[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 25th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 ET - UTC (sec) : 67 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 244)
---------------------------------------
Vector Time (GMT): 2012/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3545759
78 A = 6796692
96 meter
Y = 5781724
02 meter E =
0019295
Z = -136579
81 I = 51
97321
XDOT = -3965
166800 Wp = 348
97303
YDOT = 2577
325479 meter/sec RA = 59
38279 deg
ZDOT = 6041
913804 TA = 9
56239
MA = 9
52572
Ha = 226
848 n
mi
Hp = 218
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11633070
14 X = 3481507
28
Y = 18968910
82 feet Y = 5821015
67 meter
Z = -448096
48 Z = -119510
51
XDOT = -13009
077427 XDOT = -4023
042885
YDOT = 8455
792254 feet/sec YDOT = 2532
660877 meter/sec
ZDOT = 19822
551851 ZDOT = 6022
510408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22244459
63 X = -6780111
30
Y = 624339
39 feet Y = 190298
65 meter
Z = -378028
12 Z = -115222
97
XDOT = -735
840971 XDOT = -224
284328
YDOT = -13976
685607 feet/sec YDOT = -4260
093773 meter/sec
ZDOT = 19741
775315 ZDOT = 6017
293116
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 12326
50022449
00016717 00000-0 10270-3 0 9007
2 25544 51
6488 60
0502 0015905 311
3380 48
6402 15
51599255 2458
Satellite: ISS
Catalog Number: 25544
Epoch time: 12326
50022449 = yrday
fracday
Element set: 900
Inclination: 51
6488 deg
RA of node: 60
0502 deg
Eccentricity:
0015905
Arg of perigee: 311
3380 deg
Mean anomaly: 48
6402 deg
Mean motion: 15
51599255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 245
Checksum: 279
Coasting Arc #2 (Orbit 260)
---------------------------------------
Vector Time (GMT): 2012/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3440522
47 A = 6796309
01 meter
Y = -5815650
68 meter E =
0005605
Z = -744393
94 I = 51
95541
XDOT = 4422
429863 Wp = 304
75046
YDOT = -1847
583839 meter/sec RA = 54
44609 deg
ZDOT = -5970
641311 TA = 243
24207
MA = 243
29944
Ha = 226
964 n
mi
Hp = 218
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11287803
37 X = -3371618
78
Y = -19080218
75 feet Y = -5853739
49 meter
Z = -2442237
33 Z = -760940
73
XDOT = 14509
284329 XDOT = 4471
765698
YDOT = -6061
626767 feet/sec YDOT = -1797
853602 meter/sec
ZDOT = -19588
718212 ZDOT = -5949
037197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22152415
43 X = 6752056
22
Y = -635246
00 feet Y = -193622
98 meter
Z = -2510125
26 Z = -765086
18
XDOT = -1817
174133 XDOT = -553
874676
YDOT = 14121
116736 feet/sec YDOT = 4304
116381 meter/sec
ZDOT = -19498
905086 ZDOT = -5943
266270
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 12327
53071533
00016717 00000-0 10270-3 0 9010
2 25544 51
6481 54
9335 0015835 314
9522 45
0344 15
51643004 2612
Satellite: ISS
Catalog Number: 25544
Epoch time: 12327
53071533 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 54
9335 deg
Eccentricity:
0015835
Arg of perigee: 314
9522 deg
Mean anomaly: 45
0344 deg
Mean motion: 15
51643004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 261
Checksum: 276
Coasting Arc #3 (Orbit 276)
---------------------------------------
Vector Time (GMT): 2012/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3225458
65 A = 6795338
19 meter
Y = 5740803
95 meter E =
0018308
Z = 1628107
64 I = 51
93477
XDOT = -4943
838333 Wp = 6
12233
YDOT = 1149
224854 meter/sec RA = 49
50613 deg
ZDOT = 5753
821855 TA = 11
62765
MA = 11
58543
Ha = 227
198 n
mi
Hp = 218
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10582213
43 X = 3153114
93
Y = 18834658
61 feet Y = 5776468
53 meter
Z = 5341560
51 Z = 1643601
36
XDOT = -16219
942036 XDOT = -4984
273028
YDOT = 3770
422750 feet/sec YDOT = 1093
713646 meter/sec
ZDOT = 18877
368291 ZDOT = 5729
706276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21582463
84 X = -6578334
98
Y = 492175
12 feet Y = 150014
98 meter
Z = 5405080
31 Z = 1647468
48
XDOT = 4359
481825 XDOT = 1328
770060
YDOT = -14624
325920 feet/sec YDOT = -4457
494540 meter/sec
ZDOT = 18777
228877 ZDOT = 5723
299362
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 12328
56118643
00016717 00000-0 10270-3 0 9029
2 25544 51
6489 49
8153 0015910 319
3197 40
6765 15
51671266 2778
Satellite: ISS
Catalog Number: 25544
Epoch time: 12328
56118643 = yrday
fracday
Element set: 902
Inclination: 51
6489 deg
RA of node: 49
8153 deg
Eccentricity:
0015910
Arg of perigee: 319
3197 deg
Mean anomaly: 40
6765 deg
Mean motion: 15
51671266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 277
Checksum: 321
Coasting Arc #4 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2012/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2949014
40 A = 6793814
68 meter
Y = -5609408
36 meter E =
0010692
Z = -2458544
71 I = 51
90865
XDOT = 5452
937114 Wp = 328
29256
YDOT = -513
984076 meter/sec RA = 44
56432 deg
ZDOT = -5348
649072 TA = 239
06573
MA = 239
17086
Ha = 227
387 n
mi
Hp = 218
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9675244
10 X = -2874126
35
Y = -18403570
72 feet Y = -5641967
32 meter
Z = -8066091
58 Z = -2472689
37
XDOT = 17890
213628 XDOT = 5484
262367
YDOT = -1686
299463 feet/sec YDOT = -452
830686 meter/sec
ZDOT = -17548
061261 ZDOT = -5322
082332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20767966
34 X = 6330076
14
Y = -235423
81 feet Y = -71757
18 meter
Z = -8124022
84 Z = -2476202
16
XDOT = -6672
740298 XDOT = -2033
851243
YDOT = 15292
208008 feet/sec YDOT = 4661
065001 meter/sec
ZDOT = -17437
840248 ZDOT = -5315
053708
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 12329
52723606
00016717 00000-0 10270-3 0 9038
2 25544 51
6481 45
0185 0015912 322
9696 37
0356 15
51697767 2926
Satellite: ISS
Catalog Number: 25544
Epoch time: 12329
52723606 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 45
0185 deg
Eccentricity:
0015912
Arg of perigee: 322
9696 deg
Mean anomaly: 37
0356 deg
Mean motion: 15
51697767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 292
Checksum: 318
Coasting Arc #5 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2012/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2530347
03 A = 6791789
34 meter
Y = 5394825
19 meter E =
0014500
Z = 3240002
78 I = 51
88067
XDOT = -5985
690781 Wp = 15
40014
YDOT = -68
396082 meter/sec RA = 39
61731 deg
ZDOT = 4797
238963 TA = 21
98616
MA = 21
92402
Ha = 227
545 n
mi
Hp = 217
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8301663
50 X = 2454093
36
Y = 17699557
70 feet Y = 5422694
65 meter
Z = 10629930
37 Z = 3252110
31
XDOT = -19638
093113 XDOT = -6007
785495
YDOT = -224
396596 feet/sec YDOT = -135
455509 meter/sec
ZDOT = 15738
972976 ZDOT = 4768
106445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19519630
49 X = -5949583
37
Y = -348060
79 feet Y = -106088
93 meter
Z = 10679431
58 Z = 3255090
75
XDOT = 8818
568358 XDOT = 2687
899635
YDOT = -16219
650313 feet/sec YDOT = -4943
749415 meter/sec
ZDOT = 15618
190514 ZDOT = 4760
424469
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 12330
55766953
00016717 00000-0 10270-3 0 9046
2 25544 51
6488 39
9002 0015973 326
9668 33
0484 15
51741053 3087
Satellite: ISS
Catalog Number: 25544
Epoch time: 12330
55766953 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 39
9002 deg
Eccentricity:
0015973
Arg of perigee: 326
9668 deg
Mean anomaly: 33
0484 deg
Mean motion: 15
51741053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 317
Coasting Arc #6 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2012/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2052277
14 A = 6789750
65 meter
Y = -5160641
85 meter E =
0015877
Z = -3917260
06 I = 51
84903
XDOT = 6447
125139 Wp = 354
27356
YDOT = 552
967141 meter/sec RA = 34
66674 deg
ZDOT = -4089
349095 TA = 232
86116
MA = 233
00631
Ha = 227
772 n
mi
Hp = 217
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6733192
72 X = -1975387
65
Y = -16931239
65 feet Y = -5183161
59 meter
Z = -12851903
08 Z = -3927043
63
XDOT = 21151
985364 XDOT = 6460
328143
YDOT = 1814
196656 feet/sec YDOT = 625
136945 meter/sec
ZDOT = -13416
499654 ZDOT = -4057
996466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18158130
69 X = 5534598
23
Y = 1121710
84 feet Y = 341897
47 meter
Z = -12891789
16 Z = -3929417
34
XDOT = -10531
991158 XDOT = -3210
150905
YDOT = 17156
002426 feet/sec YDOT = 5229
149539 meter/sec
ZDOT = -13286
577749 ZDOT = -4049
748898
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 12331
52368563
00016717 00000-0 10270-3 0 9050
2 25544 51
6480 35
1029 0015996 330
9369 29
0891 15
51747377 3233
Satellite: ISS
Catalog Number: 25544
Epoch time: 12331
52368563 = yrday
fracday
Element set: 905
Inclination: 51
6480 deg
RA of node: 35
1029 deg
Eccentricity:
0015996
Arg of perigee: 330
9369 deg
Mean anomaly: 29
0891 deg
Mean motion: 15
51747377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 317
Coasting Arc #7 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2012/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1419070
34 A = 6787523
74 meter
Y = 4878471
86 meter E =
0011278
Z = 4493460
88 I = 51
81692
XDOT = -6876
839235 Wp = 6
86599
YDOT = -982
572535 meter/sec RA = 29
71016 deg
ZDOT = 3248
598342 TA = 50
57352
MA = 50
47375
Ha = 227
924 n
mi
Hp = 217
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4655742
58 X = 1342584
10
Y = 16005485
11 feet Y = 4893912
84 meter
Z = 14742325
72 Z = 4500169
34
XDOT = -22561
808514 XDOT = -6881
122081
YDOT = -3223
663173 feet/sec YDOT = -1059
497808 meter/sec
ZDOT = 10658
131042 ZDOT = 3215
179798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16479364
19 X = -5022910
20
Y = -2341017
63 feet Y = -713542
17 meter
Z = 14769490
60 Z = 4501740
73
XDOT = 11977
990433 XDOT = 3650
891484
YDOT = -18157
229040 feet/sec YDOT = -5534
323411 meter/sec
ZDOT = 10519
702493 ZDOT = 3206
405320
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 12332
55408249
00016717 00000-0 10270-3 0 9061
2 25544 51
6484 29
9846 0016073 334
8964 25
1405 15
51798257 3394
Satellite: ISS
Catalog Number: 25544
Epoch time: 12332
55408249 = yrday
fracday
Element set: 906
Inclination: 51
6484 deg
RA of node: 29
9846 deg
Eccentricity:
0016073
Arg of perigee: 334
8964 deg
Mean anomaly: 25
1405 deg
Mean motion: 15
51798257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 329
Coasting Arc #8 (Orbit 353)
---------------------------------------
Vector Time (GMT): 2012/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -755169
75 A = 6785867
52 meter
Y = -4618599
61 meter E =
0019375
Z = -4925492
91 I = 51
78395
XDOT = 7179
769053 Wp = 17
18244
YDOT = 1306
715372 meter/sec RA = 24
74945 deg
ZDOT = -2310
366415 TA = 230
14102
MA = 230
31160
Ha = 228
123 n
mi
Hp = 216
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2477591
03 X = -679540
09
Y = -15152885
87 feet Y = -4626621
13 meter
Z = -16159753
64 Z = -4928978
22
XDOT = 23555
672746 XDOT = 7175
846913
YDOT = 4287
123923 feet/sec YDOT = 1386
982289 meter/sec
ZDOT = -7579
942307 ZDOT = -2275
496186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14877478
65 X = 4534655
49
Y = 3736561
71 feet Y = 1138904
01 meter
Z = -16173582
81 Z = -4929708
04
XDOT = -12901
647605 XDOT = -3932
422190
YDOT = 18961
561514 feet/sec YDOT = 5779
483950 meter/sec
ZDOT = -7435
539835 ZDOT = -2266
352542
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 12333
52006470
00016717 00000-0 10270-3 0 9070
2 25544 51
6480 25
1866 0016092 338
9048 21
1438 15
51797758 3543
Satellite: ISS
Catalog Number: 25544
Epoch time: 12333
52006470 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 25
1866 deg
Eccentricity:
0016092
Arg of perigee: 338
9048 deg
Mean anomaly: 21
1438 deg
Mean motion: 15
51797758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 354
Checksum: 307
Coasting Arc #9 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2012/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -52153
74 A = 6784474
38 meter
Y = 4345078
93 meter E =
0013225
Z = 5209084
48 I = 51
75158
XDOT = -7390
042075 Wp = 353
53247
YDOT = -1594
758619 meter/sec RA = 19
78349 deg
ZDOT = 1269
391061 TA = 84
37078
MA = 84
21998
Ha = 228
292 n
mi
Hp = 216
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -171108
07 X = -126042
40
Y = 14255508
31 feet Y = 4344082
12 meter
Z = 17090172
17 Z = 5208652
02
XDOT = -24245
544864 XDOT = -7377
826411
YDOT = -5232
147699 feet/sec YDOT = -1677
330499 meter/sec
ZDOT = 4164
668835 ZDOT = 1233
519531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13112030
48 X = -3996546
89
Y = -5604006
34 feet Y = -1708101
13 meter
Z = 17087789
49 Z = 5208358
24
XDOT = 13545
856714 XDOT = 4128
777126
YDOT = -19579
398227 feet/sec YDOT = -5967
800580 meter/sec
ZDOT = 4016
154653 ZDOT = 1224
123938
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 12334
55042564
00016717 00000-0 10270-3 0 9089
2 25544 51
6478 20
0680 0016151 343
0713 16
9898 15
51849926 3705
Satellite: ISS
Catalog Number: 25544
Epoch time: 12334
55042564 = yrday
fracday
Element set: 908
Inclination: 51
6478 deg
RA of node: 20
0680 deg
Eccentricity:
0016151
Arg of perigee: 343
0713 deg
Mean anomaly: 16
9898 deg
Mean motion: 15
51849926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 308
Coasting Arc #10 (Orbit 384)
---------------------------------------
Vector Time (GMT): 2012/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 837454
44 A = 6784003
83 meter
Y = -4127796
81 meter E =
0019582
Z = -5328154
63 I = 51
72127
XDOT = 7439
414478 Wp = 34
23458
YDOT = 1797
770559 meter/sec RA = 14
81453 deg
ZDOT = -208
047467 TA = 233
69120
MA = 233
87218
Ha = 228
450 n
mi
Hp = 216
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2747553
94 X = 909433
38
Y = -13542640
46 feet Y = -4118028
92 meter
Z = -17480822
29 Z = -5323911
82
XDOT = 24407
527816 XDOT = 7419
769172
YDOT = 5898
197373 feet/sec YDOT = 1880
852917 meter/sec
ZDOT = -682
570431 ZDOT = -171
954229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11615071
90 X = 3540273
91
Y = 7528390
94 feet Y = 2294653
56 meter
Z = -17462667
20 Z = -5322620
96
XDOT = -13722
567897 XDOT = -4182
638695
YDOT = 19817
495610 feet/sec YDOT = 6040
372662 meter/sec
ZDOT = -533
165034 ZDOT = -162
508702
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 12335
51637373
00016717 00000-0 10270-3 0 9095
2 25544 51
6482 15
2694 0016195 346
8367 13
2360 15
51850565 3856
Satellite: ISS
Catalog Number: 25544
Epoch time: 12335
51637373 = yrday
fracday
Element set: 909
Inclination: 51
6482 deg
RA of node: 15
2694 deg
Eccentricity:
0016195
Arg of perigee: 346
8367 deg
Mean anomaly: 13
2360 deg
Mean motion: 15
51850565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 385
Checksum: 315
Coasting Arc #11 (Orbit 400)
---------------------------------------
Vector Time (GMT): 2012/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1729835
53 A = 6784125
64 meter
Y = 3919257
14 meter E =
0017871
Z = 5262447
95 I = 51
69172
XDOT = -7341
976135 Wp = 1
01548
YDOT = -2000
303480 meter/sec RA = 9
84227 deg
ZDOT = -906
157018 TA = 97
75300
MA = 97
55005
Ha = 228
598 n
mi
Hp = 215
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5675313
40 X = -1799096
93
Y = 12858455
18 feet Y = 3899525
29 meter
Z = 17265249
19 Z = 5253876
53
XDOT = -24087
848213 XDOT = -7314
660700
YDOT = -6562
675458 feet/sec YDOT = -2082
253233 meter/sec
ZDOT = -2972
956095 ZDOT = -941
758164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10096337
95 X = -3077363
81
Y = -9841617
06 feet Y = -2999724
88 meter
Z = 17229173
37 Z = 5251452
04
XDOT = 13703
368866 XDOT = 4176
786830
YDOT = -19621
298770 feet/sec YDOT = -5980
571865 meter/sec
ZDOT = -3120
293270 ZDOT = -951
065389
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 12336
54669880
00016717 00000-0 10270-3 0 9109
2 25544 51
6474 10
1504 0016223 351
1162 8
9700 15
51908968 4014
Satellite: ISS
Catalog Number: 25544
Epoch time: 12336
54669880 = yrday
fracday
Element set: 910
Inclination: 51
6474 deg
RA of node: 10
1504 deg
Eccentricity:
0016223
Arg of perigee: 351
1162 deg
Mean anomaly: 8
9700 deg
Mean motion: 15
51908968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 401
Checksum: 287
Coasting Arc #12 (Orbit 415)
---------------------------------------
Vector Time (GMT): 2012/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2533947
49 A = 6785145
58 meter
Y = -3781465
51 meter E =
0016903
Z = -5037080
49 I = 51
66590
XDOT = 7083
670856 Wp = 39
46557
YDOT = 2158
469038 meter/sec RA = 4
86954 deg
ZDOT = 1959
438044 TA = 249
47618
MA = 249
65766
Ha = 228
759 n
mi
Hp = 215
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8313476
02 X = 2600513
45
Y = -12406382
91 feet Y = -3752756
72 meter
Z = -16525854
62 Z = -5024609
23
XDOT = 23240
389946 XDOT = 7049
489357
YDOT = 7081
591332 feet/sec YDOT = 2237
491792 meter/sec
ZDOT = 6428
602507 ZDOT = 1993
767567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8976135
06 X = 2735925
96
Y = 12007692
63 feet Y = 3659944
71 meter
Z = -16473627
67 Z = -5021161
71
XDOT = -13399
866437 XDOT = -4084
279290
YDOT = 18957
406697 feet/sec YDOT = 5778
217561 meter/sec
ZDOT = 6570
645133 ZDOT = 2002
732637
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 12337
51261310
00016717 00000-0 10270-3 0 9114
2 25544 51
6484 5
3516 0016308 354
6588 5
4387 15
51904051 4166
Satellite: ISS
Catalog Number: 25544
Epoch time: 12337
51261310 = yrday
fracday
Element set: 911
Inclination: 51
6484 deg
RA of node: 5
3516 deg
Eccentricity:
0016308
Arg of perigee: 354
6588 deg
Mean anomaly: 5
4387 deg
Mean motion: 15
51904051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 416
Checksum: 284
Coasting Arc #13 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2012/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3390363
39 A = 6786711
22 meter
Y = 3654154
13 meter E =
0021139
Z = 4609214
57 I = 51
64009
XDOT = -6645
290707 Wp = 20
20453
YDOT = -2358
230858 meter/sec RA = 359
89560 deg
ZDOT = -2994
921336 TA = 99
81937
MA = 99
58061
Ha = 228
841 n
mi
Hp = 215
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11123239
46 X = -3453363
55
Y = 11988694
67 feet Y = 3615888
40 meter
Z = 15122095
04 Z = 4592591
49
XDOT = -21802
134864 XDOT = -6603
877863
YDOT = -7736
977882 feet/sec YDOT = -2432
310893 meter/sec
ZDOT = -9825
857401 ZDOT = -3027
103575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7914442
31 X = -2412322
02
Y = -14384424
60 feet Y = -4384372
62 meter
Z = 15052672
40 Z = 4588054
55
XDOT = 13057
243483 XDOT = 3979
847814
YDOT = -17686
939219 feet/sec YDOT = -5390
979074 meter/sec
ZDOT = -9958
968569 ZDOT = -3035
493620
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 12338
54290234
00016717 00000-0 10270-3 0 9126
2 25544 51
6472
2320 0016333 358
8630 1
2482 15
51973484 4326
Satellite: ISS
Catalog Number: 25544
Epoch time: 12338
54290234 = yrday
fracday
Element set: 912
Inclination: 51
6472 deg
RA of node:
2320 deg
Eccentricity:
0016333
Arg of perigee: 358
8630 deg
Mean anomaly: 1
2482 deg
Mean motion: 15
51973484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 276
Coasting Arc #14 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2012/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4094389
44 A = 6788744
29 meter
Y = -3586566
98 meter E =
0016025
Z = -4052836
52 I = 51
61755
XDOT = 6082
666473 Wp = 27
11886
YDOT = 2560
380716 meter/sec RA = 354
92369 deg
ZDOT = 3899
229065 TA = 283
25215
MA = 283
43084
Ha = 229
010 n
mi
Hp = 215
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13433036
22 X = 4153878
72
Y = -11766952
03 feet Y = -3540448
11 meter
Z = -13296707
73 Z = -4032801
78
XDOT = 19956
254833 XDOT = 6034
642031
YDOT = 8400
199201 feet/sec YDOT = 2628
132164 meter/sec
ZDOT = 12792
746275 ZDOT = 3928
661989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7272603
75 X = 2216689
62
Y = 16377787
13 feet Y = 4991949
52 meter
Z = -13213151
86 Z = -4027368
69
XDOT = -12681
469696 XDOT = -3865
311963
YDOT = 15996
945009 feet/sec YDOT = 4875
868839 meter/sec
ZDOT = 12914
428990 ZDOT = 3936
317956
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 12339
50878313
00016717 00000-0 10270-3 0 9134
2 25544 51
6484 355
4335 0016394 2
5059 357
6172 15
51968433 4473
Satellite: ISS
Catalog Number: 25544
Epoch time: 12339
50878313 = yrday
fracday
Element set: 913
Inclination: 51
6484 deg
RA of node: 355
4335 deg
Eccentricity:
0016394
Arg of perigee: 2
5059 deg
Mean anomaly: 357
6172 deg
Mean motion: 15
51968433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 321
Coasting Arc #15 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2012/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4789760
38 A = 6790919
84 meter
Y = 3507454
43 meter E =
0021434
Z = 3302289
73 I = 51
59375
XDOT = -5340
534082 Wp = 42
05857
YDOT = -2837
195188 meter/sec RA = 349
95175 deg
ZDOT = -4699
330884 TA = 99
60100
MA = 99
35876
Ha = 229
044 n
mi
Hp = 214
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15714436
93 X = -4844667
34
Y = 11507396
43 feet Y = 3453585
20 meter
Z = 10834283
88 Z = 3278887
95
XDOT = -17521
437276 XDOT = -5285
582648
YDOT = -9308
383164 feet/sec YDOT = -2896
608936 meter/sec
ZDOT = -15417
752244 ZDOT = -4725
141725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6674547
30 X = -2034402
02
Y = -18355307
50 feet Y = -5594697
73 meter
Z = 10736783
17 Z = 3272571
51
XDOT = 12443
137580 XDOT = 3792
668334
YDOT = -13670
059567 feet/sec YDOT = -4166
634156 meter/sec
ZDOT = -15524
377516 ZDOT = -4731
830267
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 12340
53903682
00016717 00000-0 10270-3 0 9148
2 25544 51
6470 350
3135 0016453 6
4274 353
7086 15
52029688 4638
Satellite: ISS
Catalog Number: 25544
Epoch time: 12340
53903682 = yrday
fracday
Element set: 914
Inclination: 51
6470 deg
RA of node: 350
3135 deg
Eccentricity:
0016453
Arg of perigee: 6
4274 deg
Mean anomaly: 353
7086 deg
Mean motion: 15
52029688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 300
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