[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 10th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 247)
---------------------------------------
Vector Time (GMT): 2012/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3735039
42 A = 6764359
09 meter
Y = -2443505
05 meter E =
0021906
Z = 5073075
64 I = 51
27549
XDOT = 2426
174271 Wp = 134
65230
YDOT = 7109
710073 meter/sec RA = 261
10749 deg
ZDOT = 1618
728735 TA = 299
57445
MA = 299
79260
Ha = 219
214 n
mi
Hp = 201
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12254066
32 X = 3737441
91
Y = -8016748
84 feet Y = -2401723
38 meter
Z = 16643948
96 Z = 5091226
34
XDOT = 7959
889341 XDOT = 2338
628379
YDOT = 23325
820449 feet/sec YDOT = 7136
351784 meter/sec
ZDOT = 5310
789813 ZDOT = 1630
301245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13663815
76 X = 4164731
05
Y = -5024233
87 feet Y = -1531386
48 meter
Z = 16718512
29 Z = 5095802
55
XDOT = 2016
650905 XDOT = 614
675196
YDOT = 23524
504790 feet/sec YDOT = 7170
269060 meter/sec
ZDOT = 5357
758406 ZDOT = 1633
044762
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 12069
55090603
00016717 00000-0 10270-3 0 9003
2 25544 51
6370 261
6753 0016965 137
5756 222
6713 15
58906986 2489
Satellite: ISS
Catalog Number: 25544
Epoch time: 12069
55090603 = yrday
fracday
Element set: 900
Inclination: 51
6370 deg
RA of node: 261
6753 deg
Eccentricity:
0016965
Arg of perigee: 137
5756 deg
Mean anomaly: 222
6713 deg
Mean motion: 15
58906986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 248
Checksum: 326
Coasting Arc #2 (Orbit 262)
---------------------------------------
Vector Time (GMT): 2012/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4430050
19 A = 6764706
41 meter
Y = -1354380
24 meter E =
0028203
Z = -4954831
14 I = 51
28273
XDOT = -101
124262 Wp = 126
26570
YDOT = -7362
453617 meter/sec RA = 256
02923 deg
ZDOT = 2094
891534 TA = 164
30978
MA = 164
22220
Ha = 219
105 n
mi
Hp = 201
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14534285
40 X = -4390506
60
Y = -4443504
72 feet Y = -1403699
32 meter
Z = -16256007
69 Z = -4976255
84
XDOT = -331
772514 XDOT = -28
964789
YDOT = -24155
031551 feet/sec YDOT = -7363
180720 meter/sec
ZDOT = 6873
003719 ZDOT = 2094
576481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13165644
98 X = -4012888
59
Y = -7402419
27 feet Y = -2256257
39 meter
Z = -16343743
55 Z = -4981573
04
XDOT = 4213
737043 XDOT = 1284
347051
YDOT = -22725
189007 feet/sec YDOT = -6926
637609 meter/sec
ZDOT = 6872
191730 ZDOT = 2094
644039
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 12070
51243531
00016717 00000-0 10270-3 0 9012
2 25544 51
6365 256
8446 0017000 141
3851 218
8524 15
58992070 2631
Satellite: ISS
Catalog Number: 25544
Epoch time: 12070
51243531 = yrday
fracday
Element set: 901
Inclination: 51
6365 deg
RA of node: 256
8446 deg
Eccentricity:
0017000
Arg of perigee: 141
3851 deg
Mean anomaly: 218
8524 deg
Mean motion: 15
58992070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 263
Checksum: 287
Coasting Arc #3 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2012/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4026234
00 A = 6771440
92 meter
Y = 4592267
86 meter E =
0027571
Z = 2884216
71 I = 51
31481
XDOT = -2428
448686 Wp = 124
83080
YDOT = 5295
385173 meter/sec RA = 250
97656 deg
ZDOT = -5022
782883 TA = 22
00366
MA = 21
88552
Ha = 218
753 n
mi
Hp = 202
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13209429
14 X = 3960572
23
Y = 15066495
61 feet Y = 4636924
86 meter
Z = 9462653
24 Z = 2903615
99
XDOT = -7967
351331 XDOT = -2463
082727
YDOT = 17373
310936 feet/sec YDOT = 5268
034590 meter/sec
ZDOT = -16478
946466 ZDOT = -5034
664842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9960005
87 X = 3035809
79
Y = 17343036
41 feet Y = 5286157
50 meter
Z = 9541880
62 Z = 2908365
21
XDOT = -9840
070667 XDOT = -2999
253539
YDOT = 14777
777223 feet/sec YDOT = 4504
266497 meter/sec
ZDOT = -16527
996855 ZDOT = -5037
733441
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 12071
53803708
00016717 00000-0 10270-3 0 9024
2 25544 51
6371 251
6934 0016753 145
5328 214
6917 15
59051797 2792
Satellite: ISS
Catalog Number: 25544
Epoch time: 12071
53803708 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 251
6934 deg
Eccentricity:
0016753
Arg of perigee: 145
5328 deg
Mean anomaly: 214
6917 deg
Mean motion: 15
59051797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 320
Coasting Arc #4 (Orbit 294)
---------------------------------------
Vector Time (GMT): 2012/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2560978
12 A = 6774916
07 meter
Y = -6270180
70 meter E =
0019090
Z = 269805
08 I = 51
33746
XDOT = 4532
786894 Wp = 108
60802
YDOT = -1578
892217 meter/sec RA = 245
95664 deg
ZDOT = 5977
910163 TA = 254
31393
MA = 254
52462
Ha = 218
783 n
mi
Hp = 202
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8402159
17 X = -2491984
00
Y = -20571458
99 feet Y = -6298433
35 meter
Z = 885187
27 Z = 257532
05
XDOT = 14871
348078 XDOT = 4521
066182
YDOT = -5180
092576 feet/sec YDOT = -1528
268857 meter/sec
ZDOT = 19612
566150 ZDOT = 5999
901870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4607739
67 X = -1404439
05
Y = -21740188
80 feet Y = -6626409
55 meter
Z = 835276
00 Z = 254592
13
XDOT = 13853
319411 XDOT = 4222
491756
YDOT = -2131
840512 feet/sec YDOT = -649
784988 meter/sec
ZDOT = 19702
824268 ZDOT = 6005
420837
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 12072
56360986
00016717 00000-0 10270-3 0 9035
2 25544 51
6368 246
5416 0016928 149
1101 211
1053 15
59087754 2952
Satellite: ISS
Catalog Number: 25544
Epoch time: 12072
56360986 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 246
5416 deg
Eccentricity:
0016928
Arg of perigee: 149
1101 deg
Mean anomaly: 211
1053 deg
Mean motion: 15
59087754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 295
Checksum: 311
Coasting Arc #5 (Orbit 309)
---------------------------------------
Vector Time (GMT): 2012/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 148369
03 A = 6769865
61 meter
Y = 5854137
75 meter E =
0019584
Z = -3392276
45 I = 51
33494
XDOT = -5607
431560 Wp = 139
64374
YDOT = -2507
891520 meter/sec RA = 240
93426 deg
ZDOT = -4602
736639 TA = 80
29462
MA = 80
07347
Ha = 218
546 n
mi
Hp = 202
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 486775
03 X = 99374
71
Y = 19206488
68 feet Y = 5855522
76 meter
Z = -11129515
91 Z = -3391675
03
XDOT = -18397
085170 XDOT = -5556
612072
YDOT = -8227
990551 feet/sec YDOT = -2570
313406 meter/sec
ZDOT = -15100
841993 ZDOT = -4629
853607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2549124
87 X = -776973
26
Y = 19044019
70 feet Y = 5804617
21 meter
Z = -11127423
68 Z = -3391638
74
XDOT = -15350
264823 XDOT = -4678
760718
YDOT = -10886
332504 feet/sec YDOT = -3318
154147 meter/sec
ZDOT = -15211
859095 ZDOT = -4636
574652
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 12073
52505447
00016717 00000-0 10270-3 0 9046
2 25544 51
6373 241
7120 0016799 152
0940 208
1119 15
59145761 3107
Satellite: ISS
Catalog Number: 25544
Epoch time: 12073
52505447 = yrday
fracday
Element set: 904
Inclination: 51
6373 deg
RA of node: 241
7120 deg
Eccentricity:
0016799
Arg of perigee: 152
0940 deg
Mean anomaly: 208
1119 deg
Mean motion: 15
59145761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 310
Checksum: 287
Coasting Arc #6 (Orbit 325)
---------------------------------------
Vector Time (GMT): 2012/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2491845
82 A = 6763430
67 meter
Y = -3634832
10 meter E =
0020825
Z = 5125244
48 I = 51
32863
XDOT = 5126
380736 Wp = 149
67817
YDOT = 5542
105913 meter/sec RA = 235
87639 deg
ZDOT = 1417
859484 TA = 286
53229
MA = 286
76096
Ha = 218
377 n
mi
Hp = 202
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8175347
18 X = 2507408
94
Y = -11925302
15 feet Y = -3606879
47 meter
Z = 16815106
57 Z = 5137387
65
XDOT = 16818
834435 XDOT = 5057
139194
YDOT = 18182
762181 feet/sec YDOT = 5599
045186 meter/sec
ZDOT = 4651
769961 ZDOT = 1442
594571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9708307
52 X = 2959092
13
Y = -10635469
32 feet Y = -3241691
05 meter
Z = 16865126
72 Z = 5140490
62
XDOT = 13216
963485 XDOT = 4028
530470
YDOT = 19706
393179 feet/sec YDOT = 6006
508641 meter/sec
ZDOT = 4752
841808 ZDOT = 1448
666183
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 12074
55056509
00016717 00000-0 10270-3 0 9051
2 25544 51
6366 236
5600 0016737 156
1192 204
0744 15
59163740 3263
Satellite: ISS
Catalog Number: 25544
Epoch time: 12074
55056509 = yrday
fracday
Element set: 905
Inclination: 51
6366 deg
RA of node: 236
5600 deg
Eccentricity:
0016737
Arg of perigee: 156
1192 deg
Mean anomaly: 204
0744 deg
Mean motion: 15
59163740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 326
Checksum: 298
Coasting Arc #7 (Orbit 340)
---------------------------------------
Vector Time (GMT): 2012/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4715660
07 A = 6764422
04 meter
Y = 364726
85 meter E =
0025912
Z = -4858216
64 I = 51
35152
XDOT = -2971
555307 Wp = 138
28353
YDOT = -6647
201029 meter/sec RA = 230
80223 deg
ZDOT = 2373
665078 TA = 155
16115
MA = 155
03620
Ha = 218
241 n
mi
Hp = 202
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15471325
70 X = -4695788
20
Y = 1196610
39 feet Y = 312104
29 meter
Z = -15939030
98 Z = -4881076
59
XDOT = -9749
197200 XDOT = -2908
534708
YDOT = -21808
402326 feet/sec YDOT = -6680
078307 meter/sec
ZDOT = 7787
615085 ZDOT = 2359
382975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15401440
41 X = -4694359
04
Y = -769139
24 feet Y = -234433
64 meter
Z = -16032796
45 Z = -4886796
36
XDOT = -6999
547295 XDOT = -2133
462016
YDOT = -21753
622233 feet/sec YDOT = -6630
504057 meter/sec
ZDOT = 7729
460617 ZDOT = 2355
939596
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 12075
51195035
00016717 00000-0 10270-3 0 9067
2 25544 51
6375 231
7302 0016790 159
6004 200
5825 15
59223781 3418
Satellite: ISS
Catalog Number: 25544
Epoch time: 12075
51195035 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 231
7302 deg
Eccentricity:
0016790
Arg of perigee: 159
6004 deg
Mean anomaly: 200
5825 deg
Mean motion: 15
59223781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 341
Checksum: 289
Coasting Arc #8 (Orbit 356)
---------------------------------------
Vector Time (GMT): 2012/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5588419
74 A = 6771494
18 meter
Y = 2760788
22 meter E =
0026182
Z = 2601499
16 I = 51
39483
XDOT = -342
412872 Wp = 136
70642
YDOT = 5631
410664 meter/sec RA = 225
75575 deg
ZDOT = -5228
256441 TA = 13
76391
MA = 13
69266
Ha = 217
957 n
mi
Hp = 202
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18334710
44 X = 5544495
40
Y = 9057704
14 feet Y = 2823035
95 meter
Z = 8535102
22 Z = 2628540
17
XDOT = -1123
401812 XDOT = -379
961686
YDOT = 18475
756771 feet/sec YDOT = 5627
371317 meter/sec
ZDOT = -17153
072312 ZDOT = -5230
011399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17174171
75 X = 5234687
55
Y = 11015850
31 feet Y = 3357631
18 meter
Z = 8645834
13 Z = 2635250
24
XDOT = -2243
573060 XDOT = -683
841069
YDOT = 16997
941809 feet/sec YDOT = 5180
972663 meter/sec
ZDOT = -17160
612296 ZDOT = -5230
554628
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 12076
53739647
00016717 00000-0 10270-3 0 9074
2 25544 51
6367 226
5776 0016709 163
5677 196
6023 15
59257687 3570
Satellite: ISS
Catalog Number: 25544
Epoch time: 12076
53739647 = yrday
fracday
Element set: 907
Inclination: 51
6367 deg
RA of node: 226
5776 deg
Eccentricity:
0016709
Arg of perigee: 163
5677 deg
Mean anomaly: 196
6023 deg
Mean motion: 15
59257687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 357
Checksum: 358
Coasting Arc #9 (Orbit 372)
---------------------------------------
Vector Time (GMT): 2012/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4731107
36 A = 6774007
58 meter
Y = -4804381
42 meter E =
0016351
Z = 692338
53 I = 51
42743
XDOT = 3859
808747 Wp = 120
16337
YDOT = -2928
488931 meter/sec RA = 220
74327 deg
ZDOT = 5940
932879 TA = 247
34352
MA = 247
51650
Ha = 217
817 n
mi
Hp = 202
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15522005
77 X = -4680395
34
Y = -15762406
23 feet Y = -4857003
98 meter
Z = 2271451
88 Z = 669478
99
XDOT = 12663
414523 XDOT = 3863
409612
YDOT = -9607
903318 feet/sec YDOT = -2885
305549 meter/sec
ZDOT = 19491
249604 ZDOT = 5959
692317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14002695
15 X = -4268021
48
Y = -17138452
37 feet Y = -5223800
28 meter
Z = 2177977
40 Z = 663847
51
XDOT = 12133
869598 XDOT = 3698
403453
YDOT = -7377
733468 feet/sec YDOT = -2248
733161 meter/sec
ZDOT = 19568
366790 ZDOT = 5964
438198
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 12077
56280805
00016717 00000-0 10270-3 0 9086
2 25544 51
6380 221
4254 0016687 167
2426 192
9155 15
59346741 3731
Satellite: ISS
Catalog Number: 25544
Epoch time: 12077
56280805 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 221
4254 deg
Eccentricity:
0016687
Arg of perigee: 167
2426 deg
Mean anomaly: 192
9155 deg
Mean motion: 15
59346741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 373
Checksum: 321
Coasting Arc #10 (Orbit 387)
---------------------------------------
Vector Time (GMT): 2012/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2110818
97 A = 6768119
30 meter
Y = 5211921
85 meter E =
0017147
Z = -3760975
23 I = 51
43179
XDOT = -6393
342324 Wp = 151
04730
YDOT = -445
226803 meter/sec RA = 215
72210 deg
ZDOT = -4227
989063 TA = 74
27348
MA = 74
08442
Ha = 217
576 n
mi
Hp = 203
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6925259
08 X = 2070650
98
Y = 17099481
15 feet Y = 5235301
36 meter
Z = -12339157
59 Z = -3750819
24
XDOT = -20975
532559 XDOT = -6367
350273
YDOT = -1460
717857 feet/sec YDOT = -516
576207 meter/sec
ZDOT = -13871
355194 ZDOT = -4258
983918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5683235
99 X = 1732250
33
Y = 17580420
93 feet Y = 5358512
30 meter
Z = -12297800
92 Z = -3748369
72
XDOT = -19437
882259 XDOT = -5924
666513
YDOT = -3456
002368 feet/sec YDOT = -1053
389522 meter/sec
ZDOT = -13998
467904 ZDOT = -4266
733017
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 12078
52410225
00016717 00000-0 10270-3 0 9095
2 25544 51
6382 216
5948 0016452 170
9313 189
2142 15
59372474 3887
Satellite: ISS
Catalog Number: 25544
Epoch time: 12078
52410225 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 216
5948 deg
Eccentricity:
0016452
Arg of perigee: 170
9313 deg
Mean anomaly: 189
2142 deg
Mean motion: 15
59372474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 388
Checksum: 316
Coasting Arc #11 (Orbit 403)
---------------------------------------
Vector Time (GMT): 2012/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1373780
10 A = 6762129
07 meter
Y = -4043247
64 meter E =
0018352
Z = 5241574
45 I = 51
43860
XDOT = 6864
102159 Wp = 166
75198
YDOT = 3355
253317 meter/sec RA = 210
66451 deg
ZDOT = 771
061104 TA = 275
76557
MA = 275
97478
Ha = 217
253 n
mi
Hp = 203
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4507152
57 X = 1393428
41
Y = -13265248
18 feet Y = -4027774
70 meter
Z = 17196766
55 Z = 5248296
31
XDOT = 22520
020206 XDOT = 6822
327299
YDOT = 11008
048941 feet/sec YDOT = 3431
778466 meter/sec
ZDOT = 2529
728033 ZDOT = 804
304221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5173253
78 X = 1576807
75
Y = -12983128
40 feet Y = -3957257
54 meter
Z = 17224570
70 Z = 5250049
15
XDOT = 20872
830972 XDOT = 6362
038880
YDOT = 11932
391791 feet/sec YDOT = 3636
993018 meter/sec
ZDOT = 2665
908603 ZDOT = 812
568942
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 12079
54944884
00016717 00000-0 10270-3 0 9103
2 25544 51
6389 211
4421 0016298 174
9606 185
1717 15
59447249 4046
Satellite: ISS
Catalog Number: 25544
Epoch time: 12079
54944884 = yrday
fracday
Element set: 910
Inclination: 51
6389 deg
RA of node: 211
4421 deg
Eccentricity:
0016298
Arg of perigee: 174
9606 deg
Mean anomaly: 185
1717 deg
Mean motion: 15
59447249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 404
Checksum: 333
Coasting Arc #12 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2012/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4683633
20 A = 6764868
52 meter
Y = 1783722
21 meter E =
0022103
Z = -4562387
83 I = 51
47556
XDOT = -4901
376621 Wp = 153
45998
YDOT = -5038
883330 meter/sec RA = 205
59860 deg
ZDOT = 3047
952974 TA = 147
17176
MA = 147
03426
Ha = 217
054 n
mi
Hp = 203
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15366250
65 X = -4681068
25
Y = 5852107
00 feet Y = 1731360
67 meter
Z = -14968464
01 Z = -4585134
44
XDOT = -16080
631959 XDOT = -4859
472622
YDOT = -16531
769455 feet/sec YDOT = -5093
458850 meter/sec
ZDOT = 9999
845716 ZDOT = 3024
245047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15504645
96 X = -4725816
09
Y = 5212428
59 feet Y = 1588748
24 meter
Z = -15061881
42 Z = -4590861
46
XDOT = -15061
170224 XDOT = -4590
644684
YDOT = -16056
110746 feet/sec YDOT = -4893
902555 meter/sec
ZDOT = 9902
864739 ZDOT = 3018
393173
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 12080
51068130
00016717 00000-0 10270-3 0 9114
2 25544 51
6394 206
6118 0016225 178
3729 181
7482 15
59477007 4197
Satellite: ISS
Catalog Number: 25544
Epoch time: 12080
51068130 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 206
6118 deg
Eccentricity:
0016225
Arg of perigee: 178
3729 deg
Mean anomaly: 181
7482 deg
Mean motion: 15
59477007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 419
Checksum: 305
Coasting Arc #13 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2012/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6426047
77 A = 6772064
27 meter
Y = 766763
54 meter E =
0024767
Z = 1937596
12 I = 51
52844
XDOT = 1076
450954 Wp = 150
27547
YDOT = 5158
381470 meter/sec RA = 200
56763 deg
ZDOT = -5601
890091 TA = 8
23404
MA = 8
19347
Ha = 216
789 n
mi
Hp = 203
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21082833
88 X = 6407583
73
Y = 2515628
40 feet Y = 838520
61 meter
Z = 6356942
66 Z = 1968768
37
XDOT = 3531
663234 XDOT = 1045
901394
YDOT = 16923
823722 feet/sec YDOT = 5170
247418 meter/sec
ZDOT = -18378
904497 ZDOT = -5596
735705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20976464
35 X = 6393626
33
Y = 3026615
88 feet Y = 922512
52 meter
Z = 6484792
22 Z = 1976564
67
XDOT = 3451
672589 XDOT = 1052
069805
YDOT = 15476
716404 feet/sec YDOT = 4717
303160 meter/sec
ZDOT = -18358
041327 ZDOT = -5595
530996
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 12081
53596290
00016717 00000-0 10270-3 0 9121
2 25544 51
6400 201
4586 0016197 182
0320 178
0772 15
59511415 4355
Satellite: ISS
Catalog Number: 25544
Epoch time: 12081
53596290 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 201
4586 deg
Eccentricity:
0016197
Arg of perigee: 182
0320 deg
Mean anomaly: 178
0772 deg
Mean motion: 15
59511415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 435
Checksum: 290
Coasting Arc #14 (Orbit 450)
---------------------------------------
Vector Time (GMT): 2012/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5938127
72 A = 6772576
06 meter
Y = -2896190
75 meter E =
0014130
Z = 1507548
89 I = 51
56060
XDOT = 3332
776721 Wp = 131
28175
YDOT = -3814
117705 meter/sec RA = 195
56530 deg
ZDOT = 5755
929272 TA = 245
21864
MA = 245
36572
Ha = 216
550 n
mi
Hp = 203
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19482046
33 X = -5912623
90
Y = -9501938
15 feet Y = -2962451
75 meter
Z = 4946026
54 Z = 1478764
20
XDOT = 10934
306827 XDOT = 3347
218348
YDOT = -12513
509532 feet/sec YDOT = -3776
766988 meter/sec
ZDOT = 18884
282388 ZDOT = 5772
155297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19443781
88 X = -5926464
72
Y = -9639974
46 feet Y = -2938264
22 meter
Z = 4828081
93 Z = 1471599
37
XDOT = 10204
971980 XDOT = 3110
475459
YDOT = -11017
459842 feet/sec YDOT = -3358
121760 meter/sec
ZDOT = 18951
066391 ZDOT = 5776
285036
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 12082
56120900
00016717 00000-0 10270-3 0 9137
2 25544 51
6408 196
3055 0015974 185
7606 174
3368 15
59588880 4513
Satellite: ISS
Catalog Number: 25544
Epoch time: 12082
56120900 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 196
3055 deg
Eccentricity:
0015974
Arg of perigee: 185
7606 deg
Mean anomaly: 174
3368 deg
Mean motion: 15
59588880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 451
Checksum: 324
Coasting Arc #15 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2012/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3169321
60 A = 6765412
74 meter
Y = 4098903
36 meter E =
0013757
Z = -4347296
73 I = 51
56667
XDOT = -6688
091607 Wp = 157
07770
YDOT = 1535
294509 meter/sec RA = 190
54387 deg
ZDOT = -3444
339402 TA = 78
06190
MA = 77
90770
Ha = 216
345 n
mi
Hp = 204
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10398036
74 X = 3144369
48
Y = 13447845
67 feet Y = 4134204
58 meter
Z = -14262784
53 Z = -4331961
45
XDOT = -21942
557767 XDOT = -6688
030674
YDOT = 5037
055476 feet/sec YDOT = 1460
504019 meter/sec
ZDOT = -11300
326123 ZDOT = -3476
829907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10619810
00 X = 3236918
09
Y = 13340463
51 feet Y = 4066173
28 meter
Z = -14200084
95 Z = -4328185
89
XDOT = -20848
695096 XDOT = -6354
682265
YDOT = 4482
709921 feet/sec YDOT = 1366
329984 meter/sec
ZDOT = -11433
726819 ZDOT = -3484
999934
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 12083
52234742
00016717 00000-0 10270-3 0 9145
2 25544 51
6410 191
4747 0015909 189
8196 170
2651 15
59616115 4666
Satellite: ISS
Catalog Number: 25544
Epoch time: 12083
52234742 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 191
4747 deg
Eccentricity:
0015909
Arg of perigee: 189
8196 deg
Mean anomaly: 170
2651 deg
Mean motion: 15
59616115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 466
Checksum: 315
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