[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 28th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 66 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
There are no maneuvers
Coasting Arc #1 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2011/056/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3652184
95 A = 6726782
52 meter
Y = -3019372
62 meter E =
0011500
Z = -4783446
57 I = 51
71043
XDOT = 6308
178021 Wp = 81
69542
YDOT = 3570
133768 meter/sec RA = 13
25497 deg
ZDOT = 2569
681705 TA = 213
46434
MA = 213
53706
Ha = 193
467 n
mi
Hp = 185
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11982234
07 X = 3708913
38
Y = -9906078
16 feet Y = -2978214
56 meter
Z = -15693722
33 Z = -4765566
76
XDOT = 20696
122116 XDOT = 6255
304462
YDOT = 11713
037298 feet/sec YDOT = 3640
380034 meter/sec
ZDOT = 8430
714255 ZDOT = 2600
197767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15509802
21 X = 4727387
71
Y = -1847698
35 feet Y = -563178
46 meter
Z = -15621436
71 Z = -4761413
91
XDOT = 10957
827716 XDOT = 3339
945888
YDOT = 19854
464176 feet/sec YDOT = 6051
640681 meter/sec
ZDOT = 8553
787603 ZDOT = 2607
194462
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 11056
49256842
00016717 00000-0 10270-3 0 9000
2 25544 51
6432 13
7370 0005233 5
3345 354
7872 15
72443641 23320
Satellite: ISS
Catalog Number: 25544
Epoch time: 11056
49256842 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 13
7370 deg
Eccentricity:
0005233
Arg of perigee: 5
3345 deg
Mean anomaly: 354
7872 deg
Mean motion: 15
72443641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 284
Coasting Arc #2 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2011/057/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6059703
58 A = 6734963
45 meter
Y = -2316368
24 meter E =
0005326
Z = -1813081
26 I = 51
70938
XDOT = 3244
034006 Wp = 94
29752
YDOT = -4058
187813 meter/sec RA = 8
17278 deg
ZDOT = -5672
217604 TA = 105
75853
MA = 105
69979
Ha = 193
436 n
mi
Hp = 185
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19880917
27 X = -6024543
73
Y = -7599633
35 feet Y = -2383934
95 meter
Z = -5948429
32 Z = -1842433
17
XDOT = 10643
156189 XDOT = 3316
726292
YDOT = -13314
264478 feet/sec YDOT = -4021
504699 meter/sec
ZDOT = -18609
637810 ZDOT = -5656
281833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12924626
44 X = -3939426
14
Y = -16868210
32 feet Y = -5141430
50 meter
Z = -6066846
12 Z = -1849174
70
XDOT = 14904
996907 XDOT = 4543
043057
YDOT = -4767
358246 feet/sec YDOT = -1453
090794 meter/sec
ZDOT = -18545
163188 ZDOT = -5652
565740
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 11057
50938482
00016717 00000-0 10270-3 0 9011
2 25544 51
6439 8
5270 0005283 8
8698 351
2557 15
72498698 23483
Satellite: ISS
Catalog Number: 25544
Epoch time: 11057
50938482 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 8
5270 deg
Eccentricity:
0005283
Arg of perigee: 8
8698 deg
Mean anomaly: 351
2557 deg
Mean motion: 15
72498698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 338
Coasting Arc #3 (Orbit 2363)
---------------------------------------
Vector Time (GMT): 2011/058/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1941099
69 A = 6725163
94 meter
Y = 3934371
52 meter E =
0009508
Z = 5094596
45 I = 51
64621
XDOT = -7368
091387 Wp = 32
30541
YDOT = -1616
809313 meter/sec RA = 3
02223 deg
ZDOT = -1549
505683 TA = 72
61398
MA = 72
51003
Ha = 193
544 n
mi
Hp = 185
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6368437
29 X = -2009698
26
Y = 12908043
04 feet Y = 3912281
53 meter
Z = 16714555
30 Z = 5085000
13
XDOT = -24173
528171 XDOT = -7341
937293
YDOT = -5304
492497 feet/sec YDOT = -1699
057571 meter/sec
ZDOT = -5083
680062 ZDOT = -1585
235330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12138502
11 X = -3699815
44
Y = 7818531
66 feet Y = 2383088
45 meter
Z = 16675678
59 Z = 5082746
83
XDOT = -17510
285240 XDOT = -5337
134941
YDOT = -15970
369171 feet/sec YDOT = -4867
768523 meter/sec
ZDOT = -5227
869299 ZDOT = -1593
454562
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 11058
52618185
00016717 00000-0 10270-3 0 9020
2 25544 51
6442 3
3177 0005253 12
5914 347
5378 15
72518726 23648
Satellite: ISS
Catalog Number: 25544
Epoch time: 11058
52618185 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 3
3177 deg
Eccentricity:
0005253
Arg of perigee: 12
5914 deg
Mean anomaly: 347
5378 deg
Mean motion: 15
72518726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2364
Checksum: 302
Coasting Arc #4 (Orbit 2379)
---------------------------------------
Vector Time (GMT): 2011/059/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6651255
30 A = 6735920
65 meter
Y = 460468
48 meter E =
0018000
Z = 886767
73 I = 51
65230
XDOT = -1131
008248 Wp = 43
90574
YDOT = 4755
152040 meter/sec RA = 357
92039 deg
ZDOT = 5954
934304 TA = 325
77236
MA = 325
88825
Ha = 193
464 n
mi
Hp = 185
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21821703
74 X = 6641304
29
Y = 1510723
35 feet Y = 534791
24 meter
Z = 2909342
96 Z = 919054
38
XDOT = -3710
656983 XDOT = -1213
024335
YDOT = 15600
892521 feet/sec YDOT = 4742
046086 meter/sec
ZDOT = 19537
186038 ZDOT = 5949
240627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18209160
20 X = 5550152
03
Y = 12088018
72 feet Y = 3684428
11 meter
Z = 3039671
64 Z = 926491
92
XDOT = -10155
596640 XDOT = -3095
425856
YDOT = 10344
521106 feet/sec YDOT = 3153
010033 meter/sec
ZDOT = 19514
039118 ZDOT = 5947
879123
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 11059
54295803
00016717 00000-0 10270-3 0 9032
2 25544 51
6442 358
1075 0005225 15
9300 344
2026 15
72557570 23803
Satellite: ISS
Catalog Number: 25544
Epoch time: 11059
54295803 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 358
1075 deg
Eccentricity:
0005225
Arg of perigee: 15
9300 deg
Mean anomaly: 344
2026 deg
Mean motion: 15
72557570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2380
Checksum: 289
Coasting Arc #5 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2011/060/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 34148
86 A = 6724257
82 meter
Y = -4208040
39 meter E =
0016986
Z = -5258583
62 I = 51
58333
XDOT = 7649
356589 Wp = 76
37555
YDOT = -564
107341 meter/sec RA = 352
78107 deg
ZDOT = 506
377756 TA = 198
41665
MA = 198
47822
Ha = 193
512 n
mi
Hp = 185
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 112036
93 X = 106745
89
Y = -13805906
79 feet Y = -4207252
92 meter
Z = -17252570
92 Z = -5258241
14
XDOT = 25096
314268 XDOT = 7652
636213
YDOT = -1850
745871 feet/sec YDOT = -478
549237 meter/sec
ZDOT = 1661
344343 ZDOT = 543
545186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6803986
19 X = 2073854
99
Y = -12015568
57 feet Y = -3662345
30 meter
Z = -17251049
30 Z = -5258119
83
XDOT = 22029
574042 XDOT = 6714
614168
YDOT = 9898
802383 feet/sec YDOT = 3017
154966 meter/sec
ZDOT = 1811
408702 ZDOT = 552
117372
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 11060
49616787
00016717 00000-0 10270-3 0 9047
2 25544 51
6450 353
2231 0005262 18
8007 341
3349 15
72578328 23955
Satellite: ISS
Catalog Number: 25544
Epoch time: 11060
49616787 = yrday
fracday
Element set: 904
Inclination: 51
6450 deg
RA of node: 353
2231 deg
Eccentricity:
0005262
Arg of perigee: 18
8007 deg
Mean anomaly: 341
3349 deg
Mean motion: 15
72578328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 306
Coasting Arc #6 (Orbit 2410)
---------------------------------------
Vector Time (GMT): 2011/061/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6580589
41 A = 6736139
74 meter
Y = 1427456
27 meter E =
0011269
Z = -15292
28 I = 51
59422
XDOT = -1008
039551 Wp = 109
26415
YDOT = -4673
035234 meter/sec RA = 347
65790 deg
ZDOT = -6030
243300 TA = 70
90190
MA = 70
77991
Ha = 193
537 n
mi
Hp = 185
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21589860
26 X = -6595988
13
Y = 4683255
47 feet Y = 1353782
03 meter
Z = -50171
53 Z = -47297
34
XDOT = -3307
216375 XDOT = -926
416907
YDOT = -15331
480425 feet/sec YDOT = -4683
851851 meter/sec
ZDOT = -19784
262795 ZDOT = -6034
941577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21297750
51 X = -6491554
36
Y = -5867801
76 feet Y = -1788505
98 meter
Z = -179418
39 Z = -54686
73
XDOT = 3860
752460 XDOT = 1176
757350
YDOT = -13508
638460 feet/sec YDOT = -4117
433003 meter/sec
ZDOT = -19803
079167 ZDOT = -6035
978530
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 11061
51290578
00016717 00000-0 10270-3 0 9058
2 25544 51
6457 348
0131 0005227 23
1404 336
9993 15
72606716 24111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11061
51290578 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 348
0131 deg
Eccentricity:
0005227
Arg of perigee: 23
1404 deg
Mean anomaly: 336
9993 deg
Mean motion: 15
72606716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2411
Checksum: 293
Coasting Arc #7 (Orbit 2426)
---------------------------------------
Vector Time (GMT): 2011/062/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1766793
07 A = 6723907
47 meter
Y = 3813405
58 meter E =
0006023
Z = 5244288
06 I = 51
52409
XDOT = -7207
745748 Wp = 50
64466
YDOT = 2674
115212 meter/sec RA = 342
53165 deg
ZDOT = 487
172129 TA = 34
74142
MA = 34
70210
Ha = 193
404 n
mi
Hp = 184
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5796565
20 X = 1698544
43
Y = 12511173
15 feet Y = 3832781
84 meter
Z = 17205669
50 Z = 5252704
76
XDOT = -23647
459804 XDOT = -7239
479047
YDOT = 8773
343871 feet/sec YDOT = 2593
336450 meter/sec
ZDOT = 1598
333755 ZDOT = 452
080534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -525058
03 X = -160037
69
Y = 13736364
82 feet Y = 4186844
00 meter
Z = 17239526
68 Z = 5254607
73
XDOT = -24076
582544 XDOT = -7338
542359
YDOT = -2734
452649 feet/sec YDOT = -833
461167 meter/sec
ZDOT = 1456
595681 ZDOT = 443
970364
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 11062
52962151
00016717 00000-0 10270-3 0 9064
2 25544 51
6456 342
8035 0005166 25
2113 334
9301 15
72683711 24275
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
52962151 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 342
8035 deg
Eccentricity:
0005166
Arg of perigee: 25
2113 deg
Mean anomaly: 334
9301 deg
Mean motion: 15
72683711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2427
Checksum: 283
Coasting Arc #8 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2011/063/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5865883
46 A = 6735686
49 meter
Y = -3181863
73 meter E =
0015556
Z = -858125
87 I = 51
53462
XDOT = 2968
050524 Wp = 35
40631
YDOT = 3884
741721 meter/sec RA = 337
38654 deg
ZDOT = 5950
450826 TA = 315
21896
MA = 315
34442
Ha = 193
604 n
mi
Hp = 184
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19245024
48 X = 5905196
22
Y = -10439185
48 feet Y = -3116048
16 meter
Z = -2815373
60 Z = -829534
27
XDOT = 9737
698571 XDOT = 2895
484495
YDOT = 12745
215619 feet/sec YDOT = 3917
527175 meter/sec
ZDOT = 19522
476462 ZDOT = 5964
692578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21882674
17 X = 6669839
09
Y = -1064507
62 feet Y = -324461
92 meter
Z = -2699867
38 Z = -822919
58
XDOT = 3071
812442 XDOT = 936
288432
YDOT = 14059
993897 feet/sec YDOT = 4285
486140 meter/sec
ZDOT = 19579
845932 ZDOT = 5967
937040
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 11063
48277700
00016717 00000-0 10270-3 0 9070
2 25544 51
6456 337
9188 0005283 29
2269 330
9189 15
72663753 24426
Satellite: ISS
Catalog Number: 25544
Epoch time: 11063
48277700 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 337
9188 deg
Eccentricity:
0005283
Arg of perigee: 29
2269 deg
Mean anomaly: 330
9189 deg
Mean motion: 15
72663753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 330
Coasting Arc #9 (Orbit 2457)
---------------------------------------
Vector Time (GMT): 2011/064/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3312583
82 A = 6724387
77 meter
Y = -2863811
10 meter E =
0018118
Z = -5119041
92 I = 51
47014
XDOT = 6080
369737 Wp = 66
94991
YDOT = -4478
947272 meter/sec RA = 332
27139 deg
ZDOT = -1425
983464 TA = 189
31290
MA = 189
34654
Ha = 193
553 n
mi
Hp = 184
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10868057
14 X = -3255447
05
Y = -9395705
70 feet Y = -2900535
55 meter
Z = -16794756
95 Z = -5134995
01
XDOT = 19948
719611 XDOT = 6136
929301
YDOT = -14694
708899 feet/sec YDOT = -4410
636819 meter/sec
ZDOT = -4678
423437 ZDOT = -1396
307722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5859075
88 X = -1785846
33
Y = -13034608
31 feet Y = -3972948
61 meter
Z = -16859063
69 Z = -5138642
61
XDOT = 23337
450016 XDOT = 7113
254765
YDOT = -4581
646000 feet/sec YDOT = -1396
485701 meter/sec
ZDOT = -4558
512326 ZDOT = -1389
434557
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 11064
49945500
00016717 00000-0 10270-3 0 9083
2 25544 51
6463 332
7083 0005280 33
7433 326
4065 15
72723290 24584
Satellite: ISS
Catalog Number: 25544
Epoch time: 11064
49945500 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 332
7083 deg
Eccentricity:
0005280
Arg of perigee: 33
7433 deg
Mean anomaly: 326
4065 deg
Mean motion: 15
72723290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2458
Checksum: 301
Coasting Arc #10 (Orbit 2473)
---------------------------------------
Vector Time (GMT): 2011/065/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4676625
15 A = 6734708
50 meter
Y = 4560505
09 meter E =
0015860
Z = 1620063
70 I = 51
47793
XDOT = -4474
192024 Wp = 97
82894
YDOT = -2536
996691 meter/sec RA = 327
10723 deg
ZDOT = -5728
275039 TA = 64
25146
MA = 64
08785
Ha = 193
592 n
mi
Hp = 184
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15343258
35 X = -4735143
86
Y = 14962287
04 feet Y = 4507881
23 meter
Z = 5315169
61 Z = 1597202
34
XDOT = -14679
107690 XDOT = -4417
663822
YDOT = -8323
479956 feet/sec YDOT = -2586
714423 meter/sec
ZDOT = -18793
553279 ZDOT = -5749
872716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20092285
75 X = -6124128
70
Y = 7520596
82 feet Y = 2292277
91 meter
Z = 5222768
91 Z = 1591899
96
XDOT = -9443
586799 XDOT = -2878
405256
YDOT = -12012
059248 feet/sec YDOT = -3661
275659 meter/sec
ZDOT = -18880
649217 ZDOT = -5754
821881
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 11065
51611319
00016717 00000-0 10270-3 0 9096
2 25544 51
6460 327
4977 0005199 37
4675 322
6850 15
72725640 24741
Satellite: ISS
Catalog Number: 25544
Epoch time: 11065
51611319 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 327
4977 deg
Eccentricity:
0005199
Arg of perigee: 37
4675 deg
Mean anomaly: 322
6850 deg
Mean motion: 15
72725640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2474
Checksum: 321
Coasting Arc #11 (Orbit 2489)
---------------------------------------
Vector Time (GMT): 2011/066/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4398127
50 A = 6725265
78 meter
Y = 1482570
85 meter E =
0008927
Z = 4859152
76 I = 51
42175
XDOT = -4494
058120 Wp = 86
74585
YDOT = 5826
001880 meter/sec RA = 322
00108 deg
ZDOT = 2287
000982 TA = 340
92380
MA = 340
95722
Ha = 193
422 n
mi
Hp = 184
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14429552
18 X = 4357617
63
Y = 4864077
58 feet Y = 1531527
41 meter
Z = 15942102
24 Z = 4880420
05
XDOT = -14744
285171 XDOT = -4569
981278
YDOT = 19114
179395 feet/sec YDOT = 5775
322346 meter/sec
ZDOT = 7503
284063 ZDOT = 2264
984040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11343744
56 X = 3457573
34
Y = 10022375
26 feet Y = 3054819
98 meter
Z = 16027891
44 Z = 4885301
31
XDOT = -20291
929011 XDOT = -6184
979963
YDOT = 11094
077766 feet/sec YDOT = 3381
474903 meter/sec
ZDOT = 7414
262207 ZDOT = 2259
867121
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 11066
53274988
00016717 00000-0 10270-3 0 9108
2 25544 51
6460 322
2869 0005202 40
5126 319
6423 15
72777582 24907
Satellite: ISS
Catalog Number: 25544
Epoch time: 11066
53274988 = yrday
fracday
Element set: 910
Inclination: 51
6460 deg
RA of node: 322
2869 deg
Eccentricity:
0005202
Arg of perigee: 40
5126 deg
Mean anomaly: 319
6423 deg
Mean motion: 15
72777582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2490
Checksum: 309
Coasting Arc #12 (Orbit 2504)
---------------------------------------
Vector Time (GMT): 2011/067/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3104713
32 A = 6733178
77 meter
Y = -5488256
53 meter E =
0010941
Z = -2354191
25 I = 51
42551
XDOT = 5444
495611 Wp = 43
88107
YDOT = 780
037448 meter/sec RA = 316
82062 deg
ZDOT = 5384
418072 TA = 289
54257
MA = 289
66069
Ha = 193
538 n
mi
Hp = 184
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10186067
32 X = 3177289
43
Y = -18006090
96 feet Y = -5453132
18 meter
Z = -7723724
58 Z = -2338931
85
XDOT = 17862
518410 XDOT = 5409
212129
YDOT = 2559
177978 feet/sec YDOT = 840
724360 meter/sec
ZDOT = 17665
413621 ZDOT = 5410
781417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16171338
11 X = 4929023
85
Y = -12938815
63 feet Y = -3943751
00 meter
Z = -7661988
95 Z = -2335374
23
XDOT = 14603
650518 XDOT = 4451
192678
YDOT = 7772
590242 feet/sec YDOT = 2369
085506 meter/sec
ZDOT = 17771
785456 ZDOT = 5416
840207
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 11067
48582895
00016717 00000-0 10270-3 0 9113
2 25544 51
6463 317
4016 0005200 43
1207 317
0362 15
72814123 25051
Satellite: ISS
Catalog Number: 25544
Epoch time: 11067
48582895 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 317
4016 deg
Eccentricity:
0005200
Arg of perigee: 43
1207 deg
Mean anomaly: 317
0362 deg
Mean motion: 15
72814123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2505
Checksum: 278
Coasting Arc #13 (Orbit 2520)
---------------------------------------
Vector Time (GMT): 2011/068/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4976590
97 A = 6726426
18 meter
Y = 133981
30 meter E =
0015132
Z = -4538431
92 I = 51
38168
XDOT = 2596
859933 Wp = 61
33843
YDOT = -6563
781109 meter/sec RA = 311
72058 deg
ZDOT = -3041
877559 TA = 178
23227
MA = 178
22692
Ha = 193
491 n
mi
Hp = 183
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16327398
18 X = -4955672
56
Y = 439571
18 feet Y = 78446
61 meter
Z = -14889868
49 Z = -4562557
23
XDOT = 8519
881671 XDOT = 2684
841168
YDOT = -21534
714923 feet/sec YDOT = -6534
249781 meter/sec
ZDOT = -9979
913252 ZDOT = -3029
047827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15340935
41 X = -4675917
11
Y = -5340779
93 feet Y = -1627869
72 meter
Z = -14987231
51 Z = -4568108
16
XDOT = 15261
214308 XDOT = 4651
618121
YDOT = -15981
707675 feet/sec YDOT = -4871
224499 meter/sec
ZDOT = -9927
955992 ZDOT = -3026
040986
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 11068
50242643
00016717 00000-0 10270-3 0 9122
2 25544 51
6463 312
1904 0005185 45
3291 314
8293 15
72846833 25217
Satellite: ISS
Catalog Number: 25544
Epoch time: 11068
50242643 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 312
1904 deg
Eccentricity:
0005185
Arg of perigee: 45
3291 deg
Mean anomaly: 314
8293 deg
Mean motion: 15
72846833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2521
Checksum: 293
Coasting Arc #14 (Orbit 2536)
---------------------------------------
Vector Time (GMT): 2011/069/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1414797
04 A = 6731656
23 meter
Y = 5874730
76 meter E =
0017295
Z = 2954022
78 I = 51
37942
XDOT = -5773
837860 Wp = 84
24014
YDOT = 1122
617393 meter/sec RA = 306
52856 deg
ZDOT = -4971
246757 TA = 61
55679
MA = 61
38264
Ha = 193
550 n
mi
Hp = 183
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4641722
56 X = -1494734
26
Y = 19274051
06 feet Y = 5858462
90 meter
Z = 9691675
80 Z = 2946955
16
XDOT = -18943
037599 XDOT = -5761
812787
YDOT = 3683
127929 feet/sec YDOT = 1058
117723 meter/sec
ZDOT = -16309
864687 ZDOT = -4999
266751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10938587
39 X = -3334081
44
Y = 16551044
71 feet Y = 5044758
43 meter
Z = 9662993
19 Z = 2945280
32
XDOT = -17773
687099 XDOT = -5417
419828
YDOT = -2107
224899 feet/sec YDOT = -642
282149 meter/sec
ZDOT = -16422
970937 ZDOT = -5005
721542
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 11069
51900489
00016717 00000-0 10270-3 0 9134
2 25544 51
6460 306
9790 0005239 49
8619 310
3002 15
72860873 25377
Satellite: ISS
Catalog Number: 25544
Epoch time: 11069
51900489 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 306
9790 deg
Eccentricity:
0005239
Arg of perigee: 49
8619 deg
Mean anomaly: 310
3002 deg
Mean motion: 15
72860873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2537
Checksum: 315
Coasting Arc #15 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2011/070/11:32:54
924
Vector Time (MET): N/A
Weight (LBS) : 849782
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4981673
00 A = 6727861
56 meter
Y = -1827470
00 meter E =
0014100
Z = 4123592
35 I = 51
34977
XDOT = -621
608958 Wp = 87
69181
YDOT = 6720
487835 meter/sec RA = 301
43086 deg
ZDOT = 3718
934271 TA = 324
09404
MA = 324
18872
Ha = 193
413 n
mi
Hp = 183
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16344071
54 X = 4981706
35
Y = -5995636
49 feet Y = -1771761
49 meter
Z = 13528846
29 Z = 4147793
32
XDOT = -2039
399468 XDOT = -714
778305
YDOT = 22048
844602 feet/sec YDOT = 6713
015903 meter/sec
ZDOT = 12201
227922 ZDOT = 3715
687824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17327057
94 X = 5281287
26
Y = -442644
16 feet Y = -134917
94 meter
Z = 13626560
20 Z = 4153375
55
XDOT = -9127
893686 XDOT = -2782
181996
YDOT = 18933
134836 feet/sec YDOT = 5770
819498 meter/sec
ZDOT = 12187
945515 ZDOT = 3714
885793
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 11070
53556208
00016717 00000-0 10270-3 0 9145
2 25544 51
6460 301
7670 0005234 52
3044 307
8593 15
72879019 25539
Satellite: ISS
Catalog Number: 25544
Epoch time: 11070
53556208 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 301
7670 deg
Eccentricity:
0005234
Arg of perigee: 52
3044 deg
Mean anomaly: 307
8593 deg
Mean motion: 15
72879019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 298
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- 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