Date:
July 16th 2006
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/185/18:37:54 951 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 79 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 22 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 19144
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
196/19:24:12
605 -0
5 -0
6 0
6
011/00:46:17
653 -0
4 0
0 190
7
000/00:00:02
507 -0
0 -0
1 176
7
198/15:17:42
965 -64
7 -101
9 102
0
012/20:39:48
014 29
1 -0
0 188
1
000/00:01:04
028 73
3 3
8 122
5
Coasting Arc #1 (begining on orbit 174)
---------------------------------------
Vector Time (GMT): 2006/196/17:51:01
000
Vector Time (MET): 010/23:13:06
049
Weight (LBS) : 237010
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1186618
23 A = 6715189
34 meter
Y = -4232256
51 meter E =
0024146
Z = -5098146
75 I = 51
81648
XDOT = 6500
185286 Wp = 78
84740
YDOT = 3768
800546 meter/sec RA = 39
85306 deg
ZDOT = -1617
613041 TA = 175
63241
MA = 175
61130
Ha = 190
755 n
mi
Hp = 176
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3893104
42 X = 1258680
08
Y = -13885355
99 feet Y = -4218566
40 meter
Z = -16726203
26 Z = -5092207
80
XDOT = 21326
067212 XDOT = 6465
363269
YDOT = 12364
831188 feet/sec YDOT = 3841
385219 meter/sec
ZDOT = -5307
129400 ZDOT = -1586
119687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1122771
25 X = 342220
68
Y = 14402037
86 feet Y = 4389741
14 meter
Z = -16704668
18 Z = -5091582
86
XDOT = -23280
520640 XDOT = -7095
902691
YDOT = -4197
429831 feet/sec YDOT = -1279
376612 meter/sec
ZDOT = -5189
740401 ZDOT = -1581
832874
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 29251U 06028A 06196
76233979
00014500 00000-0 95600-4 0 9009
2 29251 51
6330 40
2770 0010401 80
7694 279
4646 15
76019667 1758
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06196
76233979 = yrday
fracday
Element set: 900
Inclination: 51
6330 deg
RA of node: 40
2770 deg
Eccentricity:
0010401
Arg of perigee: 80
7694 deg
Mean anomaly: 279
4646 deg
Mean motion: 15
76019667 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 175
Checksum: 304
Coasting Arc #2 (begining on orbit 175)
---------------------------------------
Vector Time (GMT): 2006/196/19:24:13
858
Vector Time (MET): 011/00:46:18
907
Weight (LBS) : 236993
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1896972
98 A = 6714290
66 meter
Y = -3776957
99 meter E =
0025504
Z = -5239086
17 I = 51
81350
XDOT = 6292
855831 Wp = 82
18878
YDOT = 4330
418107 meter/sec RA = 39
51595 deg
ZDOT = -843
453447 TA = 179
78539
MA = 179
78429
Ha = 190
741 n
mi
Hp = 176
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6223664
62 X = 1964569
01
Y = -12391594
46 feet Y = -3755339
37 meter
Z = -17188602
91 Z = -5229707
14
XDOT = 20645
852465 XDOT = 6248
000666
YDOT = 14207
408489 feet/sec YDOT = 4400
625138 meter/sec
ZDOT = -2767
235718 ZDOT = -812
991567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4025439
19 X = 1226953
86
Y = 13313961
72 feet Y = 4058095
53 meter
Z = -17154239
91 Z = -5228612
33
XDOT = -23772
107400 XDOT = -7245
738335
YDOT = 3768
816245 feet/sec YDOT = 1148
735191 meter/sec
ZDOT = -2653
608132 ZDOT = -808
819759
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 29251U 06028A 06196
82574685
00014500 00000-0 95600-4 0 9019
2 29251 51
6335 39
9520 0010790 80
8839 279
3546 15
76120964 1766
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06196
82574685 = yrday
fracday
Element set: 901
Inclination: 51
6335 deg
RA of node: 39
9520 deg
Eccentricity:
0010790
Arg of perigee: 80
8839 deg
Mean anomaly: 279
3546 deg
Mean motion: 15
76120964 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 176
Checksum: 322
Coasting Arc #3 (begining on orbit 191)
---------------------------------------
Vector Time (GMT): 2006/197/19:28:54
266
Vector Time (MET): 012/00:50:59
315
Weight (LBS) : 236993
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4517496
09 A = 6724809
86 meter
Y = -4689806
29 meter E =
0016375
Z = -1680076
97 I = 51
82607
XDOT = 4557
862841 Wp = 107
79926
YDOT = -2351
573465 meter/sec RA = 34
36885 deg
ZDOT = -5741
687834 TA = 90
73016
MA = 90
54253
Ha = 190
740 n
mi
Hp = 176
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14821181
41 X = -4456490
70
Y = -15386503
56 feet Y = -4740044
72 meter
Z = -5512063
54 Z = -1701875
22
XDOT = 14953
618244 XDOT = 4611
743620
YDOT = -7715
136040 feet/sec YDOT = -2300
238868 meter/sec
ZDOT = -18837
558509 ZDOT = -5719
415403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21342544
89 X = 6505207
68
Y = 50524
02 feet Y = 15399
72 meter
Z = -5593565
90 Z = -1704918
89
XDOT = -4907
335146 XDOT = -1495
755753
YDOT = 14633
607447 feet/sec YDOT = 4460
323550 meter/sec
ZDOT = -18755
150636 ZDOT = -5716
569914
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 29251U 06028A 06197
84019681
00014500 00000-0 95600-4 0 9023
2 29251 51
6330 34
7249 0010901 84
8406 275
4002 15
76143028 1928
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06197
84019681 = yrday
fracday
Element set: 902
Inclination: 51
6330 deg
RA of node: 34
7249 deg
Eccentricity:
0010901
Arg of perigee: 84
8406 deg
Mean anomaly: 275
4002 deg
Mean motion: 15
76143028 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 192
Checksum: 278
Coasting Arc #4 (begining on orbit 204)
---------------------------------------
Vector Time (GMT): 2006/198/15:18:14
979
Vector Time (MET): 012/20:40:20
028
Weight (LBS) : 234628
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4145231
59 A = 6669537
56 meter
Y = -4673695
98 meter E =
0085641
Z = -2493194
47 I = 51
79937
XDOT = 5220
194907 Wp = 34
94645
YDOT = -1806
195692 meter/sec RA = 30
12494 deg
ZDOT = -5314
492292 TA = 173
19669
MA = 173
07969
Ha = 188
142 n
mi
Hp = 122
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13599841
18 X = -4080484
31
Y = -15333648
24 feet Y = -4719745
26 meter
Z = -8179771
87 Z = -2513175
31
XDOT = 17126
623711 XDOT = 5265
845129
YDOT = -5925
838885 feet/sec YDOT = -1747
491362 meter/sec
ZDOT = -17435
998334 ZDOT = -5289
022129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8850064
41 X = 2697499
63
Y = 18453301
81 feet Y = 5624566
39 meter
Z = -8254521
71 Z = -2515978
22
XDOT = -16840
273053 XDOT = -5132
915227
YDOT = 349
981952 feet/sec YDOT = 106
674499 meter/sec
ZDOT = -17341
650903 ZDOT = -5285
735195
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 29251U 06028A 06198
66417165
00014500 00000-0 95600-4 0 9034
2 29251 51
6309 30
4710 0086286 31
9088 328
7271 15
95257866 2050
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06198
66417165 = yrday
fracday
Element set: 903
Inclination: 51
6309 deg
RA of node: 30
4710 deg
Eccentricity:
0086286
Arg of perigee: 31
9088 deg
Mean anomaly: 328
7271 deg
Mean motion: 15
95257866 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 205
Checksum: 311
Coasting Arc #5 (begining on orbit 220)
---------------------------------------
Vector Time (GMT): 2006/199/15:22:20
828
Vector Time (MET): 013/20:44:25
877
Weight (LBS) : 234628
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4283136
92 A = 6668367
49 meter
Y = -4384118
75 meter E =
0086316
Z = -2768912
69 I = 51
77185
XDOT = 5337
103140 Wp = 38
35115
YDOT = -1985
192414 meter/sec RA = 24
82111 deg
ZDOT = -5131
593146 TA = 173
25601
MA = 173
13911
Ha = 187
750 n
mi
Hp = 122
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14052286
50 X = -4220282
10
Y = -14383591
71 feet Y = -4431722
58 meter
Z = -9084359
21 Z = -2789568
18
XDOT = 17510
180905 XDOT = 5383
860293
YDOT = -6513
098471 feet/sec YDOT = -1925
172837 meter/sec
ZDOT = -16835
935517 ZDOT = -5105
552365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10154490
87 X = 3095088
82
Y = 17315654
69 feet Y = 5277811
55 meter
Z = -9161575
52 Z = -2792448
22
XDOT = -17386
762818 XDOT = -5299
485307
YDOT = 1372
226089 feet/sec YDOT = 418
254512 meter/sec
ZDOT = -16739
488443 ZDOT = -5102
196077
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 29251U 06028A 06199
66641732
00014500 00000-0 95600-4 0 9045
2 29251 51
6315 25
1581 0085732 35
7063 324
9803 15
95449193 2217
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06199
66641732 = yrday
fracday
Element set: 904
Inclination: 51
6315 deg
RA of node: 25
1581 deg
Eccentricity:
0085732
Arg of perigee: 35
7063 deg
Mean anomaly: 324
9803 deg
Mean motion: 15
95449193 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 221
Checksum: 299
Coasting Arc #6 (begining on orbit 236)
---------------------------------------
Vector Time (GMT): 2006/200/15:25:58
265
Vector Time (MET): 014/20:48:03
313
Weight (LBS) : 234628
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4482161
21 A = 6667372
27 meter
Y = -4054694
73 meter E =
0086730
Z = -2947952
30 I = 51
74379
XDOT = 5343
114614 Wp = 41
85859
YDOT = -2287
754162 meter/sec RA = 19
51490 deg
ZDOT = -4998
287802 TA = 172
07761
MA = 171
93974
Ha = 187
354 n
mi
Hp = 121
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14705253
31 X = -4422110
09
Y = -13302804
25 feet Y = -4104542
53 meter
Z = -9671759
52 Z = -2969581
49
XDOT = 17529
903589 XDOT = 5392
611252
YDOT = -7505
755126 feet/sec YDOT = -2227
651843 meter/sec
ZDOT = -16398
582029 ZDOT = -4972
211278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11580645
71 X = 3529780
81
Y = 16047692
18 feet Y = 4891336
58 meter
Z = -9752549
86 Z = -2972577
20
XDOT = -17621
648796 XDOT = -5371
078553
YDOT = 2851
047679 feet/sec YDOT = 868
999333 meter/sec
ZDOT = -16302
033679 ZDOT = -4968
859865
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 29251U 06028A 06200
66853524
00014500 00000-0 95600-4 0 9053
2 29251 51
6321 19
8444 0085208 39
4964 321
2379 15
95644295 2376
Satellite: SHUTTLE
Catalog Number: 29251
Epoch time: 06200
66853524 = yrday
fracday
Element set: 905
Inclination: 51
6321 deg
RA of node: 19
8444 deg
Eccentricity:
0085208
Arg of perigee: 39
4964 deg
Mean anomaly: 321
2379 deg
Mean motion: 15
95644295 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 237
Checksum: 306
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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