[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: February 11th 2021

  • *
  • !!! The status of spaceflight nasa gov has been updated !!! *
  • *
  • spaceflight nasa gov will be taken offline by February 20, 2021 *
  • *
  • Current information about the International Space Station can be *
  • found at www nasa gov/station *
  • *
  • Predicted ISS and visiting vehicle sightings opportunities can be *
  • found at spotthestation nasa gov *
  • *
  • 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: *
  • https://nasa-public-data s3 amazonaws com/iss-coords/current/ISS_OEM/ISS OEM_J2K_EPH xml *
  • 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 *
  • Older archived ephemeris data can be found by searching on data nasa gov *
  • *

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15423 6072 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


046/04:45:06 000 0 0 0 0 0 0
N/A 0 0 0 0 229 7
000/00:00:00 000 0 0 0 0 222 3

046/21:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 7
000/00:00:00 000 0 0 0 0 222 4

048/06:20:28 000 0 0 0 0 0 0
N/A 0 0 0 0 229 7
000/00:00:00 000 0 0 0 0 222 2

050/19:24:00 000 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

051/17:36:44 000 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

053/09:36:25 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 222 0

054/01:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 1
000/00:00:00 000 0 0 0 0 221 9

Coasting Arc #1 (Orbit 2894)
---------------------------------------

Vector Time (GMT): 2021/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942149
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3573605
91                 A    =         6803332
62  meter
 Y    =       -5564410
74  meter          E    =           
0010265
 Z    =       -1575902
03                 I    =           51
29012
 XDOT =       3411
503609                 Wp   =           26
57604
 YDOT =      -3801
072271  meter/sec      RA   =          248
30045  deg
 ZDOT =       5708
710681                 TA   =          316
14240
                                          MA   =          316
22386
                                          Ha   =            229
276  n
mi
                                          Hp   =            222
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11724428
83                 X    =        -3503462
82
 Y    =      -18255940
76  feet           Y    =        -5603981
14  meter
 Z    =       -5170282
26                 Z    =        -1593090
37
 XDOT =      11192
597143                 XDOT =        3426
026182
 YDOT =     -12470
709550  feet/sec       YDOT =       -3762
841334  meter/sec
 ZDOT =      18729
365752                 ZDOT =        5725
316989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2827287
06                 X    =          861757
10
 Y    =      -21492256
10  feet           Y    =        -6550839
66  meter
 Z    =       -5250028
46                 Z    =        -1600208
68
 XDOT =      14928
604705                 XDOT =        4550
238714
 YDOT =      -2611
575068  feet/sec       YDOT =        -796
008081  meter/sec
 ZDOT =      18806
464212                 ZDOT =        5732
210292


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   21041
50313296  
00016717  00000-0  10270-3 0  9004
2 25544  51
6411 249
3246 0002926 353
5712   6
5400 15
48953336 28951


Satellite: ISS
Catalog Number: 25544
Epoch time:      21041
50313296   =   yrday
fracday
Element set:     900
Inclination:       51
6411  deg
RA of node:       249
3246  deg
Eccentricity:     
0002926     
Arg of perigee:   353
5712  deg
Mean anomaly:       6
5400  deg
Mean motion:   15
48953336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2895
Checksum:              289


Coasting Arc #2 (Orbit 2910)
---------------------------------------

Vector Time (GMT): 2021/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942149
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4033761
89                 A    =         6803225
29  meter
 Y    =        5245497
93  meter          E    =           
0012719
 Z    =        1560507
79                 I    =           51
30362
 XDOT =      -3073
900540                 Wp   =          104
74113
 YDOT =       4073
757094  meter/sec      RA   =          243
32905  deg
 ZDOT =      -5711
778670                 TA   =           58
15562
                                          MA   =           58
03187
                                          Ha   =            229
388  n
mi
                                          Hp   =            222
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13234126
92                 X    =         3967225
56
 Y    =       17209638
87  feet           Y    =         5290234
33  meter
 Z    =        5119776
20                 Z    =         1579939
89
 XDOT =     -10084
975525                 XDOT =       -3091
482574
 YDOT =      13365
344796  feet/sec       YDOT =        4039
284222  meter/sec
 ZDOT =     -18739
431332                 ZDOT =       -5726
752607

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -625551
17                 X    =         -190668
00
 Y    =       21679272
25  feet           Y    =         6607842
18  meter
 Z    =        5209964
88                 Z    =         1587997
30
 XDOT =     -14576
702389                 XDOT =       -4442
978888
 YDOT =       4127
476932  feet/sec       YDOT =        1258
054969  meter/sec
 ZDOT =     -18808
946870                 ZDOT =       -5732
967006


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   21042
53540313  
00016717  00000-0  10270-3 0  9011
2 25544  51
6408 244
2182 0003131 359
5161    
5985 15
48997301 29114


Satellite: ISS
Catalog Number: 25544
Epoch time:      21042
53540313   =   yrday
fracday
Element set:     901
Inclination:       51
6408  deg
RA of node:       244
2182  deg
Eccentricity:     
0003131     
Arg of perigee:   359
5161  deg
Mean anomaly:        
5985  deg
Mean motion:   15
48997301  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2911
Checksum:              279


Coasting Arc #3 (Orbit 2925)
---------------------------------------

Vector Time (GMT): 2021/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942149
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4482683
83                 A    =         6803311
86  meter
 Y    =       -4860225
35  meter          E    =           
0010398
 Z    =       -1581965
27                 I    =           51
31804
 XDOT =       2696
376012                 Wp   =           29
23356
 YDOT =      -4337
065816  meter/sec      RA   =          238
35799  deg
 ZDOT =       5708
984349                 TA   =          313
42367
                                          MA   =          313
51017
                                          Ha   =            229
417  n
mi
                                          Hp   =            222
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14706967
93                 X    =        -4420318
14
 Y    =      -15945621
24  feet           Y    =        -4910005
29  meter
 Z    =       -5190174
77                 Z    =        -1603588
01
 XDOT =       8846
377992                 XDOT =        2716
944045
 YDOT =     -14229
218556  feet/sec       YDOT =       -4306
797852  meter/sec
 ZDOT =      18730
263612                 ZDOT =        5722
131867

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1686095
82                 X    =         -513922
01
 Y    =      -21602378
08  feet           Y    =        -6584404
84  meter
 Z    =       -5290557
53                 Z    =        -1612561
94
 XDOT =      14069
448443                 XDOT =        4288
367886
 YDOT =      -5680
663518  feet/sec       YDOT =       -1731
466240  meter/sec
 ZDOT =      18791
292174                 ZDOT =        5727
585855


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   21043
50315802  
00016717  00000-0  10270-3 0  9023
2 25544  51
6389 239
4307 0002846   3
3491 356
7677 15
48954648 29266


Satellite: ISS
Catalog Number: 25544
Epoch time:      21043
50315802   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:       239
4307  deg
Eccentricity:     
0002846     
Arg of perigee:     3
3491  deg
Mean anomaly:     356
7677  deg
Mean motion:   15
48954648  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2926
Checksum:              323


Coasting Arc #4 (Orbit 2941)
---------------------------------------

Vector Time (GMT): 2021/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942149
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4879845
43                 A    =         6803172
30  meter
 Y    =        4466980
70  meter          E    =           
0012963
 Z    =        1566154
39                 I    =           51
33769
 XDOT =      -2316
395103                 Wp   =          104
74511
 YDOT =       4546
272991  meter/sec      RA   =          233
38885  deg
 ZDOT =      -5712
845092                 TA   =           58
09587
                                          MA   =           57
96984
                                          Ha   =            229
421  n
mi
                                          Hp   =            222
543

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16009991
56                 X    =         4821924
38
 Y    =       14655448
51  feet           Y    =         4521226
87  meter
 Z    =        5138301
80                 Z    =         1589717
09
 XDOT =      -7599
721468                 XDOT =       -2339
311963
 YDOT =      14915
593801  feet/sec       YDOT =        4520
240995  meter/sec
 ZDOT =     -18742
930093                 ZDOT =       -5724
152716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3875493
05                 X    =         1181250
28
 Y    =       21329468
30  feet           Y    =         6501221
94  meter
 Z    =        5247712
05                 Z    =         1599502
63
 XDOT =     -13408
391473                 XDOT =       -4086
877721
 YDOT =       7089
413547  feet/sec       YDOT =        2160
853249  meter/sec
 ZDOT =     -18795
407168                 ZDOT =       -5728
840105


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   21044
53542702  
00016717  00000-0  10270-3 0  9039
2 25544  51
6396 234
3242 0003062   3
6390 356
4781 15
49010189 29423


Satellite: ISS
Catalog Number: 25544
Epoch time:      21044
53542702   =   yrday
fracday
Element set:     903
Inclination:       51
6396  deg
RA of node:       234
3242  deg
Eccentricity:     
0003062     
Arg of perigee:     3
6390  deg
Mean anomaly:     356
4781  deg
Mean motion:   15
49010189  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2942
Checksum:              286


Coasting Arc #5 (Orbit 2956)
---------------------------------------

Vector Time (GMT): 2021/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942149
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5255195
07                 A    =         6803286
87  meter
 Y    =       -4010210
32  meter          E    =           
0010472
 Z    =       -1588064
22                 I    =           51
35858
 XDOT =       1898
512968                 Wp   =           31
38810
 YDOT =      -4739
009523  meter/sec      RA   =          228
42009  deg
 ZDOT =       5710
326868                 TA   =          311
21069
                                          MA   =          311
30092
                                          Ha   =            229
520  n
mi
                                          Hp   =            222
519

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17241453
63                 X    =        -5202247
42
 Y    =      -13156858
00  feet           Y    =        -4068681
74  meter
 Z    =       -5210184
43                 Z    =        -1613462
31
 XDOT =       6228
717088                 XDOT =        1923
628244
 YDOT =     -15547
931507  feet/sec       YDOT =       -4717
638224  meter/sec
 ZDOT =      18734
668202                 ZDOT =        5719
610096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6120050
07                 X    =        -1865391
26
 Y    =      -20776733
12  feet           Y    =        -6332748
26  meter
 Z    =       -5328133
40                 Z    =        -1624015
06
 XDOT =      12586
433877                 XDOT =        3836
345046
 YDOT =      -8501
750635  feet/sec       YDOT =       -2591
333594  meter/sec
 ZDOT =      18777
736518                 ZDOT =        5723
454091


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   21045
50318118  
00016717  00000-0  10270-3 0  9040
2 25544  51
6393 229
5364 0002799  11
3363 348
7849 15
48957792 29577


Satellite: ISS
Catalog Number: 25544
Epoch time:      21045
50318118   =   yrday
fracday
Element set:     904
Inclination:       51
6393  deg
RA of node:       229
5364  deg
Eccentricity:     
0002799     
Arg of perigee:    11
3363  deg
Mean anomaly:     348
7849  deg
Mean motion:   15
48957792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2957
Checksum:              341


Coasting Arc #6 (Orbit 2967)
---------------------------------------

Vector Time (GMT): 2021/046/04:45:06
000
Vector Time (MET): N/A
Weight (LBS)     : 942149
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3598101
22                 A    =         6792629
18  meter
 Y    =        2362274
62  meter          E    =           
0015342
 Z    =       -5267940
02                 I    =           51
34195
 XDOT =      -4930
401000                 Wp   =           84
43034
 YDOT =      -5796
722242  meter/sec      RA   =          224
96499  deg
 ZDOT =        771
568909                 TA   =          192
97193
                                          MA   =          193
01144
                                          Ha   =            229
692  n
mi
                                          Hp   =            222
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11804794
02                 X    =        -3598661
52
 Y    =        7750244
82  feet           Y    =         2322034
60  meter
 Z    =      -17283267
79                 Z    =        -5285419
23
 XDOT =     -16175
856300                 XDOT =       -4868
961586
 YDOT =     -19018
117591  feet/sec       YDOT =       -5851
513966  meter/sec
 ZDOT =       2531
394058                 ZDOT =         747
769165

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4948829
20                 X    =         1508403
14
 Y    =      -13119347
44  feet           Y    =        -3998777
10  meter
 Z    =      -17364406
54                 Z    =        -5292671
11
 XDOT =      23299
616879                 XDOT =        7101
723225
 YDOT =       5599
560556  feet/sec       YDOT =        1706
746057  meter/sec
 ZDOT =       2420
838329                 ZDOT =         737
871523


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   21046
21286629  
00016717  00000-0  10270-3 0  9051
2 25544  51
6421 226
0288 0003126  14
5494 345
5746 15
48959713 29689


Satellite: ISS
Catalog Number: 25544
Epoch time:      21046
21286629   =   yrday
fracday
Element set:     905
Inclination:       51
6421  deg
RA of node:       226
0288  deg
Eccentricity:     
0003126     
Arg of perigee:    14
5494  deg
Mean anomaly:     345
5746  deg
Mean motion:   15
48959713  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2968
Checksum:              324


Coasting Arc #7 (Orbit 2978)
---------------------------------------

Vector Time (GMT): 2021/046/21:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942149
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2872093
34                 A    =         6801143
32  meter
 Y    =        5506354
03  meter          E    =           
0005137
 Z    =       -2777277
77                 I    =           51
38868
 XDOT =      -5691
918271                 Wp   =           87
47736
 YDOT =        400
288401  meter/sec      RA   =          221
52902  deg
 ZDOT =      -5100
594467                 TA   =          124
01906
                                          MA   =          123
97025
                                          Ha   =            229
740  n
mi
                                          Hp   =            222
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9422878
43                 X    =         2823796
26
 Y    =       18065465
98  feet           Y    =         5538201
64  meter
 Z    =       -9111803
71                 Z    =        -2763444
23
 XDOT =     -18674
272543                 XDOT =       -5671
196204
 YDOT =       1313
282156  feet/sec       YDOT =         336
752825  meter/sec
 ZDOT =     -16734
233817                 ZDOT =       -5128
192614

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14327455
58                 X    =         4367008
46
 Y    =      -14527325
14  feet           Y    =        -4427928
70  meter
 Z    =       -9047513
83                 Z    =        -2757682
22
 XDOT =       5831
874858                 XDOT =        1777
555457
 YDOT =      16236
976446  feet/sec       YDOT =        4949
030421  meter/sec
 ZDOT =     -16862
379981                 ZDOT =       -5139
653418


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   21046
92254901  
00016717  00000-0  10270-3 0  9068
2 25544  51
6432 222
5183 0002985  20
9514 339
1758 15
48976188 29791


Satellite: ISS
Catalog Number: 25544
Epoch time:      21046
92254901   =   yrday
fracday
Element set:     906
Inclination:       51
6432  deg
RA of node:       222
5183  deg
Eccentricity:     
0002985     
Arg of perigee:    20
9514  deg
Mean anomaly:     339
1758  deg
Mean motion:   15
48976188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2979
Checksum:              333


Coasting Arc #8 (Orbit 2994)
---------------------------------------

Vector Time (GMT): 2021/047/21:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 942149
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3349208
25                 A    =         6801283
17  meter
 Y    =       -5226008
01  meter          E    =           
0015533
 Z    =        2759883
17                 I    =           51
41345
 XDOT =       5636
446476                 Wp   =           70
03218
 YDOT =       -901
099257  meter/sec      RA   =          216
56569  deg
 ZDOT =       5115
419083                 TA   =          321
28416
                                          MA   =          321
39539
                                          Ha   =            229
913  n
mi
                                          Hp   =            222
277

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10988216
03                 X    =        -3303926
17
 Y    =      -17145695
57  feet           Y    =        -5263207
94  meter
 Z    =        9054734
82                 Z    =         2743724
61
 XDOT =      18492
278466                 XDOT =        5621
256651
 YDOT =      -2956
362391  feet/sec       YDOT =        -838
153108  meter/sec
 ZDOT =      16782
871008                 ZDOT =        5142
761338

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12702916
34                 X    =        -3871848
90
 Y    =       15959512
55  feet           Y    =         4864459
43  meter
 Z    =        8979636
21                 Z    =         2736993
12
 XDOT =      -7521
815776                 XDOT =       -2292
649448
 YDOT =     -15535
372385  feet/sec       YDOT =       -4735
181503  meter/sec
 ZDOT =      16909
834200                 ZDOT =        5154
117464


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   21047
95481743  
00016717  00000-0  10270-3 0  9079
2 25544  51
6415 217
4125 0003128  26
1932 333
9375 15
48945481 29950


Satellite: ISS
Catalog Number: 25544
Epoch time:      21047
95481743   =   yrday
fracday
Element set:     907
Inclination:       51
6415  deg
RA of node:       217
4125  deg
Eccentricity:     
0003128     
Arg of perigee:    26
1932  deg
Mean anomaly:     333
9375  deg
Mean motion:   15
48945481  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2995
Checksum:              323


Coasting Arc #9 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2021/048/06:20:28
000
Vector Time (MET): N/A
Weight (LBS)     : 958060
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3937284
65                 A    =         6793358
06  meter
 Y    =        2212816
29  meter          E    =           
0014031
 Z    =       -5086779
10                 I    =           51
39964
 XDOT =      -5225
963886                 Wp   =           90
59996
 YDOT =      -5308
448146  meter/sec      RA   =          214
70305  deg
 ZDOT =       1739
804816                 TA   =          196
29638
                                          MA   =          196
34155
                                          Ha   =            229
722  n
mi
                                          Hp   =            222
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12917600
56                 X    =        -3937028
21
 Y    =        7259895
97  feet           Y    =         2168787
92  meter
 Z    =      -16688907
81                 Z    =        -5105904
01
 XDOT =     -17145
550808                 XDOT =       -5174
665612
 YDOT =     -17416
168459  feet/sec       YDOT =       -5366
601733  meter/sec
 ZDOT =       5708
021049                 ZDOT =        1714
544460

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -311737
27                 X    =          -95017
52
 Y    =      -14714000
46  feet           Y    =        -4484827
34  meter
 Z    =      -16777697
92                 Z    =        -5113842
33
 XDOT =      22413
118192                 XDOT =        6831
518425
 YDOT =      -6834
603381  feet/sec       YDOT =       -2083
187111  meter/sec
 ZDOT =       5590
646895                 ZDOT =        1704
029174


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
27740025  
00016717  00000-0  10270-3 0  9087
2 25544  51
6435 215
8189 0003090  19
6400 340
4868 15
48976521 30006


Satellite: ISS
Catalog Number: 25544
Epoch time:      21048
27740025   =   yrday
fracday
Element set:     908
Inclination:       51
6435  deg
RA of node:       215
8189  deg
Eccentricity:     
0003090     
Arg of perigee:    19
6400  deg
Mean anomaly:     340
4868  deg
Mean motion:   15
48976521  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3000
Checksum:              297


Coasting Arc #10 (Orbit 3015)
---------------------------------------

Vector Time (GMT): 2021/049/06:20:28
000
Vector Time (MET): N/A
Weight (LBS)     : 958060
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3733273
62                 A    =         6793256
11  meter
 Y    =       -2530064
45  meter          E    =           
0007937
 Z    =        5077180
98                 I    =           51
42905
 XDOT =       5672
018004                 Wp   =           42
87542
 YDOT =       4846
497811  meter/sec      RA   =          209
74241  deg
 ZDOT =      -1748
232411                 TA   =           64
13193
                                          MA   =           64
05012
                                          Ha   =            229
579  n
mi
                                          Hp   =            222
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12248273
02                 X    =         3736626
48
 Y    =       -8300736
37  feet           Y    =        -2488297
36  meter
 Z    =       16657417
93                 Z    =         5095323
70
 XDOT =      18608
982953                 XDOT =        5625
893203
 YDOT =      15900
583370  feet/sec       YDOT =        4909
668445  meter/sec
 ZDOT =      -5735
670640                 ZDOT =       -1720
792627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1796693
14                 X    =          547632
07
 Y    =       14590444
16  feet           Y    =         4447167
38  meter
 Z    =       16741649
30                 Z    =         5102854
71
 XDOT =     -21627
097114                 XDOT =       -6591
939200
 YDOT =       9125
631258  feet/sec       YDOT =        2781
492408  meter/sec
 ZDOT =      -5608
161077                 ZDOT =       -1709
367496


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
30966447  
00016717  00000-0  10270-3 0  9091
2 25544  51
6442 210
7131 0003092  20
7683 339
3592 15
49012003 30168


Satellite: ISS
Catalog Number: 25544
Epoch time:      21049
30966447   =   yrday
fracday
Element set:     909
Inclination:       51
6442  deg
RA of node:       210
7131  deg
Eccentricity:     
0003092     
Arg of perigee:    20
7683  deg
Mean anomaly:     339
3592  deg
Mean motion:   15
49012003  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3016
Checksum:              283


Coasting Arc #11 (Orbit 3030)
---------------------------------------

Vector Time (GMT): 2021/050/06:20:28
000
Vector Time (MET): N/A
Weight (LBS)     : 958060
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3492880
30                 A    =         6793325
59  meter
 Y    =        2854909
86  meter          E    =           
0014382
 Z    =       -5091767
71                 I    =           51
45883
 XDOT =      -6064
470031                 Wp   =           90
67553
 YDOT =      -4325
756110  meter/sec      RA   =          204
78355  deg
 ZDOT =       1738
832000                 TA   =          196
19685
                                          MA   =          196
24287
                                          Ha   =            229
822  n
mi
                                          Hp   =            222
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11459581
02                 X    =        -3499812
66
 Y    =        9366502
15  feet           Y    =         2815811
08  meter
 Z    =      -16705274
63                 Z    =        -5108751
38
 XDOT =     -19896
555219                 XDOT =       -6024
093501
 YDOT =     -14192
113223  feet/sec       YDOT =       -4393
347592  meter/sec
 ZDOT =       5704
829397                 ZDOT =        1709
471797

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3352712
16                 X    =        -1021906
67
 Y    =      -14323826
24  feet           Y    =        -4365902
24  meter
 Z    =      -16784125
93                 Z    =        -5115801
58
 XDOT =      20525
015872                 XDOT =        6256
024838
 YDOT =     -11313
314537  feet/sec       YDOT =       -3448
298271  meter/sec
 ZDOT =       5568
386222                 ZDOT =        1697
244120


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
27741283  
00016717  00000-0  10270-3 0  9100
2 25544  51
6439 205
9262 0003203  25
4231 334
7076 15
48985039 30310


Satellite: ISS
Catalog Number: 25544
Epoch time:      21050
27741283   =   yrday
fracday
Element set:     910
Inclination:       51
6439  deg
RA of node:       205
9262  deg
Eccentricity:     
0003203     
Arg of perigee:    25
4231  deg
Mean anomaly:     334
7076  deg
Mean motion:   15
48985039  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3031
Checksum:              284


Coasting Arc #12 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2021/050/19:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 958060
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         827668
26                 A    =         6792583
20  meter
 Y    =       -4195789
61  meter          E    =           
0004629
 Z    =        5273243
04                 I    =           51
47133
 XDOT =       7264
535945                 Wp   =           76
41470
 YDOT =       2333
996891  meter/sec      RA   =          202
10505  deg
 ZDOT =        717
423663                 TA   =            6
71585
                                          MA   =            6
70965
                                          Ha   =            229
879  n
mi
                                          Hp   =            222
105

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2715447
05                 X    =          848911
35
 Y    =      -13765713
94  feet           Y    =        -4186415
18  meter
 Z    =       17300666
13                 Z    =         5277315
11
 XDOT =      23833
779347                 XDOT =        7234
411787
 YDOT =       7657
470114  feet/sec       YDOT =        2415
065746  meter/sec
 ZDOT =       2353
752174                 ZDOT =         752
638184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13109383
59                 X    =        -3995740
12
 Y    =       -4935564
63  feet           Y    =        -1504360
10  meter
 Z    =       17319522
09                 Z    =         5278990
33
 XDOT =      11297
543335                 XDOT =        3443
491209
 YDOT =     -21179
827646  feet/sec       YDOT =       -6455
611466  meter/sec
 ZDOT =       2517
374544                 ZDOT =         767
295761


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
85806106  
00016717  00000-0  10270-3 0  9111
2 25544  51
6421 203
0526 0003122  33
0682 327
0662 15
48975809 30408


Satellite: ISS
Catalog Number: 25544
Epoch time:      21050
85806106   =   yrday
fracday
Element set:     911
Inclination:       51
6421  deg
RA of node:       203
0526  deg
Eccentricity:     
0003122     
Arg of perigee:    33
0682  deg
Mean anomaly:     327
0662  deg
Mean motion:   15
48975809  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3040
Checksum:              273


Coasting Arc #13 (Orbit 3053)
---------------------------------------

Vector Time (GMT): 2021/051/17:36:44
000
Vector Time (MET): N/A
Weight (LBS)     : 958060
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5163031
93                 A    =         6801881
93  meter
 Y    =        3682568
72  meter          E    =           
0005962
 Z    =       -2461899
58                 I    =           51
53131
 XDOT =      -4642
107752                 Wp   =          103
26552
 YDOT =       2962
769325  meter/sec      RA   =          197
53312  deg
 ZDOT =      -5315
748411                 TA   =          104
26464
                                          MA   =          104
19842
                                          Ha   =            229
946  n
mi
                                          Hp   =            222
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16939081
13                 X    =         5133426
89
 Y    =       12081918
37  feet           Y    =         3740139
93  meter
 Z    =       -8077098
37                 Z    =        -2436891
93
 XDOT =     -15230
012310                 XDOT =       -4649
072909
 YDOT =       9720
371802  feet/sec       YDOT =        2910
818982  meter/sec
 ZDOT =     -17440
119460                 ZDOT =       -5338
314487

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19746155
71                 X    =         6018628
26
 Y    =       -6697676
98  feet           Y    =        -2041451
94  meter
 Z    =       -7960854
02                 Z    =        -2426468
31
 XDOT =      -1460
507409                 XDOT =        -445
162658
 YDOT =      16499
638571  feet/sec       YDOT =        5029
089837  meter/sec
 ZDOT =     -17544
919262                 ZDOT =       -5347
691391


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
76129209  
00016717  00000-0  10270-3 0  9125
2 25544  51
6417 198
5850 0002989  36
1972 323
9380 15
48970247 30545


Satellite: ISS
Catalog Number: 25544
Epoch time:      21051
76129209   =   yrday
fracday
Element set:     912
Inclination:       51
6417  deg
RA of node:       198
5850  deg
Eccentricity:     
0002989     
Arg of perigee:    36
1972  deg
Mean anomaly:     323
9380  deg
Mean motion:   15
48970247  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3054
Checksum:              324


Coasting Arc #14 (Orbit 3069)
---------------------------------------

Vector Time (GMT): 2021/052/17:36:44
000
Vector Time (MET): N/A
Weight (LBS)     : 958060
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5467900
67                 A    =         6801975
57  meter
 Y    =       -3206959
47  meter          E    =           
0016334
 Z    =        2443364
51                 I    =           51
56419
 XDOT =       4363
195292                 Wp   =           68
21269
 YDOT =      -3360
695532  meter/sec      RA   =          192
57974  deg
 ZDOT =       5330
480870                 TA   =          319
11991
                                          MA   =          319
24231
                                          Ha   =            230
055  n
mi
                                          Hp   =            222
093

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17939306
66                 X    =        -5443501
32
 Y    =      -10521520
57  feet           Y    =        -3267969
08  meter
 Z    =        8016287
75                 Z    =         2416863
34
 XDOT =      14314
945184                 XDOT =        4374
559423
 YDOT =     -11025
903976  feet/sec       YDOT =       -3311
839644  meter/sec
 ZDOT =      17488
454297                 ZDOT =        5351
702715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18919337
15                 X    =        -5766613
96
 Y    =        8748702
99  feet           Y    =         2666604
67  meter
 Z    =        7893089
76                 Z    =         2405813
76
 XDOT =       -293
121621                 XDOT =         -89
343470
 YDOT =     -16569
312944  feet/sec       YDOT =       -5050
326585  meter/sec
 ZDOT =      17587
016125                 ZDOT =        5360
522515


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
79355489  
00016717  00000-0  10270-3 0  9131
2 25544  51
6416 193
4791 0003068  38
9305 321
2065 15
48954691 30705


Satellite: ISS
Catalog Number: 25544
Epoch time:      21052
79355489   =   yrday
fracday
Element set:     913
Inclination:       51
6416  deg
RA of node:       193
4791  deg
Eccentricity:     
0003068     
Arg of perigee:    38
9305  deg
Mean anomaly:     321
2065  deg
Mean motion:   15
48954691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3070
Checksum:              320


Coasting Arc #15 (Orbit 3079)
---------------------------------------

Vector Time (GMT): 2021/053/09:36:25
000
Vector Time (MET): N/A
Weight (LBS)     : 973191
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5957750
18                 A    =         6800561
74  meter
 Y    =       -1403343
08  meter          E    =           
0014848
 Z    =        2951567
96                 I    =           51
58018
 XDOT =       3565
383903                 Wp   =           87
75683
 YDOT =       4590
716493  meter/sec      RA   =          189
23265  deg
 ZDOT =      -4991
720157                 TA   =           58
57424
                                          MA   =           58
42914
                                          Ha   =            229
853  n
mi
                                          Hp   =            222
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19546424
49                 X    =         5958663
30
 Y    =       -4604143
95  feet           Y    =        -1336714
14  meter
 Z    =        9683621
91                 Z    =         2980509
94
 XDOT =      11697
453750                 XDOT =        3538
030506
 YDOT =      15061
405818  feet/sec       YDOT =        4630
434302  meter/sec
 ZDOT =     -16377
034637                 ZDOT =       -4974
467684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12598278
95                 X    =         3839955
42
 Y    =       15553828
98  feet           Y    =         4740807
07  meter
 Z    =        9818103
53                 Z    =         2992557
95
 XDOT =      -7312
353662                 XDOT =       -2228
805396
 YDOT =      16255
550891  feet/sec       YDOT =        4954
691911  meter/sec
 ZDOT =     -16296
780977                 ZDOT =       -4967
258842


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
43871668  
00016717  00000-0  10270-3 0  9146
2 25544  51
6395 190
2850 0002957  37
8203 322
3154 15
48981486 30807


Satellite: ISS
Catalog Number: 25544
Epoch time:      21053
43871668   =   yrday
fracday
Element set:     914
Inclination:       51
6395  deg
RA of node:       190
2850  deg
Eccentricity:     
0002957     
Arg of perigee:    37
8203  deg
Mean anomaly:     322
3154  deg
Mean motion:   15
48981486  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3080
Checksum:              317


Coasting Arc #16 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2021/054/01:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 973191
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         203369
16                 A    =         6792520
53  meter
 Y    =        4253518
68  meter          E    =           
0017143
 Z    =       -5306762
02                 I    =           51
57844
 XDOT =      -7618
630263                 Wp   =           77
64864
 YDOT =       -344
663599  meter/sec      RA   =          185
96628  deg
 ZDOT =       -566
195859                 TA   =          186
91692
                                          MA   =          186
94061
                                          Ha   =            230
066  n
mi
                                          Hp   =            221
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         667221
65                 X    =          181566
47
 Y    =       13955113
77  feet           Y    =         4255671
04  meter
 Z    =      -17410636
55                 Z    =        -5305827
07
 XDOT =     -24995
506112                 XDOT =       -7611
459714
 YDOT =      -1130
786086  feet/sec       YDOT =        -429
820519  meter/sec
 ZDOT =      -1857
597964                 ZDOT =        -603
185852

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         124358
79                 X    =           37904
56
 Y    =      -13976004
62  feet           Y    =        -4259886
21  meter
 Z    =      -17406219
58                 Z    =        -5305415
73
 XDOT =      23836
116328                 XDOT =        7265
248257
 YDOT =       2748
031410  feet/sec       YDOT =         837
599974  meter/sec
 ZDOT =      -2029
529771                 ZDOT =        -618
600674


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
08388071  
00016717  00000-0  10270-3 0  9150
2 25544  51
6424 187
0974 0003355  39
5727 320
5668 15
48979758 30904


Satellite: ISS
Catalog Number: 25544
Epoch time:      21054
08388071   =   yrday
fracday
Element set:     915
Inclination:       51
6424  deg
RA of node:       187
0974  deg
Eccentricity:     
0003355     
Arg of perigee:    39
5727  deg
Mean anomaly:     320
5668  deg
Mean motion:   15
48979758  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3090
Checksum:              338


Coasting Arc #17 (Orbit 3105)
---------------------------------------

Vector Time (GMT): 2021/055/01:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 973191
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -564744
39                 A    =         6792413
52  meter
 Y    =       -4207848
21  meter          E    =           
0004966
 Z    =        5297796
08                 I    =           51
61226
 XDOT =       7636
903727                 Wp   =           76
17240
 YDOT =       -312
854817  meter/sec      RA   =          181
01931  deg
 ZDOT =        566
317687                 TA   =            8
42250
                                          MA   =            8
41417
                                          Ha   =            230
015  n
mi
                                          Hp   =            221
890

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1852835
92                 X    =         -543381
89
 Y    =      -13805276
29  feet           Y    =        -4214044
14  meter
 Z    =       17381220
72                 Z    =         5295104
74
 XDOT =      25055
458423                 XDOT =        7637
083812
 YDOT =      -1026
426565  feet/sec       YDOT =        -227
452443  meter/sec
 ZDOT =       1857
997662                 ZDOT =         603
414149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1307283
07                 X    =          398459
88
 Y    =       13883335
72  feet           Y    =         4231640
73  meter
 Z    =       17368635
19                 Z    =         5293960
01
 XDOT =     -24050
084558                 XDOT =       -7330
465773
 YDOT =       -272
630748  feet/sec       YDOT =         -83
097852  meter/sec
 ZDOT =       2030
442156                 ZDOT =         618
878769


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
11613879  
00016717  00000-0  10270-3 0  9163
2 25544  51
6423 181
9925 0003259  41
4535 318
6862 15
49010391 31066


Satellite: ISS
Catalog Number: 25544
Epoch time:      21055
11613879   =   yrday
fracday
Element set:     916
Inclination:       51
6423  deg
RA of node:       181
9925  deg
Eccentricity:     
0003259     
Arg of perigee:    41
4535  deg
Mean anomaly:     318
6862  deg
Mean motion:   15
49010391  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3106
Checksum:              303


Coasting Arc #18 (Orbit 3120)
---------------------------------------

Vector Time (GMT): 2021/056/01:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 973191
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         931430
28                 A    =         6792496
73  meter
 Y    =        4148982
85  meter          E    =           
0017385
 Z    =       -5311882
94                 I    =           51
64721
 XDOT =      -7564
273774                 Wp   =           78
68240
 YDOT =        969
303316  meter/sec      RA   =          176
07359  deg
 ZDOT =       -567
537454                 TA   =          185
87695
                                          MA   =          185
89737
                                          Ha   =            230
128  n
mi
                                          Hp   =            221
836

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3055873
61                 X    =          910767
13
 Y    =       13612148
47  feet           Y    =         4159283
14  meter
 Z    =      -17427437
48                 Z    =        -5307408
83
 XDOT =     -24817
171174                 XDOT =       -7571
793948
 YDOT =       3180
128989  feet/sec       YDOT =         884
672089  meter/sec
 ZDOT =      -1861
999521                 ZDOT =        -604
298859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2754616
53                 X    =         -839607
12
 Y    =      -13702859
21  feet           Y    =        -4176631
49  meter
 Z    =      -17406558
07                 Z    =        -5305518
90
 XDOT =      23890
786759                 XDOT =        7281
911804
 YDOT =      -2212
988173  feet/sec       YDOT =        -674
518795  meter/sec
 ZDOT =      -2032
901642                 ZDOT =        -619
628421


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
08388332  
00016717  00000-0  10270-3 0  9174
2 25544  51
6432 177
2058 0003375  46
2935 313
8495 15
48987982 31211


Satellite: ISS
Catalog Number: 25544
Epoch time:      21056
08388332   =   yrday
fracday
Element set:     917
Inclination:       51
6432  deg
RA of node:       177
2058  deg
Eccentricity:     
0003375     
Arg of perigee:    46
2935  deg
Mean anomaly:     313
8495  deg
Mean motion:   15
48987982  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3121
Checksum:              329
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