[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 20th 2021
- spaceflight nasa gov will be taken offline in the next 30 days *
- *
- Current information about the International Space Station can be *
- found at www nasa gov/station *
- *
- Predicted ISS and visiting vehicle sightings opportunities can be *
- found at spotthestation nasa gov *
- *
- Updated ISS trajectory information will be made available as a CCSDS *
- Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
- system *
- Included in the OEM are a sequence of events with ISS maneuver *
- details (in the comment section), predicted post-maneuver state *
- vectors, predicted coasting state vectors at 4-minute intervals, *
- and ISS ballistic details *
- *
- OEMs will be provided in xml and txt formats *
- Links to the OEMs and more details to follow *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
021/16:17:19
647 2
1 2
2 2
2
N/A -0
8 -0
2 228
4
000/00:06:39
293 -0
1 0
0 223
7
026/07:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 223
5
029/19:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 223
3
Coasting Arc #1 (Orbit 2491)
---------------------------------------
Vector Time (GMT): 2021/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6510864
80 A = 6801894
24 meter
Y = 457805
22 meter E =
0007032
Z = -1905704
74 I = 51
77665
XDOT = 1286
262541 Wp = 38
54321
YDOT = 5038
620682 meter/sec RA = 17
31648 deg
ZDOT = 5621
494987 TA = 300
55539
MA = 300
62477
Ha = 228
593 n
mi
Hp = 222
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21361105
00 X = 6514518
12
Y = 1501985
63 feet Y = 530634
98 meter
Z = -6252312
15 Z = -1874069
60
XDOT = 4220
021461 XDOT = 1202
518414
YDOT = 16530
907750 feet/sec YDOT = 5052
535889 meter/sec
ZDOT = 18443
225024 ZDOT = 5627
539974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7421773
80 X = 2262156
65
Y = 20131692
47 feet Y = 6136139
86 meter
Z = -6105440
77 Z = -1860938
35
XDOT = -11923
799039 XDOT = -3634
373947
YDOT = 9980
789557 feet/sec YDOT = 3042
144657 meter/sec
ZDOT = 18471
023355 ZDOT = 5629
967919
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21015
50366467
00016717 00000-0 10270-3 0 9003
2 25544 51
6428 17
9288 0000133 218
1715 141
9426 15
49314799 24921
Satellite: ISS
Catalog Number: 25544
Epoch time: 21015
50366467 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 17
9288 deg
Eccentricity:
0000133
Arg of perigee: 218
1715 deg
Mean anomaly: 141
9426 deg
Mean motion: 15
49314799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2492
Checksum: 308
Coasting Arc #2 (Orbit 2507)
---------------------------------------
Vector Time (GMT): 2021/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6555741
62 A = 6802087
19 meter
Y = 6351
29 meter E =
0013601
Z = 1789676
68 I = 51
74361
XDOT = -1559
393395 Wp = 114
51942
YDOT = -4916
458751 meter/sec RA = 12
37528 deg
ZDOT = -5666
362146 TA = 45
88492
MA = 45
77310
Ha = 228
524 n
mi
Hp = 222
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21508338
64 X = -6564018
37
Y = 20837
58 feet Y = -67006
11 meter
Z = 5871642
65 Z = 1757812
32
XDOT = -5116
120063 XDOT = -1476
777051
YDOT = -16130
114011 feet/sec YDOT = -4933
434744 meter/sec
ZDOT = -18590
426988 ZDOT = -5673
736471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9206090
99 X = -2806016
53
Y = -19482620
13 feet Y = -5938302
61 meter
Z = 5723692
36 Z = 1744581
43
XDOT = 11044
009315 XDOT = 3366
214039
YDOT = -10718
235106 feet/sec YDOT = -3266
918060 meter/sec
ZDOT = -18624
404554 ZDOT = -5676
718508
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21016
53571202
00016717 00000-0 10270-3 0 9013
2 25544 51
6420 12
8209 0000305 299
3247 60
7873 15
49311686 25086
Satellite: ISS
Catalog Number: 25544
Epoch time: 21016
53571202 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 12
8209 deg
Eccentricity:
0000305
Arg of perigee: 299
3247 deg
Mean anomaly: 60
7873 deg
Mean motion: 15
49311686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2508
Checksum: 283
Coasting Arc #3 (Orbit 2522)
---------------------------------------
Vector Time (GMT): 2021/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6562669
94 A = 6802206
60 meter
Y = -501701
11 meter E =
0007698
Z = -1705608
48 I = 51
71095
XDOT = 1840
677443 Wp = 36
67060
YDOT = 4775
658986 meter/sec RA = 7
43302 deg
ZDOT = 5696
940577 TA = 304
69058
MA = 304
76309
Ha = 228
577 n
mi
Hp = 222
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21531069
37 X = 6576077
01
Y = -1646001
03 feet Y = -428237
58 meter
Z = -5595828
34 Z = -1673697
93
XDOT = 6038
967989 XDOT = 1759
466054
YDOT = 15668
172526 feet/sec YDOT = 4795
788452 meter/sec
ZDOT = 18690
749926 ZDOT = 5705
684576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11006970
72 X = 3354924
68
Y = 18622010
31 feet Y = 5675988
74 meter
Z = -5447649
94 Z = -1660443
70
XDOT = -10087
163802 XDOT = -3074
567527
YDOT = 11422
769913 feet/sec YDOT = 3481
660269 meter/sec
ZDOT = 18731
093422 ZDOT = 5709
237275
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21017
50325542
00016717 00000-0 10270-3 0 9026
2 25544 51
6424 8
0337 0000144 271
4844 88
6289 15
49309747 25236
Satellite: ISS
Catalog Number: 25544
Epoch time: 21017
50325542 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 8
0337 deg
Eccentricity:
0000144
Arg of perigee: 271
4844 deg
Mean anomaly: 88
6289 deg
Mean motion: 15
49309747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2523
Checksum: 296
Coasting Arc #4 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2021/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6536854
92 A = 6802352
29 meter
Y = 970318
39 meter E =
0013472
Z = 1585439
62 I = 51
67809
XDOT = -2086
531419 Wp = 116
53136
YDOT = -4629
704013 meter/sec RA = 2
48729 deg
ZDOT = -5737
530020 TA = 46
16957
MA = 46
05828
Ha = 228
506 n
mi
Hp = 222
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21446374
41 X = -6554920
46
Y = 3183459
28 feet Y = 897117
51 meter
Z = 5201573
54 Z = 1553643
05
XDOT = -6845
575521 XDOT = -2006
736617
YDOT = -15189
317628 feet/sec YDOT = -4652
590760 meter/sec
ZDOT = -18823
917390 ZDOT = -5747
471680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12653040
30 X = -3856646
68
Y = -17649257
33 feet Y = -5379493
63 meter
Z = 5053913
56 Z = 1540432
85
XDOT = 9151
879973 XDOT = 2789
493016
YDOT = -11995
393689 feet/sec YDOT = -3656
195996 meter/sec
ZDOT = -18869
826663 ZDOT = -5751
523167
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21018
53529845
00016717 00000-0 10270-3 0 9033
2 25544 51
6428 2
9257 0000416 319
8333 40
2787 15
49317629 25398
Satellite: ISS
Catalog Number: 25544
Epoch time: 21018
53529845 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 2
9257 deg
Eccentricity:
0000416
Arg of perigee: 319
8333 deg
Mean anomaly: 40
2787 deg
Mean motion: 15
49317629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 315
Coasting Arc #5 (Orbit 2553)
---------------------------------------
Vector Time (GMT): 2021/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6468097
76 A = 6802479
18 meter
Y = -1464422
06 meter E =
0008474
Z = -1498105
72 I = 51
64364
XDOT = 2340
973545 Wp = 35
43004
YDOT = 4465
765977 meter/sec RA = 357
54069 deg
ZDOT = 5764
956399 TA = 308
25049
MA = 308
32672
Ha = 228
566 n
mi
Hp = 222
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21220793
17 X = 6491269
44
Y = -4804534
33 feet Y = -1391961
53 meter
Z = -4915045
02 Z = -1466630
65
XDOT = 7680
359401 XDOT = 2262
859720
YDOT = 14651
463179 feet/sec YDOT = 4491
507478 meter/sec
ZDOT = 18913
898947 ZDOT = 5776
138126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14276001
38 X = 4351325
22
Y = 16462593
48 feet Y = 5017798
49 meter
Z = -4768865
77 Z = -1453550
29
XDOT = -8146
535166 XDOT = -2483
063919
YDOT = 12535
777052 feet/sec YDOT = 3820
904845 meter/sec
ZDOT = 18965
570196 ZDOT = 5780
705796
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21019
50283862
00016717 00000-0 10270-3 0 9048
2 25544 51
6420 358
1388 0000270 320
0395 40
0735 15
49309460 25543
Satellite: ISS
Catalog Number: 25544
Epoch time: 21019
50283862 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 358
1388 deg
Eccentricity:
0000270
Arg of perigee: 320
0395 deg
Mean anomaly: 40
0735 deg
Mean motion: 15
49309460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2554
Checksum: 285
Coasting Arc #6 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2021/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6370580
91 A = 6802628
99 meter
Y = 1927281
22 meter E =
0013298
Z = 1375328
29 I = 51
61047
XDOT = -2561
250129 Wp = 119
02274
YDOT = -4301
162823 meter/sec RA = 352
59072 deg
ZDOT = -5800
303410 TA = 46
01518
MA = 45
90561
Ha = 228
495 n
mi
Hp = 222
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20900856
01 X = -6398339
33
Y = 6323101
11 feet Y = 1855885
53 meter
Z = 4512231
92 Z = 1344315
69
XDOT = -8403
051604 XDOT = -2484
788796
YDOT = -14111
426584 feet/sec YDOT = -4329
376818 meter/sec
ZDOT = -19029
866831 ZDOT = -5812
559205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15725596
44 X = -4793161
80
Y = -15192503
73 feet Y = -4630675
14 meter
Z = 4368188
81 Z = 1331423
95
XDOT = 7180
788625 XDOT = 2188
704373
YDOT = -12955
834631 feet/sec YDOT = -3948
938395 meter/sec
ZDOT = -19086
528430 ZDOT = -5817
573866
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21020
53488036
00016717 00000-0 10270-3 0 9054
2 25544 51
6423 353
0312 0000493 320
8755 39
2360 15
49309423 25703
Satellite: ISS
Catalog Number: 25544
Epoch time: 21020
53488036 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 353
0312 deg
Eccentricity:
0000493
Arg of perigee: 320
8755 deg
Mean anomaly: 39
2360 deg
Mean motion: 15
49309423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 281
Coasting Arc #7 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2021/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6226632
29 A = 6802707
45 meter
Y = -2408109
34 meter E =
0009143
Z = -1285060
65 I = 51
57763
XDOT = 2789
080587 Wp = 35
07021
YDOT = 4118
491842 meter/sec RA = 347
63897 deg
ZDOT = 5824
415113 TA = 310
96869
MA = 311
04777
Ha = 228
533 n
mi
Hp = 222
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20428583
61 X = 6259339
72
Y = -7900621
20 feet Y = -2338295
71 meter
Z = -4216078
23 Z = -1254735
24
XDOT = 9150
526861 XDOT = 2714
527824
YDOT = 13512
112342 feet/sec YDOT = 4149
264208 meter/sec
ZDOT = 19108
973467 ZDOT = 5837
782302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17110175
77 X = 5215181
58
Y = 13717021
99 feet Y = 4180948
30 meter
Z = -4075211
91 Z = -1242124
59
XDOT = -6151
110424 XDOT = -1874
858457
YDOT = 13339
990614 feet/sec YDOT = 4066
029139 meter/sec
ZDOT = 19170
799168 ZDOT = 5843
259587
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21021
50241760
00016717 00000-0 10270-3 0 9064
2 25544 51
6426 348
2437 0000393 322
3345 37
7778 15
49313651 25851
Satellite: ISS
Catalog Number: 25544
Epoch time: 21021
50241760 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 348
2437 deg
Eccentricity:
0000393
Arg of perigee: 322
3345 deg
Mean anomaly: 37
7778 deg
Mean motion: 15
49313651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2585
Checksum: 299
Coasting Arc #8 (Orbit 2587)
---------------------------------------
Vector Time (GMT): 2021/021/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -229477
64 A = 6792790
90 meter
Y = -4265169
07 meter E =
0012362
Z = -5292616
43 I = 51
53803
XDOT = 7522
156989 Wp = 94
80719
YDOT = -1229
035329 meter/sec RA = 346
74859 deg
ZDOT = 664
629789 TA = 181
56053
MA = 181
56439
Ha = 228
434 n
mi
Hp = 223
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -752879
40 X = -156058
05
Y = -13993336
85 feet Y = -4267324
47 meter
Z = -17364227
15 Z = -5293553
03
XDOT = 24678
992745 XDOT = 7532
113034
YDOT = -4032
268140 feet/sec YDOT = -1144
861521 meter/sec
ZDOT = 2180
543928 ZDOT = 701
193054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1973363
94 X = -601481
33
Y = -13868770
20 feet Y = -4227201
16 meter
Z = -17368354
44 Z = -5293874
43
XDOT = 23151
400854 XDOT = 7056
546980
YDOT = -6236
173727 feet/sec YDOT = -1900
785752 meter/sec
ZDOT = 2350
297476 ZDOT = 716
370671
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21021
69592566
00016717 00000-0 10270-3 0 9078
2 25544 51
6461 347
2867 0002206 276
9398 83
1501 15
48900165 25886
Satellite: ISS
Catalog Number: 25544
Epoch time: 21021
69592566 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 347
2867 deg
Eccentricity:
0002206
Arg of perigee: 276
9398 deg
Mean anomaly: 83
1501 deg
Mean motion: 15
48900165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2588
Checksum: 328
Coasting Arc #9 (Orbit 2603)
---------------------------------------
Vector Time (GMT): 2021/022/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 630236
04 A = 6792696
31 meter
Y = 4218427
16 meter E =
0001862
Z = 5286376
50 I = 51
50522
XDOT = -7393
834970 Wp = 14
84223
YDOT = 1900
994687 meter/sec RA = 341
79638 deg
ZDOT = -633
661026 TA = 81
23505
MA = 81
21397
Ha = 228
368 n
mi
Hp = 223
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2067703
56 X = 557339
64
Y = 13839984
11 feet Y = 4225066
97 meter
Z = 17343754
92 Z = 5289261
13
XDOT = -24257
988747 XDOT = -7411
465031
YDOT = 6236
859208 feet/sec YDOT = 1818
212968 meter/sec
ZDOT = -2078
940374 ZDOT = -669
619561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3500793
21 X = 1067041
77
Y = 13531738
60 feet Y = 4124473
92 meter
Z = 17356926
29 Z = 5290391
13
XDOT = -22395
803218 XDOT = -6826
240821
YDOT = 8682
420236 feet/sec YDOT = 2646
401688 meter/sec
ZDOT = -2245
910021 ZDOT = -684
553375
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21022
72824315
00016717 00000-0 10270-3 0 9084
2 25544 51
6461 342
1813 0002271 281
5957 78
4938 15
48924581 26044
Satellite: ISS
Catalog Number: 25544
Epoch time: 21022
72824315 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 342
1813 deg
Eccentricity:
0002271
Arg of perigee: 281
5957 deg
Mean anomaly: 78
4938 deg
Mean motion: 15
48924581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2604
Checksum: 312
Coasting Arc #10 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2021/023/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1032175
83 A = 6792746
64 meter
Y = -4143039
42 meter E =
0012446
Z = -5293957
02 I = 51
47264
XDOT = 7186
601604 Wp = 92
46615
YDOT = -2555
093136 meter/sec RA = 336
84213 deg
ZDOT = 599
120646 TA = 183
27462
MA = 183
28278
Ha = 228
465 n
mi
Hp = 223
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3386403
65 X = -960055
77
Y = -13592649
00 feet Y = -4154178
26 meter
Z = -17368625
39 Z = -5298796
03
XDOT = 23578
089251 XDOT = 7211
729173
YDOT = -8382
851496 feet/sec YDOT = -2474
586936 meter/sec
ZDOT = 1965
618916 ZDOT = 634
090631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5008132
80 X = -1526478
88
Y = -13052707
45 feet Y = -3978465
23 meter
Z = -17390871
70 Z = -5300737
69
XDOT = 21320
935936 XDOT = 6498
621273
YDOT = -11012
765598 feet/sec YDOT = -3356
690954 meter/sec
ZDOT = 2128
024281 ZDOT = 648
621801
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21023
69604218
00016717 00000-0 10270-3 0 9090
2 25544 51
6455 337
3954 0002224 286
8312 73
2594 15
48904870 26196
Satellite: ISS
Catalog Number: 25544
Epoch time: 21023
69604218 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 337
3954 deg
Eccentricity:
0002224
Arg of perigee: 286
8312 deg
Mean anomaly: 73
2594 deg
Mean motion: 15
48904870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2619
Checksum: 320
Coasting Arc #11 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2021/024/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1414797
98 A = 6792686
70 meter
Y = 4022434
23 meter E =
0001991
Z = 5287405
99 I = 51
44210
XDOT = -6940
099839 Wp = 12
65212
YDOT = 3192
792115 meter/sec RA = 331
88575 deg
ZDOT = -569
973232 TA = 82
81905
MA = 82
79641
Ha = 228
373 n
mi
Hp = 223
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4641725
67 X = 1344030
02
Y = 13196962
71 feet Y = 4037859
33 meter
Z = 17347132
52 Z = 5294106
91
XDOT = -22769
356428 XDOT = -6972
518260
YDOT = 10475
039748 feet/sec YDOT = 3115
001715 meter/sec
ZDOT = -1869
990919 ZDOT = -603
763356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6415445
38 X = 1955427
75
Y = 12388489
20 feet Y = 3776011
51 meter
Z = 17378027
63 Z = 5296822
82
XDOT = -20063
192793 XDOT = -6115
261163
YDOT = 13242
069518 feet/sec YDOT = 4036
182789 meter/sec
ZDOT = -2026
944370 ZDOT = -617
812644
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21024
72835840
00016717 00000-0 10270-3 0 9104
2 25544 51
6457 332
2903 0002325 288
1845 71
9052 15
48918086 26350
Satellite: ISS
Catalog Number: 25544
Epoch time: 21024
72835840 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 332
2903 deg
Eccentricity:
0002325
Arg of perigee: 288
1845 deg
Mean anomaly: 71
9052 deg
Mean motion: 15
48918086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2635
Checksum: 308
Coasting Arc #12 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2021/025/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1793691
08 A = 6792697
36 meter
Y = -3873528
88 meter E =
0012445
Z = -5294685
55 I = 51
41284
XDOT = 6619
353152 Wp = 90
36454
YDOT = -3798
743771 meter/sec RA = 326
92655 deg
ZDOT = 537
686441 TA = 184
78786
MA = 184
79977
Ha = 228
466 n
mi
Hp = 223
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5884813
25 X = -1724524
80
Y = -12708428
07 feet Y = -3893199
95 meter
Z = -17371015
58 Z = -5303230
81
XDOT = 21717
037900 XDOT = 6658
728186
YDOT = -12463
070116 feet/sec YDOT = -3724
501294 meter/sec
ZDOT = 1764
063125 ZDOT = 569
935222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7773420
07 X = -2369338
44
Y = -11590360
57 feet Y = -3532741
90 meter
Z = -17410480
62 Z = -5306714
49
XDOT = 18518
801547 XDOT = 5644
530711
YDOT = -15290
105601 feet/sec YDOT = -4660
424187 meter/sec
ZDOT = 1913
885354 ZDOT = 583
352256
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21025
69615413
00016717 00000-0 10270-3 0 9114
2 25544 51
6459 327
5036 0002381 294
4318 65
6583 15
48912524 26500
Satellite: ISS
Catalog Number: 25544
Epoch time: 21025
69615413 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 327
5036 deg
Eccentricity:
0002381
Arg of perigee: 294
4318 deg
Mean anomaly: 65
6583 deg
Mean motion: 15
48912524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 308
Coasting Arc #13 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2021/026/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6002590
95 A = 6803301
96 meter
Y = 2700013
90 meter E =
0005768
Z = -1711446
76 I = 51
42794
XDOT = -682
485904 Wp = 149
28519
YDOT = -5102
117257 meter/sec RA = 323
81331 deg
ZDOT = -5668
848729 TA = 49
49161
MA = 49
44137
Ha = 228
622 n
mi
Hp = 223
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19693539
87 X = -6024024
19
Y = 8858313
33 feet Y = 2632768
94 meter
Z = -5614982
80 Z = -1740656
07
XDOT = -2239
126980 XDOT = -597
846404
YDOT = -16739
229847 feet/sec YDOT = -5109
275490 meter/sec
ZDOT = -18598
585069 ZDOT = -5671
958839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3124059
65 X = 952213
38
Y = -21330813
47 feet Y = -6501631
94 meter
Z = -5750644
11 Z = -1752796
32
XDOT = 13685
629988 XDOT = 4171
380020
YDOT = 7010
724104 feet/sec YDOT = 2136
868707 meter/sec
ZDOT = -18612
776356 ZDOT = -5673
174233
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21026
34135018
00016717 00000-0 10270-3 0 9126
2 25544 51
6434 324
3117 0001962 297
3111 62
7839 15
48890133 26609
Satellite: ISS
Catalog Number: 25544
Epoch time: 21026
34135018 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 324
3117 deg
Eccentricity:
0001962
Arg of perigee: 297
3111 deg
Mean anomaly: 62
7839 deg
Mean motion: 15
48890133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 289
Coasting Arc #14 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2021/027/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5736285
46 A = 6803251
89 meter
Y = -3237949
21 meter E =
0012731
Z = 1674022
20 I = 51
40052
XDOT = 1161
632926 Wp = 56
58660
YDOT = 5007
888341 meter/sec RA = 318
85170 deg
ZDOT = 5681
441828 TA = 321
78409
MA = 321
87427
Ha = 228
504 n
mi
Hp = 223
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18819834
19 X = 5763935
66
Y = -10623192
94 feet Y = -3173647
49 meter
Z = 5492198
82 Z = 1701952
89
XDOT = 3811
131647 XDOT = 1077
950467
YDOT = 16430
079860 feet/sec YDOT = 5020
410143 meter/sec
ZDOT = 18639
901012 ZDOT = 5686
881635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -796142
51 X = -242664
24
Y = 21562990
06 feet Y = 6572399
37 meter
Z = 5621943
80 Z = 1713568
47
XDOT = -14351
366344 XDOT = -4374
296462
YDOT = -5416
681503 feet/sec YDOT = -1651
004522 meter/sec
ZDOT = 18664
917327 ZDOT = 5689
066801
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21027
37366067
00016717 00000-0 10270-3 0 9131
2 25544 51
6425 319
2072 0002101 297
2899 62
8037 15
48929031 26768
Satellite: ISS
Catalog Number: 25544
Epoch time: 21027
37366067 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 319
2072 deg
Eccentricity:
0002101
Arg of perigee: 297
2899 deg
Mean anomaly: 62
8037 deg
Mean motion: 15
48929031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 313
Coasting Arc #15 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2021/028/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5435746
03 A = 6803357
69 meter
Y = 3733158
01 meter E =
0005643
Z = -1664076
11 I = 51
37526
XDOT = -1611
620420 Wp = 147
02120
YDOT = -4873
252594 meter/sec RA = 313
88725 deg
ZDOT = -5681
931283 TA = 51
23060
MA = 51
18019
Ha = 228
676 n
mi
Hp = 223
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17833812
44 X = -5469004
48
Y = 12247893
73 feet Y = 3672185
74 meter
Z = -5459567
28 Z = -1690560
47
XDOT = -5287
468571 XDOT = -1529
407780
YDOT = -15988
361530 feet/sec YDOT = -4890
814795 meter/sec
ZDOT = -18641
506835 ZDOT = -5689
560336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1475147
46 X = -449624
95
Y = -21552749
79 feet Y = -6569278
14 meter
Z = -5582612
12 Z = -1701580
17
XDOT = 14815
770809 XDOT = 4515
846943
YDOT = 3812
172217 feet/sec YDOT = 1161
950092 meter/sec
ZDOT = -18676
699904 ZDOT = -5692
658131
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21028
34145440
00016717 00000-0 10270-3 0 9140
2 25544 51
6419 314
4207 0002110 306
9730 53
1227 15
48896510 26916
Satellite: ISS
Catalog Number: 25544
Epoch time: 21028
34145440 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 314
4207 deg
Eccentricity:
0002110
Arg of perigee: 306
9730 deg
Mean anomaly: 53
1227 deg
Mean motion: 15
48896510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 280
Coasting Arc #16 (Orbit 2706)
---------------------------------------
Vector Time (GMT): 2021/029/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5077039
88 A = 6803262
77 meter
Y = -4214391
30 meter E =
0012947
Z = 1628485
91 I = 51
35302
XDOT = 2061
938794 Wp = 55
44697
YDOT = 4694
058504 meter/sec RA = 308
92213 deg
ZDOT = 5694
232292 TA = 322
41959
MA = 322
51000
Ha = 228
531 n
mi
Hp = 223
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16656955
00 X = 5115879
18
Y = -13826743
12 feet Y = -4157399
11 meter
Z = 5342801
56 Z = 1653241
44
XDOT = 6764
891056 XDOT = 1981
636796
YDOT = 15400
454409 feet/sec YDOT = 4716
667298 meter/sec
ZDOT = 18681
864474 ZDOT = 5704
053245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3799514
66 X = 1158092
07
Y = 21282722
60 feet Y = 6486973
85 meter
Z = 5457830
25 Z = 1663546
66
XDOT = -15116
164744 XDOT = -4607
407014
YDOT = -2124
643737 feet/sec YDOT = -647
591411 meter/sec
ZDOT = 18727
249030 ZDOT = 5708
065504
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21029
37376147
00016717 00000-0 10270-3 0 9155
2 25544 51
6422 309
3161 0002114 303
6541 56
4408 15
48949688 27070
Satellite: ISS
Catalog Number: 25544
Epoch time: 21029
37376147 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 309
3161 deg
Eccentricity:
0002114
Arg of perigee: 303
6541 deg
Mean anomaly: 56
4408 deg
Mean motion: 15
48949688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2707
Checksum: 309
Coasting Arc #17 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2021/029/19:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 956872
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5222188
30 A = 6797475
49 meter
Y = 1605119
48 meter E =
0006429
Z = -4051809
28 I = 51
32362
XDOT = 987
840287 Wp = 55
39350
YDOT = -6532
583064 meter/sec RA = 306
49688 deg
ZDOT = -3861
871693 TA = 174
33924
MA = 174
33196
Ha = 228
689 n
mi
Hp = 223
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17133163
72 X = -5220068
44
Y = 5266140
02 feet Y = 1546733
22 meter
Z = -13293337
53 Z = -4077170
52
XDOT = 3240
945822 XDOT = 1079
574310
YDOT = -21432
359133 feet/sec YDOT = -6521
023252 meter/sec
ZDOT = -12670
182720 ZDOT = -3856
850781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4836375
41 X = -1474127
23
Y = 17168081
01 feet Y = 5232831
09 meter
Z = -13411070
78 Z = -4087694
38
XDOT = -14935
068293 XDOT = -4552
208816
YDOT = -14084
336885 feet/sec YDOT = -4292
905883 meter/sec
ZDOT = -12646
640847 ZDOT = -3854
696130
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 21029
82539806
00016717 00000-0 10270-3 0 9169
2 25544 51
6425 307
0790 0002056 309
4190 50
6778 15
48922586 27147
Satellite: ISS
Catalog Number: 25544
Epoch time: 21029
82539806 = yrday
fracday
Element set: 916
Inclination: 51
6425 deg
RA of node: 307
0790 deg
Eccentricity:
0002056
Arg of perigee: 309
4190 deg
Mean anomaly: 50
6778 deg
Mean motion: 15
48922586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 320
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