[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 15th 2020
- spaceflight nasa gov will be taken offline by October 2020 *
- Do you use any data hosted on this site? *
- Please let us know how you use the data at the survey link below *
- *
- https://www surveymonkey com/r/KRLJMCN *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13864 993 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
263/20:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
7
267/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
7
270/23:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
5
Coasting Arc #1 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2020/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4026159
91 A = 6793037
81 meter
Y = -1783332
52 meter E =
0004911
Z = 5169327
01 I = 51
23196
XDOT = 1608
733241 Wp = 120
45757
YDOT = 7380
283730 meter/sec RA = 265
58475 deg
ZDOT = 1289
738385 TA = 317
05682
MA = 317
09515
Ha = 229
283 n
mi
Hp = 222
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13209186
07 X = 4020693
07
Y = -5850828
49 feet Y = -1738339
51 meter
Z = 16959734
27 Z = 5188871
09
XDOT = 5277
996199 XDOT = 1519
820380
YDOT = 24213
529297 feet/sec YDOT = 7397
776638 meter/sec
ZDOT = 4231
425147 ZDOT = 1297
336696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13706801
92 X = -4177833
23
Y = 4215592
64 feet Y = 1284912
64 meter
Z = 17049918
97 Z = 5196815
30
XDOT = -1960
128442 XDOT = -597
447149
YDOT = -23672
621465 feet/sec YDOT = -7215
415023 meter/sec
ZDOT = 4266
278895 ZDOT = 1300
361807
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 20258
55064888
00016717 00000-0 10270-3 0 9008
2 25544 51
6408 266
2511 0000738 96
5164 263
6070 15
48946414 5867
Satellite: ISS
Catalog Number: 25544
Epoch time: 20258
55064888 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 266
2511 deg
Eccentricity:
0000738
Arg of perigee: 96
5164 deg
Mean anomaly: 263
6070 deg
Mean motion: 15
48946414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 319
Coasting Arc #2 (Orbit 600)
---------------------------------------
Vector Time (GMT): 2020/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3862604
60 A = 6793096
10 meter
Y = 2131431
06 meter E =
0014646
Z = -5178655
22 I = 51
23500
XDOT = -2241
401991 Wp = 80
93115
YDOT = -7198
166384 meter/sec RA = 260
61232 deg
ZDOT = -1291
709515 TA = 176
56544
MA = 176
55537
Ha = 229
449 n
mi
Hp = 222
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12672587
26 X = -3860997
15
Y = 6992884
05 feet Y = 2088245
32 meter
Z = -16990338
66 Z = -5197414
26
XDOT = -7353
681074 XDOT = -2154
469025
YDOT = -23616
031445 feet/sec YDOT = -7222
745351 meter/sec
ZDOT = -4237
892108 ZDOT = -1302
385682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13217661
83 X = 4028743
33
Y = -5642617
10 feet Y = -1719869
69 meter
Z = -17076908
11 Z = -5205041
59
XDOT = 4406
765581 XDOT = 1343
182149
YDOT = 23288
159010 feet/sec YDOT = 7098
230866 meter/sec
ZDOT = -4286
973041 ZDOT = -1306
669383
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 20259
51840992
00016717 00000-0 10270-3 0 9014
2 25544 51
6400 261
4650 0000734 96
9818 263
1415 15
48932305 6016
Satellite: ISS
Catalog Number: 25544
Epoch time: 20259
51840992 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 261
4650 deg
Eccentricity:
0000734
Arg of perigee: 96
9818 deg
Mean anomaly: 263
1415 deg
Mean motion: 15
48932305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 601
Checksum: 294
Coasting Arc #3 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2020/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3650969
26 A = 6793097
87 meter
Y = -2466432
85 meter E =
0004859
Z = 5167278
82 I = 51
24023
XDOT = 2868
781022 Wp = 120
87021
YDOT = 6984
922619 meter/sec RA = 255
63928 deg
ZDOT = 1303
706377 TA = 316
50831
MA = 316
54662
Ha = 229
281 n
mi
Hp = 222
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11978245
59 X = 3653178
82
Y = -8091971
30 feet Y = -2425592
31 meter
Z = 16953014
51 Z = 5185019
23
XDOT = 9412
011226 XDOT = 2784
127694
YDOT = 22916
412793 feet/sec YDOT = 7016
530167 meter/sec
ZDOT = 4277
251892 ZDOT = 1317
435487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12523183
21 X = -3817066
24
Y = 7024638
48 feet Y = 2141109
81 meter
Z = 17034887
86 Z = 5192233
82
XDOT = -6833
676592 XDOT = -2082
904625
YDOT = -22735
067614 feet/sec YDOT = -6929
648609 meter/sec
ZDOT = 4340
444626 ZDOT = 1322
967522
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 20260
55068883
00016717 00000-0 10270-3 0 9022
2 25544 51
6385 256
3586 0000638 94
2370 265
8853 15
48932908 6177
Satellite: ISS
Catalog Number: 25544
Epoch time: 20260
55068883 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 256
3586 deg
Eccentricity:
0000638
Arg of perigee: 94
2370 deg
Mean anomaly: 265
8853 deg
Mean motion: 15
48932908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 333
Coasting Arc #4 (Orbit 631)
---------------------------------------
Vector Time (GMT): 2020/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3427640
45 A = 6793108
20 meter
Y = 2780528
30 meter E =
0014582
Z = -5176938
93 I = 51
25041
XDOT = -3459
973910 Wp = 80
78402
YDOT = -6695
458993 meter/sec RA = 250
66705 deg
ZDOT = -1306
159661 TA = 176
57314
MA = 176
56314
Ha = 229
432 n
mi
Hp = 222
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11245539
52 X = -3433331
87
Y = 9122468
17 feet Y = 2742165
62 meter
Z = -16984707
76 Z = -5193603
11
XDOT = -11351
620438 XDOT = -3378
501563
YDOT = -21966
728980 feet/sec YDOT = -6733
695492 meter/sec
ZDOT = -4285
300726 ZDOT = -1322
768254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11741695
95 X = 3578868
93
Y = -8318394
46 feet Y = -2535446
63 meter
Z = -17061616
92 Z = -5200380
84
XDOT = 9146
387720 XDOT = 2787
818977
YDOT = 21850
926904 feet/sec YDOT = 6660
162520 meter/sec
ZDOT = -4361
803271 ZDOT = -1329
477637
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 20261
51844988
00016717 00000-0 10270-3 0 9038
2 25544 51
6390 251
5718 0000698 96
2361 263
8868 15
48935069 6327
Satellite: ISS
Catalog Number: 25544
Epoch time: 20261
51844988 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 251
5718 deg
Eccentricity:
0000698
Arg of perigee: 96
2361 deg
Mean anomaly: 263
8868 deg
Mean motion: 15
48935069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 632
Checksum: 339
Coasting Arc #5 (Orbit 647)
---------------------------------------
Vector Time (GMT): 2020/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3160069
01 A = 6793106
84 meter
Y = -3072023
95 meter E =
0004867
Z = 5166259
36 I = 51
26323
XDOT = 4039
631876 Wp = 120
53947
YDOT = 6376
847343 meter/sec RA = 245
69539 deg
ZDOT = 1317
578525 TA = 316
70694
MA = 316
74517
Ha = 229
287 n
mi
Hp = 222
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10367680
47 X = 3169091
63
Y = -10078818
73 feet Y = -3036634
81 meter
Z = 16949669
81 Z = 5181632
01
XDOT = 13253
385420 XDOT = 3961
623753
YDOT = 20921
415166 feet/sec YDOT = 6421
585367 meter/sec
ZDOT = 4322
764188 ZDOT = 1337
011406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10771182
33 X = -3283056
37
Y = 9520650
62 feet Y = 2901894
31 meter
Z = 17020620
87 Z = 5187885
24
XDOT = -11402
051800 XDOT = -3475
345389
YDOT = -20807
489184 feet/sec YDOT = -6342
122703 meter/sec
ZDOT = 4412
318226 ZDOT = 1344
874595
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 20262
55072710
00016717 00000-0 10270-3 0 9040
2 25544 51
6395 246
4654 0000624 88
8655 271
2566 15
48936346 6480
Satellite: ISS
Catalog Number: 25544
Epoch time: 20262
55072710 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 246
4654 deg
Eccentricity:
0000624
Arg of perigee: 88
8655 deg
Mean anomaly: 271
2566 deg
Mean motion: 15
48936346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 648
Checksum: 324
Coasting Arc #6 (Orbit 662)
---------------------------------------
Vector Time (GMT): 2020/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2885031
49 A = 6793116
01 meter
Y = 3340946
20 meter E =
0014561
Z = -5176426
91 I = 51
27845
XDOT = -4570
509544 Wp = 80
25737
YDOT = -5989
711692 meter/sec RA = 240
72481 deg
ZDOT = -1319
297084 TA = 176
97495
MA = 176
96614
Ha = 229
423 n
mi
Hp = 222
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9465326
41 X = -2897032
20
Y = 10961109
56 feet Y = 3308616
13 meter
Z = -16983027
93 Z = -5190470
84
XDOT = -14995
110053 XDOT = -4496
782649
YDOT = -19651
285078 feet/sec YDOT = -6040
410294 meter/sec
ZDOT = -4328
402505 ZDOT = -1341
319395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9735428
35 X = 2967358
56
Y = -10618559
83 feet Y = -3236537
04 meter
Z = -17047849
92 Z = -5196184
65
XDOT = 13477
633862 XDOT = 4107
982801
YDOT = 19464
794867 feet/sec YDOT = 5932
869475 meter/sec
ZDOT = -4429
922449 ZDOT = -1350
240362
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 20263
51848619
00016717 00000-0 10270-3 0 9057
2 25544 51
6396 241
6785 0000684 86
5270 273
5958 15
48938654 6638
Satellite: ISS
Catalog Number: 25544
Epoch time: 20263
51848619 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 241
6785 deg
Eccentricity:
0000684
Arg of perigee: 86
5270 deg
Mean anomaly: 273
5958 deg
Mean motion: 15
48938654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 663
Checksum: 349
Coasting Arc #7 (Orbit 668)
---------------------------------------
Vector Time (GMT): 2020/263/20:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 38656
46 A = 6798692
83 meter
Y = -5695413
81 meter E =
0012131
Z = 3702811
76 I = 51
30460
XDOT = 5695
082827 Wp = 94
27064
YDOT = 2827
656818 meter/sec RA = 239
00550 deg
ZDOT = 4276
804558 TA = 310
02545
MA = 310
13184
Ha = 229
325 n
mi
Hp = 222
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 126825
66 X = 84355
10
Y = -18685740
84 feet Y = -5694725
69 meter
Z = 12148332
54 Z = 3703111
02
XDOT = 18684
654945 XDOT = 5642
265368
YDOT = 9277
089299 feet/sec YDOT = 2891
048361 meter/sec
ZDOT = 14031
511017 ZDOT = 4304
340787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15530251
51 X = 4733620
66
Y = -10389862
66 feet Y = -3166830
14 meter
Z = 12149774
51 Z = 3703251
27
XDOT = 1915
369338 XDOT = 583
804574
YDOT = 19469
839587 feet/sec YDOT = 5934
407106 meter/sec
ZDOT = 14158
506450 ZDOT = 4315
512766
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 20263
90558965
00016717 00000-0 10270-3 0 9063
2 25544 51
6414 239
7642 0000477 64
1557 295
9642 15
48933379 6692
Satellite: ISS
Catalog Number: 25544
Epoch time: 20263
90558965 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 239
7642 deg
Eccentricity:
0000477
Arg of perigee: 64
1557 deg
Mean anomaly: 295
9642 deg
Mean motion: 15
48933379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 669
Checksum: 349
Coasting Arc #8 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2020/264/20:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 448990
48 A = 6798643
77 meter
Y = 5681027
32 meter E =
0006010
Z = -3713682
02 I = 51
32230
XDOT = -5910
060736 Wp = 79
32542
YDOT = -2322
330308 meter/sec RA = 234
03695 deg
ZDOT = -4271
963855 TA = 145
05003
MA = 145
01056
Ha = 229
279 n
mi
Hp = 222
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1473065
89 X = 403469
32
Y = 18638541
08 feet Y = 5685793
50 meter
Z = -12183996
12 Z = -3711611
88
XDOT = -19389
963044 XDOT = -5862
901480
YDOT = -7619
193924 feet/sec YDOT = -2388
157422 meter/sec
ZDOT = -14015
629446 ZDOT = -4300
558279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14394970
96 X = -4387587
15
Y = 11940740
10 feet Y = 3639537
58 meter
Z = -12174499
37 Z = -3710787
41
XDOT = -3919
567559 XDOT = -1194
684192
YDOT = -19133
493483 feet/sec YDOT = -5831
888814 meter/sec
ZDOT = -14147
525019 ZDOT = -4312
165626
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 20264
87334868
00016717 00000-0 10270-3 0 9075
2 25544 51
6407 234
9777 0000323 77
2954 282
8232 15
48944910 6846
Satellite: ISS
Catalog Number: 25544
Epoch time: 20264
87334868 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 234
9777 deg
Eccentricity:
0000323
Arg of perigee: 77
2954 deg
Mean anomaly: 282
8232 deg
Mean motion: 15
48944910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 684
Checksum: 335
Coasting Arc #9 (Orbit 699)
---------------------------------------
Vector Time (GMT): 2020/265/20:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -959029
64 A = 6798681
47 meter
Y = -5618740
09 meter E =
0011966
Z = 3696186
20 I = 51
34375
XDOT = 6092
802455 Wp = 94
74138
YDOT = 1789
832562 meter/sec RA = 229
06896 deg
ZDOT = 4288
663902 TA = 309
42329
MA = 309
52915
Ha = 229
238 n
mi
Hp = 222
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3146422
71 X = -914082
09
Y = -18434186
65 feet Y = -5629213
19 meter
Z = 12126595
15 Z = 3691636
94
XDOT = 19989
509367 XDOT = 6051
503058
YDOT = 5872
154076 feet/sec YDOT = 1857
735888 meter/sec
ZDOT = 14070
419627 ZDOT = 4318
160319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13041204
02 X = 3974958
99
Y = -13422135
21 feet Y = -4091066
81 meter
Z = 12105651
88 Z = 3689802
69
XDOT = 5924
620103 XDOT = 1805
824207
YDOT = 18608
115321 feet/sec YDOT = 5671
753550 meter/sec
ZDOT = 14206
497421 ZDOT = 4330
140414
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 20265
90562481
00016717 00000-0 10270-3 0 9085
2 25544 51
6411 229
8712 0000236 67
9820 292
1355 15
48951666 7009
Satellite: ISS
Catalog Number: 25544
Epoch time: 20265
90562481 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 229
8712 deg
Eccentricity:
0000236
Arg of perigee: 67
9820 deg
Mean anomaly: 292
1355 deg
Mean motion: 15
48951666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 700
Checksum: 308
Coasting Arc #10 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2020/266/20:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436099
39 A = 6798643
52 meter
Y = 5518792
43 meter E =
0006097
Z = -3707835
83 I = 51
36560
XDOT = -6216
369142 Wp = 79
64995
YDOT = -1256
920469 meter/sec RA = 224
10255 deg
ZDOT = -4283
469182 TA = 144
60331
MA = 144
56283
Ha = 229
310 n
mi
Hp = 222
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4711612
16 X = 1392290
56
Y = 18106274
36 feet Y = 5534606
89 meter
Z = -12164815
71 Z = -3700966
27
XDOT = -20394
911884 XDOT = -6181
045033
YDOT = -4123
754818 feet/sec YDOT = -1326
238939 meter/sec
ZDOT = -14053
376583 ZDOT = -4313
580321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11606739
51 X = -3537734
20
Y = 14699977
44 feet Y = 4480553
12 meter
Z = -12133155
52 Z = -3698185
80
XDOT = -7808
830359 XDOT = -2380
131494
YDOT = -17866
328440 feet/sec YDOT = -5445
656909 meter/sec
ZDOT = -14192
313791 ZDOT = -4325
817244
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 20266
87338259
00016717 00000-0 10270-3 0 9097
2 25544 51
6399 225
0840 0000455 76
5686 283
5515 15
48958408 7152
Satellite: ISS
Catalog Number: 25544
Epoch time: 20266
87338259 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 225
0840 deg
Eccentricity:
0000455
Arg of perigee: 76
5686 deg
Mean anomaly: 283
5515 deg
Mean motion: 15
48958408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 343
Coasting Arc #11 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2020/267/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1930195
09 A = 6798900
00 meter
Y = 5410422
25 meter E =
0005809
Z = -3642636
01 I = 51
39051
XDOT = -6253
395772 Wp = 81
67194
YDOT = -698
784424 meter/sec RA = 219
94279 deg
ZDOT = -4356
677130 TA = 141
58923
MA = 141
54786
Ha = 229
315 n
mi
Hp = 222
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6332661
04 X = 1887244
61
Y = 17750729
17 feet Y = 5431766
88 meter
Z = -11950905
55 Z = -3633364
21
XDOT = -20516
390327 XDOT = -6223
954617
YDOT = -2292
599816 feet/sec YDOT = -768
549816 meter/sec
ZDOT = -14293
560137 ZDOT = -4386
982341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18872665
27 X = -5752388
37
Y = -183388
34 feet Y = -55896
77 meter
Z = -11908148
47 Z = -3629603
65
XDOT = 9261
162116 XDOT = 2822
802213
YDOT = -16958
005959 feet/sec YDOT = -5168
800216 meter/sec
ZDOT = -14433
413847 ZDOT = -4399
304540
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 20267
71210671
00016717 00000-0 10270-3 0 9100
2 25544 51
6432 220
9385 0000395 75
2832 284
8362 15
48942873 7287
Satellite: ISS
Catalog Number: 25544
Epoch time: 20267
71210671 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 220
9385 deg
Eccentricity:
0000395
Arg of perigee: 75
2832 deg
Mean anomaly: 284
8362 deg
Mean motion: 15
48942873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 311
Coasting Arc #12 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2020/268/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2409899
01 A = 6798980
09 meter
Y = -5215784
74 meter E =
0012446
Z = 3624905
65 I = 51
41686
XDOT = 6290
536174 Wp = 92
95021
YDOT = 142
705222 meter/sec RA = 214
98017 deg
ZDOT = 4373
728226 TA = 310
09607
MA = 310
20511
Ha = 229
397 n
mi
Hp = 222
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7906492
83 X = -2369003
18
Y = -17112154
64 feet Y = -5242505
24 meter
Z = 11892735
06 Z = 3613298
67
XDOT = 20638
242042 XDOT = 6267
227767
YDOT = 468
192986 feet/sec YDOT = 212
920236 meter/sec
ZDOT = 14349
502053 ZDOT = 4404
228630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18794491
42 X = 5728560
99
Y = -1837504
44 feet Y = -560071
35 meter
Z = 11839184
18 Z = 3608583
34
XDOT = -7411
799097 XDOT = -2259
116365
YDOT = 17842
233807 feet/sec YDOT = 5438
312864 meter/sec
ZDOT = 14490
280623 ZDOT = 4416
637534
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 20268
74438233
00016717 00000-0 10270-3 0 9111
2 25544 51
6427 215
8327 0000525 72
0734 288
0473 15
48935103 7446
Satellite: ISS
Catalog Number: 25544
Epoch time: 20268
74438233 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 215
8327 deg
Eccentricity:
0000525
Arg of perigee: 72
0734 deg
Mean anomaly: 288
0473 deg
Mean motion: 15
48935103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 301
Coasting Arc #13 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2020/269/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2847725
17 A = 6798936
23 meter
Y = 4993004
82 meter E =
0005638
Z = -3636811
01 I = 51
44555
XDOT = -6271
203334 Wp = 82
14812
YDOT = 398
059152 meter/sec RA = 210
01973 deg
ZDOT = -4369
112422 TA = 140
98636
MA = 140
94567
Ha = 229
272 n
mi
Hp = 222
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9342930
33 X = 2809345
75
Y = 16381249
42 feet Y = 5024635
46 meter
Z = -11931794
66 Z = -3623071
22
XDOT = -20574
814087 XDOT = -6253
965849
YDOT = 1305
968347 feet/sec YDOT = 328
026350 meter/sec
ZDOT = -14334
358340 ZDOT = -4399
533563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18521536
27 X = -5645364
26
Y = 3754682
32 feet Y = 1144427
17 meter
Z = -11868380
62 Z = -3617482
41
XDOT = 5517
056511 XDOT = 1681
598825
YDOT = -18485
994119 feet/sec YDOT = -5634
531007 meter/sec
ZDOT = -14474
793306 ZDOT = -4411
917000
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 20269
71213799
00016717 00000-0 10270-3 0 9128
2 25544 51
6431 211
0463 0000263 72
8669 287
2510 15
48943066 7590
Satellite: ISS
Catalog Number: 25544
Epoch time: 20269
71213799 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 211
0463 deg
Eccentricity:
0000263
Arg of perigee: 72
8669 deg
Mean anomaly: 287
2510 deg
Mean motion: 15
48943066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 312
Coasting Arc #14 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2020/270/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3285101
06 A = 6798995
72 meter
Y = -4717580
84 meter E =
0012367
Z = 3620019
28 I = 51
47573
XDOT = 6211
667871 Wp = 92
40580
YDOT = -949
847781 meter/sec RA = 205
06036 deg
ZDOT = 4385
632573 TA = 310
52470
MA = 310
63236
Ha = 229
369 n
mi
Hp = 222
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10777890
61 X = -3249687
41
Y = -15477627
44 feet Y = -4754119
06 meter
Z = 11876703
67 Z = 3604147
79
XDOT = 20379
487767 XDOT = 6200
524879
YDOT = -3116
298493 feet/sec YDOT = -880
446604 meter/sec
ZDOT = 14388
558311 ZDOT = 4415
779277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18022873
09 X = 5493371
72
Y = -5712360
70 feet Y = -1741127
54 meter
Z = 11803429
50 Z = 3597685
31
XDOT = -3532
230516 XDOT = -1076
623861
YDOT = 18966
347915 feet/sec YDOT = 5780
942844 meter/sec
ZDOT = 14527
745790 ZDOT = 4428
056917
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 20270
74441074
00016717 00000-0 10270-3 0 9133
2 25544 51
6432 205
9398 0000471 57
5909 302
5287 15
48941066 7756
Satellite: ISS
Catalog Number: 25544
Epoch time: 20270
74441074 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 205
9398 deg
Eccentricity:
0000471
Arg of perigee: 57
5909 deg
Mean anomaly: 302
5287 deg
Mean motion: 15
48941066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 313
Coasting Arc #15 (Orbit 778)
---------------------------------------
Vector Time (GMT): 2020/270/23:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4598970
31 A = 6795367
55 meter
Y = 1993324
85 meter E =
0010849
Z = -4599155
23 I = 51
47285
XDOT = -5106
365977 Wp = 111
47609
YDOT = -4835
678149 meter/sec RA = 203
50098 deg
ZDOT = 3012
189731 TA = 188
73134
MA = 188
75023
Ha = 229
310 n
mi
Hp = 222
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15088485
26 X = -4598578
49
Y = 6539779
69 feet Y = 1941897
87 meter
Z = -15089091
95 Z = -4621494
26
XDOT = -16753
169217 XDOT = -5066
543888
YDOT = -15865
085792 feet/sec YDOT = -4892
558410 meter/sec
ZDOT = 9882
512241 ZDOT = 2987
482029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14706452
70 X = -4482526
78
Y = 7143390
04 feet Y = 2177305
28 meter
Z = -15192235
82 Z = -4630593
48
XDOT = -16931
054823 XDOT = -5160
585510
YDOT = -14094
674407 feet/sec YDOT = -4296
056759 meter/sec
ZDOT = 9768
434146 ZDOT = 2977
418728
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 20271
00247898
00016717 00000-0 10270-3 0 9142
2 25544 51
6425 204
6593 0000640 129
5278 230
5929 15
48964758 7798
Satellite: ISS
Catalog Number: 25544
Epoch time: 20271
00247898 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 204
6593 deg
Eccentricity:
0000640
Arg of perigee: 129
5278 deg
Mean anomaly: 230
5929 deg
Mean motion: 15
48964758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 779
Checksum: 334
Coasting Arc #16 (Orbit 794)
---------------------------------------
Vector Time (GMT): 2020/271/23:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4404643
44 A = 6795459
93 meter
Y = -2374533
69 meter E =
0008762
Z = 4592052
19 I = 51
50421
XDOT = 5515
614554 Wp = 70
23725
YDOT = 4381
447499 meter/sec RA = 198
54508 deg
ZDOT = -3017
279263 TA = 50
00551
MA = 49
92862
Ha = 229
290 n
mi
Hp = 222
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14450929
91 X = 4408563
35
Y = -7790464
85 feet Y = -2325255
61 meter
Z = 15065788
04 Z = 4613457
81
XDOT = 18095
848275 XDOT = 5480
866117
YDOT = 14374
827754 feet/sec YDOT = 4442
932583 meter/sec
ZDOT = -9899
210182 ZDOT = -2990
571337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13872707
19 X = 4228401
15
Y = -8607011
57 feet Y = -2623417
13 meter
Z = 15164631
03 Z = 4622179
54
XDOT = 18336
909500 XDOT = 5589
090016
YDOT = 12287
565958 feet/sec YDOT = 3745
250104 meter/sec
ZDOT = -9775
873293 ZDOT = -2979
686180
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 20272
03475207
00016717 00000-0 10270-3 0 9154
2 25544 51
6424 199
5534 0000752 126
9564 233
1655 15
48933497 7956
Satellite: ISS
Catalog Number: 25544
Epoch time: 20272
03475207 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 199
5534 deg
Eccentricity:
0000752
Arg of perigee: 126
9564 deg
Mean anomaly: 233
1655 deg
Mean motion: 15
48933497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 795
Checksum: 324
Coasting Arc #17 (Orbit 809)
---------------------------------------
Vector Time (GMT): 2020/272/23:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4175009
94 A = 6795315
41 meter
Y = 2757244
68 meter E =
0010848
Z = -4608947
88 I = 51
53739
XDOT = -5873
166526 Wp = 111
82072
YDOT = -3874
965677 meter/sec RA = 193
59259 deg
ZDOT = 3003
814484 TA = 188
26462
MA = 188
28250
Ha = 229
275 n
mi
Hp = 222
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13697539
16 X = -4183144
39
Y = 9046078
34 feet Y = 2710510
88 meter
Z = -15121220
08 Z = -4629248
38
XDOT = -19268
919048 XDOT = -5843
989771
YDOT = -12713
141984 feet/sec YDOT = -3940
480264 meter/sec
ZDOT = 9855
034395 ZDOT = 2975
356169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12876759
16 X = -3924836
19
Y = 10039884
18 feet Y = 3060156
70 meter
Z = -15214966
59 Z = -4637521
82
XDOT = -19503
133594 XDOT = -5944
555120
YDOT = -10287
015484 feet/sec YDOT = -3135
482319 meter/sec
ZDOT = 9723
594097 ZDOT = 2963
751481
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 20273
00250588
00016717 00000-0 10270-3 0 9166
2 25544 51
6433 194
7679 0000626 136
7266 223
3933 15
48973340 8100
Satellite: ISS
Catalog Number: 25544
Epoch time: 20273
00250588 = yrday
fracday
Element set: 916
Inclination: 51
6433 deg
RA of node: 194
7679 deg
Eccentricity:
0000626
Arg of perigee: 136
7266 deg
Mean anomaly: 223
3933 deg
Mean motion: 15
48973340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 810
Checksum: 310
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list