SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2009/241/03:59:36 958 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 70 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 212)
---------------------------------------
Vector Time (GMT): 2009/254/13:31:04
640
Vector Time (MET): 013/09:31:27
682
Weight (LBS) : 230211
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2936480
31 A = 6703873
00 meter
Y = 3000312
52 meter E =
0041809
Z = -5254286
01 I = 51
39156
XDOT = -5594
881872 Wp = 51
87147
YDOT = -5268
038949 meter/sec RA = 222
41428 deg
ZDOT = 144
833883 TA = 219
35791
MA = 219
66247
Ha = 192
157 n
mi
Hp = 165
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9634121
74 X = -2944287
53
Y = 9843545
00 feet Y = 2967431
45 meter
Z = -17238471
15 Z = -5268570
47
XDOT = -18355
911653 XDOT = -5536
261507
YDOT = -17283
592354 feet/sec YDOT = -5330
276445 meter/sec
ZDOT = 475
176781 ZDOT = 117
796121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7135261
12 X = 2174827
59
Y = -11698926
43 feet Y = -3565832
77 meter
Z = -17294500
19 Z = -5271363
66
XDOT = 20856
907330 XDOT = 6357
185354
YDOT = 12302
625720 feet/sec YDOT = 3749
840319 meter/sec
ZDOT = 368
441959 ZDOT = 112
301109
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 00128U 09254
57890451
00020000 00000-0 20000-3 0 9009
2 00128 51
6384 223
2940 0031593 34
0342 326
2842 15
79716798 2132
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09254
57890451 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 223
2940 deg
Eccentricity:
0031593
Arg of perigee: 34
0342 deg
Mean anomaly: 326
2842 deg
Mean motion: 15
79716798 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 213
Checksum: 273
Coasting Arc #2 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2009/255/13:33:37
613
Vector Time (MET): 014/09:34:00
655
Weight (LBS) : 230211
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3139724
45 A = 6712301
96 meter
Y = 5233820
15 meter E =
0032756
Z = -2844566
00 I = 51
44410
XDOT = -5738
917773 Wp = 46
28924
YDOT = 701
567226 meter/sec RA = 217
23453 deg
ZDOT = -5057
603734 TA = 166
40824
MA = 166
31982
Ha = 192
202 n
mi
Hp = 164
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10300933
24 X = 3094784
04
Y = 17171325
95 feet Y = 5268679
16 meter
Z = -9332565
63 Z = -2829422
28
XDOT = -18828
470383 XDOT = -5721
767314
YDOT = 2301
729744 feet/sec YDOT = 637
487233 meter/sec
ZDOT = -16593
188105 ZDOT = -5085
441784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14282817
65 X = -4353402
82
Y = -14074084
59 feet Y = -4289780
98 meter
Z = -9272632
01 Z = -2826298
24
XDOT = 16552
750920 XDOT = 5045
278480
YDOT = -5824
305173 feet/sec YDOT = -1775
248217 meter/sec
ZDOT = -16702
713037 ZDOT = -5090
986934
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 00128U 09255
59104009
00020000 00000-0 20000-3 0 9010
2 00128 51
6387 218
0512 0031659 37
9791 322
3599 15
79775866 2299
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09255
59104009 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 218
0512 deg
Eccentricity:
0031659
Arg of perigee: 37
9791 deg
Mean anomaly: 322
3599 deg
Mean motion: 15
79775866 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 229
Checksum: 301
Coasting Arc #3 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2009/256/13:35:46
391
Vector Time (MET): 015/09:36:09
433
Weight (LBS) : 230211
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6075099
92 A = 6713102
52 meter
Y = 1523672
39 meter E =
0039853
Z = 2418805
24 I = 51
47211
XDOT = 780
331699 Wp = 60
23172
YDOT = 5499
534035 meter/sec RA = 211
98810 deg
ZDOT = -5339
027771 TA = 92
34837
MA = 91
89202
Ha = 192
200 n
mi
Hp = 164
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19931430
19 X = 6045860
36
Y = 4998925
18 feet Y = 1591444
23 meter
Z = 7935712
74 Z = 2448246
98
XDOT = 2560
143369 XDOT = 744
712918
YDOT = 18043
090666 feet/sec YDOT = 5508
061039 meter/sec
ZDOT = -17516
495313 ZDOT = -5335
323418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20494109
89 X = -6246604
69
Y = 623056
58 feet Y = 189907
64 meter
Z = 8051705
38 Z = 2454159
80
XDOT = -7444
324550 XDOT = -2269
030123
YDOT = -15134
853200 feet/sec YDOT = -4613
103255 meter/sec
ZDOT = -17501
563322 ZDOT = -5334
476501
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 00128U 09256
60315844
00020000 00000-0 20000-3 0 9025
2 00128 51
6389 212
8086 0031614 41
7934 318
5638 15
79799419 2451
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09256
60315844 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 212
8086 deg
Eccentricity:
0031614
Arg of perigee: 41
7934 deg
Mean anomaly: 318
5638 deg
Mean motion: 15
79799419 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 245
Checksum: 298
Coasting Arc #4 (Orbit 260)
---------------------------------------
Vector Time (GMT): 2009/257/13:38:16
134
Vector Time (MET): 016/09:38:39
176
Weight (LBS) : 230211
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2233958
62 A = 6703479
57 meter
Y = -3530668
01 meter E =
0033667
Z = 5221930
26 I = 51
46642
XDOT = 6762
049730 Wp = 47
82398
YDOT = 3727
770588 meter/sec RA = 206
80631 deg
ZDOT = -348
632289 TA = 45
61912
MA = 45
34388
Ha = 192
093 n
mi
Hp = 164
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7329260
57 X = 2247906
11
Y = -11583556
45 feet Y = -3505608
50 meter
Z = 17132317
12 Z = 5232816
68
XDOT = 22185
202526 XDOT = 6721
556166
YDOT = 12230
218466 feet/sec YDOT = 3803
161389 meter/sec
ZDOT = -1143
806723 ZDOT = -315
880898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3419715
08 X = -1042329
16
Y = 13218920
56 feet Y = 4029126
99 meter
Z = 17174947
42 Z = 5234923
97
XDOT = -23875
048247 XDOT = -7277
114706
YDOT = -4757
126257 feet/sec YDOT = -1449
972083 meter/sec
ZDOT = -1014
625736 ZDOT = -309
257924
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 00128U 09257
61525821
00020000 00000-0 20000-3 0 9036
2 00128 51
6389 207
5663 0031466 45
5078 314
8652 15
79853796 2611
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09257
61525821 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 207
5663 deg
Eccentricity:
0031466
Arg of perigee: 45
5078 deg
Mean anomaly: 314
8652 deg
Mean motion: 15
79853796 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 261
Checksum: 299
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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