SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2008/152/21:02:11 970 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 69 ET - UTC (sec) : 65 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 200)
---------------------------------------
Vector Time (GMT): 2008/165/12:39:57
000
Vector Time (MET): 012/15:37:45
030
Weight (LBS) : 211850
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2729824
93 A = 6716755
08 meter
Y = -3155864
07 meter E =
0015510
Z = -5273504
00 I = 51
80652
XDOT = 6126
857106 Wp = 53
34999
YDOT = 4636
891309 meter/sec RA = 34
73318 deg
ZDOT = 406
555540 TA = 220
44718
MA = 220
56258
Ha = 190
212 n
mi
Hp = 181
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8956118
52 X = 2790529
38
Y = -10353884
75 feet Y = -3124997
43 meter
Z = -17301522
32 Z = -5260095
39
XDOT = 20101
237223 XDOT = 6072
576300
YDOT = 15212
897997 feet/sec YDOT = 4705
101776 meter/sec
ZDOT = 1333
843634 ZDOT = 436
188916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10577360
62 X = -3223979
52
Y = -8792568
27 feet Y = -2679974
81 meter
Z = -17250155
02 Z = -5257847
25
XDOT = 14064
032542 XDOT = 4286
717119
YDOT = -19696
484764 feet/sec YDOT = -6003
488556 meter/sec
ZDOT = 1448
299913 ZDOT = 441
441814
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 32960U 08027A 08165
54286862
00020000 00000-0 70000-3 0 9002
2 32960 51
6409 35
1958 0010352 346
4377 13
6507 15
75198694 2013
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08165
54286862 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 35
1958 deg
Eccentricity:
0010352
Arg of perigee: 346
4377 deg
Mean anomaly: 13
6507 deg
Mean motion: 15
75198694 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 201
Checksum: 295
Coasting Arc #2 (Orbit 216)
---------------------------------------
Vector Time (GMT): 2008/166/12:39:57
922
Vector Time (MET): 013/15:37:45
952
Weight (LBS) : 211850
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5482670
15 A = 6728553
42 meter
Y = -3824383
92 meter E =
0005153
Z = -782943
08 I = 51
82137
XDOT = 3311
570069 Wp = 65
86842
YDOT = -3528
624316 meter/sec RA = 29
61308 deg
ZDOT = -5982
439621 TA = 122
64174
MA = 122
59201
Ha = 190
321 n
mi
Hp = 181
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17987762
97 X = -5435694
37
Y = -12547191
35 feet Y = -3885431
50 meter
Z = -2568710
88 Z = -809464
70
XDOT = 10864
731197 XDOT = 3379
843496
YDOT = -11576
851432 feet/sec YDOT = -3491
209728 meter/sec
ZDOT = -19627
426578 ZDOT = -5966
186578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11775913
00 X = -3589298
28
Y = 18487371
53 feet Y = 5634950
84 meter
Z = -2671117
65 Z = -814156
66
XDOT = -10682
660455 XDOT = -3256
074907
YDOT = -9618
290450 feet/sec YDOT = -2931
654929 meter/sec
ZDOT = -19565
133645 ZDOT = -5963
452735
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 32960U 08027A 08166
55793824
00020000 00000-0 70000-3 0 9016
2 32960 51
6409 29
9745 0010268 349
9418 10
1539 15
75175167 2172
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08166
55793824 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 29
9745 deg
Eccentricity:
0010268
Arg of perigee: 349
9418 deg
Mean anomaly: 10
1539 deg
Mean motion: 15
75175167 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 217
Checksum: 308
Coasting Arc #3 (Orbit 232)
---------------------------------------
Vector Time (GMT): 2008/167/12:40:02
705
Vector Time (MET): 014/15:37:50
735
Weight (LBS) : 211850
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3098341
06 A = 6717309
31 meter
Y = 3033301
49 meter E =
0013195
Z = 5131027
94 I = 51
75736
XDOT = -6363
670345 Wp = 10
58084
YDOT = -4107
587703 meter/sec RA = 24
45818 deg
ZDOT = -1401
098273 TA = 92
88589
MA = 92
73487
Ha = 190
468 n
mi
Hp = 181
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10165160
96 X = -3156955
50
Y = 9951776
54 feet Y = 2998325
40 meter
Z = 16834081
18 Z = 5115834
22
XDOT = -20878
183548 XDOT = -6310
459336
YDOT = -13476
337608 feet/sec YDOT = -4178
452133 meter/sec
ZDOT = -4596
779112 ZDOT = -1431
884813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10547827
15 X = 3214977
72
Y = 9647267
11 feet Y = 2940487
01 meter
Z = 16775822
57 Z = 5113270
72
XDOT = -11501
445766 XDOT = -3505
640669
YDOT = 20851
271270 feet/sec YDOT = 6355
467483 meter/sec
ZDOT = -4715
624412 ZDOT = -1437
322321
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 32960U 08027A 08167
57299218
00020000 00000-0 70000-3 0 9028
2 32960 51
6406 24
7514 0010370 353
5070 6
5958 15
75229268 2339
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08167
57299218 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 24
7514 deg
Eccentricity:
0010370
Arg of perigee: 353
5070 deg
Mean anomaly: 6
5958 deg
Mean motion: 15
75229268 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 233
Checksum: 287
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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