[ISSTLE LIST] Current ISS TLEs @ 18:30 UTC


Subject: [ISSTLE LIST] Current ISS TLEs @ 18:30 UTC
Date: February 26th 2021


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  • found at www.nasa.gov/station
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  • Updated ISS trajectory information will be made available as a CCSDS *
  • Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
  • system. *
  • Included in the OEM are a sequence of events with ISS maneuver *
  • details (in the comment section), predicted post-maneuver state *
  • vectors, predicted coasting state vectors at 4-minute intervals, *
  • and ISS ballistic details.
  • OEMs are provided in .xml and .txt formats at the following links: *
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  • https://nasa-public-data.s3.amazonaws.com/iss-coords/current/ISS_OEM/ISS.OEM_J2K_EPH.txt
  • The above links are permanent links to the most current posted ISS ephemeris data. *
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<B> ISS TRAJECTORY DATA</B>

Lift off time (UTC) : N/A
Area (sq ft) : 15144.822
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 84.1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.497 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 
   ------------------------------------------------------------------------
   050/19:22:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.9  
   000/00:00:00.000           0.0               0.0              222.1  
   
   051/17:36:48.295           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.9  
   000/00:00:00.000           0.0               0.0              222.1  
   
   053/09:40:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.8  
   000/00:00:00.000           0.0               0.0              222.0  
   
   054/01:32:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              230.0  
   000/00:00:00.000           0.0               0.0              221.9  
   
   063/11:35:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              230.2  
   000/00:00:00.000           0.0               0.0              221.8  

Coasting Arc #1 (Orbit 3005)


Vector Time (GMT): 2021/048/14:53:53.651 Vector Time (MET): N/A
Weight (LBS) : 957236.1

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4607312.46                 A    =         6794794.36  meter
     Y    =       -1531324.39  meter          E    =           .0009802
     Z    =        4749270.39                 I    =           51.41332
     XDOT =       4597.800926                 Wp   =           53.70439
     YDOT =       5516.878978  meter/sec      RA   =          212.92229  deg
     ZDOT =      -2671.990580                 TA   =           62.83971
                                              MA   =           62.73980
                                              Ha   =            229.642  n.mi
                                              Hp   =            222.317
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15115854.52                 X    =         4601024.95
     Y    =       -5024030.14  feet           Y    =        -1479837.04  meter
     Z    =       15581595.77                 Z    =         4771635.31
     XDOT =      15084.648708                 XDOT =        4548.746553
     YDOT =      18099.996647  feet/sec       YDOT =        5568.020505  meter/sec
     ZDOT =      -8766.373293                 ZDOT =       -2649.776051
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13859162.15                 X    =         4224272.62
     Y    =       -7642416.65  feet           Y    =        -2329408.60  meter
     Z    =       15685444.07                 Z    =         4780923.35
     XDOT =      17597.454665                 XDOT =        5363.704182
     YDOT =      14067.868629  feet/sec       YDOT =        4287.886358  meter/sec
     ZDOT =      -8663.135182                 ZDOT =       -2640.523603

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 21048.66450415 .00016717 00000-0 10270-3 0 9003 2 25544 51.6426 213.8989 0002614 28.5435 331.5857 15.48946158 30068

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21048.66450415   =   yrday.fracday
    Element set:     900
    Inclination:       51.6426  deg
    RA of node:       213.8989  deg
    Eccentricity:     .0002614     
    Arg of perigee:    28.5435  deg
    Mean anomaly:     331.5857  deg

Mean motion: 15.48946158 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3006
    Checksum:              315

Coasting Arc #2 (Orbit 3020)


Vector Time (GMT): 2021/049/14:57:53.651 Vector Time (MET): N/A
Weight (LBS) : 957236.1

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5490393.08                 A    =         6797632.16  meter
     Y    =         659130.13  meter          E    =           .0007812
     Z    =       -3959941.04                 I    =           51.45345
     XDOT =      -3537.444612                 Wp   =           88.20787
     YDOT =      -5483.277113  meter/sec      RA   =          207.94415  deg
     ZDOT =       3999.016471                 TA   =          223.68218
                                              MA   =          223.74403
                                              Ha   =            229.692  n.mi
                                              Hp   =            222.160
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18013100.65                 X    =        -5478120.80
     Y    =        2162500.42  feet           Y    =          597801.09  meter
     Z    =      -12991932.54                 Z    =        -3986581.00
     XDOT =     -11605.789411                 XDOT =       -3495.290646
     YDOT =     -17989.754308  feet/sec       YDOT =       -5522.599549  meter/sec
     ZDOT =      13120.132779                 ZDOT =        3981.935778
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17045447.47                 X    =        -5195452.39
     Y    =        5947327.56  feet           Y    =         1812745.44  meter
     Z    =      -13115659.71                 Z    =        -3997653.08
     XDOT =     -14840.741796                 XDOT =       -4523.458099
     YDOT =     -13826.694517  feet/sec       YDOT =       -4214.376489  meter/sec
     ZDOT =      13040.722736                 ZDOT =        3974.812290

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 21049.63224706 .00016717 00000-0 10270-3 0 9014 2 25544 51.6437 209.1130 0002665 28.2005 331.9289 15.48972457 30213

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21049.63224706   =   yrday.fracday
    Element set:     901
    Inclination:       51.6437  deg
    RA of node:       209.1130  deg
    Eccentricity:     .0002665     
    Arg of perigee:    28.2005  deg
    Mean anomaly:     331.9289  deg

Mean motion: 15.48972457 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3021
    Checksum:              291

Coasting Arc #3 (Orbit 3036)


Vector Time (GMT): 2021/050/14:57:53.651 Vector Time (MET): N/A
Weight (LBS) : 957236.1

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5418639.64                 A    =         6797717.89  meter
     Y    =       -1111044.06  meter          E    =           .0013078
     Z    =        3943801.20                 I    =           51.48381
     XDOT =       3991.520497                 Wp   =           71.44124
     YDOT =       5163.812423  meter/sec      RA   =          202.98626  deg
     ZDOT =      -4014.421611                 TA   =           60.65959
                                              MA   =           60.52901
                                              Ha   =            229.773  n.mi
                                              Hp   =            222.144
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17777689.10                 X    =         5411504.52
     Y    =       -3645157.68  feet           Y    =        -1050488.76  meter
     Z    =       12938980.30                 Z    =         3970105.10
     XDOT =      13095.539687                 XDOT =        3952.979970
     YDOT =      16941.641807  feet/sec       YDOT =        5208.232927  meter/sec
     ZDOT =     -13170.674577                 ZDOT =       -3995.126358
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16369778.04                 X    =         4989508.35
     Y    =       -7628053.26  feet           Y    =        -2325030.63  meter
     Z    =       13061155.61                 Z    =         3981040.23
     XDOT =      16183.120476                 XDOT =        4932.615121
     YDOT =      12247.314727  feet/sec       YDOT =        3732.981529  meter/sec
     ZDOT =     -13080.966786                 ZDOT =       -3987.078677

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 21050.66450645 .00016717 00000-0 10270-3 0 9023 2 25544 51.6433 204.0072 0002778 35.7489 324.3846 15.48958996 30376

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21050.66450645   =   yrday.fracday
    Element set:     902
    Inclination:       51.6433  deg
    RA of node:       204.0072  deg
    Eccentricity:     .0002778     
    Arg of perigee:    35.7489  deg
    Mean anomaly:     324.3846  deg

Mean motion: 15.48958996 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3037
    Checksum:              323

Coasting Arc #4 (Orbit 3039)


Vector Time (GMT): 2021/050/19:22:30.000 Vector Time (MET): N/A
Weight (LBS) : 957236.1

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         175255.29                 A    =         6792979.68  meter
     Y    =       -4382758.43  meter          E    =           .0005275
     Z    =        5182436.37                 I    =           51.47281
     XDOT =       7321.530633                 Wp   =           89.15575
     YDOT =       1846.647727  meter/sec      RA   =          202.11439  deg
     ZDOT =       1313.022995                 TA   =          348.18822
                                              MA   =          348.20059
                                              Ha   =            229.879  n.mi
                                              Hp   =            222.101
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         574984.56                 X    =          199078.70
     Y    =      -14379128.70  feet           Y    =        -4380665.32  meter
     Z    =       17002743.99                 Z    =         5183345.59
     XDOT =      24020.769792                 XDOT =        7293.958890
     YDOT =       6058.555534  feet/sec       YDOT =        1928.368217  meter/sec
     ZDOT =       4307.818224                 ZDOT =        1348.520575
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14063478.67                 X    =        -4286548.30
     Y    =       -3027709.92  feet           Y    =         -922845.98  meter
     Z    =       17006904.28                 Z    =         5183704.42
     XDOT =      10039.853730                 XDOT =        3060.147417
     YDOT =     -21490.571568  feet/sec       YDOT =       -6550.326214  meter/sec
     ZDOT =       4472.748436                 ZDOT =        1363.293723

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 21050.85805354 .00016717 00000-0 10270-3 0 9036 2 25544 51.6423 203.0524 0003107 32.7068 327.4273 15.48984120 30403

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21050.85805354   =   yrday.fracday
    Element set:     903
    Inclination:       51.6423  deg
    RA of node:       203.0524  deg
    Eccentricity:     .0003107     
    Arg of perigee:    32.7068  deg
    Mean anomaly:     327.4273  deg

Mean motion: 15.48984120 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3040
    Checksum:              273

Coasting Arc #5 (Orbit 3053)


Vector Time (GMT): 2021/051/17:36:48.295 Vector Time (MET): N/A
Weight (LBS) : 957236.1

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5138253.63                 A    =         6801800.83  meter
     Y    =        3698190.94  meter          E    =           .0005913
     Z    =       -2490133.25                 I    =           51.53127
     XDOT =      -4676.814531                 Wp   =          102.43350
     YDOT =       2937.932544  meter/sec      RA   =          197.53241  deg
     ZDOT =      -5299.035025                 TA   =          105.43976
                                              MA   =          105.37445
                                              Ha   =            229.925  n.mi
                                              Hp   =            222.140
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16857787.51                 X    =         5108612.88
     Y    =       12133172.38  feet           Y    =         3755484.87  meter
     Z    =       -8169728.50                 Z    =        -2465246.04
     XDOT =     -15343.879696                 XDOT =       -4683.580559
     YDOT =       9638.886299  feet/sec       YDOT =        2885.595198  meter/sec
     ZDOT =     -17385.285515                 ZDOT =       -5321.769206
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19738385.09                 X    =         6016259.78
     Y    =       -6608469.72  feet           Y    =        -2014261.57  meter
     Z    =       -8054043.53                 Z    =        -2454872.47
     XDOT =      -1581.326624                 XDOT =        -481.988355
     YDOT =      16545.418938  feet/sec       YDOT =        5043.043692  meter/sec
     ZDOT =     -17490.866733                 ZDOT =       -5331.216180

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 21051.76128002 .00016717 00000-0 10270-3 0 9046 2 25544 51.6418 198.5848 0002972 35.9148 324.2202 15.48978061 30546

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21051.76128002   =   yrday.fracday
    Element set:     904
    Inclination:       51.6418  deg
    RA of node:       198.5848  deg
    Eccentricity:     .0002972     
    Arg of perigee:    35.9148  deg
    Mean anomaly:     324.2202  deg

Mean motion: 15.48978061 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3054
    Checksum:              306

Coasting Arc #6 (Orbit 3069)


Vector Time (GMT): 2021/052/17:36:48.295 Vector Time (MET): N/A
Weight (LBS) : 957236.1

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5442568.96                 A    =         6801885.95  meter
     Y    =       -3226259.10  meter          E    =           .0016279
     Z    =        2474144.62                 I    =           51.56413
     XDOT =       4403.284433                 Wp   =           68.56677
     YDOT =      -3337.070410  meter/sec      RA   =          192.57899  deg
     ZDOT =       5312.357592                 TA   =          319.13983
                                              MA   =          319.26175
                                              Ha   =            230.033  n.mi
                                              Hp   =            222.087
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17856197.39                 X    =        -5418105.19
     Y    =      -10584839.55  feet           Y    =        -3286985.06  meter
     Z    =        8117272.38                 Z    =         2447766.66
     XDOT =      14446.471237                 XDOT =        4414.469432
     YDOT =     -10948.393733  feet/sec       YDOT =       -3287.767217  meter/sec
     ZDOT =      17428.994725                 ZDOT =        5333.773736
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18921462.07                 X    =        -5767261.64
     Y    =        8650816.33  feet           Y    =         2636768.82  meter
     Z    =        7994646.60                 Z    =         2436768.28
     XDOT =       -166.884079                 XDOT =         -50.866267
     YDOT =     -16632.844850  feet/sec       YDOT =       -5069.691110  meter/sec
     ZDOT =      17528.459807                 ZDOT =        5342.674549

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 21052.79353732 .00016717 00000-0 10270-3 0 9051 2 25544 51.6418 193.4789 0003050 38.6564 321.4804 15.48963704 30707

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21052.79353732   =   yrday.fracday
    Element set:     905
    Inclination:       51.6418  deg
    RA of node:       193.4789  deg
    Eccentricity:     .0003050     
    Arg of perigee:    38.6564  deg
    Mean anomaly:     321.4804  deg

Mean motion: 15.48963704 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3070
    Checksum:              312

Coasting Arc #7 (Orbit 3079)


Vector Time (GMT): 2021/053/09:40:00.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6546044.08                 A    =         6802833.93  meter
     Y    =        -376328.28  meter          E    =           .0014853
     Z    =        1792194.82                 I    =           51.58827
     XDOT =       1834.933309                 Wp   =          102.98119
     YDOT =       4836.953120  meter/sec      RA   =          189.22682  deg
     ZDOT =      -5650.165885                 TA   =           57.35582
                                              MA   =           57.21259
                                              Ha   =            229.850  n.mi
                                              Hp   =            221.981
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21476522.57                 X    =         6541060.52
     Y    =       -1234672.83  feet           Y    =         -303153.58  meter
     Z    =        5879904.26                 Z    =         1823980.13
     XDOT =       6020.122404                 XDOT =        1808.153309
     YDOT =      15869.268768  feet/sec       YDOT =        4857.322996  meter/sec
     ZDOT =     -18537.289649                 ZDOT =       -5641.317682
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10704252.61                 X    =         3262656.20
     Y    =       18612509.94  feet           Y    =         5673093.03  meter
     Z    =        6027616.67                 Z    =         1837217.56
     XDOT =     -10077.295644                 XDOT =       -3071.559712
     YDOT =      11823.107654  feet/sec       YDOT =        3603.683213  meter/sec
     ZDOT =     -18496.089788                 ZDOT =       -5637.608167

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 21053.43869520 .00016717 00000-0 10270-3 0 9061 2 25544 51.6397 190.2847 0003010 36.4692 323.6663 15.49008608 30809

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21053.43869520   =   yrday.fracday
    Element set:     906
    Inclination:       51.6397  deg
    RA of node:       190.2847  deg
    Eccentricity:     .0003010     
    Arg of perigee:    36.4692  deg
    Mean anomaly:     323.6663  deg

Mean motion: 15.49008608 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3080
    Checksum:              304

Coasting Arc #8 (Orbit 3089)


Vector Time (GMT): 2021/054/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1767243.70                 A    =         6793655.27  meter
     Y    =        4209025.49  meter          E    =           .0015634
     Z    =       -5045688.54                 I    =           51.58238
     XDOT =      -7359.028341                 Wp   =           68.50841
     YDOT =        770.387831  meter/sec      RA   =          185.98827  deg
     ZDOT =      -1934.094356                 TA   =          182.65668
                                              MA   =          182.66499
                                              Ha   =            230.045  n.mi
                                              Hp   =            221.949
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5798043.65                 X    =         1744554.21
     Y    =       13809138.75  feet           Y    =         4228661.27  meter
     Z    =      -16554096.28                 Z    =        -5037159.25
     XDOT =     -24143.793770                 XDOT =       -7357.701629
     YDOT =       2527.519132  feet/sec       YDOT =         688.101305  meter/sec
     ZDOT =      -6345.453923                 ZDOT =       -1969.837518
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4781574.47                 X    =        -1457423.90
     Y    =      -14239362.73  feet           Y    =        -4340157.76  meter
     Z    =      -16514382.26                 Z    =        -5033583.71
     XDOT =      23186.410923                 XDOT =        7067.218049
     YDOT =       -231.212094  feet/sec       YDOT =         -70.473446  meter/sec
     ZDOT =      -6511.571751                 ZDOT =       -1984.727070

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 21054.08385593 .00016717 00000-0 10270-3 0 9077 2 25544 51.6425 187.0972 0003366 39.4349 320.7046 15.48994477 30901

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21054.08385593   =   yrday.fracday
    Element set:     907
    Inclination:       51.6425  deg
    RA of node:       187.0972  deg
    Eccentricity:     .0003366     
    Arg of perigee:    39.4349  deg
    Mean anomaly:     320.7046  deg

Mean motion: 15.48994477 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3090
    Checksum:              332

Coasting Arc #9 (Orbit 3105)


Vector Time (GMT): 2021/055/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2118650.46                 A    =         6793589.29  meter
     Y    =       -4029131.16  meter          E    =           .0007103
     Z    =        5037009.34                 I    =           51.61616
     XDOT =       7281.893489                 Wp   =           97.38061
     YDOT =      -1402.745505  meter/sec      RA   =          181.04107  deg
     ZDOT =       1937.583248                 TA   =          333.78764
                                              MA   =          333.82358
                                              Ha   =            230.061  n.mi
                                              Hp   =            221.882
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6950952.95                 X    =        -2097904.23
     Y    =      -13218934.24  feet           Y    =        -4052707.43  meter
     Z    =       16525621.19                 Z    =         5026768.45
     XDOT =      23890.726671                 XDOT =        7287.626817
     YDOT =      -4602.183415  feet/sec       YDOT =       -1321.282059  meter/sec
     ZDOT =       6356.900419                 ZDOT =        1972.968748
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6213546.95                 X    =         1893889.11
     Y    =       13638964.17  feet           Y    =         4157156.28  meter
     Z    =       16477943.31                 Z    =         5022477.12
     XDOT =     -23095.340156                 XDOT =       -7039.459680
     YDOT =       2629.932593  feet/sec       YDOT =         801.603454  meter/sec
     ZDOT =       6521.371819                 ZDOT =        1987.714130

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 21055.11610811 .00016717 00000-0 10270-3 0 9087 2 25544 51.6423 181.9921 0003235 42.3038 317.8361 15.49012929 31068

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21055.11610811   =   yrday.fracday
    Element set:     908
    Inclination:       51.6423  deg
    RA of node:       181.9921  deg
    Eccentricity:     .0003235     
    Arg of perigee:    42.3038  deg
    Mean anomaly:     317.8361  deg

Mean motion: 15.49012929 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3106
    Checksum:              279

Coasting Arc #10 (Orbit 3120)


Vector Time (GMT): 2021/056/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2456905.87                 A    =         6793627.86  meter
     Y    =        3838772.05  meter          E    =           .0015826
     Z    =       -5052422.51                 I    =           51.65112
     XDOT =      -7120.163246                 Wp   =           69.79244
     YDOT =       2016.402552  meter/sec      RA   =          176.09538  deg
     ZDOT =      -1929.964548                 TA   =          181.43440
                                              MA   =          181.43895
                                              Ha   =            230.105  n.mi
                                              Hp   =            221.867
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8060714.79                 X    =         2438337.95
     Y    =       12594396.50  feet           Y    =         3866143.02  meter
     Z    =      -16576189.33                 Z    =        -5040533.37
     XDOT =     -23360.115635                 XDOT =       -7132.807728
     YDOT =       6615.493938  feet/sec       YDOT =        1936.709010  meter/sec
     ZDOT =      -6331.904685                 ZDOT =       -1964.581173
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7584953.72                 X    =        -2311893.90
     Y    =      -12957404.16  feet           Y    =        -3949416.79  meter
     Z    =      -16520839.96                 Z    =        -5035552.02
     XDOT =      22651.455948                 XDOT =        6904.163773
     YDOT =      -4979.489647  feet/sec       YDOT =       -1517.748445  meter/sec
     ZDOT =      -6492.815167                 ZDOT =       -1979.010063

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 21056.08384642 .00016717 00000-0 10270-3 0 9095 2 25544 51.6433 177.2054 0003378 46.0062 314.1367 15.49001131 31216

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21056.08384642   =   yrday.fracday
    Element set:     909
    Inclination:       51.6433  deg
    RA of node:       177.2054  deg
    Eccentricity:     .0003378     
    Arg of perigee:    46.0062  deg
    Mean anomaly:     314.1367  deg

Mean motion: 15.49001131 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3121
    Checksum:              275

Coasting Arc #11 (Orbit 3136)


Vector Time (GMT): 2021/057/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2771934.70                 A    =         6793589.43  meter
     Y    =       -3601705.29  meter          E    =           .0007367
     Z    =        5043504.11                 I    =           51.68550
     XDOT =       6936.524291                 Wp   =           99.24667
     YDOT =      -2625.935619  meter/sec      RA   =          171.15237  deg
     ZDOT =       1933.526405                 TA   =          331.97949
                                              MA   =          332.01913
                                              Ha   =            230.147  n.mi
                                              Hp   =            221.808
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9094273.94                 X    =        -2755950.97
     Y    =      -11816618.39  feet           Y    =        -3632613.47  meter
     Z    =       16546929.50                 Z    =         5030078.55
     XDOT =      22757.625626                 XDOT =        6955.981114
     YDOT =      -8615.274340  feet/sec       YDOT =       -2548.257523  meter/sec
     ZDOT =       6343.590567                 ZDOT =        1967.267598
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8862130.42                 X    =         2701177.35
     Y    =       12077476.15  feet           Y    =         3681214.73  meter
     Z    =       16484428.37                 Z    =         5024453.77
     XDOT =     -22072.532563                 XDOT =       -6727.707925
     YDOT =       7307.809256  feet/sec       YDOT =        2227.420261  meter/sec
     ZDOT =       6500.440380                 ZDOT =        1981.334228

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 21057.11609670 .00016717 00000-0 10270-3 0 9103 2 25544 51.6438 172.0999 0003216 48.8369 311.3058 15.49009914 31373

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21057.11609670   =   yrday.fracday
    Element set:     910
    Inclination:       51.6438  deg
    RA of node:       172.0999  deg
    Eccentricity:     .0003216     
    Arg of perigee:    48.8369  deg
    Mean anomaly:     311.3058  deg

Mean motion: 15.49009914 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3137
    Checksum:              310

Coasting Arc #12 (Orbit 3151)


Vector Time (GMT): 2021/058/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3069429.40                 A    =         6793579.80  meter
     Y    =        3358265.94  meter          E    =           .0015997
     Z    =       -5059758.50                 I    =           51.72026
     XDOT =      -6673.692051                 Wp   =           70.84080
     YDOT =       3201.044029  meter/sec      RA   =          166.21146  deg
     ZDOT =      -1923.765316                 TA   =          180.46832
                                              MA   =          180.46982
                                              Ha   =            230.148  n.mi
                                              Hp   =            221.791
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10070306.42                 X    =         3056224.77
     Y    =       11017932.88  feet           Y    =         3392516.34  meter
     Z    =      -16600257.56                 Z    =        -5044881.18
     XDOT =     -21895.315129                 XDOT =       -6699.646845
     YDOT =      10502.112955  feet/sec       YDOT =        3126.268733  meter/sec
     ZDOT =      -6311.565997                 ZDOT =       -1956.245748
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10054258.51                 X    =        -3064538.00
     Y    =      -11136087.13  feet           Y    =        -3394279.36  meter
     Z    =      -16530998.66                 Z    =        -5038648.39
     XDOT =      21161.108810                 XDOT =        6449.905965
     YDOT =      -9511.362499  feet/sec       YDOT =       -2899.063290  meter/sec
     ZDOT =      -6462.559423                 ZDOT =       -1969.788112

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 21058.08383026 .00016717 00000-0 10270-3 0 9115 2 25544 51.6452 167.3135 0003419 51.3257 308.8198 15.49013166 31525

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21058.08383026   =   yrday.fracday
    Element set:     911
    Inclination:       51.6452  deg
    RA of node:       167.3135  deg
    Eccentricity:     .0003419     
    Arg of perigee:    51.3257  deg
    Mean anomaly:     308.8198  deg

Mean motion: 15.49013166 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3152
    Checksum:              294

Coasting Arc #13 (Orbit 3167)


Vector Time (GMT): 2021/059/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3338053.47                 A    =         6793594.31  meter
     Y    =       -3072204.93  meter          E    =           .0007745
     Z    =        5050676.26                 I    =           51.75249
     XDOT =       6389.962712                 Wp   =          100.27136
     YDOT =      -3769.626593  meter/sec      RA   =          161.27292  deg
     ZDOT =       1926.370024                 TA   =          331.04352
                                              MA   =          331.08647
                                              Ha   =            230.295  n.mi
                                              Hp   =            221.688
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10951619.01                 X    =        -3327983.69
     Y    =      -10079412.49  feet           Y    =        -3109476.70  meter
     Z    =       16570460.17                 Z    =         5034486.47
     XDOT =      20964.444593                 XDOT =        6422.283967
     YDOT =     -12367.541314  feet/sec       YDOT =       -3697.988526  meter/sec
     ZDOT =       6320.111627                 ZDOT =        1957.487953
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11120277.79                 X    =         3389460.67
     Y    =       10018182.44  feet           Y    =         3053542.01  meter
     Z    =       16495093.45                 Z    =         5027704.48
     XDOT =     -20122.079390                 XDOT =       -6133.209798
     YDOT =      11670.399354  feet/sec       YDOT =        3557.137723  meter/sec
     ZDOT =       6464.772177                 ZDOT =        1970.462560

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 21059.11607758 .00016717 00000-0 10270-3 0 9122 2 25544 51.6447 162.2079 0003387 55.6935 304.4535 15.49003296 31681

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21059.11607758   =   yrday.fracday
    Element set:     912
    Inclination:       51.6447  deg
    RA of node:       162.2079  deg
    Eccentricity:     .0003387     
    Arg of perigee:    55.6935  deg
    Mean anomaly:     304.4535  deg

Mean motion: 15.49003296 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3168
    Checksum:              317

Coasting Arc #14 (Orbit 3182)


Vector Time (GMT): 2021/060/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3588395.19                 A    =         6793554.85  meter
     Y    =        2783509.85  meter          E    =           .0016034
     Z    =       -5067148.15                 I    =           51.78428
     XDOT =      -6033.531130                 Wp   =           72.05354
     YDOT =       4290.857942  meter/sec      RA   =          156.33697  deg
     ZDOT =      -1915.868828                 TA   =          179.35386
                                              MA   =          179.35178
                                              Ha   =            230.157  n.mi
                                              Hp   =            221.773
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11772950.09                 X    =         3581615.22
     Y    =        9132250.15  feet           Y    =         2823599.46  meter
     Z    =      -16624501.79                 Z    =        -5049734.24
     XDOT =     -19795.049640                 XDOT =       -6071.758399
     YDOT =      14077.617919  feet/sec       YDOT =        4223.172708  meter/sec
     ZDOT =      -6285.658885                 ZDOT =       -1945.269998
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12090969.51                 X    =        -3685327.51
     Y    =       -8859879.49  feet           Y    =        -2700491.27  meter
     Z    =      -16543439.74                 Z    =        -5042440.43
     XDOT =      18781.184340                 XDOT =        5724.504987
     YDOT =     -13639.610018  feet/sec       YDOT =       -4157.353133  meter/sec
     ZDOT =      -6422.338524                 ZDOT =       -1957.528782

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 21060.08380858 .00016717 00000-0 10270-3 0 9130 2 25544 51.6448 157.4220 0003336 56.6874 303.4595 15.49016192 31834

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21060.08380858   =   yrday.fracday
    Element set:     913
    Inclination:       51.6448  deg
    RA of node:       157.4220  deg
    Eccentricity:     .0003336     
    Arg of perigee:    56.6874  deg
    Mean anomaly:     303.4595  deg

Mean motion: 15.49016192 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3183
    Checksum:              308

Coasting Arc #15 (Orbit 3198)


Vector Time (GMT): 2021/061/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3803791.91                 A    =         6793587.04  meter
     Y    =       -2457159.51  meter          E    =           .0007880
     Z    =        5058048.35                 I    =           51.81532
     XDOT =       5657.892896                 Wp   =          102.16641
     YDOT =      -4802.391492  meter/sec      RA   =          151.40227  deg
     ZDOT =       1917.785692                 TA   =          329.24970
                                              MA   =          329.29585
                                              Ha   =            230.337  n.mi
                                              Hp   =            221.661
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12479632.26                 X    =        -3800601.22
     Y    =       -8061546.95  feet           Y    =        -2499677.93  meter
     Z    =       16594646.81                 Z    =         5039579.29
     XDOT =      18562.640735                 XDOT =        5701.858843
     YDOT =     -15755.877598  feet/sec       YDOT =       -4738.874833  meter/sec
     ZDOT =       6291.947809                 ZDOT =        1945.376333
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12904810.69                 X    =         3933386.30
     Y    =        7552582.97  feet           Y    =         2302027.29  meter
     Z    =       16508676.95                 Z    =         5031844.73
     XDOT =     -17325.526124                 XDOT =       -5280.820362
     YDOT =      15540.100995  feet/sec       YDOT =        4736.622783  meter/sec
     ZDOT =       6420.211707                 ZDOT =        1956.880528

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 21061.11605307 .00016717 00000-0 10270-3 0 9145 2 25544 51.6452 152.3160 0003328 61.0196 299.1287 15.48999787 31999

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21061.11605307   =   yrday.fracday
    Element set:     914
    Inclination:       51.6452  deg
    RA of node:       152.3160  deg
    Eccentricity:     .0003328     
    Arg of perigee:    61.0196  deg
    Mean anomaly:     299.1287  deg

Mean motion: 15.48999787 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3199
    Checksum:              318

Coasting Arc #16 (Orbit 3213)


Vector Time (GMT): 2021/062/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3998977.58                 A    =         6793516.05  meter
     Y    =        2133513.23  meter          E    =           .0016144
     Z    =       -5075159.86                 I    =           51.84405
     XDOT =      -5220.024473                 Wp   =           73.04986
     YDOT =       5254.327620  meter/sec      RA   =          146.46935  deg
     ZDOT =      -1904.729329                 TA   =          178.48654
                                              MA   =          178.48165
                                              Ha   =            230.185  n.mi
                                              Hp   =            221.730
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13120005.18                 X    =         3999474.71
     Y    =        6999715.31  feet           Y    =         2178235.05  meter
     Z    =      -16650786.93                 Z    =        -5055733.58
     XDOT =     -17126.064543                 XDOT =       -5269.140031
     YDOT =      17238.607677  feet/sec       YDOT =        5195.678759  meter/sec
     ZDOT =      -6249.111971                 ZDOT =       -1930.205590
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13611956.68                 X    =        -4148924.40
     Y    =       -6232834.57  feet           Y    =        -1899767.98  meter
     Z    =      -16560364.26                 Z    =        -5047599.03
     XDOT =      15617.144246                 XDOT =        4760.105566
     YDOT =     -17191.994391  feet/sec       YDOT =       -5240.119890  meter/sec
     ZDOT =      -6367.550557                 ZDOT =       -1940.829410

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 21062.08377886 .00016717 00000-0 10270-3 0 9151 2 25544 51.6447 147.5291 0003352 61.4044 298.7443 15.49022029 32141

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21062.08377886   =   yrday.fracday
    Element set:     915
    Inclination:       51.6447  deg
    RA of node:       147.5291  deg
    Eccentricity:     .0003352     
    Arg of perigee:    61.4044  deg
    Mean anomaly:     298.7443  deg

Mean motion: 15.49022029 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3214
    Checksum:              306

Coasting Arc #17 (Orbit 3229)


Vector Time (GMT): 2021/063/01:32:30.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4155165.94                 A    =         6793585.43  meter
     Y    =       -1777597.60  meter          E    =           .0008132
     Z    =        5065939.41                 I    =           51.87082
     XDOT =       4764.305255                 Wp   =          103.33054
     YDOT =      -5694.352986  meter/sec      RA   =          141.53850  deg
     ZDOT =       1905.262330                 TA   =          328.22451
                                              MA   =          328.27356
                                              Ha   =            230.439  n.mi
                                              Hp   =            221.586
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13632434.19                 X    =        -4159586.68
     Y    =       -5832013.12  feet           Y    =        -1824088.09  meter
     Z    =       16620536.13                 Z    =         5045744.80
     XDOT =      15630.922751                 XDOT =        4818.372575
     YDOT =     -18682.260454  feet/sec       YDOT =       -5640.772666  meter/sec
     ZDOT =       6250.860662                 ZDOT =        1928.536880
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14141311.93                 X    =         4310271.88
     Y    =        4795278.57  feet           Y    =         1461600.91  meter
     Z    =       16526538.07                 Z    =         5037288.80
     XDOT =     -13808.678853                 XDOT =       -4208.885314
     YDOT =      18755.891794  feet/sec       YDOT =        5716.795819  meter/sec
     ZDOT =       6359.070867                 ZDOT =        1938.244800

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 21063.11601991 .00016717 00000-0 10270-3 0 9164 2 25544 51.6438 142.4231 0003449 66.5010 293.6503 15.48992308 32309

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21063.11601991   =   yrday.fracday
    Element set:     916
    Inclination:       51.6438  deg
    RA of node:       142.4231  deg
    Eccentricity:     .0003449     
    Arg of perigee:    66.5010  deg
    Mean anomaly:     293.6503  deg

Mean motion: 15.48992308 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3230
    Checksum:              287

Coasting Arc #18 (Orbit 3235)


Vector Time (GMT): 2021/063/11:35:00.000 Vector Time (MET): N/A
Weight (LBS) : 972366.4

              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4575004.35                 A    =         6794354.16  meter
     Y    =        1150468.70  meter          E    =           .0014819
     Z    =       -4903560.28                 I    =           51.88356
     XDOT =      -4093.508892                 Wp   =           73.32168
     YDOT =       5991.958305  meter/sec      RA   =          139.47684  deg
     ZDOT =      -2415.314809                 TA   =          173.02297
                                              MA   =          173.00232
                                              Ha   =            230.216  n.mi
                                              Hp   =            221.806
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15009856.80                 X    =         4585617.90
     Y    =        3774503.61  feet           Y    =         1201688.82  meter
     Z    =      -16087796.18                 Z    =        -4881311.19
     XDOT =     -13430.147285                 XDOT =       -4148.476462
     YDOT =      19658.655855  feet/sec       YDOT =        5945.874277  meter/sec
     ZDOT =      -7924.261186                 ZDOT =       -2435.333062
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12158643.56                 X    =         3705954.56
     Y    =        9748394.40  feet           Y    =         2971310.61  meter
     Z    =      -15984244.06                 Z    =        -4871997.59
     XDOT =     -19656.835478                 XDOT =       -5991.403454
     YDOT =      11381.419142  feet/sec       YDOT =        3469.056554  meter/sec
     ZDOT =      -8017.324554                 ZDOT =       -2443.680524

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 21063.50310937 .00016717 00000-0 10270-3 0 9175 2 25544 51.6431 140.5059 0003089 74.7520 285.3971 15.48984602 32367

Satellite: ISS
Catalog Number: 25544

    Epoch time:      21063.50310937   =   yrday.fracday
    Element set:     917
    Inclination:       51.6431  deg
    RA of node:       140.5059  deg
    Eccentricity:     .0003089     
    Arg of perigee:    74.7520  deg
    Mean anomaly:     285.3971  deg

Mean motion: 15.48984602 rev/day Decay rate: 1.67170E-04 rev/day^2

    Epoch rev:            3236
    Checksum:              306


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