[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 15th 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) : 75 4 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
0 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
Coasting Arc #1 (Orbit 2460)
---------------------------------------
Vector Time (GMT): 2021/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6316181
33 A = 6801544
09 meter
Y = 1389538
20 meter E =
0006234
Z = -2100192
28 I = 51
83987
XDOT = 683
310003 Wp = 40
95677
YDOT = 5243
741695 meter/sec RA = 27
19164 deg
ZDOT = 5538
291346 TA = 295
91341
MA = 295
97765
Ha = 228
549 n
mi
Hp = 222
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20722379
69 X = 6310374
91
Y = 4558852
37 feet Y = 1460138
10 meter
Z = -6890394
62 Z = -2069525
51
XDOT = 2241
830718 XDOT = 597
721001
YDOT = 17203
876951 feet/sec YDOT = 5250
903656 meter/sec
ZDOT = 18170
247197 ZDOT = 5541
403338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3655779
68 X = 1114281
65
Y = 20946996
73 feet Y = 6384644
60 meter
Z = -6748058
65 Z = -2056808
28
XDOT = -13590
316149 XDOT = -4142
328362
YDOT = 8214
949746 feet/sec YDOT = 2503
916682 meter/sec
ZDOT = 18184
414411 ZDOT = 5542
609513
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 21013
50407040
00016717 00000-0 10270-3 0 9004
2 25544 51
6444 27
8241 0000339 209
5978 150
5153 15
49324000 24616
Satellite: ISS
Catalog Number: 25544
Epoch time: 21013
50407040 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 27
8241 deg
Eccentricity:
0000339
Arg of perigee: 209
5978 deg
Mean anomaly: 150
5153 deg
Mean motion: 15
49324000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2461
Checksum: 264
Coasting Arc #2 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2021/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6429669
72 A = 6801790
54 meter
Y = -942453
56 meter E =
0013770
Z = 1986630
37 I = 51
80882
XDOT = -979
604783 Wp = 112
30632
YDOT = -5150
640065 meter/sec RA = 22
25475 deg
ZDOT = -5588
042037 TA = 45
85615
MA = 45
74301
Ha = 228
581 n
mi
Hp = 222
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21094716
92 X = -6428302
67
Y = -3092039
23 feet Y = -1014347
32 meter
Z = 6517816
17 Z = 1955401
73
XDOT = -3213
926452 XDOT = -894
793281
YDOT = -16898
425410 feet/sec YDOT = -5161
119884 meter/sec
ZDOT = -18333
471250 ZDOT = -5592
595010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5509135
50 X = -1679184
50
Y = -20641364
03 feet Y = -6291487
76 meter
Z = 6372851
26 Z = 1942445
06
XDOT = 12800
356909 XDOT = 3901
548786
YDOT = -9109
941254 feet/sec YDOT = -2776
710094 meter/sec
ZDOT = -18354
334759 ZDOT = -5594
401235
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 21014
53611874
00016717 00000-0 10270-3 0 9011
2 25544 51
6435 22
7163 0000153 267
5718 92
5415 15
49308010 24779
Satellite: ISS
Catalog Number: 25544
Epoch time: 21014
53611874 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 22
7163 deg
Eccentricity:
0000153
Arg of perigee: 267
5718 deg
Mean anomaly: 92
5415 deg
Mean motion: 15
49308010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 284
Coasting Arc #3 (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 = 6511155
91 A = 6801884
20 meter
Y = 459085
09 meter E =
0007033
Z = -1904327
16 I = 51
77673
XDOT = 1284
219247 Wp = 38
40899
YDOT = 5038
491610 meter/sec RA = 17
31689 deg
ZDOT = 5622
102173 TA = 300
70539
MA = 300
77466
Ha = 228
581 n
mi
Hp = 222
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21362060
07 X = 6514788
20
Y = 1506184
69 feet Y = 531917
99 meter
Z = -6247792
53 Z = -1872690
66
XDOT = 4213
317740 XDOT = 1200
473766
YDOT = 16530
484286 feet/sec YDOT = 5052
383960 meter/sec
ZDOT = 18445
217103 ZDOT = 5628
137231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7418324
58 X = 2261105
33
Y = 20134259
67 feet Y = 6136922
35 meter
Z = -6100914
90 Z = -1859558
86
XDOT = -11925
984760 XDOT = -3635
040155
YDOT = 9974
742670 feet/sec YDOT = 3040
301566 meter/sec
ZDOT = 18472
969339 ZDOT = 5630
561055
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
50366183
00016717 00000-0 10270-3 0 9020
2 25544 51
6429 17
9291 0000138 224
5815 135
5324 15
49318972 24926
Satellite: ISS
Catalog Number: 25544
Epoch time: 21015
50366183 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 17
9291 deg
Eccentricity:
0000138
Arg of perigee: 224
5815 deg
Mean anomaly: 135
5324 deg
Mean motion: 15
49318972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2492
Checksum: 300
Coasting Arc #4 (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 = -6556557
20 A = 6802073
25 meter
Y = 3688
66 meter E =
0013587
Z = 1786661
92 I = 51
74370
XDOT = -1554
921557 Wp = 114
56262
YDOT = -4916
468318 meter/sec RA = 12
37568 deg
ZDOT = -5667
584819 TA = 45
87608
MA = 45
76439
Ha = 228
509 n
mi
Hp = 222
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21511014
45 X = -6564789
48
Y = 12101
89 feet Y = -69677
62 meter
Z = 5861751
69 Z = 1754793
70
XDOT = -5101
448677 XDOT = -1472
299499
YDOT = -16130
145400 feet/sec YDOT = -4933
394272 meter/sec
ZDOT = -18594
438383 ZDOT = -5674
937408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9199300
44 X = -2803946
77
Y = -19488703
65 feet Y = -5940156
87 meter
Z = 5713783
65 Z = 1741561
26
XDOT = 11049
860961 XDOT = 3367
997621
YDOT = -10705
447972 feet/sec YDOT = -3263
020542 meter/sec
ZDOT = -18628
315027 ZDOT = -5677
910420
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
53570568
00016717 00000-0 10270-3 0 9039
2 25544 51
6421 12
8212 0000319 299
0089 61
1029 15
49317968 25084
Satellite: ISS
Catalog Number: 25544
Epoch time: 21016
53570568 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 12
8212 deg
Eccentricity:
0000319
Arg of perigee: 299
0089 deg
Mean anomaly: 61
1029 deg
Mean motion: 15
49317968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2508
Checksum: 297
Coasting Arc #5 (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 = 6564387
13 A = 6802188
97 meter
Y = -497122
63 meter E =
0007711
Z = -1700197
49 I = 51
71105
XDOT = 1832
754290 Wp = 36
57976
YDOT = 4776
276550 meter/sec RA = 7
43339 deg
ZDOT = 5699
014828 TA = 304
84265
MA = 304
91515
Ha = 228
560 n
mi
Hp = 222
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21536703
18 X = 6577716
59
Y = -1630979
75 feet Y = -423640
33 meter
Z = -5578075
76 Z = -1668278
79
XDOT = 6012
973394 XDOT = 1751
526509
YDOT = 15670
198656 feet/sec YDOT = 4796
317322 meter/sec
ZDOT = 18697
555210 ZDOT = 5707
720300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10995929
83 X = 3351559
41
Y = 18633592
20 feet Y = 5679518
90 meter
Z = -5429859
75 Z = -1655021
25
XDOT = -10099
643073 XDOT = -3078
371209
YDOT = 11401
109443 feet/sec YDOT = 3475
058158 meter/sec
ZDOT = 18737
719807 ZDOT = 5711
256997
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
50324443
00016717 00000-0 10270-3 0 9047
2 25544 51
6425 8
0340 0000155 272
4021 87
7111 15
49318368 25234
Satellite: ISS
Catalog Number: 25544
Epoch time: 21017
50324443 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 8
0340 deg
Eccentricity:
0000155
Arg of perigee: 272
4021 deg
Mean anomaly: 87
7111 deg
Mean motion: 15
49318368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2523
Checksum: 265
Coasting Arc #6 (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 = -6539917
55 A = 6802331
98 meter
Y = 963406
53 meter E =
0013460
Z = 1576924
66 I = 51
67820
XDOT = -2074
176405 Wp = 116
65556
YDOT = -4631
541939 meter/sec RA = 2
48762 deg
ZDOT = -5740
537374 TA = 46
14117
MA = 46
03003
Ha = 228
485 n
mi
Hp = 222
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21456422
41 X = -6557864
21
Y = 3160782
58 feet Y = 890172
07 meter
Z = 5173637
34 Z = 1545113
51
XDOT = -6805
040700 XDOT = -1994
347362
YDOT = -15195
347570 feet/sec YDOT = -4654
290332 meter/sec
ZDOT = -18833
784035 ZDOT = -5750
418936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12637377
59 X = -3851872
69
Y = -17668391
23 feet Y = -5385325
65 meter
Z = 5025910
00 Z = 1531897
37
XDOT = 9174
411346 XDOT = 2796
360578
YDOT = -11963
183511 feet/sec YDOT = -3646
378334 meter/sec
ZDOT = -18879
414222 ZDOT = -5754
445455
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
53528102
00016717 00000-0 10270-3 0 9050
2 25544 51
6429 2
9261 0000423 318
9511 41
1608 15
49328353 25398
Satellite: ISS
Catalog Number: 25544
Epoch time: 21018
53528102 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 2
9261 deg
Eccentricity:
0000423
Arg of perigee: 318
9511 deg
Mean anomaly: 41
1608 deg
Mean motion: 15
49328353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 282
Coasting Arc #7 (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 = 6473079
87 A = 6802455
84 meter
Y = -1454778
01 meter E =
0008504
Z = -1485707
46 I = 51
64375
XDOT = 2323
309902 Wp = 35
40008
YDOT = 4469
764687 meter/sec RA = 357
54097 deg
ZDOT = 5769
058144 TA = 308
41914
MA = 308
49546
Ha = 228
542 n
mi
Hp = 222
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21237138
69 X = 6496083
12
Y = -4772893
74 feet Y = -1382262
70 meter
Z = -4874368
31 Z = -1454208
60
XDOT = 7622
407814 XDOT = 2245
132750
YDOT = 14664
582306 feet/sec YDOT = 4495
308306 meter/sec
ZDOT = 18927
356117 ZDOT = 5780
153917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14255702
92 X = 4345138
25
Y = 16491702
24 feet Y = 5026670
84 meter
Z = -4728079
13 Z = -1441118
52
XDOT = -8183
397448 XDOT = -2494
299542
YDOT = 12492
298833 feet/sec YDOT = 3807
652684 meter/sec
ZDOT = 18978
628166 ZDOT = 5784
685865
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
50281374
00016717 00000-0 10270-3 0 9066
2 25544 51
6421 358
1391 0000274 318
3319 41
7810 15
49322637 25541
Satellite: ISS
Catalog Number: 25544
Epoch time: 21019
50281374 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 358
1391 deg
Eccentricity:
0000274
Arg of perigee: 318
3319 deg
Mean anomaly: 41
7810 deg
Mean motion: 15
49322637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2554
Checksum: 291
Coasting Arc #8 (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 = -6378029
67 A = 6802603
28 meter
Y = 1914601
97 meter E =
0013283
Z = 1358285
97 I = 51
61060
XDOT = -2537
446615 Wp = 119
26867
YDOT = -4308
352013 meter/sec RA = 352
59095 deg
ZDOT = -5805
445610 TA = 45
95887
MA = 45
84953
Ha = 228
467 n
mi
Hp = 222
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20925294
20 X = -6405562
97
Y = 6281502
51 feet Y = 1843124
24 meter
Z = 4456318
79 Z = 1327237
74
XDOT = -8324
956085 XDOT = -2460
881681
YDOT = -14135
013165 feet/sec YDOT = -4336
299240 meter/sec
ZDOT = -19046
737566 ZDOT = -5817
585527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15701000
97 X = -4785665
10
Y = -15233786
67 feet Y = -4643258
18 meter
Z = 4312110
93 Z = 1314331
41
XDOT = 7236
502045 XDOT = 2205
685823
YDOT = -12900
842420 feet/sec YDOT = -3932
176770 meter/sec
ZDOT = -19102
860953 ZDOT = -5822
552019
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
53484601
00016717 00000-0 10270-3 0 9070
2 25544 51
6423 353
0314 0000495 319
8466 40
2647 15
49324734 25706
Satellite: ISS
Catalog Number: 25544
Epoch time: 21020
53484601 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 353
0314 deg
Eccentricity:
0000495
Arg of perigee: 319
8466 deg
Mean anomaly: 40
2647 deg
Mean motion: 15
49324734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 290
Coasting Arc #9 (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 = 6237295
71 A = 6802678
59 meter
Y = -2392161
93 meter E =
0009196
Z = -1262574
89 I = 51
57778
XDOT = 2758
553338 Wp = 35
12940
YDOT = 4130
261879 meter/sec RA = 347
63914 deg
ZDOT = 5830
695278 TA = 311
15850
MA = 311
23780
Ha = 228
501 n
mi
Hp = 222
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20463568
60 X = 6269714
80
Y = -7848300
31 feet Y = -2322230
67 meter
Z = -4142306
08 Z = -1232198
39
XDOT = 9050
371843 XDOT = 2683
840722
YDOT = 13550
727951 feet/sec YDOT = 4160
691974 meter/sec
ZDOT = 19129
577683 ZDOT = 5843
913792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17082260
68 X = 5206673
05
Y = 13773122
31 feet Y = 4198047
68 meter
Z = -4001203
43 Z = -1219566
81
XDOT = -6230
802567 XDOT = -1899
148623
YDOT = 13274
716656 feet/sec YDOT = 4046
133637 meter/sec
ZDOT = 19190
712767 ZDOT = 5849
329252
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
50237294
00016717 00000-0 10270-3 0 9083
2 25544 51
6427 348
2439 0000391 320
6671 39
4450 15
49331542 25850
Satellite: ISS
Catalog Number: 25544
Epoch time: 21021
50237294 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 348
2439 deg
Eccentricity:
0000391
Arg of perigee: 320
6671 deg
Mean anomaly: 39
4450 deg
Mean motion: 15
49331542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2585
Checksum: 297
Coasting Arc #10 (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 = -199093
49 A = 6792751
54 meter
Y = -4270044
26 meter E =
0012333
Z = -5289838
59 I = 51
53814
XDOT = 7523
289358 Wp = 95
05280
YDOT = -1207
254554 meter/sec RA = 346
74831 deg
ZDOT = 691
695750 TA = 181
57539
MA = 181
57928
Ha = 228
403 n
mi
Hp = 223
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -653193
85 X = -125635
13
Y = -14009331
56 feet Y = -4271859
66 meter
Z = -17355113
49 Z = -5290627
50
XDOT = 24682
707869 XDOT = 7532
870291
YDOT = -3960
808905 feet/sec YDOT = -1123
070182 meter/sec
ZDOT = 2269
343013 ZDOT = 728
263606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1875737
74 X = -571724
86
Y = -13894249
50 feet Y = -4234967
25 meter
Z = -17358555
12 Z = -5290887
60
XDOT = 23159
490340 XDOT = 7059
012656
YDOT = -6172
457105 feet/sec YDOT = -1881
364926 meter/sec
ZDOT = 2439
116744 ZDOT = 743
442784
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
69587876
00016717 00000-0 10270-3 0 9098
2 25544 51
6462 347
2868 0002215 276
9241 83
1657 15
48918060 25880
Satellite: ISS
Catalog Number: 25544
Epoch time: 21021
69587876 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 347
2868 deg
Eccentricity:
0002215
Arg of perigee: 276
9241 deg
Mean anomaly: 83
1657 deg
Mean motion: 15
48918060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2588
Checksum: 342
Coasting Arc #11 (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 = 592460
06 A = 6792651
90 meter
Y = 4228024
99 meter E =
0001929
Z = 5283016
00 I = 51
50534
XDOT = -7397
823952 Wp = 14
98308
YDOT = 1873
641430 meter/sec RA = 341
79591 deg
ZDOT = -667
982649 TA = 81
42449
MA = 81
40263
Ha = 228
333 n
mi
Hp = 223
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1943766
59 X = 519475
46
Y = 13871473
07 feet Y = 4234241
87 meter
Z = 17332729
65 Z = 5285716
91
XDOT = -24271
075959 XDOT = -7414
981132
YDOT = 6147
117551 feet/sec YDOT = 1790
817749 meter/sec
ZDOT = -2191
544125 ZDOT = -703
959414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3381289
21 X = 1030616
95
Y = 13577028
56 feet Y = 4138278
31 meter
Z = 17345047
98 Z = 5286770
62
XDOT = -22414
881404 XDOT = -6832
055852
YDOT = 8603
355359 feet/sec YDOT = 2622
302713 meter/sec
ZDOT = -2358
596974 ZDOT = -718
900358
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
72818342
00016717 00000-0 10270-3 0 9100
2 25544 51
6462 342
1814 0002280 281
5264 78
5630 15
48945206 26044
Satellite: ISS
Catalog Number: 25544
Epoch time: 21022
72818342 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 342
1814 deg
Eccentricity:
0002280
Arg of perigee: 281
5264 deg
Mean anomaly: 78
5630 deg
Mean motion: 15
48945206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2604
Checksum: 288
Coasting Arc #12 (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 = -986830
20 A = 6792699
47 meter
Y = -4158994
44 meter E =
0012406
Z = -5289996
31 I = 51
47276
XDOT = 7194
682698 Wp = 92
87161
YDOT = -2522
048164 meter/sec RA = 336
84144 deg
ZDOT = 641
389385 TA = 183
27594
MA = 183
28407
Ha = 228
426 n
mi
Hp = 223
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3237631
89 X = -914554
33
Y = -13644994
88 feet Y = -4169625
33 meter
Z = -17355630
92 Z = -5294614
67
XDOT = 23604
602026 XDOT = 7219
234833
YDOT = -8274
436233 feet/sec YDOT = -2441
454816 meter/sec
ZDOT = 2104
295882 ZDOT = 676
397229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4867530
10 X = -1483623
18
Y = -13123955
83 feet Y = -4000181
74 meter
Z = -17376852
54 Z = -5296464
65
XDOT = 21355
191400 XDOT = 6509
062339
YDOT = -10918
844986 feet/sec YDOT = -3328
063952 meter/sec
ZDOT = 2266
875263 ZDOT = 690
943580
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
69596900
00016717 00000-0 10270-3 0 9111
2 25544 51
6455 337
3953 0002231 286
6246 73
4659 15
48927366 26196
Satellite: ISS
Catalog Number: 25544
Epoch time: 21023
69596900 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 337
3953 deg
Eccentricity:
0002231
Arg of perigee: 286
6246 deg
Mean anomaly: 73
4659 deg
Mean motion: 15
48927366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2619
Checksum: 331
Coasting Arc #13 (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 = 1361807
31 A = 6792633
66 meter
Y = 4046587
30 meter E =
0002086
Z = 5282816
12 I = 51
44224
XDOT = -6953
555870 Wp = 12
92907
YDOT = 3153
791435 meter/sec RA = 331
88481 deg
ZDOT = -621
243626 TA = 83
03543
MA = 83
01171
Ha = 228
330 n
mi
Hp = 223
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4467871
75 X = 1290795
49
Y = 13276205
06 feet Y = 4061418
46 meter
Z = 17332073
87 Z = 5289259
04
XDOT = -22813
503512 XDOT = -6985
288136
YDOT = 10347
084762 feet/sec YDOT = 3075
854401 meter/sec
ZDOT = -2038
200873 ZDOT = -655
097450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6255253
00 X = 1906601
12
Y = 12492438
28 feet Y = 3807695
19 meter
Z = 17361770
63 Z = 5291867
69
XDOT = -20116
966662 XDOT = -6131
651439
YDOT = 13133
508432 feet/sec YDOT = 4003
093370 meter/sec
ZDOT = -2195
447978 ZDOT = -669
172544
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
72826931
00016717 00000-0 10270-3 0 9127
2 25544 51
6458 332
2902 0002334 287
9363 72
1533 15
48943694 26352
Satellite: ISS
Catalog Number: 25544
Epoch time: 21024
72826931 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 332
2902 deg
Eccentricity:
0002334
Arg of perigee: 287
9363 deg
Mean anomaly: 72
1533 deg
Mean motion: 15
48943694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2635
Checksum: 313
Coasting Arc #14 (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 = -1733456
63 A = 6792643
08 meter
Y = -3907774
20 meter E =
0012389
Z = -5289463
62 I = 51
41299
XDOT = 6639
623364 Wp = 90
95748
YDOT = -3754
144900 meter/sec RA = 326
92534 deg
ZDOT = 598
592098 TA = 184
78106
MA = 184
79290
Ha = 228
419 n
mi
Hp = 223
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5687193
66 X = -1663937
24
Y = -12820781
50 feet Y = -3926769
72 meter
Z = -17353883
28 Z = -5297715
44
XDOT = 21783
541222 XDOT = 6678
202335
YDOT = -12316
748360 feet/sec YDOT = -3679
680204 meter/sec
ZDOT = 1963
884836 ZDOT = 630
937414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7597046
40 X = -2315579
74
Y = -11733610
55 feet Y = -3576404
50 meter
Z = -17391985
05 Z = -5301077
04
XDOT = 18596
622150 XDOT = 5668
250431
YDOT = -15169
312901 feet/sec YDOT = -4623
606572 meter/sec
ZDOT = 2114
152847 ZDOT = 644
393788
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
69604874
00016717 00000-0 10270-3 0 9135
2 25544 51
6459 327
5034 0002385 294
0900 66
0000 15
48939505 26502
Satellite: ISS
Catalog Number: 25544
Epoch time: 21025
69604874 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 327
5034 deg
Eccentricity:
0002385
Arg of perigee: 294
0900 deg
Mean anomaly: 66
0000 deg
Mean motion: 15
48939505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 301
Coasting Arc #15 (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 = -6008978
18 A = 6803134
23 meter
Y = 2648481
21 meter E =
0005597
Z = -1768367
64 I = 51
42771
XDOT = -605
831453 Wp = 149
32466
YDOT = -5136
292909 meter/sec RA = 323
81294 deg
ZDOT = -5646
618563 TA = 50
10151
MA = 50
05232
Ha = 228
572 n
mi
Hp = 223
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19714495
34 X = -6029558
20
Y = 8689242
81 feet Y = 2581169
60 meter
Z = -5801731
10 Z = -1797605
91
XDOT = -1987
636000 XDOT = -520
923467
YDOT = -16851
354687 feet/sec YDOT = -5142
592437 meter/sec
ZDOT = -18525
651455 ZDOT = -5649
355676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3277108
36 X = 998862
63
Y = -21256310
03 feet Y = -6478923
30 meter
Z = -5937524
35 Z = -1809757
42
XDOT = 13650
331721 XDOT = 4160
621108
YDOT = 7271
418305 feet/sec YDOT = 2216
328299 meter/sec
ZDOT = -18538
110391 ZDOT = -5650
416047
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
34123314
00016717 00000-0 10270-3 0 9144
2 25544 51
6435 324
3114 0001964 296
7814 63
3134 15
48918267 26606
Satellite: ISS
Catalog Number: 25544
Epoch time: 21026
34123314 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 324
3114 deg
Eccentricity:
0001964
Arg of perigee: 296
7814 deg
Mean anomaly: 63
3134 deg
Mean motion: 15
48918267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 294
Coasting Arc #16 (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 = 5749333
42 A = 6803064
81 meter
Y = -3178870
46 meter E =
0012694
Z = 1740561
33 I = 51
40024
XDOT = 1075
977238 Wp = 57
53619
YDOT = 5055
776718 meter/sec RA = 318
85119 deg
ZDOT = 5655
924285 TA = 321
59300
MA = 321
68329
Ha = 228
448 n
mi
Hp = 223
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18862642
45 X = 5775998
81
Y = -10429365
04 feet Y = -3114428
34 meter
Z = 5710503
06 Z = 1768553
01
XDOT = 3530
109050 XDOT = 991
889589
YDOT = 16587
193957 feet/sec YDOT = 5067
338393 meter/sec
ZDOT = 18556
182036 ZDOT = 5660
947042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -982875
11 X = -299580
33
Y = 21496580
31 feet Y = 6552157
68 meter
Z = 5840528
40 Z = 1780193
06
XDOT = -14343
037361 XDOT = -4371
757788
YDOT = -5724
245257 feet/sec YDOT = -1744
749954 meter/sec
ZDOT = 18579
261074 ZDOT = 5662
958775
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
37352357
00016717 00000-0 10270-3 0 9150
2 25544 51
6425 319
2068 0002108 296
8380 63
2554 15
48959458 26765
Satellite: ISS
Catalog Number: 25544
Epoch time: 21027
37352357 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 319
2068 deg
Eccentricity:
0002108
Arg of perigee: 296
8380 deg
Mean anomaly: 63
2554 deg
Mean motion: 15
48959458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 329
Coasting Arc #17 (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 = -5456851
58 A = 6803145
85 meter
Y = 3666588
25 meter E =
0005413
Z = -1740946
17 I = 51
37495
XDOT = -1517
937071 Wp = 147
03902
YDOT = -4936
961007 meter/sec RA = 313
88659 deg
ZDOT = -5652
603865 TA = 52
08816
MA = 52
03923
Ha = 228
616 n
mi
Hp = 223
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17903056
36 X = -5488990
68
Y = 12029489
00 feet Y = 3605386
23 meter
Z = -5711765
65 Z = -1767530
34
XDOT = -4980
108502 XDOT = -1435
161438
YDOT = -16197
378631 feet/sec YDOT = -4953
472427 meter/sec
ZDOT = -18545
288271 ZDOT = -5659
776493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1252802
96 X = -381854
34
Y = -21499590
67 feet Y = -6553075
24 meter
Z = -5835270
78 Z = -1778590
53
XDOT = 14843
295707 XDOT = 4524
236531
YDOT = 4166
345630 feet/sec YDOT = 1269
902148 meter/sec
ZDOT = -18578
360846 ZDOT = -5662
684386
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
34129669
00016717 00000-0 10270-3 0 9167
2 25544 51
6420 314
4201 0002108 306
2916 53
8039 15
48930364 26912
Satellite: ISS
Catalog Number: 25544
Epoch time: 21028
34129669 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 314
4201 deg
Eccentricity:
0002108
Arg of perigee: 306
2916 deg
Mean anomaly: 53
8039 deg
Mean motion: 15
48930364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 293
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