[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 11th 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
012/13:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
4
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
Coasting Arc #1 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2021/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 983715
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5986678
28 A = 6801230
48 meter
Y = 2275011
19 meter E =
0005653
Z = -2285426
79 I = 51
89685
XDOT = 31
665758 Wp = 45
11768
YDOT = 5378
860712 meter/sec RA = 37
05812 deg
ZDOT = 5449
427064 TA = 289
59787
MA = 289
65889
Ha = 228
585 n
mi
Hp = 222
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19641332
94 X = 5971894
59
Y = 7463947
46 feet Y = 2341876
22 meter
Z = -7498119
38 Z = -2256381
88
XDOT = 103
890283 XDOT = -54
954409
YDOT = 17647
180815 feet/sec YDOT = 5378
729662 meter/sec
ZDOT = 17878
697715 ZDOT = 5449
371325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -165135
89 X = -50333
42
Y = 21058678
90 feet Y = 6418685
33 meter
Z = -7363357
86 Z = -2244351
48
XDOT = -15021
995026 XDOT = -4578
704084
YDOT = 6119
289238 feet/sec YDOT = 1865
159360 meter/sec
ZDOT = 17878
155033 ZDOT = 5449
261654
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 21011
50446529
00016717 00000-0 10270-3 0 9007
2 25544 51
6453 37
7188 0000412 194
9326 165
1812 15
49315091 24302
Satellite: ISS
Catalog Number: 25544
Epoch time: 21011
50446529 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 37
7188 deg
Eccentricity:
0000412
Arg of perigee: 194
9326 deg
Mean anomaly: 165
1812 deg
Mean motion: 15
49315091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2430
Checksum: 283
Coasting Arc #2 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2021/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 983715
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6164183
78 A = 6801511
18 meter
Y = -1851445
83 meter E =
0013848
Z = 2178388
85 I = 51
86782
XDOT = -354
066036 Wp = 110
64483
YDOT = -5322
098995 meter/sec RA = 32
12598 deg
ZDOT = -5501
727565 TA = 45
30266
MA = 45
18994
Ha = 228
635 n
mi
Hp = 222
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20223700
06 X = -6153603
34
Y = -6074297
33 feet Y = -1920319
33 meter
Z = 7146945
05 Z = 2148471
75
XDOT = -1161
633975 XDOT = -267
802753
YDOT = -17460
954707 feet/sec YDOT = -5325
575262 meter/sec
ZDOT = -18050
287287 ZDOT = -5503
238726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1702495
95 X = -518920
77
Y = -21094118
07 feet Y = -6429487
19 meter
Z = 7008112
86 Z = 2136072
80
XDOT = 14354
727258 XDOT = 4375
320868
YDOT = -7183
786751 feet/sec YDOT = -2189
618202 meter/sec
ZDOT = -18057
018656 ZDOT = -5503
779286
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 21012
53652298
00016717 00000-0 10270-3 0 9014
2 25544 51
6434 32
6118 0000290 204
3908 155
7229 15
49289697 24460
Satellite: ISS
Catalog Number: 25544
Epoch time: 21012
53652298 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 32
6118 deg
Eccentricity:
0000290
Arg of perigee: 204
3908 deg
Mean anomaly: 155
7229 deg
Mean motion: 15
49289697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2446
Checksum: 308
Coasting Arc #3 (Orbit 2446)
---------------------------------------
Vector Time (GMT): 2021/012/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6159983
42 A = 6802573
40 meter
Y = -2471115
86 meter E =
0013633
Z = 1460527
11 I = 51
86786
XDOT = 612
953806 Wp = 119
65693
YDOT = -4973
822579 meter/sec RA = 31
80585 deg
ZDOT = -5796
131698 TA = 44
48714
MA = 44
37774
Ha = 228
549 n
mi
Hp = 222
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20209919
37 X = -6138987
08
Y = -8107335
49 feet Y = -2539884
04 meter
Z = 4791755
61 Z = 1430655
63
XDOT = 2011
003299 XDOT = 696
680688
YDOT = -16318
315547 feet/sec YDOT = -4966
499077 meter/sec
ZDOT = -19016
180112 ZDOT = -5792
951667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8618873
09 X = -2627032
52
Y = -20029820
23 feet Y = -6105089
21 meter
Z = 4653168
76 Z = 1418285
84
XDOT = 11574
161731 XDOT = 3527
804496
YDOT = -9421
288761 feet/sec YDOT = -2871
608814 meter/sec
ZDOT = -19001
144597 ZDOT = -5791
548873
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 21012
60102621
00016717 00000-0 10270-3 0 9023
2 25544 51
6418 32
2924 0000270 249
3245 110
7876 15
49294127 24478
Satellite: ISS
Catalog Number: 25544
Epoch time: 21012
60102621 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 32
2924 deg
Eccentricity:
0000270
Arg of perigee: 249
3245 deg
Mean anomaly: 110
7876 deg
Mean motion: 15
49294127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2447
Checksum: 275
Coasting Arc #4 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2021/013/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6349604
71 A = 6802636
17 meter
Y = 2001213
58 meter E =
0008452
Z = -1380559
70 I = 51
83885
XDOT = -306
917089 Wp = 37
60033
YDOT = 4970
394118 meter/sec RA = 26
87186 deg
ZDOT = 5818
616686 TA = 307
43392
MA = 307
51080
Ha = 228
583 n
mi
Hp = 222
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20832036
43 X = 6333460
40
Y = 6565661
35 feet Y = 2072129
34 meter
Z = -4529395
35 Z = -1349755
61
XDOT = -1006
945830 XDOT = -390
737454
YDOT = 16307
067315 feet/sec YDOT = 4966
492507 meter/sec
ZDOT = 19089
949757 ZDOT = 5816
922928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10478156
69 X = 3193742
16
Y = 19198029
00 feet Y = 5851559
24 meter
Z = -4386455
08 Z = -1336991
51
XDOT = -10729
203921 XDOT = -3270
261355
YDOT = 10196
245799 feet/sec YDOT = 3107
815719 meter/sec
ZDOT = 19081
814663 ZDOT = 5816
137109
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
56857831
00016717 00000-0 10270-3 0 9030
2 25544 51
6420 27
5050 0000310 210
5892 149
5240 15
49302615 24625
Satellite: ISS
Catalog Number: 25544
Epoch time: 21013
56857831 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 27
5050 deg
Eccentricity:
0000310
Arg of perigee: 210
5892 deg
Mean anomaly: 149
5240 deg
Mean motion: 15
49302615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 269
Coasting Arc #5 (Orbit 2477)
---------------------------------------
Vector Time (GMT): 2021/014/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6496699
10 A = 6802766
19 meter
Y = -1544437
38 meter E =
0013407
Z = 1263796
44 I = 51
80896
XDOT = 30
875148 Wp = 121
49323
YDOT = -4948
390711 meter/sec RA = 21
93458 deg
ZDOT = -5849
618595 TA = 44
82102
MA = 44
71280
Ha = 228
514 n
mi
Hp = 222
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21314629
59 X = -6485084
50
Y = -5067051
78 feet Y = -1617023
34 meter
Z = 4146313
79 Z = 1232267
04
XDOT = 101
296416 XDOT = 114
620481
YDOT = -16234
877660 feet/sec YDOT = -4947
576560 meter/sec
ZDOT = -19191
662056 ZDOT = -5849
265760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12178817
00 X = -3712103
42
Y = -18244366
28 feet Y = -5560882
84 meter
Z = 3999985
21 Z = 1219195
49
XDOT = 9896
583792 XDOT = 3016
478740
YDOT = -10842
614946 feet/sec YDOT = -3304
829035 meter/sec
ZDOT = -19189
755580 ZDOT = -5849
037501
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
60063006
00016717 00000-0 10270-3 0 9040
2 25544 51
6425 22
3967 0000291 285
3988 74
7130 15
49303770 24781
Satellite: ISS
Catalog Number: 25544
Epoch time: 21014
60063006 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 22
3967 deg
Eccentricity:
0000291
Arg of perigee: 285
3988 deg
Mean anomaly: 74
7130 deg
Mean motion: 15
49303770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2478
Checksum: 295
Coasting Arc #6 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2021/015/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6612849
06 A = 6802848
26 meter
Y = 1049480
05 meter E =
0009173
Z = -1180066
86 I = 51
77653
XDOT = 262
042914 Wp = 36
88077
YDOT = 4913
807183 meter/sec RA = 16
99669 deg
ZDOT = 5869
304515 TA = 310
35509
MA = 310
43516
Ha = 228
559 n
mi
Hp = 222
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21695699
02 X = 6606353
89
Y = 3443176
03 feet Y = 1123393
47 meter
Z = -3871610
44 Z = -1147960
93
XDOT = 859
720845 XDOT = 178
566931
YDOT = 16121
414644 feet/sec YDOT = 4916
270318 meter/sec
ZDOT = 19256
248408 ZDOT = 5870
375032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13858111
03 X = 4223952
24
Y = 17077567
19 feet Y = 5205242
48 meter
Z = -3722585
42 Z = -1134644
03
XDOT = -8987
839819 XDOT = -2739
493577
YDOT = 11469
048876 feet/sec YDOT = 3495
766097 meter/sec
ZDOT = 19260
954912 ZDOT = 5870
739057
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
56817754
00016717 00000-0 10270-3 0 9054
2 25544 51
6418 17
6095 0000223 257
1584 102
9541 15
49302297 24936
Satellite: ISS
Catalog Number: 25544
Epoch time: 21015
56817754 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 17
6095 deg
Eccentricity:
0000223
Arg of perigee: 257
1584 deg
Mean anomaly: 102
9541 deg
Mean motion: 15
49302297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 304
Coasting Arc #7 (Orbit 2508)
---------------------------------------
Vector Time (GMT): 2021/016/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6688830
98 A = 6802974
03 meter
Y = -573551
26 meter E =
0013142
Z = 1060439
54 I = 51
74458
XDOT = -524
644544 Wp = 123
83789
YDOT = -4865
314205 meter/sec RA = 12
05571 deg
ZDOT = -5895
358298 TA = 44
70162
MA = 44
59576
Ha = 228
486 n
mi
Hp = 222
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21944983
52 X = -6687071
08
Y = -1881729
86 feet Y = -648340
80 meter
Z = 3479132
35 Z = 1027953
04
XDOT = -1721
274750 XDOT = -441
564715
YDOT = -15962
316945 feet/sec YDOT = -4870
716295 meter/sec
ZDOT = -19341
726700 ZDOT = -5897
705235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15359398
77 X = -4681544
75
Y = -15818934
62 feet Y = -4821611
27 meter
Z = 3328325
08 Z = 1014473
49
XDOT = 8108
906454 XDOT = 2471
594687
YDOT = -11977
834125 feet/sec YDOT = -3650
843841 meter/sec
ZDOT = -19352
364341 ZDOT = -5898
600651
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
60022655
00016717 00000-0 10270-3 0 9069
2 25544 51
6423 12
5018 0000387 292
4204 67
6905 15
49298465 25093
Satellite: ISS
Catalog Number: 25544
Epoch time: 21016
60022655 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 12
5018 deg
Eccentricity:
0000387
Arg of perigee: 292
4204 deg
Mean anomaly: 67
6905 deg
Mean motion: 15
49298465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2509
Checksum: 296
Coasting Arc #8 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2021/017/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6728157
56 A = 6803013
97 meter
Y = 65286
48 meter E =
0009773
Z = -973331
82 I = 51
71186
XDOT = 803
085596 Wp = 36
88820
YDOT = 4803
429899 meter/sec RA = 7
11320 deg
ZDOT = 5911
980698 TA = 312
60208
MA = 312
68447
Ha = 228
512 n
mi
Hp = 222
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22074007
73 X = 6731655
22
Y = 214194
50 feet Y = 140545
18 meter
Z = -3193345
87 Z = -940641
46
XDOT = 2634
795261 XDOT = 720
596260
YDOT = 15759
284444 feet/sec YDOT = 4811
949116 meter/sec
ZDOT = 19396
262132 ZDOT = 5915
681514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16797663
10 X = 5119927
71
Y = 14355921
18 feet Y = 4375684
78 meter
Z = -3041577
85 Z = -927072
93
XDOT = -7158
645694 XDOT = -2181
955207
YDOT = 12461
221731 feet/sec YDOT = 3798
180384 meter/sec
ZDOT = 19413
190085 ZDOT = 5917
140338
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
56776994
00016717 00000-0 10270-3 0 9078
2 25544 51
6428 7
7145 0000323 281
1177 78
9937 15
49307459 25240
Satellite: ISS
Catalog Number: 25544
Epoch time: 21017
56776994 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 7
7145 deg
Eccentricity:
0000323
Arg of perigee: 281
1177 deg
Mean anomaly: 78
9937 deg
Mean motion: 15
49307459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 332
Coasting Arc #9 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2021/018/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6730779
48 A = 6803132
19 meter
Y = 416953
19 meter E =
0012835
Z = 849337
86 I = 51
67930
XDOT = -1048
862728 Wp = 125
79618
YDOT = -4732
285250 meter/sec RA = 2
16789 deg
ZDOT = -5933
176886 TA = 45
03908
MA = 44
93508
Ha = 228
474 n
mi
Hp = 222
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22082609
84 X = -6739067
23
Y = 1367956
66 feet Y = 341638
40 meter
Z = 2786541
54 Z = 816623
03
XDOT = -3441
150682 XDOT = -967
047628
YDOT = -15525
870244 feet/sec YDOT = -4743
556738 meter/sec
ZDOT = -19465
803432 ZDOT = -5938
073175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18041824
13 X = -5499147
99
Y = -12838574
11 feet Y = -3913197
39 meter
Z = 2634648
66 Z = 803040
91
XDOT = 6259
372848 XDOT = 1907
856844
YDOT = -12835
061560 feet/sec YDOT = -3912
126764 meter/sec
ZDOT = -19488
285180 ZDOT = -5940
029323
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
59981311
00016717 00000-0 10270-3 0 9084
2 25544 51
6438 2
6069 0000469 307
8539 52
2569 15
49299595 25404
Satellite: ISS
Catalog Number: 25544
Epoch time: 21018
59981311 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 2
6069 deg
Eccentricity:
0000469
Arg of perigee: 307
8539 deg
Mean anomaly: 52
2569 deg
Mean motion: 15
49299595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2540
Checksum: 332
Coasting Arc #10 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2021/019/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6691951
00 A = 6803169
56 meter
Y = -925840
68 meter E =
0010513
Z = -758606
79 I = 51
64459
XDOT = 1311
230760 Wp = 37
31099
YDOT = 4647
395685 meter/sec RA = 357
22102 deg
ZDOT = 5946
368940 TA = 314
50792
MA = 314
59378
Ha = 228
513 n
mi
Hp = 222
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21955219
83 X = 6705491
48
Y = -3037535
04 feet Y = -850930
73 meter
Z = -2488867
43 Z = -726067
72
XDOT = 4301
938189 XDOT = 1230
281241
YDOT = 15247
361171 feet/sec YDOT = 4661
605998 meter/sec
ZDOT = 19509
084448 ZDOT = 5952
541803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19185697
41 X = 5847800
57
Y = 11130883
43 feet Y = 3392693
27 meter
Z = -2337778
22 Z = -712554
80
XDOT = -5289
857600 XDOT = -1612
348596
YDOT = 13183
501580 feet/sec YDOT = 4018
331282 meter/sec
ZDOT = 19537
495686 ZDOT = 5955
028685
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
56735170
00016717 00000-0 10270-3 0 9093
2 25544 51
6429 357
8198 0000442 313
0831 47
0282 15
49305151 25553
Satellite: ISS
Catalog Number: 25544
Epoch time: 21019
56735170 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 357
8198 deg
Eccentricity:
0000442
Arg of perigee: 313
0831 deg
Mean anomaly: 47
0282 deg
Mean motion: 15
49305151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 300
Coasting Arc #11 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2021/020/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6620680
38 A = 6803263
13 meter
Y = 1403600
33 meter E =
0012527
Z = 631761
54 I = 51
61170
XDOT = -1542
077180 Wp = 127
99996
YDOT = -4557
435634 meter/sec RA = 352
27159 deg
ZDOT = -5961
966395 TA = 45
19001
MA = 45
08824
Ha = 228
469 n
mi
Hp = 222
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21721392
33 X = -6638952
49
Y = 4604987
95 feet Y = 1329460
92 meter
Z = 2072708
47 Z = 599557
10
XDOT = -5059
308333 XDOT = -1462
040615
YDOT = -14952
216647 feet/sec YDOT = -4574
232503 meter/sec
ZDOT = -19560
257200 ZDOT = -5969
262863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20128767
55 X = -6135248
35
Y = -9405056
42 feet Y = -2866661
20 meter
Z = 1923161
46 Z = 586179
61
XDOT = 4381
804008 XDOT = 1335
573862
YDOT = -13437
479762 feet/sec YDOT = -4095
743831 meter/sec
ZDOT = -19593
886957 ZDOT = -5972
216745
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
59939180
00016717 00000-0 10270-3 0 9107
2 25544 51
6437 352
7127 0000508 313
0443 47
0665 15
49298061 25714
Satellite: ISS
Catalog Number: 25544
Epoch time: 21020
59939180 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 352
7127 deg
Eccentricity:
0000508
Arg of perigee: 313
0443 deg
Mean anomaly: 47
0665 deg
Mean motion: 15
49298061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2571
Checksum: 295
Coasting Arc #12 (Orbit 2585)
---------------------------------------
Vector Time (GMT): 2021/021/13:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 957119
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6504537
01 A = 6803265
02 meter
Y = -1900705
97 meter E =
0011070
Z = -537725
63 I = 51
57838
XDOT = 1788
588979 Wp = 38
33244
YDOT = 4452
576880 meter/sec RA = 347
31965 deg
ZDOT = 5971
463194 TA = 315
87279
MA = 315
96106
Ha = 228
477 n
mi
Hp = 222
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21340344
52 X = 6527919
78
Y = -6235911
98 feet Y = -1827836
79 meter
Z = -1764191
72 Z = -506072
92
XDOT = 5868
074079 XDOT = 1709
660466
YDOT = 14608
191863 feet/sec YDOT = 4472
136550 meter/sec
ZDOT = 19591
414679 ZDOT = 5979
959854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20936776
79 X = 6381529
57
Y = 7513011
51 feet Y = 2289965
91 meter
Z = -1617192
16 Z = -492920
17
XDOT = -3406
380875 XDOT = -1038
264891
YDOT = 13660
757844 feet/sec YDOT = 4163
798991 meter/sec
ZDOT = 19630
618601 ZDOT = 5983
412550
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
56692587
00016717 00000-0 10270-3 0 9113
2 25544 51
6437 347
9251 0000550 315
6241 44
4865 15
49310865 25865
Satellite: ISS
Catalog Number: 25544
Epoch time: 21021
56692587 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 347
9251 deg
Eccentricity:
0000550
Arg of perigee: 315
6241 deg
Mean anomaly: 44
4865 deg
Mean motion: 15
49310865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2586
Checksum: 312
Coasting Arc #13 (Orbit 2587)
---------------------------------------
Vector Time (GMT): 2021/021/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -232909
95 A = 6792775
03 meter
Y = -4264576
81 meter E =
0012333
Z = -5292898
47 I = 51
53807
XDOT = 7522
064166 Wp = 94
84531
YDOT = -1231
466504 meter/sec RA = 346
74918 deg
ZDOT = 661
526679 TA = 181
49261
MA = 181
49629
Ha = 228
414 n
mi
Hp = 223
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -764140
26 X = -159495
36
Y = -13991393
72 feet Y = -4266770
61 meter
Z = -17365152
45 Z = -5293851
75
XDOT = 24678
688210 XDOT = 7532
062478
YDOT = -4040
244436 feet/sec YDOT = -1147
293497 meter/sec
ZDOT = 2170
363121 ZDOT = 698
089596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1984379
81 X = -604838
97
Y = -13865756
20 feet Y = -4226282
49 meter
Z = -17369357
21 Z = -5294180
08
XDOT = 23150
621776 XDOT = 7056
309517
YDOT = -6243
287885 feet/sec YDOT = -1902
954147 meter/sec
ZDOT = 2340
115180 ZDOT = 713
267107
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
69593094
00016717 00000-0 10270-3 0 9121
2 25544 51
6462 347
2871 0002237 276
5533 83
5363 15
48905071 25884
Satellite: ISS
Catalog Number: 25544
Epoch time: 21021
69593094 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 347
2871 deg
Eccentricity:
0002237
Arg of perigee: 276
5533 deg
Mean anomaly: 83
5363 deg
Mean motion: 15
48905071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2588
Checksum: 319
Coasting Arc #14 (Orbit 2603)
---------------------------------------
Vector Time (GMT): 2021/022/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 631369
96 A = 6792677
80 meter
Y = 4218129
41 meter E =
0001841
Z = 5286482
79 I = 51
50526
XDOT = -7393
712653 Wp = 13
93344
YDOT = 1901
766545 meter/sec RA = 341
79691 deg
ZDOT = -632
602587 TA = 82
13358
MA = 82
11269
Ha = 228
345 n
mi
Hp = 223
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2071423
74 X = 558476
29
Y = 13839007
24 feet Y = 4224781
91 meter
Z = 17344103
65 Z = 5289372
94
XDOT = -24257
587445 XDOT = -7411
356496
YDOT = 6239
391552 feet/sec YDOT = 1818
986117 meter/sec
ZDOT = -2075
467805 ZDOT = -668
560561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3504376
64 X = 1068134
00
Y = 13530347
68 feet Y = 4124049
97 meter
Z = 17357300
63 Z = 5290505
23
XDOT = -22395
243315 XDOT = -6826
070163
YDOT = 8684
632521 feet/sec YDOT = 2647
075992 meter/sec
ZDOT = -2242
434892 ZDOT = -683
494155
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
72824472
00016717 00000-0 10270-3 0 9134
2 25544 51
6462 342
1818 0002302 281
1587 78
9304 15
48930740 26046
Satellite: ISS
Catalog Number: 25544
Epoch time: 21022
72824472 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 342
1818 deg
Eccentricity:
0002302
Arg of perigee: 281
1587 deg
Mean anomaly: 78
9304 deg
Mean motion: 15
48930740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2604
Checksum: 294
Coasting Arc #15 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2021/023/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1030503
28 A = 6792725
43 meter
Y = -4143596
91 meter E =
0012412
Z = -5293790
29 I = 51
47269
XDOT = 7186
951610 Wp = 92
53794
YDOT = -2553
864555 meter/sec RA = 336
84260 deg
ZDOT = 600
635315 TA = 183
21745
MA = 183
22544
Ha = 228
441 n
mi
Hp = 223
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3380916
28 X = -958377
92
Y = -13594478
07 feet Y = -4154717
03 meter
Z = -17368078
37 Z = -5298621
16
XDOT = 23579
237567 XDOT = 7212
058058
YDOT = -8378
820719 feet/sec YDOT = -2473
354559 meter/sec
ZDOT = 1970
588304 ZDOT = 635
606949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5002933
97 X = -1524894
27
Y = -13055234
53 feet Y = -3979235
48 meter
Z = -17390286
89 Z = -5300559
44
XDOT = 21322
380888 XDOT = 6499
061695
YDOT = -11009
292963 feet/sec YDOT = -3355
632495 meter/sec
ZDOT = 2133
001261 ZDOT = 650
138784
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
69603945
00016717 00000-0 10270-3 0 9142
2 25544 51
6455 337
3958 0002253 286
3195 73
7707 15
48912322 26198
Satellite: ISS
Catalog Number: 25544
Epoch time: 21023
69603945 = yrday
fracday
Element set: 914
Inclination: 51
6455 deg
RA of node: 337
3958 deg
Eccentricity:
0002253
Arg of perigee: 286
3195 deg
Mean anomaly: 73
7707 deg
Mean motion: 15
48912322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2619
Checksum: 324
Coasting Arc #16 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2021/024/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1410088
94 A = 6792662
80 meter
Y = 4024589
11 meter E =
0001982
Z = 5287021
31 I = 51
44215
XDOT = -6941
324128 Wp = 11
79761
YDOT = 3189
289360 meter/sec RA = 331
88614 deg
ZDOT = -574
509431 TA = 83
71711
MA = 83
69454
Ha = 228
346 n
mi
Hp = 223
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4626276
05 X = 1339299
09
Y = 13204032
52 feet Y = 4039961
43 meter
Z = 17345870
45 Z = 5293699
30
XDOT = -22773
373122 XDOT = -6973
681254
YDOT = 10463
547769 feet/sec YDOT = 3111
485612 meter/sec
ZDOT = -1884
873461 ZDOT = -608
305353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6401213
39 X = 1951089
84
Y = 12397754
36 feet Y = 3778835
53 meter
Z = 17376659
06 Z = 5296405
68
XDOT = -20068
080219 XDOT = -6116
750851
YDOT = 13232
315881 feet/sec YDOT = 4033
209881 meter/sec
ZDOT = -2041
853647 ZDOT = -622
356992
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
72835024
00016717 00000-0 10270-3 0 9153
2 25544 51
6457 332
2906 0002355 287
6796 72
4097 15
48926891 26353
Satellite: ISS
Catalog Number: 25544
Epoch time: 21024
72835024 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 332
2906 deg
Eccentricity:
0002355
Arg of perigee: 287
6796 deg
Mean anomaly: 72
4097 deg
Mean motion: 15
48926891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2635
Checksum: 330
Coasting Arc #17 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2021/025/16:20:39
293
Vector Time (MET): N/A
Weight (LBS) : 956872
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1785686
40 A = 6792671
16 meter
Y = -3878072
71 meter E =
0012404
Z = -5293996
69 I = 51
41289
XDOT = 6622
133611 Wp = 90
48641
YDOT = -3792
834745 meter/sec RA = 326
92684 deg
ZDOT = 545
746300 TA = 184
74356
MA = 184
75532
Ha = 228
437 n
mi
Hp = 223
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5858551
18 X = -1716473
25
Y = -12723335
65 feet Y = -3897654
01 meter
Z = -17368755
55 Z = -5302502
96
XDOT = 21726
160142 XDOT = 6661
403212
YDOT = -12443
683547 feet/sec YDOT = -3718
561765 meter/sec
ZDOT = 1790
506232 ZDOT = 578
008332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7749977
47 X = -2362193
13
Y = -11609374
39 feet Y = -3538537
31 meter
Z = -17408039
42 Z = -5305970
42
XDOT = 18529
416738 XDOT = 5647
766222
YDOT = -15274
157966 feet/sec YDOT = -4655
563348 meter/sec
ZDOT = 1940
389663 ZDOT = 591
430769
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
69614008
00016717 00000-0 10270-3 0 9168
2 25544 51
6459 327
5040 0002408 293
8638 66
2259 15
48922532 26500
Satellite: ISS
Catalog Number: 25544
Epoch time: 21025
69614008 = yrday
fracday
Element set: 916
Inclination: 51
6459 deg
RA of node: 327
5040 deg
Eccentricity:
0002408
Arg of perigee: 293
8638 deg
Mean anomaly: 66
2259 deg
Mean motion: 15
48922532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 312
Coasting Arc #18 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2021/026/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 956872
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6003625
35 A = 6803257
40 meter
Y = 2691978
92 meter E =
0005731
Z = -1720290
21 I = 51
42794
XDOT = -670
533163 Wp = 149
62985
YDOT = -5107
493748 meter/sec RA = 323
81370 deg
ZDOT = -5665
461004 TA = 49
24776
MA = 49
19802
Ha = 228
591 n
mi
Hp = 223
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19696933
57 X = -6024925
70
Y = 8831951
85 feet Y = 2624723
14 meter
Z = -5643996
74 Z = -1749504
22
XDOT = -2199
911953 XDOT = -585
850886
YDOT = -16756
869253 feet/sec YDOT = -5114
518078 meter/sec
ZDOT = -18587
470485 ZDOT = -5668
512950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3147991
43 X = 959507
79
Y = -21319303
92 feet Y = -6498123
83 meter
Z = -5779679
49 Z = -1761646
31
XDOT = 13680
248352 XDOT = 4169
739698
YDOT = 7051
454718 feet/sec YDOT = 2149
283398 meter/sec
ZDOT = -18601
391633 ZDOT = -5669
704170
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
34133177
00016717 00000-0 10270-3 0 9175
2 25544 51
6434 324
3120 0001989 296
5738 63
5208 15
48900898 26607
Satellite: ISS
Catalog Number: 25544
Epoch time: 21026
34133177 = yrday
fracday
Element set: 917
Inclination: 51
6434 deg
RA of node: 324
3120 deg
Eccentricity:
0001989
Arg of perigee: 296
5738 deg
Mean anomaly: 63
5208 deg
Mean motion: 15
48900898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 316
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