SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/344/01:47:34 973 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 06121
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
355/18:52:39
158 0
6 2
0 2
0
011/17:05:04
185 1
2 -0
0 184
7
000/00:00:08
371 1
4 0
0 168
6
Coasting Arc #1 (Orbit 172)
---------------------------------------
Vector Time (GMT): 2006/354/21:41:06
000
Vector Time (MET): 010/19:53:31
027
Weight (LBS) : 236149
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5018142
22 A = 6707578
73 meter
Y = -3481572
81 meter E =
0024983
Z = 2732371
10 I = 51
37799
XDOT = 1118
419508 Wp = 38
92837
YDOT = 5655
617196 meter/sec RA = 304
30582 deg
ZDOT = 5146
234882 TA = 352
58449
MA = 352
62137
Ha = 183
445 n
mi
Hp = 168
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16463721
19 X = 5043442
61
Y = -11422482
97 feet Y = -3425293
80 meter
Z = 8964472
11 Z = 2756810
00
XDOT = 3669
355340 XDOT = 1030
069693
YDOT = 18555
174529 feet/sec YDOT = 5667
633735 meter/sec
ZDOT = 16883
972710 ZDOT = 5151
454727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 450063
00 X = 137179
20
Y = -19992108
40 feet Y = -6093594
64 meter
Z = 9055497
66 Z = 2760115
69
XDOT = 15637
913870 XDOT = 4766
436147
YDOT = 8017
786281 feet/sec YDOT = 2443
821258 meter/sec
ZDOT = 16904
138507 ZDOT = 5152
381417
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 29647U 06055A 06354
96118119
00014500 00000-0 95600-4 0 9004
2 29647 51
6315 304
5708 0017119 8
1770 351
9673 15
81496875 1739
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06354
96118119 = yrday
fracday
Element set: 900
Inclination: 51
6315 deg
RA of node: 304
5708 deg
Eccentricity:
0017119
Arg of perigee: 8
1770 deg
Mean anomaly: 351
9673 deg
Mean motion: 15
81496875 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 173
Checksum: 320
Coasting Arc #2 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2006/355/18:52:43
344
Vector Time (MET): 011/17:05:08
371
Weight (LBS) : 236094
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4455449
05 A = 6710075
37 meter
Y = -4569388
07 meter E =
0029101
Z = 2009856
37 I = 51
37166
XDOT = 2393
159773 Wp = 35
37912
YDOT = 4791
820562 meter/sec RA = 299
70116 deg
ZDOT = 5572
499567 TA = 347
23397
MA = 347
30751
Ha = 184
733 n
mi
Hp = 168
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14617614
99 X = 4496470
14
Y = -14991430
68 feet Y = -4519315
83 meter
Z = 6594016
96 Z = 2031599
58
XDOT = 7851
574057 XDOT = 2312
307522
YDOT = 15721
196068 feet/sec YDOT = 4818
139525 meter/sec
ZDOT = 18282
478894 ZDOT = 5583
930055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10943275
63 X = 3335510
41
Y = -17821054
01 feet Y = -5431857
26 meter
Z = 6674838
86 Z = 2034490
88
XDOT = 9705
776556 XDOT = 2958
320694
YDOT = 12843
887759 feet/sec YDOT = 3914
816989 meter/sec
ZDOT = 18325
786323 ZDOT = 5585
699671
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 29647U 06055A 06355
84582753
00014500 00000-0 95600-4 0 9012
2 29647 51
6335 299
9800 0018958 11
5381 348
6216 15
81158211 1879
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06355
84582753 = yrday
fracday
Element set: 901
Inclination: 51
6335 deg
RA of node: 299
9800 deg
Eccentricity:
0018958
Arg of perigee: 11
5381 deg
Mean anomaly: 348
6216 deg
Mean motion: 15
81158211 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 187
Checksum: 328
Coasting Arc #3 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2006/356/18:54:58
152
Vector Time (MET): 012/17:07:23
179
Weight (LBS) : 236094
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 279582
24 A = 6708376
09 meter
Y = -6070233
36 meter E =
0022406
Z = -2822216
87 I = 51
35186
XDOT = 5416
807040 Wp = 23
87729
YDOT = -2097
310533 meter/sec RA = 294
43860 deg
ZDOT = 5081
863399 TA = 303
48397
MA = 303
69791
Ha = 184
906 n
mi
Hp = 168
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 917264
56 X = 361176
43
Y = -19915463
77 feet Y = -6066648
75 meter
Z = -9259241
69 Z = -2820661
59
XDOT = 17771
676640 XDOT = 5415
179417
YDOT = -6880
940068 feet/sec YDOT = -2036
722647 meter/sec
ZDOT = 16672
780180 ZDOT = 5108
173678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3946682
33 X = -1202948
77
Y = -19544450
97 feet Y = -5957148
66 meter
Z = -9254121
42 Z = -2820656
21
XDOT = 14025
516793 XDOT = 4274
977518
YDOT = -10719
975702 feet/sec YDOT = -3267
448594 meter/sec
ZDOT = 16770
975084 ZDOT = 5111
793206
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 29647U 06055A 06356
79386316
00014500 00000-0 95600-4 0 9025
2 29647 51
6325 295
0583 0018943 15
3475 344
8263 15
81158818 2024
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06356
79386316 = yrday
fracday
Element set: 902
Inclination: 51
6325 deg
RA of node: 295
0583 deg
Eccentricity:
0018943
Arg of perigee: 15
3475 deg
Mean anomaly: 344
8263 deg
Mean motion: 15
81158818 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 202
Checksum: 326
Coasting Arc #4 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2006/357/18:56:59
577
Vector Time (MET): 013/17:09:24
604
Weight (LBS) : 236094
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3900904
21 A = 6699658
49 meter
Y = -1553986
39 meter E =
0027626
Z = -5238417
76 I = 51
31104
XDOT = 2666
643791 Wp = 50
71156
YDOT = -7218
503917 meter/sec RA = 289
24075 deg
ZDOT = 173
465834 TA = 220
83918
MA = 221
04652
Ha = 184
934 n
mi
Hp = 167
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12798242
14 X = -3857783
28
Y = -5098380
55 feet Y = -1597383
85 meter
Z = -17186409
96 Z = -5257263
63
XDOT = 8748
831335 XDOT = 2746
353349
YDOT = -23682
755633 feet/sec YDOT = -7188
226296 meter/sec
ZDOT = 569
113628 ZDOT = 186
612712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13608310
38 X = -4147813
00
Y = -1472197
90 feet Y = -448725
92 meter
Z = -17257105
65 Z = -5259965
80
XDOT = 1906
120395 XDOT = 580
985496
YDOT = -24173
188654 feet/sec YDOT = -7367
987902 meter/sec
ZDOT = 617
462810 ZDOT = 188
202665
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 29647U 06055A 06357
80507940
00014500 00000-0 95600-4 0 9037
2 29647 51
6315 289
8085 0018905 19
6245 340
5645 15
81204734 2184
Satellite: SHUTTLE
Catalog Number: 29647
Epoch time: 06357
80507940 = yrday
fracday
Element set: 903
Inclination: 51
6315 deg
RA of node: 289
8085 deg
Eccentricity:
0018905
Arg of perigee: 19
6245 deg
Mean anomaly: 340
5645 deg
Mean motion: 15
81204734 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 218
Checksum: 318
SPACE SHUTTLE ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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