[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 15th 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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