Date:
November 28th 2009
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2009/320/19:28:09 949 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 36 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
330/09:29:20
327 17
7 0
1 18
2
009/14:01:10
378 4
4 -0
2 191
2
000/00:00:12
757 -0
3 18
2 177
5
330/14:08:52
309 -15
4 -0
1 18
2
009/18:40:42
361 -7
7 0
0 189
8
000/00:00:12
721 5
7 -18
2 179
4
Coasting Arc #1 (Orbit 149)
---------------------------------------
Vector Time (GMT): 2009/330/04:29:51
000
Vector Time (MET): 009/09:01:41
051
Weight (LBS) : 216648
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 12141
98 A = 6715284
60 meter
Y = 4256187
30 meter E =
0018414
Z = -5209243
14 I = 51
54304
XDOT = -7563
019209 Wp = 61
74170
YDOT = -1076
457213 meter/sec RA = 193
41543 deg
ZDOT = -890
962164 TA = 199
71535
MA = 199
78663
Ha = 189
061 n
mi
Hp = 179
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 39835
90 X = -10146
32
Y = 13963869
10 feet Y = 4256198
66 meter
Z = -17090692
71 Z = -5209238
13
XDOT = -24813
055149 XDOT = -7546
091758
YDOT = -3531
683771 feet/sec YDOT = -1160
936677 meter/sec
ZDOT = -2923
104213 ZDOT = -927
662913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10294241
86 X = 3137684
92
Y = -9435415
27 feet Y = -2875914
58 meter
Z = -17090480
61 Z = -5209178
49
XDOT = 13254
833288 XDOT = 4040
073186
YDOT = 20055
296017 feet/sec YDOT = 6112
854226 meter/sec
ZDOT = -3068
084716 ZDOT = -935
152221
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 36094U 09062A 09330
20484076
00020000 00000-0 20000-3 0 9004
2 36094 51
6422 194
3430 0007188 13
4604 346
6751 15
75795618 1502
Satellite: SHUTTLE
Catalog Number: 36094
Epoch time: 09330
20484076 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 194
3430 deg
Eccentricity:
0007188
Arg of perigee: 13
4604 deg
Mean anomaly: 346
6751 deg
Mean motion: 15
75795618 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 150
Checksum: 281
Coasting Arc #2 (Orbit 153)
---------------------------------------
Vector Time (GMT): 2009/330/09:29:26
705
Vector Time (MET): 009/14:01:16
757
Weight (LBS) : 216214
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6516640
02 A = 6727088
10 meter
Y = -1608997
75 meter E =
0023902
Z = 226168
07 I = 51
59276
XDOT = 1359
382625 Wp = 49
68224
YDOT = -4600
890132 meter/sec RA = 192
33857 deg
ZDOT = 6035
729191 TA = 312
78076
MA = 312
98155
Ha = 191
179 n
mi
Hp = 177
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21380052
55 X = -6499262
29
Y = -5278864
00 feet Y = -1681773
51 meter
Z = 742021
22 Z = 194551
77
XDOT = 4459
916748 XDOT = 1381
408505
YDOT = -15094
783899 feet/sec YDOT = -4585
565785 meter/sec
ZDOT = 19802
261124 ZDOT = 6042
386529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21446549
63 X = 6536908
33
Y = -5018799
94 feet Y = -1529730
22 meter
Z = 617093
28 Z = 188090
03
XDOT = 2626
316908 XDOT = 800
501394
YDOT = 13855
427473 feet/sec YDOT = 4223
134294 meter/sec
ZDOT = 19828
343466 ZDOT = 6043
679089
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 36094U 09062A 09330
45850837
00020000 00000-0 20000-3 0 9014
2 36094 51
6460 193
0381 0011284 51
9431 308
2750 15
75789932 1541
Satellite: SHUTTLE
Catalog Number: 36094
Epoch time: 09330
45850837 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 193
0381 deg
Eccentricity:
0011284
Arg of perigee: 51
9431 deg
Mean anomaly: 308
2750 deg
Mean motion: 15
75789932 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 154
Checksum: 290
Coasting Arc #3 (Orbit 156)
---------------------------------------
Vector Time (GMT): 2009/330/14:08:58
670
Vector Time (MET): 009/18:40:48
721
Weight (LBS) : 215826
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5649244
92 A = 6724947
29 meter
Y = -2896467
17 meter E =
0020905
Z = 2178952
92 I = 51
58846
XDOT = 3997
234131 Wp = 47
75418
YDOT = -3644
678062 meter/sec RA = 191
35289 deg
ZDOT = 5498
958175 TA = 336
72119
MA = 336
81573
Ha = 189
838 n
mi
Hp = 179
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18534268
13 X = -5627021
42
Y = -9502845
03 feet Y = -2959516
18 meter
Z = 7148795
68 Z = 2151562
22
XDOT = 13114
285206 XDOT = 4010
978995
YDOT = -11957
605189 feet/sec YDOT = -3599
901981 meter/sec
ZDOT = 18041
201360 ZDOT = 5518
410378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7129619
65 X = 2173108
07
Y = -19609395
44 feet Y = -5976943
73 meter
Z = 7040495
19 Z = 2145942
94
XDOT = 12045
899679 XDOT = 3671
590222
YDOT = 10908
082753 feet/sec YDOT = 3324
783623 meter/sec
ZDOT = 18117
856013 ZDOT = 5522
322513
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 36094U 09062A 09330
64875676
00020000 00000-0 20000-3 0 9024
2 36094 51
6428 192
0558 0009698 12
7489 347
3919 15
75840803 1573
Satellite: SHUTTLE
Catalog Number: 36094
Epoch time: 09330
64875676 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 192
0558 deg
Eccentricity:
0009698
Arg of perigee: 12
7489 deg
Mean anomaly: 347
3919 deg
Mean motion: 15
75840803 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 157
Checksum: 332
Coasting Arc #4 (Orbit 171)
---------------------------------------
Vector Time (GMT): 2009/331/14:13:50
943
Vector Time (MET): 010/18:45:40
994
Weight (LBS) : 215826
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5435769
87 A = 6721931
61 meter
Y = 2088980
68 meter E =
0012054
Z = -3354654
69 I = 51
60797
XDOT = -4475
566980 Wp = 40
34428
YDOT = -4193
919260 meter/sec RA = 186
13678 deg
ZDOT = 4658
766211 TA = 280
09677
MA = 280
23274
Ha = 189
832 n
mi
Hp = 179
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17833890
64 X = -5442428
52
Y = 6853611
15 feet Y = 2028157
60 meter
Z = -11006084
94 Z = -3381078
38
XDOT = -14683
618701 XDOT = -4450
969186
YDOT = -13759
577624 feet/sec YDOT = -4243
830345 meter/sec
ZDOT = 15284
666045 ZDOT = 4637
082968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9640312
69 X = -2938367
31
Y = -16424921
44 feet Y = -5006316
05 meter
Z = -11110349
86 Z = -3386434
64
XDOT = 9987
733622 XDOT = 3044
261208
YDOT = -16102
861849 feet/sec YDOT = -4908
152291 meter/sec
ZDOT = 15198
841182 ZDOT = 4632
606792
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 36094U 09062A 09331
59999235
00020000 00000-0 20000-3 0 9038
2 36094 51
6423 187
1570 0009695 17
0539 343
0949 15
75842736 1728
Satellite: SHUTTLE
Catalog Number: 36094
Epoch time: 09331
59999235 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 187
1570 deg
Eccentricity:
0009695
Arg of perigee: 17
0539 deg
Mean anomaly: 343
0949 deg
Mean motion: 15
75842736 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 172
Checksum: 321
Coasting Arc #5 (Orbit 187)
---------------------------------------
Vector Time (GMT): 2009/332/14:18:40
650
Vector Time (MET): 011/18:50:30
701
Weight (LBS) : 215826
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1501261
51 A = 6715471
47 meter
Y = 4089251
84 meter E =
0020884
Z = -5128228
54 I = 51
61603
XDOT = -7495
832262 Wp = 56
31060
YDOT = 981
178410 meter/sec RA = 181
00657 deg
ZDOT = -1404
693194 TA = 200
17103
MA = 200
25367
Ha = 189
982 n
mi
Hp = 178
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4925398
65 X = 1480335
89
Y = 13416180
58 feet Y = 4105923
11 meter
Z = -16824896
79 Z = -5120985
82
XDOT = -24592
625532 XDOT = -7499
422925
YDOT = 3219
089271 feet/sec YDOT = 897
335590 meter/sec
ZDOT = -4608
573472 ZDOT = -1441
117612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12142903
69 X = -3701157
05
Y = 7600737
52 feet Y = 2316704
80 meter
Z = -16796109
20 Z = -5119454
09
XDOT = -7503
793225 XDOT = -2287
156175
YDOT = -22542
741312 feet/sec YDOT = -6871
027552 meter/sec
ZDOT = -4752
397818 ZDOT = -1448
530855
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 36094U 09062A 09332
61462892
00020000 00000-0 20000-3 0 9047
2 36094 51
6420 181
9326 0009718 21
7396 338
4179 15
75874085 1887
Satellite: SHUTTLE
Catalog Number: 36094
Epoch time: 09332
61462892 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 181
9326 deg
Eccentricity:
0009718
Arg of perigee: 21
7396 deg
Mean anomaly: 338
4179 deg
Mean motion: 15
75874085 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 188
Checksum: 319
Coasting Arc #6 (Orbit 203)
---------------------------------------
Vector Time (GMT): 2009/333/14:23:16
704
Vector Time (MET): 012/18:55:06
755
Weight (LBS) : 215826
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6630464
90 A = 6726195
66 meter
Y = 374114
61 meter E =
0010211
Z = -1081015
48 I = 51
68293
XDOT = -1225
483734 Wp = 82
87298
YDOT = 4772
691101 meter/sec RA = 175
83876 deg
ZDOT = -5911
123491 TA = 108
94330
MA = 108
83260
Ha = 190
021 n
mi
Hp = 178
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21753493
76 X = 6631040
22
Y = 1227410
15 feet Y = 448263
69 meter
Z = -3546638
73 Z = -1048802
31
XDOT = -4020
615926 XDOT = -1250
045704
YDOT = 15658
435370 feet/sec YDOT = 4758
850148 meter/sec
ZDOT = -19393
449775 ZDOT = -5917
136357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3947275
67 X = 1203129
62
Y = 21448229
62 feet Y = 6537420
39 meter
Z = -3419376
23 Z = -1042225
87
XDOT = -14573
752866 XDOT = -4442
079874
YDOT = -388
328303 feet/sec YDOT = -118
362467 meter/sec
ZDOT = -19416
995750 ZDOT = -5918
300305
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 36094U 09062A 09333
62924828
00020000 00000-0 20000-3 0 9052
2 36094 51
6419 176
7070 0009903 24
7333 335
4304 15
75935147 2046
Satellite: SHUTTLE
Catalog Number: 36094
Epoch time: 09333
62924828 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 176
7070 deg
Eccentricity:
0009903
Arg of perigee: 24
7333 deg
Mean anomaly: 335
4304 deg
Mean motion: 15
75935147 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 204
Checksum: 293
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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