[list_settings.list_name] Current STS TLEs @ 12:30 UTC
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2011/122/18:34:00 000 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 14 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 0
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
122/19:12:21
438 47
5 207
4 207
4
000/00:38:21
438 -120
9 -0
0 146
0
000/00:02:17
175 -161
7 0
1 123
7
122/21:26:34
569 -20
2 88
2 88
2
000/02:52:34
569 51
3 0
0 173
6
000/00:00:58
980 68
8 0
0 146
1
123/11:41:42
282 -0
8 74
5 74
5
000/17:07:42
282 -50
3 -0
0 189
0
000/00:00:49
879 -55
0 0
1 172
1
123/11:51:25
950 0
6 0
0 1
6
000/17:17:25
950 -1
1 -1
6 188
9
000/00:00:07
054 1
0 0
0 172
1
123/21:30:59
754 0
7 3
0 3
0
001/02:56:59
754 2
1 0
0 189
0
000/00:00:13
117 2
0 -0
0 173
9
124/11:14:37
964 0
6 6
4 6
4
001/16:40:37
964 4
3 -0
0 188
8
000/00:00:10
705 4
7 0
0 177
4
124/12:46:12
427 0
6 8
9 8
9
001/18:12:12
427 5
9 -0
0 189
0
000/00:00:13
843 6
6 0
1 181
6
124/14:03:06
308 1
4 2
6 3
1
001/19:29:06
308 2
2 0
1 188
9
000/00:00:13
604 1
7 1
7 183
1
Coasting Arc #1 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2011/122/18:44:28
240
Vector Time (MET): 000/00:10:28
240
Weight (LBS) : 255984
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 900173
67 A = 6518757
92 meter
Y = 4712876
77 meter E =
0127688
Z = 4363564
61 I = 51
82533
XDOT = -6981
546963 Wp = 351
70314
YDOT = -1555
819453 meter/sec RA = 33
54269 deg
ZDOT = 3257
380929 TA = 67
15132
MA = 65
80796
Ha = 123
894 n
mi
Hp = 31
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2953325
70 X = 826208
70
Y = 15462194
14 feet Y = 4722529
44 meter
Z = 14316156
86 Z = 4367758
14
XDOT = -22905
337806 XDOT = -6979
454645
YDOT = -5104
394530 feet/sec YDOT = -1633
879697 meter/sec
ZDOT = 10686
945306 ZDOT = 3223
469046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7583580
62 X = 2311475
37
Y = -13777185
07 feet Y = -4199286
01 meter
Z = 14332913
31 Z = 4368671
98
XDOT = 13525
175777 XDOT = 4122
473577
YDOT = 17953
923473 feet/sec YDOT = 5472
355875 meter/sec
ZDOT = 10549
787452 ZDOT = 3215
575215
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
SHUTTLE
1 00134U 11122
83109682
00020000 00000-0 20000-3 0 9001
2 00134 51
6445 33
7825 0024382 169
0043 191
1723 16
94748563 24
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11122
83109682 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 33
7825 deg
Eccentricity:
0024382
Arg of perigee: 169
0043 deg
Mean anomaly: 191
1723 deg
Mean motion: 16
94748563 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 247
Coasting Arc #2 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2011/122/19:13:30
025
Vector Time (MET): 000/00:39:30
025
Weight (LBS) : 250774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5621331
55 A = 6633779
26 meter
Y = -3462566
43 meter E =
0039991
Z = 259767
69 I = 51
85631
XDOT = 2316
762305 Wp = 174
17690
YDOT = -4222
826375 meter/sec RA = 33
40248 deg
ZDOT = -6112
997409 TA = 2
95769
MA = 2
93412
Ha = 145
961 n
mi
Hp = 123
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18442688
80 X = -5583456
60
Y = -11360126
10 feet Y = -3525215
81 meter
Z = 852256
19 Z = 232550
73
XDOT = 7600
926199 XDOT = 2393
506922
YDOT = -13854
417240 feet/sec YDOT = -4196
489737 meter/sec
ZDOT = -20055
765778 ZDOT = -6101
556031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9604407
57 X = 2927423
43
Y = 19419473
64 feet Y = 5919055
57 meter
Z = 742276
55 Z = 226245
89
XDOT = -12481
680299 XDOT = -3804
416155
YDOT = 6943
819557 feet/sec YDOT = 2116
476201 meter/sec
ZDOT = -20009
275799 ZDOT = -6098
827264
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
SHUTTLE
1 00134U 11122
83253556
00020000 00000-0 20000-3 0 9012
2 00134 51
6450 33
7951 0031474 190
5074 169
5454 16
09232826 29
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11122
83253556 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 33
7951 deg
Eccentricity:
0031474
Arg of perigee: 190
5074 deg
Mean anomaly: 169
5454 deg
Mean motion: 16
09232826 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 243
Coasting Arc #3 (Orbit 2)
---------------------------------------
Vector Time (GMT): 2011/122/21:27:04
059
Vector Time (MET): 000/02:53:04
059
Weight (LBS) : 248593
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5760847
53 A = 6679989
26 meter
Y = 3285756
00 meter E =
0046820
Z = -471632
46 I = 51
85652
XDOT = -2003
621033 Wp = 351
72056
YDOT = 4389
392891 meter/sec RA = 32
90023 deg
ZDOT = 6078
663759 TA = 3
10461
MA = 3
07565
Ha = 173
560 n
mi
Hp = 146
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18900418
39 X = 5725968
55
Y = 10780039
37 feet Y = 3349982
28 meter
Z = -1547350
58 Z = -443730
44
XDOT = -6573
559821 XDOT = -2082
084714
YDOT = 14400
895311 feet/sec YDOT = 4366
548366 meter/sec
ZDOT = 19943
122568 ZDOT = 6068
739482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19171439
08 X = -5843454
63
Y = -10306659
43 feet Y = -3141469
80 meter
Z = -1434591
54 Z = -437263
50
XDOT = 5581
296321 XDOT = 1701
179119
YDOT = -13165
662917 feet/sec YDOT = -4012
894057 meter/sec
ZDOT = 19902
763513 ZDOT = 6066
362319
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
SHUTTLE
1 00134U 11122
89463217
00020000 00000-0 20000-3 0 9026
2 00134 51
6482 33
4595 0040300 339
6722 20
2845 15
92497564 30
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11122
89463217 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 33
4595 deg
Eccentricity:
0040300
Arg of perigee: 339
6722 deg
Mean anomaly: 20
2845 deg
Mean motion: 15
92497564 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3
Checksum: 248
Coasting Arc #4 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2011/123/11:42:07
221
Vector Time (MET): 000/17:08:07
221
Weight (LBS) : 246764
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6166822
92 A = 6718139
25 meter
Y = -2012746
80 meter E =
0030658
Z = 1672903
54 I = 51
83702
XDOT = 108
919809 Wp = 138
17653
YDOT = -5149
447277 meter/sec RA = 29
76877 deg
ZDOT = -5756
610500 TA = 23
30551
MA = 23
16681
Ha = 189
041 n
mi
Hp = 172
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20232358
68 X = -6151984
47
Y = -6603500
00 feet Y = -2081625
04 meter
Z = 5488528
67 Z = 1642980
57
XDOT = 357
348455 XDOT = 194
458882
YDOT = -16894
512065 feet/sec YDOT = -5147
750825 meter/sec
ZDOT = -18886
517388 ZDOT = -5755
873732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20301833
89 X = -6187998
97
Y = 6488727
29 feet Y = 1977764
08 meter
Z = 5367537
20 Z = 1636025
34
XDOT = -9021
640827 XDOT = -2749
796124
YDOT = -12502
504173 feet/sec YDOT = -3810
763272 meter/sec
ZDOT = -18883
296679 ZDOT = -5755
628828
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
SHUTTLE
1 00134U 11123
52248487
00020000 00000-0 20000-3 0 9038
2 00134 51
6486 30
1552 0018351 155
5751 204
6288 15
78537646 139
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11123
52248487 = yrday
fracday
Element set: 903
Inclination: 51
6486 deg
RA of node: 30
1552 deg
Eccentricity:
0018351
Arg of perigee: 155
5751 deg
Mean anomaly: 204
6288 deg
Mean motion: 15
78537646 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 13
Checksum: 259
Coasting Arc #5 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2011/123/11:51:29
477
Vector Time (MET): 000/17:17:29
477
Weight (LBS) : 246718
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4861474
57 A = 6718028
43 meter
Y = -4302576
10 meter E =
0025858
Z = -1681343
35 I = 51
83369
XDOT = 4369
026050 Wp = 151
43843
YDOT = -2710
914015 meter/sec RA = 29
76497 deg
ZDOT = -5753
692764 TA = 47
15717
MA = 46
94019
Ha = 188
940 n
mi
Hp = 172
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15949719
73 X = -4804833
22
Y = -14116063
33 feet Y = -4356623
31 meter
Z = -5516218
35 Z = -1704823
36
XDOT = 14334
074966 XDOT = 4426
966179
YDOT = -8894
074851 feet/sec YDOT = -2661
732782 meter/sec
ZDOT = -18876
944764 ZDOT = -5732
327005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21235925
31 X = -6472710
03
Y = -1279558
38 feet Y = -390009
39 meter
Z = -5611031
55 Z = -1710242
42
XDOT = 5780
927596 XDOT = 1762
026731
YDOT = -14367
639260 feet/sec YDOT = -4379
256447 meter/sec
ZDOT = -18790
360953 ZDOT = -5727
302018
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
SHUTTLE
1 00134U 11123
52248435
00020000 00000-0 20000-3 0 9042
2 00134 51
6456 30
1535 0018324 155
8859 204
3169 15
78533565 130
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11123
52248435 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 30
1535 deg
Eccentricity:
0018324
Arg of perigee: 155
8859 deg
Mean anomaly: 204
3169 deg
Mean motion: 15
78533565 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 13
Checksum: 254
Coasting Arc #6 (Orbit 18)
---------------------------------------
Vector Time (GMT): 2011/123/21:31:06
313
Vector Time (MET): 001/02:57:06
313
Weight (LBS) : 246632
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6057063
25 A = 6717371
82 meter
Y = 633007
93 meter E =
0016376
Z = -2860382
08 I = 51
81441
XDOT = 1828
229493 Wp = 142
57521
YDOT = 5472
384299 meter/sec RA = 27
64550 deg
ZDOT = 5084
877718 TA = 184
68241
MA = 184
69775
Ha = 189
021 n
mi
Hp = 173
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19872254
76 X = 6063430
11
Y = 2076797
67 feet Y = 700777
39 meter
Z = -9384455
66 Z = -2830940
87
XDOT = 5998
128258 XDOT = 1742
198522
YDOT = 17954
016730 feet/sec YDOT = 5492
347452 meter/sec
ZDOT = 16682
669677 ZDOT = 5093
550646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20016514
69 X = -6101033
68
Y = -883190
33 feet Y = -269196
41 meter
Z = -9265350
53 Z = -2824078
84
XDOT = -7023
692810 XDOT = -2140
821568
YDOT = -16111
057867 feet/sec YDOT = -4910
650438 meter/sec
ZDOT = 16717
506948 ZDOT = 5095
496118
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
SHUTTLE
1 00134U 11123
90231858
00020000 00000-0 20000-3 0 9056
2 00134 51
6449 28
1860 0016335 159
3988 200
7839 15
77987113 193
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11123
90231858 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 28
1860 deg
Eccentricity:
0016335
Arg of perigee: 159
3988 deg
Mean anomaly: 200
7839 deg
Mean motion: 15
77987113 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 19
Checksum: 281
Coasting Arc #7 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2011/124/11:14:43
316
Vector Time (MET): 001/16:40:43
316
Weight (LBS) : 246476
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6324461
44 A = 6722583
03 meter
Y = 1237840
40 meter E =
0009157
Z = -1930692
50 I = 51
80521
XDOT = 697
125852 Wp = 120
91255
YDOT = 5197
469503 meter/sec RA = 24
70755 deg
ZDOT = 5630
919010 TA = 217
66978
MA = 217
73395
Ha = 188
821 n
mi
Hp = 177
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20749545
40 X = 6319528
72
Y = 4061156
16 feet Y = 1308536
88 meter
Z = -6334292
99 Z = -1899979
68
XDOT = 2287
158308 XDOT = 611
600503
YDOT = 17052
065299 feet/sec YDOT = 5204
786709 meter/sec
ZDOT = 18474
143735 ZDOT = 5634
098218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20045788
51 X = 6109956
34
Y = -6838220
30 feet Y = -2084289
55 meter
Z = -6210072
27 Z = -1892830
03
XDOT = 9886
351203 XDOT = 3013
359847
YDOT = 12238
219613 feet/sec YDOT = 3730
209338 meter/sec
ZDOT = 18486
758681 ZDOT = 5634
764046
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
SHUTTLE
1 00134U 11124
47227098
00020000 00000-0 20000-3 0 9061
2 00134 51
6450 25
2461 0010839 161
8619 198
2935 15
76823011 285
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11124
47227098 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 25
2461 deg
Eccentricity:
0010839
Arg of perigee: 161
8619 deg
Mean anomaly: 198
2935 deg
Mean motion: 15
76823011 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 28
Checksum: 258
Coasting Arc #8 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2011/124/12:46:19
349
Vector Time (MET): 001/18:12:19
349
Weight (LBS) : 246260
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6344450
58 A = 6727462
34 meter
Y = 1307397
65 meter E =
0005936
Z = -1815287
89 I = 51
80524
XDOT = 557
529601 Wp = 67
67302
YDOT = 5161
798381 meter/sec RA = 24
38120 deg
ZDOT = 5683
095392 TA = 272
24623
MA = 272
31419
Ha = 189
024 n
mi
Hp = 181
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20815126
56 X = 6338177
95
Y = 4289362
38 feet Y = 1378310
17 meter
Z = -5955668
94 Z = -1784481
22
XDOT = 1829
165357 XDOT = 472
160044
YDOT = 16935
034060 feet/sec YDOT = 5167
555399 meter/sec
ZDOT = 18645
326090 ZDOT = 5685
596812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16009645
97 X = 4879740
09
Y = -14029538
57 feet Y = -4276203
36 meter
Z = -5831071
92 Z = -1777310
72
XDOT = 13513
394133 XDOT = 4118
882532
YDOT = 7690
589984 feet/sec YDOT = 2344
091827 meter/sec
ZDOT = 18655
199569 ZDOT = 5686
104829
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
SHUTTLE
1 00134U 11124
53564505
00020000 00000-0 20000-3 0 9076
2 00134 51
6462 24
9194 0003776 166
1525 193
9743 15
75171615 298
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11124
53564505 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 24
9194 deg
Eccentricity:
0003776
Arg of perigee: 166
1525 deg
Mean anomaly: 193
9743 deg
Mean motion: 15
75171615 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 266
Coasting Arc #9 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2011/124/14:03:13
110
Vector Time (MET): 001/19:29:13
110
Weight (LBS) : 246171
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3042297
57 A = 6718788
86 meter
Y = -3082194
39 meter E =
0013681
Z = -5148679
98 I = 51
76909
XDOT = 6401
864053 Wp = 111
41580
YDOT = 4040
713245 meter/sec RA = 24
11190 deg
ZDOT = 1361
860033 TA = 171
62154
MA = 171
59868
Ha = 188
896 n
mi
Hp = 183
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9981291
25 X = 3101548
91
Y = -10112186
32 feet Y = -3047842
01 meter
Z = -16891994
69 Z = -5133756
50
XDOT = 21003
490986 XDOT = 6349
588440
YDOT = 13256
933219 feet/sec YDOT = 4112
010414 meter/sec
ZDOT = 4468
044728 ZDOT = 1392
834027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6531057
21 X = -1990666
24
Y = -12699184
65 feet Y = -3870711
48 meter
Z = -16831457
83 Z = -5130228
35
XDOT = 18128
454234 XDOT = 5525
552850
YDOT = -15419
824387 feet/sec YDOT = -4699
962473 meter/sec
ZDOT = 4593
186872 ZDOT = 1400
003359
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
SHUTTLE
1 00134U 11124
59908594
00020000 00000-0 20000-3 0 9083
2 00134 51
6455 24
5929 0002712 203
7620 156
3419 15
74688844 306
Satellite: SHUTTLE
Catalog Number: 00134
Epoch time: 11124
59908594 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 24
5929 deg
Eccentricity:
0002712
Arg of perigee: 203
7620 deg
Mean anomaly: 156
3419 deg
Mean motion: 15
74688844 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 30
Checksum: 271
SPACE SHUTTLE 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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