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

 
Date: January 21st 2021

  • spaceflight nasa gov will be taken offline in the next 30 days *
  • *
  • 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 will be provided in xml and txt formats *
  • Links to the OEMs and more details to follow *
  • *

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 0 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


021/16:17:19 647 2 1 2 2 2 2
N/A -0 8 -0 2 228 4
000/00:06:39 293 -0 1 0 0 223 7

026/07:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 223 5

029/19:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 223 3

Coasting Arc #1 (Orbit 2491)
---------------------------------------

Vector Time (GMT): 2021/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6510864
80                 A    =         6801894
24  meter
 Y    =         457805
22  meter          E    =           
0007032
 Z    =       -1905704
74                 I    =           51
77665
 XDOT =       1286
262541                 Wp   =           38
54321
 YDOT =       5038
620682  meter/sec      RA   =           17
31648  deg
 ZDOT =       5621
494987                 TA   =          300
55539
                                          MA   =          300
62477
                                          Ha   =            228
593  n
mi
                                          Hp   =            222
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21361105
00                 X    =         6514518
12
 Y    =        1501985
63  feet           Y    =          530634
98  meter
 Z    =       -6252312
15                 Z    =        -1874069
60
 XDOT =       4220
021461                 XDOT =        1202
518414
 YDOT =      16530
907750  feet/sec       YDOT =        5052
535889  meter/sec
 ZDOT =      18443
225024                 ZDOT =        5627
539974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7421773
80                 X    =         2262156
65
 Y    =       20131692
47  feet           Y    =         6136139
86  meter
 Z    =       -6105440
77                 Z    =        -1860938
35
 XDOT =     -11923
799039                 XDOT =       -3634
373947
 YDOT =       9980
789557  feet/sec       YDOT =        3042
144657  meter/sec
 ZDOT =      18471
023355                 ZDOT =        5629
967919


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   21015
50366467  
00016717  00000-0  10270-3 0  9003
2 25544  51
6428  17
9288 0000133 218
1715 141
9426 15
49314799 24921


Satellite: ISS
Catalog Number: 25544
Epoch time:      21015
50366467   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:        17
9288  deg
Eccentricity:     
0000133     
Arg of perigee:   218
1715  deg
Mean anomaly:     141
9426  deg
Mean motion:   15
49314799  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2492
Checksum:              308


Coasting Arc #2 (Orbit 2507)
---------------------------------------

Vector Time (GMT): 2021/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6555741
62                 A    =         6802087
19  meter
 Y    =           6351
29  meter          E    =           
0013601
 Z    =        1789676
68                 I    =           51
74361
 XDOT =      -1559
393395                 Wp   =          114
51942
 YDOT =      -4916
458751  meter/sec      RA   =           12
37528  deg
 ZDOT =      -5666
362146                 TA   =           45
88492
                                          MA   =           45
77310
                                          Ha   =            228
524  n
mi
                                          Hp   =            222
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21508338
64                 X    =        -6564018
37
 Y    =          20837
58  feet           Y    =          -67006
11  meter
 Z    =        5871642
65                 Z    =         1757812
32
 XDOT =      -5116
120063                 XDOT =       -1476
777051
 YDOT =     -16130
114011  feet/sec       YDOT =       -4933
434744  meter/sec
 ZDOT =     -18590
426988                 ZDOT =       -5673
736471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9206090
99                 X    =        -2806016
53
 Y    =      -19482620
13  feet           Y    =        -5938302
61  meter
 Z    =        5723692
36                 Z    =         1744581
43
 XDOT =      11044
009315                 XDOT =        3366
214039
 YDOT =     -10718
235106  feet/sec       YDOT =       -3266
918060  meter/sec
 ZDOT =     -18624
404554                 ZDOT =       -5676
718508


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   21016
53571202  
00016717  00000-0  10270-3 0  9013
2 25544  51
6420  12
8209 0000305 299
3247  60
7873 15
49311686 25086


Satellite: ISS
Catalog Number: 25544
Epoch time:      21016
53571202   =   yrday
fracday
Element set:     901
Inclination:       51
6420  deg
RA of node:        12
8209  deg
Eccentricity:     
0000305     
Arg of perigee:   299
3247  deg
Mean anomaly:      60
7873  deg
Mean motion:   15
49311686  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2508
Checksum:              283


Coasting Arc #3 (Orbit 2522)
---------------------------------------

Vector Time (GMT): 2021/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6562669
94                 A    =         6802206
60  meter
 Y    =        -501701
11  meter          E    =           
0007698
 Z    =       -1705608
48                 I    =           51
71095
 XDOT =       1840
677443                 Wp   =           36
67060
 YDOT =       4775
658986  meter/sec      RA   =            7
43302  deg
 ZDOT =       5696
940577                 TA   =          304
69058
                                          MA   =          304
76309
                                          Ha   =            228
577  n
mi
                                          Hp   =            222
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21531069
37                 X    =         6576077
01
 Y    =       -1646001
03  feet           Y    =         -428237
58  meter
 Z    =       -5595828
34                 Z    =        -1673697
93
 XDOT =       6038
967989                 XDOT =        1759
466054
 YDOT =      15668
172526  feet/sec       YDOT =        4795
788452  meter/sec
 ZDOT =      18690
749926                 ZDOT =        5705
684576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11006970
72                 X    =         3354924
68
 Y    =       18622010
31  feet           Y    =         5675988
74  meter
 Z    =       -5447649
94                 Z    =        -1660443
70
 XDOT =     -10087
163802                 XDOT =       -3074
567527
 YDOT =      11422
769913  feet/sec       YDOT =        3481
660269  meter/sec
 ZDOT =      18731
093422                 ZDOT =        5709
237275


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   21017
50325542  
00016717  00000-0  10270-3 0  9026
2 25544  51
6424   8
0337 0000144 271
4844  88
6289 15
49309747 25236


Satellite: ISS
Catalog Number: 25544
Epoch time:      21017
50325542   =   yrday
fracday
Element set:     902
Inclination:       51
6424  deg
RA of node:         8
0337  deg
Eccentricity:     
0000144     
Arg of perigee:   271
4844  deg
Mean anomaly:      88
6289  deg
Mean motion:   15
49309747  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2523
Checksum:              296


Coasting Arc #4 (Orbit 2538)
---------------------------------------

Vector Time (GMT): 2021/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6536854
92                 A    =         6802352
29  meter
 Y    =         970318
39  meter          E    =           
0013472
 Z    =        1585439
62                 I    =           51
67809
 XDOT =      -2086
531419                 Wp   =          116
53136
 YDOT =      -4629
704013  meter/sec      RA   =            2
48729  deg
 ZDOT =      -5737
530020                 TA   =           46
16957
                                          MA   =           46
05828
                                          Ha   =            228
506  n
mi
                                          Hp   =            222
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21446374
41                 X    =        -6554920
46
 Y    =        3183459
28  feet           Y    =          897117
51  meter
 Z    =        5201573
54                 Z    =         1553643
05
 XDOT =      -6845
575521                 XDOT =       -2006
736617
 YDOT =     -15189
317628  feet/sec       YDOT =       -4652
590760  meter/sec
 ZDOT =     -18823
917390                 ZDOT =       -5747
471680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12653040
30                 X    =        -3856646
68
 Y    =      -17649257
33  feet           Y    =        -5379493
63  meter
 Z    =        5053913
56                 Z    =         1540432
85
 XDOT =       9151
879973                 XDOT =        2789
493016
 YDOT =     -11995
393689  feet/sec       YDOT =       -3656
195996  meter/sec
 ZDOT =     -18869
826663                 ZDOT =       -5751
523167


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   21018
53529845  
00016717  00000-0  10270-3 0  9033
2 25544  51
6428   2
9257 0000416 319
8333  40
2787 15
49317629 25398


Satellite: ISS
Catalog Number: 25544
Epoch time:      21018
53529845   =   yrday
fracday
Element set:     903
Inclination:       51
6428  deg
RA of node:         2
9257  deg
Eccentricity:     
0000416     
Arg of perigee:   319
8333  deg
Mean anomaly:      40
2787  deg
Mean motion:   15
49317629  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2539
Checksum:              315


Coasting Arc #5 (Orbit 2553)
---------------------------------------

Vector Time (GMT): 2021/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6468097
76                 A    =         6802479
18  meter
 Y    =       -1464422
06  meter          E    =           
0008474
 Z    =       -1498105
72                 I    =           51
64364
 XDOT =       2340
973545                 Wp   =           35
43004
 YDOT =       4465
765977  meter/sec      RA   =          357
54069  deg
 ZDOT =       5764
956399                 TA   =          308
25049
                                          MA   =          308
32672
                                          Ha   =            228
566  n
mi
                                          Hp   =            222
342

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21220793
17                 X    =         6491269
44
 Y    =       -4804534
33  feet           Y    =        -1391961
53  meter
 Z    =       -4915045
02                 Z    =        -1466630
65
 XDOT =       7680
359401                 XDOT =        2262
859720
 YDOT =      14651
463179  feet/sec       YDOT =        4491
507478  meter/sec
 ZDOT =      18913
898947                 ZDOT =        5776
138126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14276001
38                 X    =         4351325
22
 Y    =       16462593
48  feet           Y    =         5017798
49  meter
 Z    =       -4768865
77                 Z    =        -1453550
29
 XDOT =      -8146
535166                 XDOT =       -2483
063919
 YDOT =      12535
777052  feet/sec       YDOT =        3820
904845  meter/sec
 ZDOT =      18965
570196                 ZDOT =        5780
705796


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   21019
50283862  
00016717  00000-0  10270-3 0  9048
2 25544  51
6420 358
1388 0000270 320
0395  40
0735 15
49309460 25543


Satellite: ISS
Catalog Number: 25544
Epoch time:      21019
50283862   =   yrday
fracday
Element set:     904
Inclination:       51
6420  deg
RA of node:       358
1388  deg
Eccentricity:     
0000270     
Arg of perigee:   320
0395  deg
Mean anomaly:      40
0735  deg
Mean motion:   15
49309460  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2554
Checksum:              285


Coasting Arc #6 (Orbit 2569)
---------------------------------------

Vector Time (GMT): 2021/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6370580
91                 A    =         6802628
99  meter
 Y    =        1927281
22  meter          E    =           
0013298
 Z    =        1375328
29                 I    =           51
61047
 XDOT =      -2561
250129                 Wp   =          119
02274
 YDOT =      -4301
162823  meter/sec      RA   =          352
59072  deg
 ZDOT =      -5800
303410                 TA   =           46
01518
                                          MA   =           45
90561
                                          Ha   =            228
495  n
mi
                                          Hp   =            222
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20900856
01                 X    =        -6398339
33
 Y    =        6323101
11  feet           Y    =         1855885
53  meter
 Z    =        4512231
92                 Z    =         1344315
69
 XDOT =      -8403
051604                 XDOT =       -2484
788796
 YDOT =     -14111
426584  feet/sec       YDOT =       -4329
376818  meter/sec
 ZDOT =     -19029
866831                 ZDOT =       -5812
559205

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15725596
44                 X    =        -4793161
80
 Y    =      -15192503
73  feet           Y    =        -4630675
14  meter
 Z    =        4368188
81                 Z    =         1331423
95
 XDOT =       7180
788625                 XDOT =        2188
704373
 YDOT =     -12955
834631  feet/sec       YDOT =       -3948
938395  meter/sec
 ZDOT =     -19086
528430                 ZDOT =       -5817
573866


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   21020
53488036  
00016717  00000-0  10270-3 0  9054
2 25544  51
6423 353
0312 0000493 320
8755  39
2360 15
49309423 25703


Satellite: ISS
Catalog Number: 25544
Epoch time:      21020
53488036   =   yrday
fracday
Element set:     905
Inclination:       51
6423  deg
RA of node:       353
0312  deg
Eccentricity:     
0000493     
Arg of perigee:   320
8755  deg
Mean anomaly:      39
2360  deg
Mean motion:   15
49309423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2570
Checksum:              281


Coasting Arc #7 (Orbit 2584)
---------------------------------------

Vector Time (GMT): 2021/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6226632
29                 A    =         6802707
45  meter
 Y    =       -2408109
34  meter          E    =           
0009143
 Z    =       -1285060
65                 I    =           51
57763
 XDOT =       2789
080587                 Wp   =           35
07021
 YDOT =       4118
491842  meter/sec      RA   =          347
63897  deg
 ZDOT =       5824
415113                 TA   =          310
96869
                                          MA   =          311
04777
                                          Ha   =            228
533  n
mi
                                          Hp   =            222
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20428583
61                 X    =         6259339
72
 Y    =       -7900621
20  feet           Y    =        -2338295
71  meter
 Z    =       -4216078
23                 Z    =        -1254735
24
 XDOT =       9150
526861                 XDOT =        2714
527824
 YDOT =      13512
112342  feet/sec       YDOT =        4149
264208  meter/sec
 ZDOT =      19108
973467                 ZDOT =        5837
782302

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17110175
77                 X    =         5215181
58
 Y    =       13717021
99  feet           Y    =         4180948
30  meter
 Z    =       -4075211
91                 Z    =        -1242124
59
 XDOT =      -6151
110424                 XDOT =       -1874
858457
 YDOT =      13339
990614  feet/sec       YDOT =        4066
029139  meter/sec
 ZDOT =      19170
799168                 ZDOT =        5843
259587


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   21021
50241760  
00016717  00000-0  10270-3 0  9064
2 25544  51
6426 348
2437 0000393 322
3345  37
7778 15
49313651 25851


Satellite: ISS
Catalog Number: 25544
Epoch time:      21021
50241760   =   yrday
fracday
Element set:     906
Inclination:       51
6426  deg
RA of node:       348
2437  deg
Eccentricity:     
0000393     
Arg of perigee:   322
3345  deg
Mean anomaly:      37
7778  deg
Mean motion:   15
49313651  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2585
Checksum:              299


Coasting Arc #8 (Orbit 2587)
---------------------------------------

Vector Time (GMT): 2021/021/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -229477
64                 A    =         6792790
90  meter
 Y    =       -4265169
07  meter          E    =           
0012362
 Z    =       -5292616
43                 I    =           51
53803
 XDOT =       7522
156989                 Wp   =           94
80719
 YDOT =      -1229
035329  meter/sec      RA   =          346
74859  deg
 ZDOT =        664
629789                 TA   =          181
56053
                                          MA   =          181
56439
                                          Ha   =            228
434  n
mi
                                          Hp   =            223
684

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -752879
40                 X    =         -156058
05
 Y    =      -13993336
85  feet           Y    =        -4267324
47  meter
 Z    =      -17364227
15                 Z    =        -5293553
03
 XDOT =      24678
992745                 XDOT =        7532
113034
 YDOT =      -4032
268140  feet/sec       YDOT =       -1144
861521  meter/sec
 ZDOT =       2180
543928                 ZDOT =         701
193054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1973363
94                 X    =         -601481
33
 Y    =      -13868770
20  feet           Y    =        -4227201
16  meter
 Z    =      -17368354
44                 Z    =        -5293874
43
 XDOT =      23151
400854                 XDOT =        7056
546980
 YDOT =      -6236
173727  feet/sec       YDOT =       -1900
785752  meter/sec
 ZDOT =       2350
297476                 ZDOT =         716
370671


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   21021
69592566  
00016717  00000-0  10270-3 0  9078
2 25544  51
6461 347
2867 0002206 276
9398  83
1501 15
48900165 25886


Satellite: ISS
Catalog Number: 25544
Epoch time:      21021
69592566   =   yrday
fracday
Element set:     907
Inclination:       51
6461  deg
RA of node:       347
2867  deg
Eccentricity:     
0002206     
Arg of perigee:   276
9398  deg
Mean anomaly:      83
1501  deg
Mean motion:   15
48900165  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2588
Checksum:              328


Coasting Arc #9 (Orbit 2603)
---------------------------------------

Vector Time (GMT): 2021/022/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         630236
04                 A    =         6792696
31  meter
 Y    =        4218427
16  meter          E    =           
0001862
 Z    =        5286376
50                 I    =           51
50522
 XDOT =      -7393
834970                 Wp   =           14
84223
 YDOT =       1900
994687  meter/sec      RA   =          341
79638  deg
 ZDOT =       -633
661026                 TA   =           81
23505
                                          MA   =           81
21397
                                          Ha   =            228
368  n
mi
                                          Hp   =            223
683

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2067703
56                 X    =          557339
64
 Y    =       13839984
11  feet           Y    =         4225066
97  meter
 Z    =       17343754
92                 Z    =         5289261
13
 XDOT =     -24257
988747                 XDOT =       -7411
465031
 YDOT =       6236
859208  feet/sec       YDOT =        1818
212968  meter/sec
 ZDOT =      -2078
940374                 ZDOT =        -669
619561

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3500793
21                 X    =         1067041
77
 Y    =       13531738
60  feet           Y    =         4124473
92  meter
 Z    =       17356926
29                 Z    =         5290391
13
 XDOT =     -22395
803218                 XDOT =       -6826
240821
 YDOT =       8682
420236  feet/sec       YDOT =        2646
401688  meter/sec
 ZDOT =      -2245
910021                 ZDOT =        -684
553375


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   21022
72824315  
00016717  00000-0  10270-3 0  9084
2 25544  51
6461 342
1813 0002271 281
5957  78
4938 15
48924581 26044


Satellite: ISS
Catalog Number: 25544
Epoch time:      21022
72824315   =   yrday
fracday
Element set:     908
Inclination:       51
6461  deg
RA of node:       342
1813  deg
Eccentricity:     
0002271     
Arg of perigee:   281
5957  deg
Mean anomaly:      78
4938  deg
Mean motion:   15
48924581  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2604
Checksum:              312


Coasting Arc #10 (Orbit 2618)
---------------------------------------

Vector Time (GMT): 2021/023/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1032175
83                 A    =         6792746
64  meter
 Y    =       -4143039
42  meter          E    =           
0012446
 Z    =       -5293957
02                 I    =           51
47264
 XDOT =       7186
601604                 Wp   =           92
46615
 YDOT =      -2555
093136  meter/sec      RA   =          336
84213  deg
 ZDOT =        599
120646                 TA   =          183
27462
                                          MA   =          183
28278
                                          Ha   =            228
465  n
mi
                                          Hp   =            223
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3386403
65                 X    =         -960055
77
 Y    =      -13592649
00  feet           Y    =        -4154178
26  meter
 Z    =      -17368625
39                 Z    =        -5298796
03
 XDOT =      23578
089251                 XDOT =        7211
729173
 YDOT =      -8382
851496  feet/sec       YDOT =       -2474
586936  meter/sec
 ZDOT =       1965
618916                 ZDOT =         634
090631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5008132
80                 X    =        -1526478
88
 Y    =      -13052707
45  feet           Y    =        -3978465
23  meter
 Z    =      -17390871
70                 Z    =        -5300737
69
 XDOT =      21320
935936                 XDOT =        6498
621273
 YDOT =     -11012
765598  feet/sec       YDOT =       -3356
690954  meter/sec
 ZDOT =       2128
024281                 ZDOT =         648
621801


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   21023
69604218  
00016717  00000-0  10270-3 0  9090
2 25544  51
6455 337
3954 0002224 286
8312  73
2594 15
48904870 26196


Satellite: ISS
Catalog Number: 25544
Epoch time:      21023
69604218   =   yrday
fracday
Element set:     909
Inclination:       51
6455  deg
RA of node:       337
3954  deg
Eccentricity:     
0002224     
Arg of perigee:   286
8312  deg
Mean anomaly:      73
2594  deg
Mean motion:   15
48904870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2619
Checksum:              320


Coasting Arc #11 (Orbit 2634)
---------------------------------------

Vector Time (GMT): 2021/024/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1414797
98                 A    =         6792686
70  meter
 Y    =        4022434
23  meter          E    =           
0001991
 Z    =        5287405
99                 I    =           51
44210
 XDOT =      -6940
099839                 Wp   =           12
65212
 YDOT =       3192
792115  meter/sec      RA   =          331
88575  deg
 ZDOT =       -569
973232                 TA   =           82
81905
                                          MA   =           82
79641
                                          Ha   =            228
373  n
mi
                                          Hp   =            223
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4641725
67                 X    =         1344030
02
 Y    =       13196962
71  feet           Y    =         4037859
33  meter
 Z    =       17347132
52                 Z    =         5294106
91
 XDOT =     -22769
356428                 XDOT =       -6972
518260
 YDOT =      10475
039748  feet/sec       YDOT =        3115
001715  meter/sec
 ZDOT =      -1869
990919                 ZDOT =        -603
763356

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6415445
38                 X    =         1955427
75
 Y    =       12388489
20  feet           Y    =         3776011
51  meter
 Z    =       17378027
63                 Z    =         5296822
82
 XDOT =     -20063
192793                 XDOT =       -6115
261163
 YDOT =      13242
069518  feet/sec       YDOT =        4036
182789  meter/sec
 ZDOT =      -2026
944370                 ZDOT =        -617
812644


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   21024
72835840  
00016717  00000-0  10270-3 0  9104
2 25544  51
6457 332
2903 0002325 288
1845  71
9052 15
48918086 26350


Satellite: ISS
Catalog Number: 25544
Epoch time:      21024
72835840   =   yrday
fracday
Element set:     910
Inclination:       51
6457  deg
RA of node:       332
2903  deg
Eccentricity:     
0002325     
Arg of perigee:   288
1845  deg
Mean anomaly:      71
9052  deg
Mean motion:   15
48918086  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2635
Checksum:              308


Coasting Arc #12 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2021/025/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1793691
08                 A    =         6792697
36  meter
 Y    =       -3873528
88  meter          E    =           
0012445
 Z    =       -5294685
55                 I    =           51
41284
 XDOT =       6619
353152                 Wp   =           90
36454
 YDOT =      -3798
743771  meter/sec      RA   =          326
92655  deg
 ZDOT =        537
686441                 TA   =          184
78786
                                          MA   =          184
79977
                                          Ha   =            228
466  n
mi
                                          Hp   =            223
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5884813
25                 X    =        -1724524
80
 Y    =      -12708428
07  feet           Y    =        -3893199
95  meter
 Z    =      -17371015
58                 Z    =        -5303230
81
 XDOT =      21717
037900                 XDOT =        6658
728186
 YDOT =     -12463
070116  feet/sec       YDOT =       -3724
501294  meter/sec
 ZDOT =       1764
063125                 ZDOT =         569
935222

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7773420
07                 X    =        -2369338
44
 Y    =      -11590360
57  feet           Y    =        -3532741
90  meter
 Z    =      -17410480
62                 Z    =        -5306714
49
 XDOT =      18518
801547                 XDOT =        5644
530711
 YDOT =     -15290
105601  feet/sec       YDOT =       -4660
424187  meter/sec
 ZDOT =       1913
885354                 ZDOT =         583
352256


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   21025
69615413  
00016717  00000-0  10270-3 0  9114
2 25544  51
6459 327
5036 0002381 294
4318  65
6583 15
48912524 26500


Satellite: ISS
Catalog Number: 25544
Epoch time:      21025
69615413   =   yrday
fracday
Element set:     911
Inclination:       51
6459  deg
RA of node:       327
5036  deg
Eccentricity:     
0002381     
Arg of perigee:   294
4318  deg
Mean anomaly:      65
6583  deg
Mean motion:   15
48912524  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2650
Checksum:              308


Coasting Arc #13 (Orbit 2659)
---------------------------------------

Vector Time (GMT): 2021/026/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6002590
95                 A    =         6803301
96  meter
 Y    =        2700013
90  meter          E    =           
0005768
 Z    =       -1711446
76                 I    =           51
42794
 XDOT =       -682
485904                 Wp   =          149
28519
 YDOT =      -5102
117257  meter/sec      RA   =          323
81331  deg
 ZDOT =      -5668
848729                 TA   =           49
49161
                                          MA   =           49
44137
                                          Ha   =            228
622  n
mi
                                          Hp   =            223
522

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19693539
87                 X    =        -6024024
19
 Y    =        8858313
33  feet           Y    =         2632768
94  meter
 Z    =       -5614982
80                 Z    =        -1740656
07
 XDOT =      -2239
126980                 XDOT =        -597
846404
 YDOT =     -16739
229847  feet/sec       YDOT =       -5109
275490  meter/sec
 ZDOT =     -18598
585069                 ZDOT =       -5671
958839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3124059
65                 X    =          952213
38
 Y    =      -21330813
47  feet           Y    =        -6501631
94  meter
 Z    =       -5750644
11                 Z    =        -1752796
32
 XDOT =      13685
629988                 XDOT =        4171
380020
 YDOT =       7010
724104  feet/sec       YDOT =        2136
868707  meter/sec
 ZDOT =     -18612
776356                 ZDOT =       -5673
174233


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   21026
34135018  
00016717  00000-0  10270-3 0  9126
2 25544  51
6434 324
3117 0001962 297
3111  62
7839 15
48890133 26609


Satellite: ISS
Catalog Number: 25544
Epoch time:      21026
34135018   =   yrday
fracday
Element set:     912
Inclination:       51
6434  deg
RA of node:       324
3117  deg
Eccentricity:     
0001962     
Arg of perigee:   297
3111  deg
Mean anomaly:      62
7839  deg
Mean motion:   15
48890133  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2660
Checksum:              289


Coasting Arc #14 (Orbit 2675)
---------------------------------------

Vector Time (GMT): 2021/027/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5736285
46                 A    =         6803251
89  meter
 Y    =       -3237949
21  meter          E    =           
0012731
 Z    =        1674022
20                 I    =           51
40052
 XDOT =       1161
632926                 Wp   =           56
58660
 YDOT =       5007
888341  meter/sec      RA   =          318
85170  deg
 ZDOT =       5681
441828                 TA   =          321
78409
                                          MA   =          321
87427
                                          Ha   =            228
504  n
mi
                                          Hp   =            223
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18819834
19                 X    =         5763935
66
 Y    =      -10623192
94  feet           Y    =        -3173647
49  meter
 Z    =        5492198
82                 Z    =         1701952
89
 XDOT =       3811
131647                 XDOT =        1077
950467
 YDOT =      16430
079860  feet/sec       YDOT =        5020
410143  meter/sec
 ZDOT =      18639
901012                 ZDOT =        5686
881635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -796142
51                 X    =         -242664
24
 Y    =       21562990
06  feet           Y    =         6572399
37  meter
 Z    =        5621943
80                 Z    =         1713568
47
 XDOT =     -14351
366344                 XDOT =       -4374
296462
 YDOT =      -5416
681503  feet/sec       YDOT =       -1651
004522  meter/sec
 ZDOT =      18664
917327                 ZDOT =        5689
066801


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   21027
37366067  
00016717  00000-0  10270-3 0  9131
2 25544  51
6425 319
2072 0002101 297
2899  62
8037 15
48929031 26768


Satellite: ISS
Catalog Number: 25544
Epoch time:      21027
37366067   =   yrday
fracday
Element set:     913
Inclination:       51
6425  deg
RA of node:       319
2072  deg
Eccentricity:     
0002101     
Arg of perigee:   297
2899  deg
Mean anomaly:      62
8037  deg
Mean motion:   15
48929031  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2676
Checksum:              313


Coasting Arc #15 (Orbit 2690)
---------------------------------------

Vector Time (GMT): 2021/028/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5435746
03                 A    =         6803357
69  meter
 Y    =        3733158
01  meter          E    =           
0005643
 Z    =       -1664076
11                 I    =           51
37526
 XDOT =      -1611
620420                 Wp   =          147
02120
 YDOT =      -4873
252594  meter/sec      RA   =          313
88725  deg
 ZDOT =      -5681
931283                 TA   =           51
23060
                                          MA   =           51
18019
                                          Ha   =            228
676  n
mi
                                          Hp   =            223
489

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17833812
44                 X    =        -5469004
48
 Y    =       12247893
73  feet           Y    =         3672185
74  meter
 Z    =       -5459567
28                 Z    =        -1690560
47
 XDOT =      -5287
468571                 XDOT =       -1529
407780
 YDOT =     -15988
361530  feet/sec       YDOT =       -4890
814795  meter/sec
 ZDOT =     -18641
506835                 ZDOT =       -5689
560336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1475147
46                 X    =         -449624
95
 Y    =      -21552749
79  feet           Y    =        -6569278
14  meter
 Z    =       -5582612
12                 Z    =        -1701580
17
 XDOT =      14815
770809                 XDOT =        4515
846943
 YDOT =       3812
172217  feet/sec       YDOT =        1161
950092  meter/sec
 ZDOT =     -18676
699904                 ZDOT =       -5692
658131


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   21028
34145440  
00016717  00000-0  10270-3 0  9140
2 25544  51
6419 314
4207 0002110 306
9730  53
1227 15
48896510 26916


Satellite: ISS
Catalog Number: 25544
Epoch time:      21028
34145440   =   yrday
fracday
Element set:     914
Inclination:       51
6419  deg
RA of node:       314
4207  deg
Eccentricity:     
0002110     
Arg of perigee:   306
9730  deg
Mean anomaly:      53
1227  deg
Mean motion:   15
48896510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2691
Checksum:              280


Coasting Arc #16 (Orbit 2706)
---------------------------------------

Vector Time (GMT): 2021/029/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5077039
88                 A    =         6803262
77  meter
 Y    =       -4214391
30  meter          E    =           
0012947
 Z    =        1628485
91                 I    =           51
35302
 XDOT =       2061
938794                 Wp   =           55
44697
 YDOT =       4694
058504  meter/sec      RA   =          308
92213  deg
 ZDOT =       5694
232292                 TA   =          322
41959
                                          MA   =          322
51000
                                          Ha   =            228
531  n
mi
                                          Hp   =            223
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16656955
00                 X    =         5115879
18
 Y    =      -13826743
12  feet           Y    =        -4157399
11  meter
 Z    =        5342801
56                 Z    =         1653241
44
 XDOT =       6764
891056                 XDOT =        1981
636796
 YDOT =      15400
454409  feet/sec       YDOT =        4716
667298  meter/sec
 ZDOT =      18681
864474                 ZDOT =        5704
053245

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3799514
66                 X    =         1158092
07
 Y    =       21282722
60  feet           Y    =         6486973
85  meter
 Z    =        5457830
25                 Z    =         1663546
66
 XDOT =     -15116
164744                 XDOT =       -4607
407014
 YDOT =      -2124
643737  feet/sec       YDOT =        -647
591411  meter/sec
 ZDOT =      18727
249030                 ZDOT =        5708
065504


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   21029
37376147  
00016717  00000-0  10270-3 0  9155
2 25544  51
6422 309
3161 0002114 303
6541  56
4408 15
48949688 27070


Satellite: ISS
Catalog Number: 25544
Epoch time:      21029
37376147   =   yrday
fracday
Element set:     915
Inclination:       51
6422  deg
RA of node:       309
3161  deg
Eccentricity:     
0002114     
Arg of perigee:   303
6541  deg
Mean anomaly:      56
4408  deg
Mean motion:   15
48949688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2707
Checksum:              309


Coasting Arc #17 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2021/029/19:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5222188
30                 A    =         6797475
49  meter
 Y    =        1605119
48  meter          E    =           
0006429
 Z    =       -4051809
28                 I    =           51
32362
 XDOT =        987
840287                 Wp   =           55
39350
 YDOT =      -6532
583064  meter/sec      RA   =          306
49688  deg
 ZDOT =      -3861
871693                 TA   =          174
33924
                                          MA   =          174
33196
                                          Ha   =            228
689  n
mi
                                          Hp   =            223
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17133163
72                 X    =        -5220068
44
 Y    =        5266140
02  feet           Y    =         1546733
22  meter
 Z    =      -13293337
53                 Z    =        -4077170
52
 XDOT =       3240
945822                 XDOT =        1079
574310
 YDOT =     -21432
359133  feet/sec       YDOT =       -6521
023252  meter/sec
 ZDOT =     -12670
182720                 ZDOT =       -3856
850781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4836375
41                 X    =        -1474127
23
 Y    =       17168081
01  feet           Y    =         5232831
09  meter
 Z    =      -13411070
78                 Z    =        -4087694
38
 XDOT =     -14935
068293                 XDOT =       -4552
208816
 YDOT =     -14084
336885  feet/sec       YDOT =       -4292
905883  meter/sec
 ZDOT =     -12646
640847                 ZDOT =       -3854
696130


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   21029
82539806  
00016717  00000-0  10270-3 0  9169
2 25544  51
6425 307
0790 0002056 309
4190  50
6778 15
48922586 27147


Satellite: ISS
Catalog Number: 25544
Epoch time:      21029
82539806   =   yrday
fracday
Element set:     916
Inclination:       51
6425  deg
RA of node:       307
0790  deg
Eccentricity:     
0002056     
Arg of perigee:   309
4190  deg
Mean anomaly:      50
6778  deg
Mean motion:   15
48922586  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2714
Checksum:              320
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