SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/252/15:14:54 972 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 16339
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 167)
---------------------------------------
Vector Time (GMT): 2006/263/04:34:05
000
Vector Time (MET): 010/13:19:10
028
Weight (LBS) : 208781
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 892131
76 A = 6718517
66 meter
Y = -5017089
41 meter E =
0018407
Z = -4395627
54 I = 51
89241
XDOT = 5660
131808 Wp = 30
68421
YDOT = 3967
146018 meter/sec RA = 57
50831 deg
ZDOT = -3369
934885 TA = 205
42522
MA = 205
51589
Ha = 190
478 n
mi
Hp = 179
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2926941
47 X = 969579
93
Y = -16460267
08 feet Y = -5006669
10 meter
Z = -14421350
18 Z = -4391105
32
XDOT = 18569
986248 XDOT = 5631
672385
YDOT = 13015
570926 feet/sec YDOT = 4030
348792 meter/sec
ZDOT = -11056
216813 ZDOT = -3342
507369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13933083
20 X = -4246803
76
Y = -9265121
31 feet Y = -2824008
97 meter
Z = -14405187
93 Z = -4390701
28
XDOT = 18642
010747 XDOT = 5682
084876
YDOT = -10956
427887 feet/sec YDOT = -3339
519220 meter/sec
ZDOT = -10953
492430 ZDOT = -3338
624493
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 29391U 06036A 06263
21213075
00014500 00000-0 95600-4 0 9003
2 29391 51
6343 57
9641 0012551 3
8079 356
3178 15
75859728 1686
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06263
21213075 = yrday
fracday
Element set: 900
Inclination: 51
6343 deg
RA of node: 57
9641 deg
Eccentricity:
0012551
Arg of perigee: 3
8079 deg
Mean anomaly: 356
3178 deg
Mean motion: 15
75859728 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 168
Checksum: 307
Coasting Arc #2 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2006/264/04:38:54
662
Vector Time (MET): 011/13:23:59
691
Weight (LBS) : 208781
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4518638
40 A = 6726730
63 meter
Y = -4933638
44 meter E =
0012892
Z = 716088
71 I = 51
90346
XDOT = 3081
215850 Wp = 70
90744
YDOT = -3706
135505 meter/sec RA = 52
32764 deg
ZDOT = -5999
758025 TA = 101
32026
MA = 101
17537
Ha = 190
596 n
mi
Hp = 178
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14824929
15 X = -4466553
19
Y = -16186477
83 feet Y = -4983930
64 meter
Z = 2349372
42 Z = 694263
93
XDOT = 10108
975887 XDOT = 3151
618799
YDOT = -12159
237221 feet/sec YDOT = -3671
249120 meter/sec
ZDOT = -19684
245490 ZDOT = -5984
618343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20439416
34 X = -6229934
10
Y = 8024296
77 feet Y = 2445805
66 meter
Z = 2267390
71 Z = 691100
69
XDOT = -7086
231585 XDOT = -2159
883387
YDOT = -12415
860847 feet/sec YDOT = -3784
354386 meter/sec
ZDOT = -19628
349063 ZDOT = -5982
720795
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 29391U 06036A 06264
22676979
00014500 00000-0 95600-4 0 9012
2 29391 51
6344 52
7377 0012471 7
5128 352
6220 15
75840138 1843
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06264
22676979 = yrday
fracday
Element set: 901
Inclination: 51
6344 deg
RA of node: 52
7377 deg
Eccentricity:
0012471
Arg of perigee: 7
5128 deg
Mean anomaly: 352
6220 deg
Mean motion: 15
75840138 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 184
Checksum: 303
Coasting Arc #3 (Orbit 199)
---------------------------------------
Vector Time (GMT): 2006/265/04:43:28
513
Vector Time (MET): 012/13:28:33
541
Weight (LBS) : 208781
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4257286
53 A = 6715676
94 meter
Y = 1234933
20 meter E =
0016983
Z = 5043309
05 I = 51
84901
XDOT = -3977
820960 Wp = 23
05156
YDOT = -6353
424803 meter/sec RA = 47
16973 deg
ZDOT = -1784
794028 TA = 84
17551
MA = 83
98193
Ha = 190
691 n
mi
Hp = 178
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13967475
48 X = -4295293
01
Y = 4051618
10 feet Y = 1187062
65 meter
Z = 16546289
53 Z = 5022534
71
XDOT = -13050
593700 XDOT = -3897
733991
YDOT = -20844
569565 feet/sec YDOT = -6397
506215 meter/sec
ZDOT = -5855
623451 ZDOT = -1803
923504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -732611
69 X = -223300
04
Y = 14612283
78 feet Y = 4453824
09 meter
Z = 16469065
56 Z = 5019771
18
XDOT = -22876
407143 XDOT = -6972
728897
YDOT = 5598
428033 feet/sec YDOT = 1706
400864 meter/sec
ZDOT = -5927
754121 ZDOT = -1806
779456
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 29391U 06036A 06265
24139054
00014500 00000-0 95600-4 0 9024
2 29391 51
6348 47
5116 0012663 10
4103 349
7320 15
75935782 2006
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06265
24139054 = yrday
fracday
Element set: 902
Inclination: 51
6348 deg
RA of node: 47
5116 deg
Eccentricity:
0012663
Arg of perigee: 10
4103 deg
Mean anomaly: 349
7320 deg
Mean motion: 15
75935782 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 200
Checksum: 278
Coasting Arc #4 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2006/266/04:48:38
170
Vector Time (MET): 013/13:33:43
198
Weight (LBS) : 208781
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1609166
28 A = 6720734
34 meter
Y = 5362286
82 meter E =
0018575
Z = 3695802
23 I = 51
84628
XDOT = -6292
190562 Wp = 53
05017
YDOT = -1097
386879 meter/sec RA = 42
05669 deg
ZDOT = 4327
984739 TA = 351
42513
MA = 351
45682
Ha = 190
787 n
mi
Hp = 178
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5279416
95 X = 1531067
07
Y = 17592804
52 feet Y = 5379863
62 meter
Z = 12125335
39 Z = 3703429
65
XDOT = -20643
669823 XDOT = -6300
462609
YDOT = -3600
350653 feet/sec YDOT = -1167
870699 meter/sec
ZDOT = 14199
424997 ZDOT = 4297
396989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18348534
50 X = 5592633
32
Y = 52209
91 feet Y = 15913
58 meter
Z = 12154477
70 Z = 3704684
80
XDOT = -9388
568869 XDOT = -2861
635791
YDOT = 17480
454528 feet/sec YDOT = 5328
042540 meter/sec
ZDOT = 14085
328547 ZDOT = 4293
208141
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 29391U 06036A 06266
25599269
00014500 00000-0 95600-4 0 9035
2 29391 51
6354 42
2853 0012758 14
7859 345
3675 15
75913782 2161
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06266
25599269 = yrday
fracday
Element set: 903
Inclination: 51
6354 deg
RA of node: 42
2853 deg
Eccentricity:
0012758
Arg of perigee: 14
7859 deg
Mean anomaly: 345
3675 deg
Mean motion: 15
75913782 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 216
Checksum: 334
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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