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
253/16:02:45
062 18
1 -23
0 23
0
012/12:03:08
104 3
2 -0
0 192
1
000/00:00:16
208 13
8 0
2 166
0
Coasting Arc #1 (Orbit 196)
---------------------------------------
Vector Time (GMT): 2009/253/13:29:58
400
Vector Time (MET): 012/09:30:21
442
Weight (LBS) : 231344
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5360254
54 A = 6726911
71 meter
Y = -3535809
91 meter E =
0019884
Z = -1971490
48 I = 51
40484
XDOT = 1347
212420 Wp = 21
59280
YDOT = -5137
557464 meter/sec RA = 227
59488 deg
ZDOT = 5587
138931 TA = 316
35062
MA = 316
50772
Ha = 191
987 n
mi
Hp = 179
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17586136
94 X = -5310740
87
Y = -11600426
21 feet Y = -3595474
60 meter
Z = -6468144
61 Z = -1997410
54
XDOT = 4419
988254 XDOT = 1377
419761
YDOT = -16855
503491 feet/sec YDOT = -5122
323183 meter/sec
ZDOT = 18330
508303 ZDOT = 5593
757185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19500693
99 X = 5943811
53
Y = 7888743
88 feet Y = 2404489
14 meter
Z = -6570361
41 Z = -2002646
16
XDOT = -308
320297 XDOT = -93
976026
YDOT = 15953
828365 feet/sec YDOT = 4862
726886 meter/sec
ZDOT = 18356
232073 ZDOT = 5594
979536
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 09253
56641467
00020000 00000-0 20000-3 0 9008
2 00128 51
6380 228
5357 0013656 12
2896 347
8598 15
75235358 1972
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09253
56641467 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 228
5357 deg
Eccentricity:
0013656
Arg of perigee: 12
2896 deg
Mean anomaly: 347
8598 deg
Mean motion: 15
75235358 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 197
Checksum: 302
Coasting Arc #2 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2009/253/16:02:53
166
Vector Time (MET): 012/12:03:16
208
Weight (LBS) : 230821
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1468557
83 A = 6711286
25 meter
Y = 5604356
65 meter E =
0033760
Z = -3432106
81 I = 51
39819
XDOT = -6071
684879 Wp = 35
72142
YDOT = -1197
602857 meter/sec RA = 227
09134 deg
ZDOT = -4549
156411 TA = 184
98474
MA = 185
01844
Ha = 192
063 n
mi
Hp = 166
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4818103
11 X = 1422452
52
Y = 18386996
87 feet Y = 5620521
11 meter
Z = -11260192
95 Z = -3425084
53
XDOT = -19920
225982 XDOT = -6035
742618
YDOT = -3929
143230 feet/sec YDOT = -1265
299083 meter/sec
ZDOT = -14925
053842 ZDOT = -4578
565628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17192446
88 X = -5240257
81
Y = -8145239
13 feet Y = -2482668
89 meter
Z = -11232211
12 Z = -3423577
95
XDOT = 15214
037779 XDOT = 4637
238715
YDOT = -11351
490010 feet/sec YDOT = -3459
934155 meter/sec
ZDOT = -15040
856424 ZDOT = -4584
453038
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 09253
69324889
00020000 00000-0 20000-3 0 9019
2 00128 51
6406 227
8828 0031019 28
2166 332
0673 15
79565420 1998
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09253
69324889 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 227
8828 deg
Eccentricity:
0031019
Arg of perigee: 28
2166 deg
Mean anomaly: 332
0673 deg
Mean motion: 15
79565420 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 199
Checksum: 289
Coasting Arc #3 (Orbit 214)
---------------------------------------
Vector Time (GMT): 2009/254/16:05:23
767
Vector Time (MET): 013/12:05:46
809
Weight (LBS) : 230821
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5638363
32 A = 6715073
07 meter
Y = 3249433
72 meter E =
0035453
Z = 1681532
46 I = 51
43229
XDOT = -1176
247871 Wp = 55
67663
YDOT = 5042
600408 meter/sec RA = 221
84518 deg
ZDOT = -5695
224094 TA = 105
66230
MA = 105
27084
Ha = 192
102 n
mi
Hp = 165
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18498567
33 X = 5593439
90
Y = 10660871
78 feet Y = 3312234
02 meter
Z = 5516838
79 Z = 1708814
71
XDOT = -3859
080943 XDOT = -1204
881134
YDOT = 16543
964594 feet/sec YDOT = 5029
286860 meter/sec
ZDOT = -18685
118418 ZDOT = -5701
007854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19853734
05 X = -6051418
14
Y = 7777013
05 feet Y = 2370433
58 meter
Z = 5624411
34 Z = 1714320
58
XDOT = -10020
188590 XDOT = -3054
153482
YDOT = -11806
111518 feet/sec YDOT = -3598
502791 meter/sec
ZDOT = -18707
565876 ZDOT = -5702
066079
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
70550150
00020000 00000-0 20000-3 0 9025
2 00128 51
6401 222
6409 0030924 32
0998 328
2043 15
79576555 2159
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09254
70550150 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 222
6409 deg
Eccentricity:
0030924
Arg of perigee: 32
0998 deg
Mean anomaly: 328
2043 deg
Mean motion: 15
79576555 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 215
Checksum: 256
Coasting Arc #4 (Orbit 230)
---------------------------------------
Vector Time (GMT): 2009/255/16:08:22
233
Vector Time (MET): 014/12:08:45
275
Weight (LBS) : 230821
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3676832
04 A = 6704636
27 meter
Y = -2324315
57 meter E =
0035068
Z = 5089045
16 I = 51
42117
XDOT = 5366
984204 Wp = 38
13381
YDOT = 5374
834703 meter/sec RA = 216
64521 deg
ZDOT = -1390
465333 TA = 65
36571
MA = 65
00084
Ha = 191
956 n
mi
Hp = 165
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12063097
25 X = 3677827
97
Y = -7625707
24 feet Y = -2283193
57 meter
Z = 16696342
39 Z = 5106909
63
XDOT = 17608
215891 XDOT = 5313
237627
YDOT = 17633
972122 feet/sec YDOT = 5434
550981 meter/sec
ZDOT = -4561
894137 ZDOT = -1364
522967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1081163
54 X = -329538
65
Y = 14147536
12 feet Y = 4312169
01 meter
Z = 16766510
74 Z = 5110432
47
XDOT = -23656
715838 XDOT = -7210
566987
YDOT = 3602
305900 feet/sec YDOT = 1097
982838 meter/sec
ZDOT = -4459
447005 ZDOT = -1359
239447
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
71773271
00020000 00000-0 20000-3 0 9039
2 00128 51
6401 217
3992 0030877 35
6158 324
7060 15
79658887 2318
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09255
71773271 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 217
3992 deg
Eccentricity:
0030877
Arg of perigee: 35
6158 deg
Mean anomaly: 324
7060 deg
Mean motion: 15
79658887 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 231
Checksum: 289
Coasting Arc #5 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2009/256/16:11:22
078
Vector Time (MET): 015/12:11:45
120
Weight (LBS) : 230821
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2446700
75 A = 6710115
23 meter
Y = -4979803
56 meter E =
0038602
Z = 3728049
03 I = 51
46461
XDOT = 6470
933820 Wp = 54
69175
YDOT = 1
874864 meter/sec RA = 211
48041 deg
ZDOT = 4240
805705 TA = 350
78636
MA = 350
85698
Ha = 192
219 n
mi
Hp = 165
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8027233
43 X = -2408944
01
Y = -16337938
19 feet Y = -5006952
91 meter
Z = 12231131
99 Z = 3716254
69
XDOT = 21230
097834 XDOT = 6449
830925
YDOT = 6
151129 feet/sec YDOT = 74
118641 meter/sec
ZDOT = 13913
404545 ZDOT = 4272
190131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18021326
32 X = 5492900
26
Y = 2781693
94 feet Y = 847860
31 meter
Z = 12184386
21 Z = 3713800
92
XDOT = -11975
528537 XDOT = -3650
141098
YDOT = 15976
069683 feet/sec YDOT = 4869
506039 meter/sec
ZDOT = 14036
949256 ZDOT = 4278
462133
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
72994774
00020000 00000-0 20000-3 0 9045
2 00128 51
6405 212
1575 0030948 39
7901 320
5527 15
79634151 2479
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09256
72994774 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 212
1575 deg
Eccentricity:
0030948
Arg of perigee: 39
7901 deg
Mean anomaly: 320
5527 deg
Mean motion: 15
79634151 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 247
Checksum: 286
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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