Date:
May 26th 2009
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2009/131/18:01:55 956 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
There are no maneuvers
Coasting Arc #1 (Orbit 135)
---------------------------------------
Vector Time (GMT): 2009/140/13:37:48
000
Vector Time (MET): 008/19:35:52
044
Weight (LBS) : 234633
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5914311
30 A = 6813720
11 meter
Y = -771946
92 meter E =
0204425
Z = 3016283
88 I = 28
13035
XDOT = 514
229004 Wp = 51
62881
YDOT = 7702
046410 meter/sec RA = 281
49633 deg
ZDOT = 1090
097222 TA = 21
54086
MA = 20
69288
Ha = 305
261 n
mi
Hp = 159
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19403908
47 X = 5907850
95
Y = -2532634
26 feet Y = -705845
96 meter
Z = 9895944
48 Z = 3045000
38
XDOT = 1687
103030 XDOT = 422
769612
YDOT = 25269
181134 feet/sec YDOT = 7707
285372 meter/sec
ZDOT = 3576
434456 ZDOT = 1092
373731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 174360
96 X = 53145
22
Y = -19510510
64 feet Y = -5946803
64 meter
Z = 10008256
12 Z = 3050516
46
XDOT = 23833
476359 XDOT = 7264
443594
YDOT = 1840
652458 feet/sec YDOT = 561
030869 meter/sec
ZDOT = 3585
783267 ZDOT = 1092
946740
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 34933U 09025A 09140
61984605
00020000 00000-0 70000-3 0 9005
2 34933 28
4699 281
7509 0194182 50
5046 311
2716 15
44381453 1368
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09140
61984605 = yrday
fracday
Element set: 900
Inclination: 28
4699 deg
RA of node: 281
7509 deg
Eccentricity:
0194182
Arg of perigee: 50
5046 deg
Mean anomaly: 311
2716 deg
Mean motion: 15
44381453 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 136
Checksum: 294
Coasting Arc #2 (Orbit 150)
---------------------------------------
Vector Time (GMT): 2009/141/13:42:12
767
Vector Time (MET): 009/19:40:16
810
Weight (LBS) : 234633
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6100459
00 A = 6813196
02 meter
Y = 728659
56 meter E =
0192314
Z = -3220953
38 I = 28
12370
XDOT = -527
539079 Wp = 61
23337
YDOT = -7469
446608 meter/sec RA = 274
41281 deg
ZDOT = -588
298562 TA = 198
83963
MA = 199
56110
Ha = 305
547 n
mi
Hp = 159
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20014629
28 X = -6092506
44
Y = 2390615
35 feet Y = 660485
39 meter
Z = -10567432
34 Z = -3250570
68
XDOT = -1730
771257 XDOT = -441
117348
YDOT = -24506
058424 feet/sec YDOT = -7474
862601 meter/sec
ZDOT = -1930
113394 ZDOT = -590
652090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 334482
16 X = 101950
16
Y = 20092955
11 feet Y = 6124332
72 meter
Z = -10683273
37 Z = -3256261
72
XDOT = -23088
138724 XDOT = -7037
264683
YDOT = -823
560252 feet/sec YDOT = -251
021165 meter/sec
ZDOT = -1939
747969 ZDOT = -591
235181
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 34933U 09025A 09141
58913800
00020000 00000-0 70000-3 0 9012
2 34933 28
4708 274
9858 0194257 61
5337 300
4853 15
44511769 1512
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09141
58913800 = yrday
fracday
Element set: 901
Inclination: 28
4708 deg
RA of node: 274
9858 deg
Eccentricity:
0194257
Arg of perigee: 61
5337 deg
Mean anomaly: 300
4853 deg
Mean motion: 15
44511769 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 151
Checksum: 305
Coasting Arc #3 (Orbit 166)
---------------------------------------
Vector Time (GMT): 2009/142/13:46:10
820
Vector Time (MET): 010/19:44:14
864
Weight (LBS) : 234633
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5869788
08 A = 6813304
25 meter
Y = -489666
03 meter E =
0205436
Z = 3145781
72 I = 28
12128
XDOT = 620
073295 Wp = 73
71207
YDOT = 7776
774611 meter/sec RA = 267
32054 deg
ZDOT = 136
729805 TA = 14
44518
MA = 13
86659
Ha = 305
465 n
mi
Hp = 159
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19257834
90 X = 5859545
34
Y = -1606515
85 feet Y = -424084
25 meter
Z = 10320806
16 Z = 3174272
91
XDOT = 2034
361204 XDOT = 532
401779
YDOT = 25514
352397 feet/sec YDOT = 7783
218420 meter/sec
ZDOT = 448
588600 ZDOT = 139
530079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -297643
86 X = -90721
85
Y = -19262489
77 feet Y = -5871206
88 meter
Z = 10432259
30 Z = 3179752
64
XDOT = 24188
809547 XDOT = 7372
749150
YDOT = -270
938575 feet/sec YDOT = -82
582078 meter/sec
ZDOT = 459
984322 ZDOT = 140
203221
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 34933U 09025A 09142
62303457
00020000 00000-0 70000-3 0 9020
2 34933 28
4701 267
7618 0194176 73
3098 288
8884 15
44398568 1674
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09142
62303457 = yrday
fracday
Element set: 902
Inclination: 28
4701 deg
RA of node: 267
7618 deg
Eccentricity:
0194176
Arg of perigee: 73
3098 deg
Mean anomaly: 288
8884 deg
Mean motion: 15
44398568 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 167
Checksum: 335
Coasting Arc #4 (Orbit 181)
---------------------------------------
Vector Time (GMT): 2009/143/13:50:38
376
Vector Time (MET): 011/19:48:42
420
Weight (LBS) : 234633
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6121394
21 A = 6813061
24 meter
Y = 338299
52 meter E =
0192653
Z = -3255446
48 I = 28
12670
XDOT = -577
618737 Wp = 84
07600
YDOT = -7474
485034 meter/sec RA = 260
23453 deg
ZDOT = 373
403962 TA = 191
75228
MA = 192
20838
Ha = 305
666 n
mi
Hp = 159
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20083314
35 X = -6108907
43
Y = 1109906
57 feet Y = 269916
80 meter
Z = -10680598
68 Z = -3285154
55
XDOT = -1895
074596 XDOT = -495
808826
YDOT = -24522
588693 feet/sec YDOT = -7480
486933 meter/sec
ZDOT = 1225
078614 ZDOT = 370
795492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 482305
94 X = 147006
85
Y = 20046008
30 feet Y = 6110023
33 meter
Z = -10796829
55 Z = -3290873
65
XDOT = -23108
326718 XDOT = -7043
417984
YDOT = 1098
202360 feet/sec YDOT = 334
732079 meter/sec
ZDOT = 1214
455311 ZDOT = 370
165979
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 34933U 09025A 09143
59229056
00020000 00000-0 70000-3 0 9030
2 34933 28
4709 260
9968 0194278 84
3207 277
9682 15
44527969 1823
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09143
59229056 = yrday
fracday
Element set: 903
Inclination: 28
4709 deg
RA of node: 260
9968 deg
Eccentricity:
0194278
Arg of perigee: 84
3207 deg
Mean anomaly: 277
9682 deg
Mean motion: 15
44527969 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 182
Checksum: 344
Coasting Arc #5 (Orbit 197)
---------------------------------------
Vector Time (GMT): 2009/144/13:54:42
762
Vector Time (MET): 012/19:52:46
806
Weight (LBS) : 234633
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5932496
77 A = 6813497
80 meter
Y = -125115
46 meter E =
0206194
Z = 3055629
74 I = 28
13656
XDOT = 637
521996 Wp = 95
75978
YDOT = 7731
300833 meter/sec RA = 253
14447 deg
ZDOT = -872
548169 TA = 8
11436
MA = 7
78589
Ha = 305
481 n
mi
Hp = 159
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19463572
09 X = 5918610
92
Y = -410483
80 feet Y = -58852
98 meter
Z = 10025031
95 Z = 3084416
65
XDOT = 2091
607598 XDOT = 555
260670
YDOT = 25365
160214 feet/sec YDOT = 7737
970178 meter/sec
ZDOT = -2862
690843 ZDOT = -869
649525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -482245
25 X = -146988
35
Y = -19403486
08 feet Y = -5914182
56 meter
Z = 10137680
64 Z = 3089965
06
XDOT = 23942
202405 XDOT = 7297
583293
YDOT = -2166
999600 feet/sec YDOT = -660
501478 meter/sec
ZDOT = -2850
921575 ZDOT = -868
960896
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 34933U 09025A 09144
62614228
00020000 00000-0 70000-3 0 9045
2 34933 28
4699 253
7735 0194205 96
0835 266
2095 15
44416947 1989
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09144
62614228 = yrday
fracday
Element set: 904
Inclination: 28
4699 deg
RA of node: 253
7735 deg
Eccentricity:
0194205
Arg of perigee: 96
0835 deg
Mean anomaly: 266
2095 deg
Mean motion: 15
44416947 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 198
Checksum: 325
Coasting Arc #6 (Orbit 212)
---------------------------------------
Vector Time (GMT): 2009/145/13:58:49
514
Vector Time (MET): 013/19:56:53
557
Weight (LBS) : 234633
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6231846
94 A = 6813457
40 meter
Y = 63917
68 meter E =
0191772
Z = -3062065
62 I = 28
15329
XDOT = -685
135178 Wp = 106
84950
YDOT = -7364
733679 meter/sec RA = 246
06605 deg
ZDOT = 1263
761838 TA = 183
98533
MA = 184
14028
Ha = 305
592 n
mi
Hp = 159
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20445692
05 X = -6217223
34
Y = 209703
66 feet Y = -5688
13 meter
Z = -10046147
05 Z = -3092304
83
XDOT = -2247
818825 XDOT = -608
869774
YDOT = -24162
512070 feet/sec YDOT = -7371
969077 meter/sec
ZDOT = 4146
200256 ZDOT = 1260
617263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1002282
92 X = 305495
83
Y = 20363541
31 feet Y = 6206807
39 meter
Z = -10164496
25 Z = -3098138
46
XDOT = -22570
875630 XDOT = -6879
602892
YDOT = 3136
740647 feet/sec YDOT = 956
078549 meter/sec
ZDOT = 4133
489444 ZDOT = 1259
887583
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 34933U 09025A 09145
59535319
00020000 00000-0 70000-3 0 9056
2 34933 28
4703 247
0080 0194331 107
0805 255
1348 15
44558514 2137
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09145
59535319 = yrday
fracday
Element set: 905
Inclination: 28
4703 deg
RA of node: 247
0080 deg
Eccentricity:
0194331
Arg of perigee: 107
0805 deg
Mean anomaly: 255
1348 deg
Mean motion: 15
44558514 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 213
Checksum: 284
Coasting Arc #7 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2009/146/14:03:02
391
Vector Time (MET): 014/20:01:06
434
Weight (LBS) : 234633
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6075866
80 A = 6814246
11 meter
Y = 112708
43 meter E =
0206609
Z = 2757994
90 I = 28
17456
XDOT = 671
660088 Wp = 117
78190
YDOT = 7572
180314 meter/sec RA = 238
98477 deg
ZDOT = -1781
513125 TA = 1
13874
MA = 1
09240
Ha = 305
325 n
mi
Hp = 159
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19933946
21 X = 6060756
97
Y = 369778
31 feet Y = 180567
30 meter
Z = 9048539
70 Z = 2787475
00
XDOT = 2203
609211 XDOT = 595
591098
YDOT = 24843
111267 feet/sec YDOT = 7579
266228 meter/sec
ZDOT = -5844
859335 ZDOT = -1778
433494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1111756
17 X = -338863
28
Y = -19853492
95 feet Y = -6051344
65 meter
Z = 9163942
07 Z = 2793169
54
XDOT = 23159
649482 XDOT = 7059
061162
YDOT = -4000
363182 feet/sec YDOT = -1219
310698 meter/sec
ZDOT = -5832
388415 ZDOT = -1777
711989
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 34933U 09025A 09146
62915748
00020000 00000-0 70000-3 0 9060
2 34933 28
4694 239
7850 0194256 118
8267 243
2147 15
44427164 2295
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09146
62915748 = yrday
fracday
Element set: 906
Inclination: 28
4694 deg
RA of node: 239
7850 deg
Eccentricity:
0194256
Arg of perigee: 118
8267 deg
Mean anomaly: 243
2147 deg
Mean motion: 15
44427164 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 229
Checksum: 326
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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