[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 8th 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) : 14538 8138 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
036/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 223
2
040/05:21:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
9
040/13:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
9
046/21:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 222
4
048/06:18:00
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
3
050/19:22:30
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
2
Coasting Arc #1 (Orbit 2817)
---------------------------------------
Vector Time (GMT): 2021/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 858497
65 A = 6803551
85 meter
Y = 6570398
19 meter E =
0012102
Z = 1521106
66 I = 51
26744
XDOT = -4704
659113 Wp = 110
27608
YDOT = 1947
192155 meter/sec RA = 273
16593 deg
ZDOT = -5722
514152 TA = 53
05647
MA = 52
94569
Ha = 229
089 n
mi
Hp = 223
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2816593
35 X = 777573
11
Y = 21556424
52 feet Y = 6579546
00 meter
Z = 4990507
43 Z = 1525080
52
XDOT = -15435
233312 XDOT = -4698
287311
YDOT = 6388
425706 feet/sec YDOT = 1894
617091 meter/sec
ZDOT = -18774
652731 ZDOT = -5745
351626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13291086
70 X = -4051123
22
Y = 17198156
60 feet Y = 5241998
13 meter
Z = 5008814
68 Z = 1526686
71
XDOT = -14079
693961 XDOT = -4291
490719
YDOT = -5350
747229 feet/sec YDOT = -1630
907755 meter/sec
ZDOT = -18880
644073 ZDOT = -5754
820313
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 21036
53527748
00016717 00000-0 10270-3 0 9000
2 25544 51
6442 273
8970 0002442 338
7265 21
3783 15
48913095 28184
Satellite: ISS
Catalog Number: 25544
Epoch time: 21036
53527748 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 273
8970 deg
Eccentricity:
0002442
Arg of perigee: 338
7265 deg
Mean anomaly: 21
3783 deg
Mean motion: 15
48913095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2818
Checksum: 318
Coasting Arc #2 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2021/036/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4185593
12 A = 6793414
85 meter
Y = -1603870
42 meter E =
0003096
Z = 5102220
05 I = 51
23278
XDOT = 901
416264 Wp = 97
76109
YDOT = 7439
251643 meter/sec RA = 272
95056 deg
ZDOT = 1597
788503 TA = 336
71921
MA = 336
73323
Ha = 228
925 n
mi
Hp = 223
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13732260
88 X = 4178433
75
Y = -5262042
05 feet Y = -1557104
31 meter
Z = 16739567
10 Z = 5122534
24
XDOT = 2957
402442 XDOT = 810
400274
YDOT = 24406
993578 feet/sec YDOT = 7448
822969 meter/sec
ZDOT = 5242
088264 ZDOT = 1601
946365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14507547
80 X = 4421900
57
Y = 1621693
98 feet Y = 494292
33 meter
Z = 16833845
30 Z = 5130956
05
XDOT = -8562
098803 XDOT = -2609
727715
YDOT = 21939
873825 feet/sec YDOT = 6687
273542 meter/sec
ZDOT = 5261
232853 ZDOT = 1603
623774
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 21036
59979446
00016717 00000-0 10270-3 0 9013
2 25544 51
6434 273
5771 0002604 338
0787 22
0251 15
48916724 28194
Satellite: ISS
Catalog Number: 25544
Epoch time: 21036
59979446 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 273
5771 deg
Eccentricity:
0002604
Arg of perigee: 338
0787 deg
Mean anomaly: 22
0251 deg
Mean motion: 15
48916724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2819
Checksum: 321
Coasting Arc #3 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2021/037/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4034840
03 A = 6793344
97 meter
Y = 1975439
51 meter E =
0013318
Z = -5107739
28 I = 51
23167
XDOT = -1548
389915 Wp = 66
24463
YDOT = -7317
581892 meter/sec RA = 267
97633 deg
ZDOT = -1605
038221 TA = 188
13390
MA = 188
15552
Ha = 229
051 n
mi
Hp = 222
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13237664
13 X = -4031820
13
Y = 6481100
76 feet Y = 1930336
18 meter
Z = -16757674
80 Z = -5127331
13
XDOT = -5080
019405 XDOT = -1458
651198
YDOT = -24007
814606 feet/sec YDOT = -7334
395255 meter/sec
ZDOT = -5265
873430 ZDOT = -1612
341990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14634916
95 X = -4460722
69
Y = -60220
09 feet Y = -18355
08 meter
Z = -16848610
11 Z = -5135456
36
XDOT = 6201
753213 XDOT = 1890
294379
YDOT = -22666
933117 feet/sec YDOT = -6908
881214 meter/sec
ZDOT = -5299
633485 ZDOT = -1615
328286
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 21037
56755943
00016717 00000-0 10270-3 0 9026
2 25544 51
6427 268
7894 0002701 338
7839 21
3199 15
48949420 28340
Satellite: ISS
Catalog Number: 25544
Epoch time: 21037
56755943 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 268
7894 deg
Eccentricity:
0002701
Arg of perigee: 338
7839 deg
Mean anomaly: 21
3199 deg
Mean motion: 15
48949420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2834
Checksum: 340
Coasting Arc #4 (Orbit 2849)
---------------------------------------
Vector Time (GMT): 2021/038/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3839318
70 A = 6793455
90 meter
Y = -2322652
18 meter E =
0003448
Z = 5097657
01 I = 51
23392
XDOT = 2186
612487 Wp = 94
56851
YDOT = 7163
767955 meter/sec RA = 263
00329 deg
ZDOT = 1615
962956 TA = 339
73183
MA = 339
74551
Ha = 229
077 n
mi
Hp = 223
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12596189
96 X = 3840245
06
Y = -7620249
95 feet Y = -2279713
30 meter
Z = 16724596
50 Z = 5116308
57
XDOT = 7173
925482 XDOT = 2098
493303
YDOT = 23503
175706 feet/sec YDOT = 7187
727423 meter/sec
ZDOT = 5301
715735 ZDOT = 1626
370841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14546175
00 X = 4433674
14
Y = -1495820
47 feet Y = -455926
08 meter
Z = 16811176
42 Z = 5124046
57
XDOT = -3799
388077 XDOT = -1158
053486
YDOT = 23223
691260 feet/sec YDOT = 7078
581096 meter/sec
ZDOT = 5349
902088 ZDOT = 1630
650156
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 21038
59984320
00016717 00000-0 10270-3 0 9034
2 25544 51
6425 263
6837 0002679 345
8440 14
2634 15
48912579 28508
Satellite: ISS
Catalog Number: 25544
Epoch time: 21038
59984320 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 263
6837 deg
Eccentricity:
0002679
Arg of perigee: 345
8440 deg
Mean anomaly: 14
2634 deg
Mean motion: 15
48912579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2850
Checksum: 326
Coasting Arc #5 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2021/039/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3625212
21 A = 6793397
69 meter
Y = 2661243
61 meter E =
0013691
Z = -5104038
75 I = 51
23707
XDOT = -2801
070766 Wp = 66
59482
YDOT = -6930
904062 meter/sec RA = 258
03026 deg
ZDOT = -1622
420849 TA = 187
61120
MA = 187
63201
Ha = 229
213 n
mi
Hp = 222
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11893740
86 X = -3629909
85
Y = 8731114
22 feet Y = 2620677
92 meter
Z = -16745533
95 Z = -5121659
34
XDOT = -9189
864719 XDOT = -2715
478542
YDOT = -22739
186556 feet/sec YDOT = -6961
748978 meter/sec
ZDOT = -5322
903049 ZDOT = -1635
819496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14340705
63 X = -4371047
07
Y = 3048160
56 feet Y = 929079
34 meter
Z = -16827335
31 Z = -5128971
80
XDOT = 1343
363536 XDOT = 409
457206
YDOT = -23441
041365 feet/sec YDOT = -7144
829408 meter/sec
ZDOT = -5384
995618 ZDOT = -1641
346664
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 21039
56760700
00016717 00000-0 10270-3 0 9047
2 25544 51
6402 258
8969 0002638 347
8335 12
2751 15
48941399 28651
Satellite: ISS
Catalog Number: 25544
Epoch time: 21039
56760700 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 258
8969 deg
Eccentricity:
0002638
Arg of perigee: 347
8335 deg
Mean anomaly: 12
2751 deg
Mean motion: 15
48941399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 332
Coasting Arc #6 (Orbit 2875)
---------------------------------------
Vector Time (GMT): 2021/040/05:21:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2569953
25 A = 6795642
78 meter
Y = -4364308
38 meter E =
0007669
Z = 4524711
35 I = 51
25098
XDOT = 4132
549835 Wp = 96
57107
YDOT = 5657
752253 meter/sec RA = 254
68625 deg
ZDOT = 3104
555086 TA = 322
10637
MA = 322
16032
Ha = 229
077 n
mi
Hp = 222
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8431605
14 X = 2596587
53
Y = -14318597
04 feet Y = -4335420
63 meter
Z = 14844853
51 Z = 4537259
23
XDOT = 13558
234368 XDOT = 4053
896326
YDOT = 18562
179309 feet/sec YDOT = 5703
525459 meter/sec
ZDOT = 10185
548181 ZDOT = 3124
438014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2535475
00 X = 772812
78
Y = 16369237
63 feet Y = 4989343
63 meter
Z = 14903130
15 Z = 4542474
07
XDOT = -20969
465686 XDOT = -6391
493141
YDOT = -6125
332648 feet/sec YDOT = -1867
001391 meter/sec
ZDOT = 10277
764720 ZDOT = 3132
662687
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 21040
27730115
00016717 00000-0 10270-3 0 9055
2 25544 51
6410 255
3880 0002566 349
7276 10
3822 15
48976074 28767
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
27730115 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 255
3880 deg
Eccentricity:
0002566
Arg of perigee: 349
7276 deg
Mean anomaly: 10
3822 deg
Mean motion: 15
48976074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2876
Checksum: 306
Coasting Arc #7 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2021/040/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4070863
78 A = 6799822
30 meter
Y = 4356669
29 meter E =
0012189
Z = 3260680
13 I = 51
26750
XDOT = -2227
554125 Wp = 80
06535
YDOT = 5617
838795 meter/sec RA = 252
95846 deg
ZDOT = -4707
916286 TA = 61
97778
MA = 61
85453
Ha = 229
110 n
mi
Hp = 222
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13355852
30 X = 4006005
64
Y = 14293534
43 feet Y = 4401829
83 meter
Z = 10697769
44 Z = 3280296
80
XDOT = -7308
248440 XDOT = -2267
341372
YDOT = 18431
229641 feet/sec YDOT = 5592
706438 meter/sec
ZDOT = -15445
919575 ZDOT = -4718
832871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7850295
86 X = 2392770
18
Y = 17863411
07 feet Y = 5444767
69 meter
Z = 10788771
38 Z = 3288417
52
XDOT = -11553
096858 XDOT = -3521
383922
YDOT = 14470
221081 feet/sec YDOT = 4410
523385 meter/sec
ZDOT = -15496
633573 ZDOT = -4723
373913
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 21040
59988798
00016717 00000-0 10270-3 0 9063
2 25544 51
6404 253
7904 0002702 346
6981 13
4097 15
48966443 28813
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
59988798 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 253
7904 deg
Eccentricity:
0002702
Arg of perigee: 346
6981 deg
Mean anomaly: 13
4097 deg
Mean motion: 15
48966443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 340
Coasting Arc #8 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2021/041/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4442501
96 A = 6799813
28 meter
Y = -3966280
66 meter E =
0005297
Z = -3282477
72 I = 51
27746
XDOT = 1715
249511 Wp = 56
96781
YDOT = -5799
423435 meter/sec RA = 247
98563 deg
ZDOT = 4694
504582 TA = 264
81022
MA = 264
87067
Ha = 229
240 n
mi
Hp = 222
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14575137
66 X = -4381875
82
Y = -13012731
81 feet Y = -4015620
85 meter
Z = -10769283
84 Z = -3303909
71
XDOT = 5627
459027 XDOT = 1757
170579
YDOT = -19026
979773 feet/sec YDOT = -5780
008004 meter/sec
ZDOT = 15401
917921 ZDOT = 4702
937950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9714073
56 X = -2960849
62
Y = -16889364
32 feet Y = -5147878
24 meter
Z = -10868737
26 Z = -3312791
12
XDOT = 9952
949463 XDOT = 3033
658996
YDOT = -15643
764270 feet/sec YDOT = -4768
219350 meter/sec
ZDOT = 15441
092894 ZDOT = 4706
445114
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
56765254
00016717 00000-0 10270-3 0 9072
2 25544 51
6394 249
0028 0002505 354
7360 5
3763 15
48945437 28964
Satellite: ISS
Catalog Number: 25544
Epoch time: 21041
56765254 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 249
0028 deg
Eccentricity:
0002505
Arg of perigee: 354
7360 deg
Mean anomaly: 5
3763 deg
Mean motion: 15
48945437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 320
Coasting Arc #9 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2021/042/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4763462
86 A = 6799812
79 meter
Y = 3575356
22 meter E =
0012628
Z = 3272304
66 I = 51
29121
XDOT = -1208
389956 Wp = 80
34465
YDOT = 5927
812014 meter/sec RA = 243
01431 deg
ZDOT = -4700
096362 TA = 61
55251
MA = 61
42533
Ha = 229
267 n
mi
Hp = 222
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15628158
98 X = 4707233
72
Y = 11730171
34 feet Y = 3628310
30 meter
Z = 10735907
67 Z = 3295306
26
XDOT = -3964
533977 XDOT = -1251
757234
YDOT = 19448
202146 feet/sec YDOT = 5914
056443 meter/sec
ZDOT = -15420
263655 ZDOT = -4706
071353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11388593
24 X = 3471243
22
Y = 15806088
32 feet Y = 4817695
72 meter
Z = 10842670
44 Z = 3304845
95
XDOT = -8284
977133 XDOT = -2525
261030
YDOT = 16605
865276 feet/sec YDOT = 5061
467736 meter/sec
ZDOT = -15448
010731 ZDOT = -4708
553671
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
59993063
00016717 00000-0 10270-3 0 9088
2 25544 51
6392 243
8965 0002604 356
6304 3
4828 15
48954070 29126
Satellite: ISS
Catalog Number: 25544
Epoch time: 21042
59993063 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 243
8965 deg
Eccentricity:
0002604
Arg of perigee: 356
6304 deg
Mean anomaly: 3
4828 deg
Mean motion: 15
48954070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 318
Coasting Arc #10 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2021/043/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5060891
07 A = 6799763
49 meter
Y = -3126823
69 meter E =
0005691
Z = -3294835
80 I = 51
30699
XDOT = 671
487651 Wp = 61
29028
YDOT = -6016
021548 meter/sec RA = 238
04391 deg
ZDOT = 4686
705513 TA = 260
33824
MA = 260
40254
Ha = 229
397 n
mi
Hp = 222
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16603973
32 X = -5009545
99
Y = -10258607
92 feet Y = -3183131
22 meter
Z = -10809828
73 Z = -3319293
94
XDOT = 2203
043475 XDOT = 715
946233
YDOT = -19737
603505 feet/sec YDOT = -6008
263784 meter/sec
ZDOT = 15376
330422 ZDOT = 4690
075350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13006253
69 X = -3964306
12
Y = -14467226
57 feet Y = -4409610
66 meter
Z = -10923373
29 Z = -3329444
18
XDOT = 6471
042227 XDOT = 1972
373671
YDOT = -17417
420516 feet/sec YDOT = -5308
829773 meter/sec
ZDOT = 15391
965957 ZDOT = 4691
471224
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
56769366
00016717 00000-0 10270-3 0 9094
2 25544 51
6386 239
1094 0002429 6
8161 353
3022 15
48946622 29273
Satellite: ISS
Catalog Number: 25544
Epoch time: 21043
56769366 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 239
1094 deg
Eccentricity:
0002429
Arg of perigee: 6
8161 deg
Mean anomaly: 353
3022 deg
Mean motion: 15
48946622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 321
Coasting Arc #11 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2021/044/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5307662
68 A = 6799812
84 meter
Y = 2686918
79 meter E =
0013005
Z = 3284404
53 I = 51
32590
XDOT = -149
441786 Wp = 81
25403
YDOT = 6053
737102 meter/sec RA = 233
07521 deg
ZDOT = -4693
034624 TA = 60
49695
MA = 60
36731
Ha = 229
396 n
mi
Hp = 222
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17413591
47 X = 5261269
04
Y = 8815350
36 feet Y = 2746013
65 meter
Z = 10775605
43 Z = 3310073
41
XDOT = -490
294574 XDOT = -194
330104
YDOT = 19861
342199 feet/sec YDOT = 6051
814733 meter/sec
ZDOT = -15397
095222 ZDOT = -4693
869830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14413754
16 X = 4393312
27
Y = 13061567
40 feet Y = 3981165
74 meter
Z = 10894787
28 Z = 3320731
16
XDOT = -4636
344249 XDOT = -1413
157727
YDOT = 18010
934495 feet/sec YDOT = 5489
732834 meter/sec
ZDOT = -15400
946022 ZDOT = -4694
208348
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
59997182
00016717 00000-0 10270-3 0 9109
2 25544 51
6384 234
0034 0002431 6
5571 353
5610 15
48938828 29436
Satellite: ISS
Catalog Number: 25544
Epoch time: 21044
59997182 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 234
0034 deg
Eccentricity:
0002431
Arg of perigee: 6
5571 deg
Mean anomaly: 353
5610 deg
Mean motion: 15
48938828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 309
Coasting Arc #12 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2021/045/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5521966
77 A = 6799701
11 meter
Y = -2194813
52 meter E =
0005967
Z = -3307319
99 I = 51
34939
XDOT = -394
752241 Wp = 63
81523
YDOT = -6045
351221 meter/sec RA = 228
10743 deg
ZDOT = 4680
098062 TA = 257
66926
MA = 257
73607
Ha = 229
494 n
mi
Hp = 222
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18116688
89 X = -5480948
70
Y = -7200831
76 feet Y = -2256334
98 meter
Z = -10850787
38 Z = -3334043
00
XDOT = -1295
118902 XDOT = -349
854507
YDOT = -19833
829464 feet/sec YDOT = -6049
514314 meter/sec
ZDOT = 15354
652433 ZDOT = 4678
289962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15714574
73 X = -4789802
38
Y = -11419729
20 feet Y = -3480733
46 meter
Z = -10974876
19 Z = -3345142
26
XDOT = 2690
398354 XDOT = 820
033418
YDOT = -18422
025137 feet/sec YDOT = -5615
033262 meter/sec
ZDOT = 15346
214680 ZDOT = 4677
526235
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
56773220
00016717 00000-0 10270-3 0 9113
2 25544 51
6407 229
2162 0002459 14
6024 345
5197 15
48952918 29586
Satellite: ISS
Catalog Number: 25544
Epoch time: 21045
56773220 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 229
2162 deg
Eccentricity:
0002459
Arg of perigee: 14
6024 deg
Mean anomaly: 345
5197 deg
Mean motion: 15
48952918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 313
Coasting Arc #13 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2021/046/13:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5687798
35 A = 6799778
85 meter
Y = 1721147
66 meter E =
0013492
Z = 3295610
06 I = 51
37233
XDOT = 914
171896 Wp = 81
65641
YDOT = 5990
565244 meter/sec RA = 223
14142 deg
ZDOT = -4687
904018 TA = 59
96792
MA = 59
83414
Ha = 229
561 n
mi
Hp = 222
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18660755
74 X = 5652121
44
Y = 5646809
89 feet Y = 1784553
44 meter
Z = 10812368
96 Z = 3323151
70
XDOT = 2999
251626 XDOT = 869
886206
YDOT = 19654
085447 feet/sec YDOT = 6000
540273 meter/sec
ZDOT = -15380
262525 ZDOT = -4683
571362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16794956
13 X = 5119102
63
Y = 9759997
23 feet Y = 2974847
16 meter
Z = 10940269
28 Z = 3334594
08
XDOT = -774
254923 XDOT = -235
992900
YDOT = 18616
931425 feet/sec YDOT = 5674
440698 meter/sec
ZDOT = -15360
088904 ZDOT = -4681
755098
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
60000804
00016717 00000-0 10270-3 0 9121
2 25544 51
6399 224
1099 0002489 18
6484 341
4757 15
48937105 29742
Satellite: ISS
Catalog Number: 25544
Epoch time: 21046
60000804 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 224
1099 deg
Eccentricity:
0002489
Arg of perigee: 18
6484 deg
Mean anomaly: 341
4757 deg
Mean motion: 15
48937105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 317
Coasting Arc #14 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2021/046/21:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4010202
36 A = 6793132
32 meter
Y = -1925333
86 meter E =
0007060
Z = 5131158
09 I = 51
36061
XDOT = 4741
639561 Wp = 41
30466
YDOT = 5825
868216 meter/sec RA = 221
58964 deg
ZDOT = -1513
373887 TA = 63
37805
MA = 63
30575
Ha = 229
498 n
mi
Hp = 222
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13156831
87 X = 4006510
34
Y = -6316712
13 feet Y = -1880509
22 meter
Z = 16834508
17 Z = 5150628
76
XDOT = 15556
560239 XDOT = 4683
491446
YDOT = 19113
740867 feet/sec YDOT = 5878
567434 meter/sec
ZDOT = -4965
137426 ZDOT = -1490
482985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8647839
07 X = -2635861
35
Y = -11626107
96 feet Y = -3543637
71 meter
Z = 16924899
86 Z = 5158709
48
XDOT = 15005
641683 XDOT = 4573
719585
YDOT = -18265
292897 feet/sec YDOT = -5567
261275 meter/sec
ZDOT = -4858
787419 ZDOT = -1480
958405
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
92259244
00016717 00000-0 10270-3 0 9131
2 25544 51
6422 222
5187 0002784 17
0121 343
1122 15
48971730 29790
Satellite: ISS
Catalog Number: 25544
Epoch time: 21046
92259244 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 222
5187 deg
Eccentricity:
0002784
Arg of perigee: 17
0121 deg
Mean anomaly: 343
1122 deg
Mean motion: 15
48971730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
Checksum: 295
Coasting Arc #15 (Orbit 2993)
---------------------------------------
Vector Time (GMT): 2021/047/21:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3819278
06 A = 6793240
53 meter
Y = 2281987
72 meter E =
0014421
Z = -5146160
13 I = 51
38756
XDOT = -5228
520570 Wp = 90
45553
YDOT = -5378
462919 meter/sec RA = 216
62648 deg
ZDOT = 1498
948474 TA = 194
04825
MA = 194
08841
Ha = 229
728 n
mi
Hp = 222
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12530439
84 X = -3819515
49
Y = 7486836
34 feet Y = 2239276
19 meter
Z = -16883727
47 Z = -5164713
01
XDOT = -17153
938878 XDOT = -5175
269250
YDOT = -17645
875720 feet/sec YDOT = -5436
634183 meter/sec
ZDOT = 4917
809954 ZDOT = 1473
680498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9863982
50 X = 3006541
86
Y = 10623119
14 feet Y = 3237926
71 meter
Z = -16969858
08 Z = -5172412
74
XDOT = -12988
277430 XDOT = -3958
826961
YDOT = 19710
032105 feet/sec YDOT = 6007
617786 meter/sec
ZDOT = 4800
407002 ZDOT = 1463
164054
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
89035180
00016717 00000-0 10270-3 0 9140
2 25544 51
6429 217
7320 0002799 20
0298 340
0961 15
48930799 29941
Satellite: ISS
Catalog Number: 25544
Epoch time: 21047
89035180 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 217
7320 deg
Eccentricity:
0002799
Arg of perigee: 20
0298 deg
Mean anomaly: 340
0961 deg
Mean motion: 15
48930799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2994
Checksum: 325
Coasting Arc #16 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2021/048/06:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3085139
68 A = 6792582
91 meter
Y = 2987047
85 meter E =
0015480
Z = -5276219
01 I = 51
39711
XDOT = -5904
870041 Wp = 85
08976
YDOT = -4805
869907 meter/sec RA = 214
72030 deg
ZDOT = 735
128248 TA = 191
95615
MA = 191
99294
Ha = 229
681 n
mi
Hp = 222
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10121849
34 X = -3092684
10
Y = 9800025
77 feet Y = 2952505
16 meter
Z = -17310429
82 Z = -5291223
60
XDOT = -19372
933205 XDOT = -5854
261240
YDOT = -15767
289720 feet/sec YDOT = -4871
619416 meter/sec
ZDOT = 2411
838083 ZDOT = 706
568395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3731115
49 X = -1137244
00
Y = -13496483
52 feet Y = -4113728
18 meter
Z = -17380075
65 Z = -5297447
06
XDOT = 22199
379877 XDOT = 6766
370987
YDOT = -9058
678889 feet/sec YDOT = -2761
085326 meter/sec
ZDOT = 2279
147073 ZDOT = 694
684028
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
27745511
00016717 00000-0 10270-3 0 9150
2 25544 51
6438 215
8192 0002939 17
7841 342
3411 15
48968438 30005
Satellite: ISS
Catalog Number: 25544
Epoch time: 21048
27745511 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 215
8192 deg
Eccentricity:
0002939
Arg of perigee: 17
7841 deg
Mean anomaly: 342
3411 deg
Mean motion: 15
48968438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 309
Coasting Arc #17 (Orbit 3015)
---------------------------------------
Vector Time (GMT): 2021/049/06:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2811495
28 A = 6792506
60 meter
Y = -3232468
34 meter E =
0005507
Z = 5268344
80 I = 51
42649
XDOT = 6310
987674 Wp = 42
31135
YDOT = 4283
784022 meter/sec RA = 209
75979 deg
ZDOT = -735
092416 TA = 54
76244
MA = 54
71092
Ha = 229
557 n
mi
Hp = 222
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9224065
88 X = 2821842
59
Y = -10605211
10 feet Y = -3200970
13 meter
Z = 17284595
78 Z = 5282026
96
XDOT = 20705
340139 XDOT = 6266
186648
YDOT = 14054
409521 feet/sec YDOT = 4354
107514 meter/sec
ZDOT = -2411
720524 ZDOT = -704
545583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5094853
32 X = 1552911
29
Y = 13015261
04 feet Y = 3967051
56 meter
Z = 17348100
62 Z = 5287701
07
XDOT = -21182
732616 XDOT = -6456
496901
YDOT = 11336
787361 feet/sec YDOT = 3455
452787 meter/sec
ZDOT = -2269
787617 ZDOT = -691
831266
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
30972786
00016717 00000-0 10270-3 0 9162
2 25544 51
6445 210
7135 0002899 19
3013 340
8246 15
48990258 30169
Satellite: ISS
Catalog Number: 25544
Epoch time: 21049
30972786 = yrday
fracday
Element set: 916
Inclination: 51
6445 deg
RA of node: 210
7135 deg
Eccentricity:
0002899
Arg of perigee: 19
3013 deg
Mean anomaly: 340
8246 deg
Mean motion: 15
48990258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3016
Checksum: 315
Coasting Arc #18 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2021/050/06:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2510601
10 A = 6792557
52 meter
Y = 3475501
54 meter E =
0015809
Z = -5281997
91 I = 51
45628
XDOT = -6650
143018 Wp = 85
11284
YDOT = -3708
374597 meter/sec RA = 204
80112 deg
ZDOT = 724
019869 TA = 191
82007
MA = 191
85722
Ha = 229
780 n
mi
Hp = 222
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8236880
26 X = -2523622
11
Y = 11402564
10 feet Y = 3447353
27 meter
Z = -17329389
47 Z = -5294224
94
XDOT = -21818
054521 XDOT = -6611
697409
YDOT = -12166
583325 feet/sec YDOT = -3782
526315 meter/sec
ZDOT = 2375
393272 ZDOT = 691
810038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6476612
64 X = -1974071
53
Y = -12407584
08 feet Y = -3781831
63 meter
Z = -17386136
72 Z = -5299294
47
XDOT = 19844
935320 XDOT = 6048
736285
YDOT = -13462
975977 feet/sec YDOT = -4103
515078 meter/sec
ZDOT = 2225
721955 ZDOT = 678
400052
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
27748372
00016717 00000-0 10270-3 0 9173
2 25544 51
6442 205
9267 0003054 23
3477 336
7811 15
48974633 30319
Satellite: ISS
Catalog Number: 25544
Epoch time: 21050
27748372 = yrday
fracday
Element set: 917
Inclination: 51
6442 deg
RA of node: 205
9267 deg
Eccentricity:
0003054
Arg of perigee: 23
3477 deg
Mean anomaly: 336
7811 deg
Mean motion: 15
48974633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 306
Coasting Arc #19 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2021/050/19:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 122948
84 A = 6793081
47 meter
Y = -4395934
17 meter E =
0005200
Z = 5173009
28 I = 51
47304
XDOT = 7322
688886 Wp = 90
78791
YDOT = 1806
896053 meter/sec RA = 202
11644 deg
ZDOT = 1360
171416 TA = 346
09269
MA = 346
10700
Ha = 229
847 n
mi
Hp = 222
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 403375
44 X = 146969
25
Y = -14422356
19 feet Y = -4394424
89 meter
Z = 16971815
21 Z = 5173664
90
XDOT = 24024
569836 XDOT = 7295
332557
YDOT = 5928
136656 feet/sec YDOT = 1888
630701 meter/sec
ZDOT = 4462
504645 ZDOT = 1395
675146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14136727
38 X = -4308874
51
Y = -2866841
48 feet Y = -873813
28 meter
Z = 16974797
20 Z = 5173918
19
XDOT = 9923
774324 XDOT = 3024
766414
YDOT = -21511
296236 feet/sec YDOT = -6556
643093 meter/sec
ZDOT = 4627
462842 ZDOT = 1410
450674
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
85813658
00016717 00000-0 10270-3 0 9188
2 25544 51
6424 203
0531 0002957 31
0095 329
1229 15
48964210 30404
Satellite: ISS
Catalog Number: 25544
Epoch time: 21050
85813658 = yrday
fracday
Element set: 918
Inclination: 51
6424 deg
RA of node: 203
0531 deg
Eccentricity:
0002957
Arg of perigee: 31
0095 deg
Mean anomaly: 329
1229 deg
Mean motion: 15
48964210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 286
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