[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 22nd 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) : 15144 822 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 84 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
050/19:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 222
1
051/17:36:48
295 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 222
1
053/09:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 222
0
054/01:32:30
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 221
9
063/11:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
2
000/00:00:00
000 0
0 0
0 221
8
Coasting Arc #1 (Orbit 3005)
---------------------------------------
Vector Time (GMT): 2021/048/14:53:53
651
Vector Time (MET): N/A
Weight (LBS) : 957236
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4607312
46 A = 6794794
36 meter
Y = -1531324
39 meter E =
0009802
Z = 4749270
39 I = 51
41332
XDOT = 4597
800926 Wp = 53
70439
YDOT = 5516
878978 meter/sec RA = 212
92229 deg
ZDOT = -2671
990580 TA = 62
83971
MA = 62
73980
Ha = 229
642 n
mi
Hp = 222
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15115854
52 X = 4601024
95
Y = -5024030
14 feet Y = -1479837
04 meter
Z = 15581595
77 Z = 4771635
31
XDOT = 15084
648708 XDOT = 4548
746553
YDOT = 18099
996647 feet/sec YDOT = 5568
020505 meter/sec
ZDOT = -8766
373293 ZDOT = -2649
776051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13859162
15 X = 4224272
62
Y = -7642416
65 feet Y = -2329408
60 meter
Z = 15685444
07 Z = 4780923
35
XDOT = 17597
454665 XDOT = 5363
704182
YDOT = 14067
868629 feet/sec YDOT = 4287
886358 meter/sec
ZDOT = -8663
135182 ZDOT = -2640
523603
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21048
66450415
00016717 00000-0 10270-3 0 9003
2 25544 51
6426 213
8989 0002614 28
5435 331
5857 15
48946158 30068
Satellite: ISS
Catalog Number: 25544
Epoch time: 21048
66450415 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 213
8989 deg
Eccentricity:
0002614
Arg of perigee: 28
5435 deg
Mean anomaly: 331
5857 deg
Mean motion: 15
48946158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3006
Checksum: 315
Coasting Arc #2 (Orbit 3020)
---------------------------------------
Vector Time (GMT): 2021/049/14:57:53
651
Vector Time (MET): N/A
Weight (LBS) : 957236
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5490393
08 A = 6797632
16 meter
Y = 659130
13 meter E =
0007812
Z = -3959941
04 I = 51
45345
XDOT = -3537
444612 Wp = 88
20787
YDOT = -5483
277113 meter/sec RA = 207
94415 deg
ZDOT = 3999
016471 TA = 223
68218
MA = 223
74403
Ha = 229
692 n
mi
Hp = 222
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18013100
65 X = -5478120
80
Y = 2162500
42 feet Y = 597801
09 meter
Z = -12991932
54 Z = -3986581
00
XDOT = -11605
789411 XDOT = -3495
290646
YDOT = -17989
754308 feet/sec YDOT = -5522
599549 meter/sec
ZDOT = 13120
132779 ZDOT = 3981
935778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17045447
47 X = -5195452
39
Y = 5947327
56 feet Y = 1812745
44 meter
Z = -13115659
71 Z = -3997653
08
XDOT = -14840
741796 XDOT = -4523
458099
YDOT = -13826
694517 feet/sec YDOT = -4214
376489 meter/sec
ZDOT = 13040
722736 ZDOT = 3974
812290
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21049
63224706
00016717 00000-0 10270-3 0 9014
2 25544 51
6437 209
1130 0002665 28
2005 331
9289 15
48972457 30213
Satellite: ISS
Catalog Number: 25544
Epoch time: 21049
63224706 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 209
1130 deg
Eccentricity:
0002665
Arg of perigee: 28
2005 deg
Mean anomaly: 331
9289 deg
Mean motion: 15
48972457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3021
Checksum: 291
Coasting Arc #3 (Orbit 3036)
---------------------------------------
Vector Time (GMT): 2021/050/14:57:53
651
Vector Time (MET): N/A
Weight (LBS) : 957236
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5418639
64 A = 6797717
89 meter
Y = -1111044
06 meter E =
0013078
Z = 3943801
20 I = 51
48381
XDOT = 3991
520497 Wp = 71
44124
YDOT = 5163
812423 meter/sec RA = 202
98626 deg
ZDOT = -4014
421611 TA = 60
65959
MA = 60
52901
Ha = 229
773 n
mi
Hp = 222
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17777689
10 X = 5411504
52
Y = -3645157
68 feet Y = -1050488
76 meter
Z = 12938980
30 Z = 3970105
10
XDOT = 13095
539687 XDOT = 3952
979970
YDOT = 16941
641807 feet/sec YDOT = 5208
232927 meter/sec
ZDOT = -13170
674577 ZDOT = -3995
126358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16369778
04 X = 4989508
35
Y = -7628053
26 feet Y = -2325030
63 meter
Z = 13061155
61 Z = 3981040
23
XDOT = 16183
120476 XDOT = 4932
615121
YDOT = 12247
314727 feet/sec YDOT = 3732
981529 meter/sec
ZDOT = -13080
966786 ZDOT = -3987
078677
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21050
66450645
00016717 00000-0 10270-3 0 9023
2 25544 51
6433 204
0072 0002778 35
7489 324
3846 15
48958996 30376
Satellite: ISS
Catalog Number: 25544
Epoch time: 21050
66450645 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 204
0072 deg
Eccentricity:
0002778
Arg of perigee: 35
7489 deg
Mean anomaly: 324
3846 deg
Mean motion: 15
48958996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3037
Checksum: 323
Coasting Arc #4 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2021/050/19:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 957236
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 175255
29 A = 6792979
68 meter
Y = -4382758
43 meter E =
0005275
Z = 5182436
37 I = 51
47281
XDOT = 7321
530633 Wp = 89
15575
YDOT = 1846
647727 meter/sec RA = 202
11439 deg
ZDOT = 1313
022995 TA = 348
18822
MA = 348
20059
Ha = 229
879 n
mi
Hp = 222
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 574984
56 X = 199078
70
Y = -14379128
70 feet Y = -4380665
32 meter
Z = 17002743
99 Z = 5183345
59
XDOT = 24020
769792 XDOT = 7293
958890
YDOT = 6058
555534 feet/sec YDOT = 1928
368217 meter/sec
ZDOT = 4307
818224 ZDOT = 1348
520575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14063478
67 X = -4286548
30
Y = -3027709
92 feet Y = -922845
98 meter
Z = 17006904
28 Z = 5183704
42
XDOT = 10039
853730 XDOT = 3060
147417
YDOT = -21490
571568 feet/sec YDOT = -6550
326214 meter/sec
ZDOT = 4472
748436 ZDOT = 1363
293723
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21050
85805354
00016717 00000-0 10270-3 0 9036
2 25544 51
6423 203
0524 0003107 32
7068 327
4273 15
48984120 30403
Satellite: ISS
Catalog Number: 25544
Epoch time: 21050
85805354 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 203
0524 deg
Eccentricity:
0003107
Arg of perigee: 32
7068 deg
Mean anomaly: 327
4273 deg
Mean motion: 15
48984120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 273
Coasting Arc #5 (Orbit 3053)
---------------------------------------
Vector Time (GMT): 2021/051/17:36:48
295
Vector Time (MET): N/A
Weight (LBS) : 957236
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5138253
63 A = 6801800
83 meter
Y = 3698190
94 meter E =
0005913
Z = -2490133
25 I = 51
53127
XDOT = -4676
814531 Wp = 102
43350
YDOT = 2937
932544 meter/sec RA = 197
53241 deg
ZDOT = -5299
035025 TA = 105
43976
MA = 105
37445
Ha = 229
925 n
mi
Hp = 222
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16857787
51 X = 5108612
88
Y = 12133172
38 feet Y = 3755484
87 meter
Z = -8169728
50 Z = -2465246
04
XDOT = -15343
879696 XDOT = -4683
580559
YDOT = 9638
886299 feet/sec YDOT = 2885
595198 meter/sec
ZDOT = -17385
285515 ZDOT = -5321
769206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19738385
09 X = 6016259
78
Y = -6608469
72 feet Y = -2014261
57 meter
Z = -8054043
53 Z = -2454872
47
XDOT = -1581
326624 XDOT = -481
988355
YDOT = 16545
418938 feet/sec YDOT = 5043
043692 meter/sec
ZDOT = -17490
866733 ZDOT = -5331
216180
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21051
76128002
00016717 00000-0 10270-3 0 9046
2 25544 51
6418 198
5848 0002972 35
9148 324
2202 15
48978061 30546
Satellite: ISS
Catalog Number: 25544
Epoch time: 21051
76128002 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 198
5848 deg
Eccentricity:
0002972
Arg of perigee: 35
9148 deg
Mean anomaly: 324
2202 deg
Mean motion: 15
48978061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3054
Checksum: 306
Coasting Arc #6 (Orbit 3069)
---------------------------------------
Vector Time (GMT): 2021/052/17:36:48
295
Vector Time (MET): N/A
Weight (LBS) : 957236
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5442568
96 A = 6801885
95 meter
Y = -3226259
10 meter E =
0016279
Z = 2474144
62 I = 51
56413
XDOT = 4403
284433 Wp = 68
56677
YDOT = -3337
070410 meter/sec RA = 192
57899 deg
ZDOT = 5312
357592 TA = 319
13983
MA = 319
26175
Ha = 230
033 n
mi
Hp = 222
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17856197
39 X = -5418105
19
Y = -10584839
55 feet Y = -3286985
06 meter
Z = 8117272
38 Z = 2447766
66
XDOT = 14446
471237 XDOT = 4414
469432
YDOT = -10948
393733 feet/sec YDOT = -3287
767217 meter/sec
ZDOT = 17428
994725 ZDOT = 5333
773736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18921462
07 X = -5767261
64
Y = 8650816
33 feet Y = 2636768
82 meter
Z = 7994646
60 Z = 2436768
28
XDOT = -166
884079 XDOT = -50
866267
YDOT = -16632
844850 feet/sec YDOT = -5069
691110 meter/sec
ZDOT = 17528
459807 ZDOT = 5342
674549
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21052
79353732
00016717 00000-0 10270-3 0 9051
2 25544 51
6418 193
4789 0003050 38
6564 321
4804 15
48963704 30707
Satellite: ISS
Catalog Number: 25544
Epoch time: 21052
79353732 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 193
4789 deg
Eccentricity:
0003050
Arg of perigee: 38
6564 deg
Mean anomaly: 321
4804 deg
Mean motion: 15
48963704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3070
Checksum: 312
Coasting Arc #7 (Orbit 3079)
---------------------------------------
Vector Time (GMT): 2021/053/09:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6546044
08 A = 6802833
93 meter
Y = -376328
28 meter E =
0014853
Z = 1792194
82 I = 51
58827
XDOT = 1834
933309 Wp = 102
98119
YDOT = 4836
953120 meter/sec RA = 189
22682 deg
ZDOT = -5650
165885 TA = 57
35582
MA = 57
21259
Ha = 229
850 n
mi
Hp = 221
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21476522
57 X = 6541060
52
Y = -1234672
83 feet Y = -303153
58 meter
Z = 5879904
26 Z = 1823980
13
XDOT = 6020
122404 XDOT = 1808
153309
YDOT = 15869
268768 feet/sec YDOT = 4857
322996 meter/sec
ZDOT = -18537
289649 ZDOT = -5641
317682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10704252
61 X = 3262656
20
Y = 18612509
94 feet Y = 5673093
03 meter
Z = 6027616
67 Z = 1837217
56
XDOT = -10077
295644 XDOT = -3071
559712
YDOT = 11823
107654 feet/sec YDOT = 3603
683213 meter/sec
ZDOT = -18496
089788 ZDOT = -5637
608167
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21053
43869520
00016717 00000-0 10270-3 0 9061
2 25544 51
6397 190
2847 0003010 36
4692 323
6663 15
49008608 30809
Satellite: ISS
Catalog Number: 25544
Epoch time: 21053
43869520 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 190
2847 deg
Eccentricity:
0003010
Arg of perigee: 36
4692 deg
Mean anomaly: 323
6663 deg
Mean motion: 15
49008608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3080
Checksum: 304
Coasting Arc #8 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2021/054/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1767243
70 A = 6793655
27 meter
Y = 4209025
49 meter E =
0015634
Z = -5045688
54 I = 51
58238
XDOT = -7359
028341 Wp = 68
50841
YDOT = 770
387831 meter/sec RA = 185
98827 deg
ZDOT = -1934
094356 TA = 182
65668
MA = 182
66499
Ha = 230
045 n
mi
Hp = 221
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5798043
65 X = 1744554
21
Y = 13809138
75 feet Y = 4228661
27 meter
Z = -16554096
28 Z = -5037159
25
XDOT = -24143
793770 XDOT = -7357
701629
YDOT = 2527
519132 feet/sec YDOT = 688
101305 meter/sec
ZDOT = -6345
453923 ZDOT = -1969
837518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4781574
47 X = -1457423
90
Y = -14239362
73 feet Y = -4340157
76 meter
Z = -16514382
26 Z = -5033583
71
XDOT = 23186
410923 XDOT = 7067
218049
YDOT = -231
212094 feet/sec YDOT = -70
473446 meter/sec
ZDOT = -6511
571751 ZDOT = -1984
727070
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21054
08385593
00016717 00000-0 10270-3 0 9077
2 25544 51
6425 187
0972 0003366 39
4349 320
7046 15
48994477 30901
Satellite: ISS
Catalog Number: 25544
Epoch time: 21054
08385593 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 187
0972 deg
Eccentricity:
0003366
Arg of perigee: 39
4349 deg
Mean anomaly: 320
7046 deg
Mean motion: 15
48994477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 332
Coasting Arc #9 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2021/055/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2118650
46 A = 6793589
29 meter
Y = -4029131
16 meter E =
0007103
Z = 5037009
34 I = 51
61616
XDOT = 7281
893489 Wp = 97
38061
YDOT = -1402
745505 meter/sec RA = 181
04107 deg
ZDOT = 1937
583248 TA = 333
78764
MA = 333
82358
Ha = 230
061 n
mi
Hp = 221
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6950952
95 X = -2097904
23
Y = -13218934
24 feet Y = -4052707
43 meter
Z = 16525621
19 Z = 5026768
45
XDOT = 23890
726671 XDOT = 7287
626817
YDOT = -4602
183415 feet/sec YDOT = -1321
282059 meter/sec
ZDOT = 6356
900419 ZDOT = 1972
968748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6213546
95 X = 1893889
11
Y = 13638964
17 feet Y = 4157156
28 meter
Z = 16477943
31 Z = 5022477
12
XDOT = -23095
340156 XDOT = -7039
459680
YDOT = 2629
932593 feet/sec YDOT = 801
603454 meter/sec
ZDOT = 6521
371819 ZDOT = 1987
714130
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21055
11610811
00016717 00000-0 10270-3 0 9087
2 25544 51
6423 181
9921 0003235 42
3038 317
8361 15
49012929 31068
Satellite: ISS
Catalog Number: 25544
Epoch time: 21055
11610811 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 181
9921 deg
Eccentricity:
0003235
Arg of perigee: 42
3038 deg
Mean anomaly: 317
8361 deg
Mean motion: 15
49012929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3106
Checksum: 279
Coasting Arc #10 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2021/056/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2456905
87 A = 6793627
86 meter
Y = 3838772
05 meter E =
0015826
Z = -5052422
51 I = 51
65112
XDOT = -7120
163246 Wp = 69
79244
YDOT = 2016
402552 meter/sec RA = 176
09538 deg
ZDOT = -1929
964548 TA = 181
43440
MA = 181
43895
Ha = 230
105 n
mi
Hp = 221
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8060714
79 X = 2438337
95
Y = 12594396
50 feet Y = 3866143
02 meter
Z = -16576189
33 Z = -5040533
37
XDOT = -23360
115635 XDOT = -7132
807728
YDOT = 6615
493938 feet/sec YDOT = 1936
709010 meter/sec
ZDOT = -6331
904685 ZDOT = -1964
581173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7584953
72 X = -2311893
90
Y = -12957404
16 feet Y = -3949416
79 meter
Z = -16520839
96 Z = -5035552
02
XDOT = 22651
455948 XDOT = 6904
163773
YDOT = -4979
489647 feet/sec YDOT = -1517
748445 meter/sec
ZDOT = -6492
815167 ZDOT = -1979
010063
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21056
08384642
00016717 00000-0 10270-3 0 9095
2 25544 51
6433 177
2054 0003378 46
0062 314
1367 15
49001131 31216
Satellite: ISS
Catalog Number: 25544
Epoch time: 21056
08384642 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 177
2054 deg
Eccentricity:
0003378
Arg of perigee: 46
0062 deg
Mean anomaly: 314
1367 deg
Mean motion: 15
49001131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 275
Coasting Arc #11 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2021/057/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2771934
70 A = 6793589
43 meter
Y = -3601705
29 meter E =
0007367
Z = 5043504
11 I = 51
68550
XDOT = 6936
524291 Wp = 99
24667
YDOT = -2625
935619 meter/sec RA = 171
15237 deg
ZDOT = 1933
526405 TA = 331
97949
MA = 332
01913
Ha = 230
147 n
mi
Hp = 221
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9094273
94 X = -2755950
97
Y = -11816618
39 feet Y = -3632613
47 meter
Z = 16546929
50 Z = 5030078
55
XDOT = 22757
625626 XDOT = 6955
981114
YDOT = -8615
274340 feet/sec YDOT = -2548
257523 meter/sec
ZDOT = 6343
590567 ZDOT = 1967
267598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8862130
42 X = 2701177
35
Y = 12077476
15 feet Y = 3681214
73 meter
Z = 16484428
37 Z = 5024453
77
XDOT = -22072
532563 XDOT = -6727
707925
YDOT = 7307
809256 feet/sec YDOT = 2227
420261 meter/sec
ZDOT = 6500
440380 ZDOT = 1981
334228
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21057
11609670
00016717 00000-0 10270-3 0 9103
2 25544 51
6438 172
0999 0003216 48
8369 311
3058 15
49009914 31373
Satellite: ISS
Catalog Number: 25544
Epoch time: 21057
11609670 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 172
0999 deg
Eccentricity:
0003216
Arg of perigee: 48
8369 deg
Mean anomaly: 311
3058 deg
Mean motion: 15
49009914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 310
Coasting Arc #12 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2021/058/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3069429
40 A = 6793579
80 meter
Y = 3358265
94 meter E =
0015997
Z = -5059758
50 I = 51
72026
XDOT = -6673
692051 Wp = 70
84080
YDOT = 3201
044029 meter/sec RA = 166
21146 deg
ZDOT = -1923
765316 TA = 180
46832
MA = 180
46982
Ha = 230
148 n
mi
Hp = 221
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10070306
42 X = 3056224
77
Y = 11017932
88 feet Y = 3392516
34 meter
Z = -16600257
56 Z = -5044881
18
XDOT = -21895
315129 XDOT = -6699
646845
YDOT = 10502
112955 feet/sec YDOT = 3126
268733 meter/sec
ZDOT = -6311
565997 ZDOT = -1956
245748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10054258
51 X = -3064538
00
Y = -11136087
13 feet Y = -3394279
36 meter
Z = -16530998
66 Z = -5038648
39
XDOT = 21161
108810 XDOT = 6449
905965
YDOT = -9511
362499 feet/sec YDOT = -2899
063290 meter/sec
ZDOT = -6462
559423 ZDOT = -1969
788112
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21058
08383026
00016717 00000-0 10270-3 0 9115
2 25544 51
6452 167
3135 0003419 51
3257 308
8198 15
49013166 31525
Satellite: ISS
Catalog Number: 25544
Epoch time: 21058
08383026 = yrday
fracday
Element set: 911
Inclination: 51
6452 deg
RA of node: 167
3135 deg
Eccentricity:
0003419
Arg of perigee: 51
3257 deg
Mean anomaly: 308
8198 deg
Mean motion: 15
49013166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 294
Coasting Arc #13 (Orbit 3167)
---------------------------------------
Vector Time (GMT): 2021/059/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3338053
47 A = 6793594
31 meter
Y = -3072204
93 meter E =
0007745
Z = 5050676
26 I = 51
75249
XDOT = 6389
962712 Wp = 100
27136
YDOT = -3769
626593 meter/sec RA = 161
27292 deg
ZDOT = 1926
370024 TA = 331
04352
MA = 331
08647
Ha = 230
295 n
mi
Hp = 221
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10951619
01 X = -3327983
69
Y = -10079412
49 feet Y = -3109476
70 meter
Z = 16570460
17 Z = 5034486
47
XDOT = 20964
444593 XDOT = 6422
283967
YDOT = -12367
541314 feet/sec YDOT = -3697
988526 meter/sec
ZDOT = 6320
111627 ZDOT = 1957
487953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11120277
79 X = 3389460
67
Y = 10018182
44 feet Y = 3053542
01 meter
Z = 16495093
45 Z = 5027704
48
XDOT = -20122
079390 XDOT = -6133
209798
YDOT = 11670
399354 feet/sec YDOT = 3557
137723 meter/sec
ZDOT = 6464
772177 ZDOT = 1970
462560
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21059
11607758
00016717 00000-0 10270-3 0 9122
2 25544 51
6447 162
2079 0003387 55
6935 304
4535 15
49003296 31681
Satellite: ISS
Catalog Number: 25544
Epoch time: 21059
11607758 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 162
2079 deg
Eccentricity:
0003387
Arg of perigee: 55
6935 deg
Mean anomaly: 304
4535 deg
Mean motion: 15
49003296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3168
Checksum: 317
Coasting Arc #14 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2021/060/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3588395
19 A = 6793554
85 meter
Y = 2783509
85 meter E =
0016034
Z = -5067148
15 I = 51
78428
XDOT = -6033
531130 Wp = 72
05354
YDOT = 4290
857942 meter/sec RA = 156
33697 deg
ZDOT = -1915
868828 TA = 179
35386
MA = 179
35178
Ha = 230
157 n
mi
Hp = 221
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11772950
09 X = 3581615
22
Y = 9132250
15 feet Y = 2823599
46 meter
Z = -16624501
79 Z = -5049734
24
XDOT = -19795
049640 XDOT = -6071
758399
YDOT = 14077
617919 feet/sec YDOT = 4223
172708 meter/sec
ZDOT = -6285
658885 ZDOT = -1945
269998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12090969
51 X = -3685327
51
Y = -8859879
49 feet Y = -2700491
27 meter
Z = -16543439
74 Z = -5042440
43
XDOT = 18781
184340 XDOT = 5724
504987
YDOT = -13639
610018 feet/sec YDOT = -4157
353133 meter/sec
ZDOT = -6422
338524 ZDOT = -1957
528782
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21060
08380858
00016717 00000-0 10270-3 0 9130
2 25544 51
6448 157
4220 0003336 56
6874 303
4595 15
49016192 31834
Satellite: ISS
Catalog Number: 25544
Epoch time: 21060
08380858 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 157
4220 deg
Eccentricity:
0003336
Arg of perigee: 56
6874 deg
Mean anomaly: 303
4595 deg
Mean motion: 15
49016192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 308
Coasting Arc #15 (Orbit 3198)
---------------------------------------
Vector Time (GMT): 2021/061/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3803791
91 A = 6793587
04 meter
Y = -2457159
51 meter E =
0007880
Z = 5058048
35 I = 51
81532
XDOT = 5657
892896 Wp = 102
16641
YDOT = -4802
391492 meter/sec RA = 151
40227 deg
ZDOT = 1917
785692 TA = 329
24970
MA = 329
29585
Ha = 230
337 n
mi
Hp = 221
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12479632
26 X = -3800601
22
Y = -8061546
95 feet Y = -2499677
93 meter
Z = 16594646
81 Z = 5039579
29
XDOT = 18562
640735 XDOT = 5701
858843
YDOT = -15755
877598 feet/sec YDOT = -4738
874833 meter/sec
ZDOT = 6291
947809 ZDOT = 1945
376333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12904810
69 X = 3933386
30
Y = 7552582
97 feet Y = 2302027
29 meter
Z = 16508676
95 Z = 5031844
73
XDOT = -17325
526124 XDOT = -5280
820362
YDOT = 15540
100995 feet/sec YDOT = 4736
622783 meter/sec
ZDOT = 6420
211707 ZDOT = 1956
880528
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21061
11605307
00016717 00000-0 10270-3 0 9145
2 25544 51
6452 152
3160 0003328 61
0196 299
1287 15
48999787 31999
Satellite: ISS
Catalog Number: 25544
Epoch time: 21061
11605307 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 152
3160 deg
Eccentricity:
0003328
Arg of perigee: 61
0196 deg
Mean anomaly: 299
1287 deg
Mean motion: 15
48999787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3199
Checksum: 318
Coasting Arc #16 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2021/062/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3998977
58 A = 6793516
05 meter
Y = 2133513
23 meter E =
0016144
Z = -5075159
86 I = 51
84405
XDOT = -5220
024473 Wp = 73
04986
YDOT = 5254
327620 meter/sec RA = 146
46935 deg
ZDOT = -1904
729329 TA = 178
48654
MA = 178
48165
Ha = 230
185 n
mi
Hp = 221
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13120005
18 X = 3999474
71
Y = 6999715
31 feet Y = 2178235
05 meter
Z = -16650786
93 Z = -5055733
58
XDOT = -17126
064543 XDOT = -5269
140031
YDOT = 17238
607677 feet/sec YDOT = 5195
678759 meter/sec
ZDOT = -6249
111971 ZDOT = -1930
205590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13611956
68 X = -4148924
40
Y = -6232834
57 feet Y = -1899767
98 meter
Z = -16560364
26 Z = -5047599
03
XDOT = 15617
144246 XDOT = 4760
105566
YDOT = -17191
994391 feet/sec YDOT = -5240
119890 meter/sec
ZDOT = -6367
550557 ZDOT = -1940
829410
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21062
08377886
00016717 00000-0 10270-3 0 9151
2 25544 51
6447 147
5291 0003352 61
4044 298
7443 15
49022029 32141
Satellite: ISS
Catalog Number: 25544
Epoch time: 21062
08377886 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 147
5291 deg
Eccentricity:
0003352
Arg of perigee: 61
4044 deg
Mean anomaly: 298
7443 deg
Mean motion: 15
49022029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 306
Coasting Arc #17 (Orbit 3229)
---------------------------------------
Vector Time (GMT): 2021/063/01:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4155165
94 A = 6793585
43 meter
Y = -1777597
60 meter E =
0008132
Z = 5065939
41 I = 51
87082
XDOT = 4764
305255 Wp = 103
33054
YDOT = -5694
352986 meter/sec RA = 141
53850 deg
ZDOT = 1905
262330 TA = 328
22451
MA = 328
27356
Ha = 230
439 n
mi
Hp = 221
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13632434
19 X = -4159586
68
Y = -5832013
12 feet Y = -1824088
09 meter
Z = 16620536
13 Z = 5045744
80
XDOT = 15630
922751 XDOT = 4818
372575
YDOT = -18682
260454 feet/sec YDOT = -5640
772666 meter/sec
ZDOT = 6250
860662 ZDOT = 1928
536880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14141311
93 X = 4310271
88
Y = 4795278
57 feet Y = 1461600
91 meter
Z = 16526538
07 Z = 5037288
80
XDOT = -13808
678853 XDOT = -4208
885314
YDOT = 18755
891794 feet/sec YDOT = 5716
795819 meter/sec
ZDOT = 6359
070867 ZDOT = 1938
244800
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21063
11601991
00016717 00000-0 10270-3 0 9164
2 25544 51
6438 142
4231 0003449 66
5010 293
6503 15
48992308 32309
Satellite: ISS
Catalog Number: 25544
Epoch time: 21063
11601991 = yrday
fracday
Element set: 916
Inclination: 51
6438 deg
RA of node: 142
4231 deg
Eccentricity:
0003449
Arg of perigee: 66
5010 deg
Mean anomaly: 293
6503 deg
Mean motion: 15
48992308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3230
Checksum: 287
Coasting Arc #18 (Orbit 3235)
---------------------------------------
Vector Time (GMT): 2021/063/11:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 972366
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4575004
35 A = 6794354
16 meter
Y = 1150468
70 meter E =
0014819
Z = -4903560
28 I = 51
88356
XDOT = -4093
508892 Wp = 73
32168
YDOT = 5991
958305 meter/sec RA = 139
47684 deg
ZDOT = -2415
314809 TA = 173
02297
MA = 173
00232
Ha = 230
216 n
mi
Hp = 221
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15009856
80 X = 4585617
90
Y = 3774503
61 feet Y = 1201688
82 meter
Z = -16087796
18 Z = -4881311
19
XDOT = -13430
147285 XDOT = -4148
476462
YDOT = 19658
655855 feet/sec YDOT = 5945
874277 meter/sec
ZDOT = -7924
261186 ZDOT = -2435
333062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12158643
56 X = 3705954
56
Y = 9748394
40 feet Y = 2971310
61 meter
Z = -15984244
06 Z = -4871997
59
XDOT = -19656
835478 XDOT = -5991
403454
YDOT = 11381
419142 feet/sec YDOT = 3469
056554 meter/sec
ZDOT = -8017
324554 ZDOT = -2443
680524
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21063
50310937
00016717 00000-0 10270-3 0 9175
2 25544 51
6431 140
5059 0003089 74
7520 285
3971 15
48984602 32367
Satellite: ISS
Catalog Number: 25544
Epoch time: 21063
50310937 = yrday
fracday
Element set: 917
Inclination: 51
6431 deg
RA of node: 140
5059 deg
Eccentricity:
0003089
Arg of perigee: 74
7520 deg
Mean anomaly: 285
3971 deg
Mean motion: 15
48984602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3236
Checksum: 306
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list