Date:
February 21st 2008
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2008/038/19:45:29 952 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 65 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 31789
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 169)
---------------------------------------
Vector Time (GMT): 2008/049/11:11:28
000
Vector Time (MET): 010/15:25:58
048
Weight (LBS) : 215846
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157881
54 A = 6709633
99 meter
Y = 1400275
00 meter E =
0023836
Z = -5097069
08 I = 51
29713
XDOT = -774
853244 Wp = 63
62081
YDOT = -7516
204362 meter/sec RA = 272
82048 deg
ZDOT = -1427
502225 TA = 192
58814
MA = 192
64778
Ha = 187
700 n
mi
Hp = 174
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13641343
65 X = -4148439
37
Y = 4594078
09 feet Y = 1353928
00 meter
Z = -16722667
60 Z = -5117244
58
XDOT = -2542
169436 XDOT = -683
988386
YDOT = -24659
463129 feet/sec YDOT = -7524
344329 meter/sec
ZDOT = -4683
406249 ZDOT = -1431
045238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12818580
08 X = -3907103
21
Y = -6347668
16 feet Y = -1934769
25 meter
Z = -16799718
31 Z = -5120554
14
XDOT = 15221
396978 XDOT = 4639
481799
YDOT = -18259
534266 feet/sec YDOT = -5565
506044 meter/sec
ZDOT = -4697
780279 ZDOT = -1431
883429
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 32486U 08005A 08049
48457895
00014500 00000-0 95600-3 0 9002
2 32486 51
6397 273
4460 0010986 44
0040 316
1998 15
77928038 1703
Satellite: SHUTTLE
Catalog Number: 32486
Epoch time: 08049
48457895 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 273
4460 deg
Eccentricity:
0010986
Arg of perigee: 44
0040 deg
Mean anomaly: 316
1998 deg
Mean motion: 15
77928038 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 170
Checksum: 326
Coasting Arc #2 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2008/050/11:14:41
147
Vector Time (MET): 011/15:29:11
195
Weight (LBS) : 215846
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -708311
86 A = 6720465
03 meter
Y = 6571847
96 meter E =
0013618
Z = -1225449
77 I = 51
33287
XDOT = -4749
048566 Wp = 90
28507
YDOT = -1591
700909 meter/sec RA = 267
61993 deg
ZDOT = -5847
031843 TA = 103
21629
MA = 103
06434
Ha = 187
756 n
mi
Hp = 174
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2323857
79 X = -775641
67
Y = 21561180
97 feet Y = 6563567
85 meter
Z = -4020504
51 Z = -1229054
71
XDOT = -15580
868000 XDOT = -4702
532194
YDOT = -5222
115844 feet/sec YDOT = -1644
438319 meter/sec
ZDOT = -19183
175338 ZDOT = -5869
988844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16458124
06 X = -5016436
21
Y = 14117709
96 feet Y = 4303078
00 meter
Z = -4033573
39 Z = -1229433
17
XDOT = -6652
762756 XDOT = -2027
762088
YDOT = -13209
297253 feet/sec YDOT = -4026
193803 meter/sec
ZDOT = -19271
203195 ZDOT = -5873
862734
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 32486U 08005A 08050
49789132
00014500 00000-0 95600-3 0 9018
2 32486 51
6392 268
2119 0010825 48
1960 312
0128 15
77896917 1866
Satellite: SHUTTLE
Catalog Number: 32486
Epoch time: 08050
49789132 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 268
2119 deg
Eccentricity:
0010825
Arg of perigee: 48
1960 deg
Mean anomaly: 312
0128 deg
Mean motion: 15
77896917 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 186
Checksum: 315
Coasting Arc #3 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2008/051/11:18:11
313
Vector Time (MET): 012/15:32:41
362
Weight (LBS) : 215846
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3691195
22 A = 6714108
62 meter
Y = 4017304
46 meter E =
0021357
Z = 3903749
95 I = 51
31452
XDOT = -2413
643252 Wp = 65
05256
YDOT = 6133
162659 meter/sec RA = 262
37968 deg
ZDOT = -4003
363191 TA = 66
74660
MA = 66
52189
Ha = 187
626 n
mi
Hp = 174
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12110220
55 X = 3627129
73
Y = 13180132
75 feet Y = 4058138
91 meter
Z = 12807578
59 Z = 3921525
16
XDOT = -7918
777074 XDOT = -2462
457302
YDOT = 20121
924733 feet/sec YDOT = 6105
955068 meter/sec
ZDOT = -13134
393671 ZDOT = -4015
207532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 306436
95 X = 93401
98
Y = 17847148
08 feet Y = 5439810
73 meter
Z = 12876055
78 Z = 3924621
80
XDOT = -17893
240092 XDOT = -5453
859580
YDOT = 9876
581955 feet/sec YDOT = 3010
382180 meter/sec
ZDOT = -13179
031714 ZDOT = -4016
968867
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 32486U 08005A 08051
51119057
00014500 00000-0 95600-3 0 9026
2 32486 51
6388 262
9766 0010969 50
4603 309
7530 15
78002475 2027
Satellite: SHUTTLE
Catalog Number: 32486
Epoch time: 08051
51119057 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 262
9766 deg
Eccentricity:
0010969
Arg of perigee: 50
4603 deg
Mean anomaly: 309
7530 deg
Mean motion: 15
78002475 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 202
Checksum: 294
Coasting Arc #4 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2008/052/11:22:07
342
Vector Time (MET): 013/15:36:37
390
Weight (LBS) : 215846
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3411375
27 A = 6710058
76 meter
Y = -2935886
46 meter E =
0013990
Z = 4964141
50 I = 51
30442
XDOT = 3100
971996 Wp = 77
34965
YDOT = 6809
083985 meter/sec RA = 257
21748 deg
ZDOT = 1894
578514 TA = 354
31089
MA = 354
32677
Ha = 187
703 n
mi
Hp = 174
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11192176
07 X = 3419769
87
Y = -9632173
44 feet Y = -2897770
10 meter
Z = 16286553
47 Z = 4980734
26
XDOT = 10173
792639 XDOT = 3015
556669
YDOT = 22339
514388 feet/sec YDOT = 6843
212600 meter/sec
ZDOT = 6215
808773 ZDOT = 1909
434231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14691284
06 X = 4477903
38
Y = -384996
55 feet Y = -117346
95 meter
Z = 16349720
02 Z = 4983394
66
XDOT = -6394
075603 XDOT = -1948
914244
YDOT = 22620
765210 feet/sec YDOT = 6894
809236 meter/sec
ZDOT = 6273
440812 ZDOT = 1912
144759
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 32486U 08005A 08052
52447433
00014500 00000-0 95600-3 0 9031
2 32486 51
6375 257
7413 0010985 54
9271 305
2923 15
77964622 2186
Satellite: SHUTTLE
Catalog Number: 32486
Epoch time: 08052
52447433 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 257
7413 deg
Eccentricity:
0010985
Arg of perigee: 54
9271 deg
Mean anomaly: 305
2923 deg
Mean motion: 15
77964622 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 218
Checksum: 308
Coasting Arc #5 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2008/053/11:25:50
616
Vector Time (MET): 014/15:40:20
664
Weight (LBS) : 215846
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1287663
55 A = 6720351
64 meter
Y = -6510353
42 meter E =
0024534
Z = 982997
90 I = 51
34659
XDOT = 4951
282896 Wp = 56
82411
YDOT = -72
087289 meter/sec RA = 252
00827 deg
ZDOT = 5915
650171 TA = 313
98998
MA = 314
19199
Ha = 187
651 n
mi
Hp = 174
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4224617
95 X = -1219694
42
Y = -21359427
24 feet Y = -6524343
57 meter
Z = 3225058
73 Z = 976908
64
XDOT = 16244
366458 XDOT = 4922
984128
YDOT = -236
506854 feet/sec YDOT = -16
991015 meter/sec
ZDOT = 19408
301086 ZDOT = 5939
634200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9647508
61 X = 2940560
62
Y = -19523132
50 feet Y = -5950650
79 meter
Z = 3201001
03 Z = 975665
11
XDOT = 11515
060095 XDOT = 3509
790317
YDOT = 8937
761842 feet/sec YDOT = 2724
229809 meter/sec
ZDOT = 19500
083436 ZDOT = 5943
625431
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 32486U 08005A 08053
53773270
00014500 00000-0 95600-3 0 9045
2 32486 51
6365 252
5055 0010790 58
4797 301
7421 15
78040205 2341
Satellite: SHUTTLE
Catalog Number: 32486
Epoch time: 08053
53773270 = yrday
fracday
Element set: 904
Inclination: 51
6365 deg
RA of node: 252
5055 deg
Eccentricity:
0010790
Arg of perigee: 58
4797 deg
Mean anomaly: 301
7421 deg
Mean motion: 15
78040205 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 234
Checksum: 287
Coasting Arc #6 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2008/054/11:29:00
109
Vector Time (MET): 015/15:43:30
157
Weight (LBS) : 215846
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672511
48 A = 6713151
57 meter
Y = -2506270
37 meter E =
0017180
Z = -4130454
06 I = 51
33210
XDOT = 343
279513 Wp = 82
34717
YDOT = -6732
999059 meter/sec RA = 246
77200 deg
ZDOT = 3712
536292 TA = 225
73874
MA = 225
87986
Ha = 187
636 n
mi
Hp = 173
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15329762
09 X = -4624133
39
Y = -8222671
82 feet Y = -2558143
45 meter
Z = -13551358
48 Z = -4153034
80
XDOT = 1126
245122 XDOT = 400
352964
YDOT = -22089
891926 feet/sec YDOT = -6728
849245 meter/sec
ZDOT = 12180
237177 ZDOT = 3714
343577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7573445
57 X = -2308386
21
Y = -15585222
20 feet Y = -4750375
73 meter
Z = -13638072
64 Z = -4156884
54
XDOT = 12628
808328 XDOT = 3849
260778
YDOT = -16756
659923 feet/sec YDOT = -5107
429945 meter/sec
ZDOT = 12186
368127 ZDOT = 3714
405005
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 32486U 08005A 08054
48764535
00014500 00000-0 95600-3 0 9055
2 32486 51
6357 247
5963 0010791 62
1166 298
1091 15
78046765 2492
Satellite: SHUTTLE
Catalog Number: 32486
Epoch time: 08054
48764535 = yrday
fracday
Element set: 905
Inclination: 51
6357 deg
RA of node: 247
5963 deg
Eccentricity:
0010791
Arg of perigee: 62
1166 deg
Mean anomaly: 298
1091 deg
Mean motion: 15
78046765 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 249
Checksum: 328
Coasting Arc #7 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2008/055/11:32:32
666
Vector Time (MET): 016/15:47:02
714
Weight (LBS) : 215846
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2165350
01 A = 6710370
09 meter
Y = 4138329
13 meter E =
0022934
Z = -4839536
83 I = 51
33498
XDOT = -5010
078487 Wp = 69
78522
YDOT = -5347
057621 meter/sec RA = 241
61503 deg
ZDOT = -2331
787220 TA = 177
36793
MA = 177
35584
Ha = 187
674 n
mi
Hp = 173
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7104166
72 X = -2187859
89
Y = 13577195
29 feet Y = 4114038
82 meter
Z = -15877745
50 Z = -4850111
24
XDOT = -16437
265377 XDOT = -4938
712497
YDOT = -17542
839965 feet/sec YDOT = -5402
569186 meter/sec
ZDOT = -7650
220539 ZDOT = -2355
951685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13391880
61 X = -4081845
21
Y = 7361764
89 feet Y = 2243865
94 meter
Z = -15917731
32 Z = -4851724
51
XDOT = -3293
689480 XDOT = -1003
916553
YDOT = -22726
375137 feet/sec YDOT = -6926
999142 meter/sec
ZDOT = -7743
333269 ZDOT = -2360
167980
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 32486U 08005A 08055
50086393
00014500 00000-0 95600-3 0 9069
2 32486 51
6350 242
3607 0010829 66
0714 294
1584 15
78079244 2656
Satellite: SHUTTLE
Catalog Number: 32486
Epoch time: 08055
50086393 = yrday
fracday
Element set: 906
Inclination: 51
6350 deg
RA of node: 242
3607 deg
Eccentricity:
0010829
Arg of perigee: 66
0714 deg
Mean anomaly: 294
1584 deg
Mean motion: 15
78079244 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 265
Checksum: 306
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 may contain past, current and future orbital data 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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