[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 11th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
343/19:50:40
740 3
2 4
3 4
3
N/A 1
3 -0
4 223
3
000/00:01:21
480 2
5 -0
0 201
3
Coasting Arc #1 (Orbit 2827)
---------------------------------------
Vector Time (GMT): 2011/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 765380
31 A = 6764153
79 meter
Y = -4203487
52 meter E =
0039454
Z = -5273524
33 I = 51
61531
XDOT = 7601
041571 Wp = 128
04099
YDOT = 380
243455 meter/sec RA = 358
20496 deg
ZDOT = 780
344672 TA = 149
55078
MA = 149
32108
Ha = 223
485 n
mi
Hp = 198
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2511090
25 X = 837945
75
Y = -13790969
55 feet Y = -4194522
20 meter
Z = -17301589
00 Z = -5269630
31
XDOT = 24937
800429 XDOT = 7592
433867
YDOT = 1247
517897 feet/sec YDOT = 465
194742 meter/sec
ZDOT = 2560
185931 ZDOT = 817
250069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12858871
75 X = 3919384
11
Y = 5631080
86 feet Y = 1716353
45 meter
Z = -17285304
25 Z = -5268560
73
XDOT = -6373
769722 XDOT = -1942
725011
YDOT = 23075
391719 feet/sec YDOT = 7033
379396 meter/sec
ZDOT = 2710
892848 ZDOT = 826
280140
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 11343
51469094
00016717 00000-0 10270-3 0 9007
2 25544 51
6431 358
6573 0028199 144
4123 215
8919 15
58760058 28287
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
51469094 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 358
6573 deg
Eccentricity:
0028199
Arg of perigee: 144
4123 deg
Mean anomaly: 215
8919 deg
Mean motion: 15
58760058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2828
Checksum: 328
Coasting Arc #2 (Orbit 2832)
---------------------------------------
Vector Time (GMT): 2011/343/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4652817
93 A = 6772235
26 meter
Y = -3244393
85 meter E =
0028935
Z = -3735476
55 I = 51
62663
XDOT = 5561
775632 Wp = 138
46781
YDOT = 3053
772370 meter/sec RA = 356
54239 deg
ZDOT = 4273
176079 TA = 176
98119
MA = 176
96369
Ha = 223
314 n
mi
Hp = 201
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15265150
69 X = 4706898
02
Y = -10644336
78 feet Y = -3192060
35 meter
Z = -12255500
50 Z = -3712741
98
XDOT = 18247
295380 XDOT = 5506
455862
YDOT = 10018
938221 feet/sec YDOT = 3115
657717 meter/sec
ZDOT = 14019
606559 ZDOT = 4300
061453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11998490
86 X = 3657140
01
Y = -14305158
76 feet Y = -4360212
39 meter
Z = -12162346
56 Z = -3707083
23
XDOT = 19115
123315 XDOT = 5826
289586
YDOT = 4014
189034 feet/sec YDOT = 1223
524817 meter/sec
ZDOT = 14129
144762 ZDOT = 4306
563323
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 11343
83523815
00016717 00000-0 10270-3 0 9015
2 25544 51
6445 357
0478 0024687 147
0951 213
1746 15
58014102 28332
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
83523815 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 357
0478 deg
Eccentricity:
0024687
Arg of perigee: 147
0951 deg
Mean anomaly: 213
1746 deg
Mean motion: 15
58014102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2833
Checksum: 301
Coasting Arc #3 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2011/344/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6416199
81 A = 6777659
44 meter
Y = 1817231
48 meter E =
0037475
Z = 1077564
17 I = 51
61441
XDOT = -2249
498093 Wp = 140
91001
YDOT = -4393
082680 meter/sec RA = 351
54097 deg
ZDOT = -5902
941289 TA = 27
34786
MA = 27
15107
Ha = 223
287 n
mi
Hp = 201
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21050524
32 X = -6441278
23
Y = 5962045
54 feet Y = 1745341
23 meter
Z = 3535315
53 Z = 1046333
42
XDOT = -7380
243086 XDOT = -2171
531002
YDOT = -14413
000919 feet/sec YDOT = -4417
801229 meter/sec
ZDOT = -19366
605280 ZDOT = -5913
680612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18563895
63 X = -5658275
39
Y = 11616331
66 feet Y = 3540657
89 meter
Z = 3407584
91 Z = 1038631
88
XDOT = -10156
585594 XDOT = -3095
727289
YDOT = -10454
622931 feet/sec YDOT = -3186
569069 meter/sec
ZDOT = -19410
072211 ZDOT = -5916
190010
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 11344
86149591
00016717 00000-0 10270-3 0 9025
2 25544 51
6445 351
9013 0024832 151
0399 209
2139 15
57999648 28498
Satellite: ISS
Catalog Number: 25544
Epoch time: 11344
86149591 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 351
9013 deg
Eccentricity:
0024832
Arg of perigee: 151
0399 deg
Mean anomaly: 209
2139 deg
Mean motion: 15
57999648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 337
Coasting Arc #4 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2011/345/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6520700
78 A = 6776366
24 meter
Y = -41958
43 meter E =
0028774
Z = 1861008
55 I = 51
58122
XDOT = -1593
785467 Wp = 125
01276
YDOT = 4962
998571 meter/sec RA = 346
54888 deg
ZDOT = 5618
437713 TA = 255
49134
MA = 255
81072
Ha = 222
985 n
mi
Hp = 201
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21393375
25 X = 6511644
87
Y = -137658
88 feet Y = 30909
17 meter
Z = 6105671
11 Z = 1892664
16
XDOT = -5228
954943 XDOT = -1676
457635
YDOT = 16282
803709 feet/sec YDOT = 4944
712897 meter/sec
ZDOT = 18433
194595 ZDOT = 5610
494935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20357799
31 X = 6205057
23
Y = -6454434
40 feet Y = -1967311
60 meter
Z = 6234978
58 Z = 1900421
47
XDOT = -750
103565 XDOT = -228
631567
YDOT = 15650
397461 feet/sec YDOT = 4770
241146 meter/sec
ZDOT = 18400
300184 ZDOT = 5608
411496
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 11345
88772921
00016717 00000-0 10270-3 0 9038
2 25544 51
6446 346
7548 0024550 154
7388 205
4973 15
58068284 28655
Satellite: ISS
Catalog Number: 25544
Epoch time: 11345
88772921 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 346
7548 deg
Eccentricity:
0024550
Arg of perigee: 154
7388 deg
Mean anomaly: 205
4973 deg
Mean motion: 15
58068284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 347
Coasting Arc #5 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2011/346/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4855469
64 A = 6769849
20 meter
Y = -1971015
99 meter E =
0026070
Z = -4288477
16 I = 51
53079
XDOT = 4982
971486 Wp = 138
87891
YDOT = -4632
742969 meter/sec RA = 341
53421 deg
ZDOT = -3544
002176 TA = 95
10995
MA = 94
81235
Ha = 222
720 n
mi
Hp = 201
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15930018
51 X = -4812235
89
Y = -6466587
90 feet Y = -2025070
57 meter
Z = -14069806
94 Z = -4311960
20
XDOT = 16348
331647 XDOT = 5051
621465
YDOT = -15199
287957 feet/sec YDOT = -4576
636047 meter/sec
ZDOT = -11627
303727 ZDOT = -3519
628778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17072105
74 X = -5203577
83
Y = -1192500
55 feet Y = -363474
17 meter
Z = -14165552
04 Z = -4317660
26
XDOT = 10759
678085 XDOT = 3279
549880
YDOT = -18324
235174 feet/sec YDOT = -5585
226881 meter/sec
ZDOT = -11527
325270 ZDOT = -3513
528742
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 11346
84980284
00016717 00000-0 10270-3 0 9049
2 25544 51
6448 341
9294 0024469 158
6577 201
5604 15
58102535 28807
Satellite: ISS
Catalog Number: 25544
Epoch time: 11346
84980284 = yrday
fracday
Element set: 904
Inclination: 51
6448 deg
RA of node: 341
9294 deg
Eccentricity:
0024469
Arg of perigee: 158
6577 deg
Mean anomaly: 201
5604 deg
Mean motion: 15
58102535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 330
Coasting Arc #6 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2011/347/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2067895
54 A = 6765698
01 meter
Y = 3681342
82 meter E =
0026011
Z = 5278874
43 I = 51
48902
XDOT = -6915
472941 Wp = 156
95588
YDOT = 3325
680410 meter/sec RA = 336
48995 deg
ZDOT = 365
650135 TA = 289
41639
MA = 289
69733
Ha = 222
578 n
mi
Hp = 201
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6784434
19 X = 2000932
67
Y = 12077896
39 feet Y = 3704092
32 meter
Z = 17319141
84 Z = 5288757
96
XDOT = -22688
559517 XDOT = -6953
923636
YDOT = 10911
024966 feet/sec YDOT = 3248
132320 meter/sec
ZDOT = 1199
639549 ZDOT = 331
961908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10279375
74 X = 3133153
73
Y = 9211402
52 feet Y = 2807635
49 meter
Z = 17359184
91 Z = 5291079
56
XDOT = -17174
844720 XDOT = -5234
892671
YDOT = 17016
498546 feet/sec YDOT = 5186
628757 meter/sec
ZDOT = 1061
730861 ZDOT = 323
615566
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 11347
87599404
00016717 00000-0 10270-3 0 9054
2 25544 51
6450 336
7833 0024526 162
2723 197
9293 15
58148124 28962
Satellite: ISS
Catalog Number: 25544
Epoch time: 11347
87599404 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 336
7833 deg
Eccentricity:
0024526
Arg of perigee: 162
2723 deg
Mean anomaly: 197
9293 deg
Mean motion: 15
58148124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 340
Coasting Arc #7 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2011/348/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1220910
17 A = 6768638
92 meter
Y = -4836717
36 meter E =
0031251
Z = -4601939
14 I = 51
47110
XDOT = 6965
101652 Wp = 150
02120
YDOT = -1091
935503 meter/sec RA = 331
43763 deg
ZDOT = 2977
768036 TA = 149
89470
MA = 149
71471
Ha = 222
434 n
mi
Hp = 202
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4005610
78 X = 1297259
79
Y = -15868495
27 feet Y = -4822637
09 meter
Z = -15098225
52 Z = -4595822
97
XDOT = 22851
383373 XDOT = 6962
328870
YDOT = -3582
465561 feet/sec YDOT = -1014
063227 meter/sec
ZDOT = 9769
580169 ZDOT = 3011
597435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1628971
66 X = -496510
56
Y = -16308501
05 feet Y = -4970831
12 meter
Z = -15072813
89 Z = -4594193
67
XDOT = 18967
920410 XDOT = 5781
422141
YDOT = -11105
641746 feet/sec YDOT = -3384
999604 meter/sec
ZDOT = 9907
864952 ZDOT = 3019
917237
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 11348
83802779
00016717 00000-0 10270-3 0 9064
2 25544 51
6445 331
9571 0024423 166
0228 194
1608 15
58180799 29111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11348
83802779 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 331
9571 deg
Eccentricity:
0024423
Arg of perigee: 166
0228 deg
Mean anomaly: 194
1608 deg
Mean motion: 15
58180799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 329
Coasting Arc #8 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2011/349/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3955599
94 A = 6775086
00 meter
Y = 4919576
71 meter E =
0033038
Z = 2398234
74 I = 51
46711
XDOT = -5275
041211 Wp = 147
17672
YDOT = -1623
602589 meter/sec RA = 326
41206 deg
ZDOT = -5362
759196 TA = 5
82234
MA = 5
78403
Ha = 222
260 n
mi
Hp = 202
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12977690
11 X = -4021967
75
Y = 16140343
53 feet Y = 4874971
51 meter
Z = 7868224
21 Z = 2378857
69
XDOT = -17306
565654 XDOT = -5230
442568
YDOT = -5326
780146 feet/sec YDOT = -1682
341602 meter/sec
ZDOT = -17594
354319 ZDOT = -5388
276963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6318640
04 X = -1925921
49
Y = 19754794
77 feet Y = 6021261
45 meter
Z = 7788642
60 Z = 2373978
27
XDOT = -16522
643870 XDOT = -5036
101852
YDOT = 1702
528779 feet/sec YDOT = 518
930772 meter/sec
ZDOT = -17698
447999 ZDOT = -5394
486950
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 11349
86417616
00016717 00000-0 10270-3 0 9071
2 25544 51
6448 326
8109 0024400 169
5737 190
5928 15
58211104 29279
Satellite: ISS
Catalog Number: 25544
Epoch time: 11349
86417616 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 326
8109 deg
Eccentricity:
0024400
Arg of perigee: 169
5737 deg
Mean anomaly: 190
5928 deg
Mean motion: 15
58211104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 324
Coasting Arc #9 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2011/350/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5557377
32 A = 6777165
89 meter
Y = -3854145
52 meter E =
0020739
Z = 569874
23 I = 51
44901
XDOT = 2307
859975 Wp = 140
76250
YDOT = 4227
962104 meter/sec RA = 321
40776 deg
ZDOT = 5953
366711 TA = 225
40095
MA = 225
57035
Ha = 222
056 n
mi
Hp = 202
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18232865
21 X = 5597293
76
Y = -12644834
39 feet Y = -3791776
36 meter
Z = 1869666
11 Z = 596968
60
XDOT = 7571
719079 XDOT = 2231
490283
YDOT = 13871
266744 feet/sec YDOT = 4253
342679 meter/sec
ZDOT = 19532
043015 ZDOT = 5964
392977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12108726
57 X = 3690739
86
Y = -18581725
95 feet Y = -5663710
07 meter
Z = 1980672
52 Z = 603708
98
XDOT = 10778
826874 XDOT = 3285
386431
YDOT = 9155
246014 feet/sec YDOT = 2790
518985 meter/sec
ZDOT = 19576
717615 ZDOT = 5966
983529
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 11350
89030002
00016717 00000-0 10270-3 0 9087
2 25544 51
6437 321
6632 0024481 173
7907 186
3556 15
58263791 29433
Satellite: ISS
Catalog Number: 25544
Epoch time: 11350
89030002 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 321
6632 deg
Eccentricity:
0024481
Arg of perigee: 173
7907 deg
Mean anomaly: 186
3556 deg
Mean motion: 15
58263791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 314
Coasting Arc #10 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2011/351/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5620268
94 A = 6772301
15 meter
Y = 1604518
57 meter E =
0025006
Z = -3401237
85 I = 51
40868
XDOT = 1037
043267 Wp = 165
63236
YDOT = -6062
360990 meter/sec RA = 316
39525 deg
ZDOT = -4604
542988 TA = 54
42022
MA = 54
18742
Ha = 221
772 n
mi
Hp = 202
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18439202
55 X = -5621270
69
Y = 5264168
53 feet Y = 1541663
84 meter
Z = -11158916
82 Z = -3428543
45
XDOT = 3402
372924 XDOT = 1127
124736
YDOT = -19889
635793 feet/sec YDOT = -6050
260237 meter/sec
ZDOT = -15106
768333 ZDOT = -4599
286524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14825594
25 X = -4518841
13
Y = 12058718
33 feet Y = 3675497
35 meter
Z = -11270587
98 Z = -3435275
22
XDOT = -3723
370451 XDOT = -1134
883313
YDOT = -18582
387805 feet/sec YDOT = -5663
911803 meter/sec
ZDOT = -15084
779432 ZDOT = -4597
840771
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 11351
85227326
00016717 00000-0 10270-3 0 9092
2 25544 51
6427 316
8374 0024417 177
4708 182
6575 15
58258153 29582
Satellite: ISS
Catalog Number: 25544
Epoch time: 11351
85227326 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 316
8374 deg
Eccentricity:
0024417
Arg of perigee: 177
4708 deg
Mean anomaly: 182
6575 deg
Mean motion: 15
58258153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 338
Coasting Arc #11 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2011/352/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4336133
52 A = 6766310
78 meter
Y = 1193095
72 meter E =
0027644
Z = 5059015
56 I = 51
36717
XDOT = -3816
961769 Wp = 171
46758
YDOT = 6427
196935 meter/sec RA = 311
35006 deg
ZDOT = 1727
708687 TA = 261
62092
MA = 261
93441
Ha = 221
645 n
mi
Hp = 202
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14226159
84 X = 4297893
96
Y = 3914356
03 feet Y = 1241370
94 meter
Z = 16597820
08 Z = 5079987
74
XDOT = -12522
840451 XDOT = -3896
941197
YDOT = 21086
604117 feet/sec YDOT = 6384
066041 meter/sec
ZDOT = 5668
335586 ZDOT = 1708
971909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14492091
89 X = 4417189
61
Y = -2199431
67 feet Y = -670386
77 meter
Z = 16683381
29 Z = 5085094
62
XDOT = -3002
918903 XDOT = -915
289682
YDOT = 23320
550954 feet/sec YDOT = 7108
103931 meter/sec
ZDOT = 5591
258371 ZDOT = 1704
215552
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 11352
87835648
00016717 00000-0 10270-3 0 9109
2 25544 51
6425 311
6897 0024375 180
9431 179
1682 15
58267166 29740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11352
87835648 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 311
6897 deg
Eccentricity:
0024375
Arg of perigee: 180
9431 deg
Mean anomaly: 179
1682 deg
Mean motion: 15
58267166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 343
Coasting Arc #12 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2011/353/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2061068
06 A = 6766217
92 meter
Y = -4021573
46 meter E =
0029561
Z = -5052855
86 I = 51
34688
XDOT = 5472
496509 Wp = 158
16839
YDOT = -5060
123331 meter/sec RA = 306
28356 deg
ZDOT = 1771
524083 TA = 129
18677
MA = 128
92384
Ha = 221
457 n
mi
Hp = 202
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6762034
33 X = -1991398
84
Y = -13194138
66 feet Y = -4044231
69 meter
Z = -16577611
10 Z = -5062699
65
XDOT = 17954
384872 XDOT = 5520
067288
YDOT = -16601
454498 feet/sec YDOT = -4998
660660 meter/sec
ZDOT = 5812
086887 ZDOT = 1798
224817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11631107
05 X = -3545161
43
Y = -9121642
04 feet Y = -2780276
49 meter
Z = -16617478
40 Z = -5065007
42
XDOT = 8516
381019 XDOT = 2595
792935
YDOT = -21787
721017 feet/sec YDOT = -6640
897366 meter/sec
ZDOT = 5921
574896 ZDOT = 1804
896028
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 11353
84028634
00016717 00000-0 10270-3 0 9117
2 25544 51
6412 306
8618 0024470 184
6195 175
4737 15
58342536 29898
Satellite: ISS
Catalog Number: 25544
Epoch time: 11353
84028634 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 306
8618 deg
Eccentricity:
0024470
Arg of perigee: 184
6195 deg
Mean anomaly: 175
4737 deg
Mean motion: 15
58342536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 329
Coasting Arc #13 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2011/354/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -436917
62 A = 6772212
74 meter
Y = 5859965
63 meter E =
0025947
Z = 3332846
95 I = 51
35099
XDOT = -5702
698681 Wp = 159
76758
YDOT = 2217
403233 meter/sec RA = 301
23666 deg
ZDOT = -4659
431625 TA = 341
05700
MA = 341
15334
Ha = 221
142 n
mi
Hp = 203
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1433456
77 X = -518602
93
Y = 19225609
02 feet Y = 5854622
70 meter
Z = 10934537
24 Z = 3330526
54
XDOT = -18709
641342 XDOT = -5704
435454
YDOT = 7274
944989 feet/sec YDOT = 2153
622896 meter/sec
ZDOT = -15286
849165 ZDOT = -4687
139532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7109605
72 X = 2167007
82
Y = 17926247
22 feet Y = 5463920
15 meter
Z = 10924564
62 Z = 3329807
30
XDOT = -12212
746980 XDOT = -3722
445279
YDOT = 14202
554909 feet/sec YDOT = 4328
938736 meter/sec
ZDOT = -15400
211524 ZDOT = -4693
984472
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 11354
86632358
00016717 00000-0 10270-3 0 9125
2 25544 51
6418 301
7146 0024402 188
8759 171
1968 15
58393205 30059
Satellite: ISS
Catalog Number: 25544
Epoch time: 11354
86632358 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 301
7146 deg
Eccentricity:
0024402
Arg of perigee: 188
8759 deg
Mean anomaly: 171
1968 deg
Mean motion: 15
58393205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 318
Coasting Arc #14 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2011/355/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2647529
14 A = 6776825
77 meter
Y = -6232020
45 meter E =
0015865
Z = -472688
64 I = 51
35063
XDOT = 4574
582384 Wp = 171
36608
YDOT = 1492
439182 meter/sec RA = 296
21741 deg
ZDOT = 5956
344194 TA = 183
51804
MA = 183
52921
Ha = 221
060 n
mi
Hp = 203
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8686119
22 X = 2719316
31
Y = -20446261
33 feet Y = -6202012
72 meter
Z = -1550815
76 Z = -459653
27
XDOT = 15008
472387 XDOT = 4528
618645
YDOT = 4896
454010 feet/sec YDOT = 1543
337242 meter/sec
ZDOT = 19541
811659 ZDOT = 5978
456170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1565382
50 X = -477128
59
Y = -22163297
00 feet Y = -6755372
93 meter
Z = -1497044
58 Z = -456299
19
XDOT = 13870
986534 XDOT = 4227
876695
YDOT = -2303
305431 feet/sec YDOT = -702
047496 meter/sec
ZDOT = 19632
007161 ZDOT = 5983
835783
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 11355
82821525
00016717 00000-0 10270-3 0 9139
2 25544 51
6406 296
8870 0024553 192
0180 168
0392 15
58402336 30205
Satellite: ISS
Catalog Number: 25544
Epoch time: 11355
82821525 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 296
8870 deg
Eccentricity:
0024553
Arg of perigee: 192
0180 deg
Mean anomaly: 168
0392 deg
Mean motion: 15
58402336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 298
Coasting Arc #15 (Orbit 3035)
---------------------------------------
Vector Time (GMT): 2011/356/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4050825
29 A = 6773940
18 meter
Y = 4760334
35 meter E =
0026755
Z = -2567474
69 I = 51
32920
XDOT = -2564
788916 Wp = 185
25122
YDOT = -5001
228994 meter/sec RA = 291
20426 deg
ZDOT = -5248
009152 TA = 23
86949
MA = 23
74566
Ha = 220
663 n
mi
Hp = 203
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13290109
23 X = -4091282
89
Y = 15617894
86 feet Y = 4714809
69 meter
Z = -8423473
38 Z = -2587251
21
XDOT = -8414
661797 XDOT = -2483
179653
YDOT = -16408
231607 feet/sec YDOT = -5029
452986 meter/sec
ZDOT = -17217
877794 ZDOT = -5260
271396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4334762
51 X = -1321235
61
Y = 20009526
49 feet Y = 6098903
67 meter
Z = -8504659
36 Z = -2592220
17
XDOT = -13594
022650 XDOT = -4143
458104
YDOT = -10253
986144 feet/sec YDOT = -3125
414977 meter/sec
ZDOT = -17267
548892 ZDOT = -5263
148902
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 11356
85421020
00016717 00000-0 10270-3 0 9140
2 25544 51
6409 291
7391 0024428 195
6780 164
3622 15
58444257 30366
Satellite: ISS
Catalog Number: 25544
Epoch time: 11356
85421020 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 291
7391 deg
Eccentricity:
0024428
Arg of perigee: 195
6780 deg
Mean anomaly: 164
3622 deg
Mean motion: 15
58444257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3036
Checksum: 310
Coasting Arc #16 (Orbit 3051)
---------------------------------------
Vector Time (GMT): 2011/357/19:51:21
480
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4482135
47 A = 6767234
02 meter
Y = -1911945
47 meter E =
0026747
Z = 4708633
44 I = 51
29647
XDOT = 183
539065 Wp = 182
59602
YDOT = 7167
236128 meter/sec RA = 286
16188 deg
ZDOT = 2709
884727 TA = 240
33102
MA = 240
59761
Ha = 220
531 n
mi
Hp = 203
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14705168
87 X = 4480308
52
Y = -6272786
98 feet Y = -1861834
41 meter
Z = 15448272
44 Z = 4730402
83
XDOT = 602
162286 XDOT = 90
215898
YDOT = 23514
554226 feet/sec YDOT = 7168
766364 meter/sec
ZDOT = 8890
697924 ZDOT = 2710
550766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9727721
45 X = 2965009
50
Y = -12577785
00 feet Y = -3833708
87 meter
Z = 15537365
59 Z = 4735789
03
XDOT = 10980
504641 XDOT = 3346
857815
YDOT = 19581
134172 feet/sec YDOT = 5968
329696 meter/sec
ZDOT = 8892
822704 ZDOT = 2710
532360
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 11357
88018342
00016717 00000-0 10270-3 0 9154
2 25544 51
6405 286
5903 0024522 199
5779 160
4437 15
58461851 30527
Satellite: ISS
Catalog Number: 25544
Epoch time: 11357
88018342 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 286
5903 deg
Eccentricity:
0024522
Arg of perigee: 199
5779 deg
Mean anomaly: 160
4437 deg
Mean motion: 15
58461851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3052
Checksum: 325
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
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