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   20031.87705412  .00016717  00000-0  10270-3 0  9131
    2 25544  51.6403 307.8651 0005603 213.1744 146.9055 15.49121225 10729
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20031.87705412   =   yrday.fracday
    Element set:     913
    Inclination:       51.6403  deg
    RA of node:       307.8651  deg
    Eccentricity:     .0005603     
    Arg of perigee:   213.1744  deg
    Mean anomaly:     146.9055  deg
    Mean motion:   15.49121225  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1072
    Checksum:              274
 
 
    Coasting Arc #15 (Orbit 1086)
    ---------------------------------------
 
    Vector Time (GMT): 2020/032/19:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920821.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5113034.46                 A    =         6797576.89  meter
     Y    =        2281838.60  meter          E    =           .0004002
     Z    =       -3854838.31                 I    =           51.31305
     XDOT =        211.837156                 Wp   =          132.48314
     YDOT =      -6457.984394  meter/sec      RA   =          302.49255  deg
     ZDOT =      -4109.118461                 TA   =           94.10933
                                              MA   =           94.06358
                                              Ha   =            228.618  n.mi
                                              Hp   =            223.494
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16775047.45                 X    =        -5119446.29
     Y    =        7486347.11  feet           Y    =         2224625.18  meter
     Z    =      -12647107.31                 Z    =        -3879690.66
     XDOT =        695.003793                 XDOT =         303.995968
     YDOT =     -21187.612840  feet/sec       YDOT =       -6455.100181  meter/sec
     ZDOT =     -13481.359780                 ZDOT =       -4107.865631
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =          78494.84                 X    =           23925.23
     Y    =       18290680.07  feet           Y    =         5574999.28  meter
     Z    =      -12760948.02                 Z    =        -3889536.96
     XDOT =     -17717.233537                 XDOT =       -5400.212782
     YDOT =      -9312.989701  feet/sec       YDOT =       -2838.599261  meter/sec
     ZDOT =     -13475.118326                 ZDOT =       -4107.216066
  
  
    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   20032.84471721  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6404 303.0786 0005468 216.2211 143.8569 15.49111671 10875
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20032.84471721   =   yrday.fracday
    Element set:     914
    Inclination:       51.6404  deg
    RA of node:       303.0786  deg
    Eccentricity:     .0005468     
    Arg of perigee:   216.2211  deg
    Mean anomaly:     143.8569  deg
    Mean motion:   15.49111671  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1087
    Checksum:              292
 
 
    Coasting Arc #16 (Orbit 1102)
    ---------------------------------------
 
    Vector Time (GMT): 2020/033/19:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920821.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4898018.86                 A    =         6797472.55  meter
     Y    =       -2680927.16  meter          E    =           .0009544
     Z    =        3875046.40                 I    =           51.29615
     XDOT =        309.173844                 Wp   =          129.37356
     YDOT =       6475.959649  meter/sec      RA   =          297.52168  deg
     ZDOT =       4076.853242                 TA   =          277.56231
                                              MA   =          277.67071
                                              Ha   =            228.545  n.mi
                                              Hp   =            223.711
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16069615.68                 X    =         4908811.22
     Y    =       -8795692.80  feet           Y    =        -2626093.77  meter
     Z    =       12713406.82                 Z    =         3898864.92
     XDOT =       1014.349882                 XDOT =         216.932012
     YDOT =      21246.586775  feet/sec       YDOT =        6478.901221  meter/sec
     ZDOT =      13375.502762                 ZDOT =        4078.131148
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1873988.69                 X    =         -571191.75
     Y    =      -18146569.94  feet           Y    =        -5531074.52  meter
     Z    =       12822544.15                 Z    =         3908311.46
     XDOT =      18605.473800                 XDOT =        5670.948414
     YDOT =       7562.865292  feet/sec       YDOT =        2305.161341  meter/sec
     ZDOT =      13380.845486                 ZDOT =        4078.481704
  
  
    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   20033.87688844  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6407 297.9716 0005669 220.5350 139.5378 15.49127696 11030
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20033.87688844   =   yrday.fracday
    Element set:     915
    Inclination:       51.6407  deg
    RA of node:       297.9716  deg
    Eccentricity:     .0005669     
    Arg of perigee:   220.5350  deg
    Mean anomaly:     139.5378  deg
    Mean motion:   15.49127696  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1103
    Checksum:              338
 
 
    Coasting Arc #17 (Orbit 1117)
    ---------------------------------------
 
    Vector Time (GMT): 2020/034/19:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920821.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4657520.64                 A    =         6797383.64  meter
     Y    =        3029520.64  meter          E    =           .0003247
     Z    =       -3916407.36                 I    =           51.28223
     XDOT =       -816.198911                 Wp   =          129.30751
     YDOT =      -6459.493248  meter/sec      RA   =          292.55015  deg
     ZDOT =      -4030.334043                 TA   =           98.28893
                                              MA   =           98.25211
                                              Ha   =            228.339  n.mi
                                              Hp   =            223.793
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15280579.52                 X    =        -4672028.06
     Y    =        9939372.18  feet           Y    =         2977355.96  meter
     Z    =      -12849105.51                 Z    =        -3939066.60
     XDOT =      -2677.817949                 XDOT =        -724.329505
     YDOT =     -21192.563149  feet/sec       YDOT =       -6468.106746  meter/sec
     ZDOT =     -13222.880719                 ZDOT =       -4034.075863
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3541853.22                 X    =         1079556.86
     Y    =       17806256.75  feet           Y    =         5427347.06  meter
     Z    =      -12952962.54                 Z    =        -3948062.98
     XDOT =     -19326.890033                 XDOT =       -5890.836082
     YDOT =      -5776.496440  feet/sec       YDOT =       -1760.676115  meter/sec
     ZDOT =     -13239.505086                 ZDOT =       -4035.401150
  
  
    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   20034.84454796  .00016717  00000-0  10270-3 0  9160
    2 25544  51.6417 293.1843 0005533 224.4137 135.6570 15.49111817 11181
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20034.84454796   =   yrday.fracday
    Element set:     916
    Inclination:       51.6417  deg
    RA of node:       293.1843  deg
    Eccentricity:     .0005533     
    Arg of perigee:   224.4137  deg
    Mean anomaly:     135.6570  deg
    Mean motion:   15.49111817  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1118
    Checksum:              305
 
 
    Coasting Arc #18 (Orbit 1122)
    ---------------------------------------
 
    Vector Time (GMT): 2020/035/03:40:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920821.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3494610.20                 A    =         6792418.95  meter
     Y    =       -2596504.49  meter          E    =           .0011620
     Z    =       -5223466.49                 I    =           51.26303
     XDOT =       3460.292154                 Wp   =          118.40887
     YDOT =      -6746.085994  meter/sec      RA   =          290.86945  deg
     ZDOT =       1034.707305                 TA   =          161.59497
                                              MA   =          161.55289
                                              Ha   =            228.293  n.mi
                                              Hp   =            223.820
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11465256.57                 X    =        -3439943.35
     Y    =       -8518715.53  feet           Y    =        -2635277.83  meter
     Z    =      -17137357.24                 Z    =        -5240309.03
     XDOT =      11352.664546                 XDOT =        3530.445747
     YDOT =     -22132.828064  feet/sec       YDOT =       -6706.998343  meter/sec
     ZDOT =       3394.709007                 ZDOT =        1051.685927
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12410458.49                 X    =         3782707.75
     Y    =        6881993.29  feet           Y    =         2097631.56  meter
     Z    =      -17214189.62                 Z    =        -5246884.99
     XDOT =      -7683.646278                 XDOT =       -2341.975386
     YDOT =      22572.794062  feet/sec       YDOT =        6880.187630  meter/sec
     ZDOT =       3472.863495                 ZDOT =        1058.528793
  
  
    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   20035.16709933  .00016717  00000-0  10270-3 0  9173
    2 25544  51.6435 291.5926 0005270 227.8266 132.2437 15.49096583 11236
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20035.16709933   =   yrday.fracday
    Element set:     917
    Inclination:       51.6435  deg
    RA of node:       291.5926  deg
    Eccentricity:     .0005270     
    Arg of perigee:   227.8266  deg
    Mean anomaly:     132.2437  deg
    Mean motion:   15.49096583  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1123
    Checksum:              313
 
 
    Coasting Arc #19 (Orbit 1138)
    ---------------------------------------
 
    Vector Time (GMT): 2020/036/03:40:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920821.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3682423.82                 A    =         6792380.37  meter
     Y    =        2333449.73  meter          E    =           .0001347
     Z    =        5209205.43                 I    =           51.25064
     XDOT =      -2902.416055                 Wp   =          212.33061
     YDOT =       7005.078493  meter/sec      RA   =          285.89653  deg
     ZDOT =      -1087.416495                 TA   =          248.14982
                                              MA   =          248.16415
                                              Ha   =            228.027  n.mi
                                              Hp   =            223.980
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12081442.97                 X    =         3630753.91
     Y    =        7655674.96  feet           Y    =         2374340.02  meter
     Z    =       17090569.00                 Z    =         5226967.53
     XDOT =      -9522.362386                 XDOT =       -2975.251230
     YDOT =      22982.540986  feet/sec       YDOT =        6972.214430  meter/sec
     ZDOT =      -3567.639420                 ZDOT =       -1101.691579
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13003005.30                 X    =        -3963316.01
     Y    =       -5719704.02  feet           Y    =        -1743365.79  meter
     Z    =       17171633.91                 Z    =         5233914.02
     XDOT =       5422.773759                 XDOT =        1652.861442
     YDOT =     -23223.996339  feet/sec       YDOT =       -7078.674084  meter/sec
     ZDOT =      -3633.435935                 ZDOT =       -1107.471273
  
  
    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   20036.19926591  .00016717  00000-0  10270-3 0  9189
    2 25544  51.6419 286.4861 0005086 230.7257 129.3443 15.49118417 11399
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20036.19926591   =   yrday.fracday
    Element set:     918
    Inclination:       51.6419  deg
    RA of node:       286.4861  deg
    Eccentricity:     .0005086     
    Arg of perigee:   230.7257  deg
    Mean anomaly:     129.3443  deg
    Mean motion:   15.49118417  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1139
    Checksum:              322
 
 
    Coasting Arc #20 (Orbit 1153)
    ---------------------------------------
 
    Vector Time (GMT): 2020/037/03:40:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920821.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3854584.96                 A    =         6792496.70  meter
     Y    =       -2073218.85  meter          E    =           .0010945
     Z    =       -5203717.28                 I    =           51.24202
     XDOT =       2324.711672                 Wp   =          117.86873
     YDOT =      -7200.524474  meter/sec      RA   =          280.92353  deg
     ZDOT =       1143.602720                 TA   =          163.19813
                                              MA   =          163.16184
                                              Ha   =            228.004  n.mi
                                              Hp   =            224.008
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12646276.10                 X    =        -3805839.00
     Y    =       -6801899.12  feet           Y    =        -2116050.69  meter
     Z    =      -17072563.24                 Z    =        -5222322.67
     XDOT =       7627.006797                 XDOT =        2399.502426
     YDOT =     -23623.767959  feet/sec       YDOT =       -7174.109785  meter/sec
     ZDOT =       3751.977429                 ZDOT =        1155.076247
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13509896.87                 X    =         4117816.57
     Y    =        4557299.70  feet           Y    =         1389064.95  meter
     Z    =      -17157513.00                 Z    =        -5229609.96
     XDOT =      -3112.540817                 XDOT =        -948.702441
     YDOT =      23590.972857  feet/sec       YDOT =        7190.528527  meter/sec
     ZDOT =       3804.959800                 ZDOT =        1159.751747
  
  
    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   20037.16692164  .00016717  00000-0  10270-3 0  9194
    2 25544  51.6411 281.6997 0005209 235.6004 124.4654 15.49095508 11541
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20037.16692164   =   yrday.fracday
    Element set:     919
    Inclination:       51.6411  deg
    RA of node:       281.6997  deg
    Eccentricity:     .0005209     
    Arg of perigee:   235.6004  deg
    Mean anomaly:     124.4654  deg
    Mean motion:   15.49095508  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1154
    Checksum:              309
 
 
    Coasting Arc #21 (Orbit 1155)
    ---------------------------------------
 
    Vector Time (GMT): 2020/037/05:49:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 905713.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4256826.10                 A    =         6794735.40  meter
     Y    =       -2571982.70  meter          E    =           .0007012
     Z    =        4630045.13                 I    =           51.24780
     XDOT =       1068.916495                 Wp   =          154.96616
     YDOT =       7006.797992  meter/sec      RA   =          280.50940  deg
     ZDOT =       2901.650260                 TA   =          265.92818
                                              MA   =          266.00833
                                              Ha   =            227.826  n.mi
                                              Hp   =            224.171
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13965964.88                 X    =         4262780.78
     Y    =       -8438263.46  feet           Y    =        -2524346.83  meter
     Z    =       15190436.78                 Z    =         4650736.98
     XDOT =       3506.943880                 XDOT =         976.390734
     YDOT =      22988.182388  feet/sec       YDOT =        7018.233861  meter/sec
     ZDOT =       9519.849936                 ZDOT =        2906.618208
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4603104.24                 X    =        -1403026.17
     Y    =       15561948.02  feet           Y    =         4743281.76  meter
     Z    =       15285255.64                 Z    =         4658945.92
     XDOT =     -16856.216524                 XDOT =       -5137.774797
     YDOT =     -14383.538494  feet/sec       YDOT =       -4384.102533  meter/sec
     ZDOT =       9542.081213                 ZDOT =        2908.426354
  
  
    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   20037.29594227  .00016717  00000-0  10270-3 0  9201
    2 25544  51.6396 281.0613 0005286 237.6362 122.4277 15.49136037 11560
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      20037.29594227   =   yrday.fracday
    Element set:     920
    Inclination:       51.6396  deg
    RA of node:       281.0613  deg
    Eccentricity:     .0005286     
    Arg of perigee:   237.6362  deg
    Mean anomaly:     122.4277  deg
    Mean motion:   15.49136037  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1156
    Checksum:              305
 
             

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