SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2007/159/23:38:03 976 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 81 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 15216
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
170/15:57:09
269 -1
4 0
0 2
9
010/16:19:05
292 -1
6 0
0 184
9
000/00:00:10
584 1
9 -2
9 177
1
170/16:25:05
792 0
4 1
0 1
0
010/16:47:01
816 0
8 0
0 185
0
000/00:00:03
632 -0
5 -0
0 177
8
Coasting Arc #1 (Orbit 138)
---------------------------------------
Vector Time (GMT): 2007/168/15:53:48
000
Vector Time (MET): 008/16:15:44
024
Weight (LBS) : 208821
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227204
63 A = 6708336
58 meter
Y = -433643
71 meter E =
0014034
Z = -5200989
37 I = 51
93110
XDOT = -567
369344 Wp = 46
51944
YDOT = 7600
998997 meter/sec RA = 100
68352 deg
ZDOT = -1087
260729 TA = 213
10331
MA = 213
19122
Ha = 184
411 n
mi
Hp = 178
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13868781
61 X = 4257000
43
Y = -1422715
58 feet Y = -386252
29 meter
Z = -17063613
43 Z = -5180381
54
XDOT = -1861
447978 XDOT = -646
956737
YDOT = 24937
660750 feet/sec YDOT = 7594
216289 meter/sec
ZDOT = -3567
128376 ZDOT = -1090
208950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12038402
80 X = -3669305
17
Y = -7217659
92 feet Y = -2199942
74 meter
Z = -16985769
62 Z = -5177262
58
XDOT = 15873
997695 XDOT = 4838
394497
YDOT = -17998
268940 feet/sec YDOT = -5485
872373 meter/sec
ZDOT = -3577
411033 ZDOT = -1090
394883
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 31600U 07024A 07168
68002704
00014500 00000-0 95600-4 0 9008
2 31600 51
6352 101
3657 0008612 331
3656 28
7035 15
78276342 1394
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07168
68002704 = yrday
fracday
Element set: 900
Inclination: 51
6352 deg
RA of node: 101
3657 deg
Eccentricity:
0008612
Arg of perigee: 331
3656 deg
Mean anomaly: 28
7035 deg
Mean motion: 15
78276342 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 139
Checksum: 262
Coasting Arc #2 (Orbit 154)
---------------------------------------
Vector Time (GMT): 2007/169/15:57:16
993
Vector Time (MET): 009/16:19:13
016
Weight (LBS) : 208821
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1959418
82 A = 6718751
26 meter
Y = -6190595
87 meter E =
0001807
Z = -1730558
03 I = 51
97022
XDOT = 4220
126935 Wp = 30
22491
YDOT = 2938
006648 meter/sec RA = 95
53200 deg
ZDOT = -5732
730897 TA = 168
85810
MA = 168
85410
Ha = 184
437 n
mi
Hp = 177
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6428539
45 X = 2036835
53
Y = -20310353
91 feet Y = -6168273
60 meter
Z = -5677683
81 Z = -1720852
19
XDOT = 13845
560812 XDOT = 4214
841404
YDOT = 9639
129424 feet/sec YDOT = 2985
122999 meter/sec
ZDOT = -18808
172233 ZDOT = -5712
242167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16919587
66 X = -5157090
32
Y = 12960382
27 feet Y = 3950324
51 meter
Z = -5641695
98 Z = -1719588
94
XDOT = -4980
534008 XDOT = -1518
066766
YDOT = -14653
911058 feet/sec YDOT = -4466
512090 meter/sec
ZDOT = -18730
390035 ZDOT = -5709
022883
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 31600U 07024A 07169
69310541
00014500 00000-0 95600-4 0 9012
2 31600 51
6351 96
1297 0008504 333
8062 26
2672 15
78271522 1555
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07169
69310541 = yrday
fracday
Element set: 901
Inclination: 51
6351 deg
RA of node: 96
1297 deg
Eccentricity:
0008504
Arg of perigee: 333
8062 deg
Mean anomaly: 26
2672 deg
Mean motion: 15
78271522 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 155
Checksum: 267
Coasting Arc #3 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2007/170/15:57:14
561
Vector Time (MET): 010/16:19:10
584
Weight (LBS) : 208751
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3374178
02 A = 6711549
50 meter
Y = -3851815
51 meter E =
0013737
Z = 4340271
95 I = 51
94847
XDOT = 2743
524302 Wp = 27
94102
YDOT = -6316
406992 meter/sec RA = 90
34460 deg
ZDOT = -3456
451373 TA = 96
86374
MA = 96
70743
Ha = 184
903 n
mi
Hp = 177
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11070137
88 X = -3351982
84
Y = -12637189
99 feet Y = -3889386
60 meter
Z = 14239737
38 Z = 4323933
81
XDOT = 9001
063983 XDOT = 2830
672256
YDOT = -20723
120051 feet/sec YDOT = -6285
270576 meter/sec
ZDOT = -11340
063561 ZDOT = -3442
912624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2197827
42 X = 669897
80
Y = 16708788
83 feet Y = 5092838
84 meter
Z = 14177537
67 Z = 4321313
48
XDOT = -17869
228721 XDOT = -5446
540914
YDOT = 11975
233000 feet/sec YDOT = 3650
051018 meter/sec
ZDOT = -11289
597907 ZDOT = -3441
069442
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 31600U 07024A 07170
70615465
00014500 00000-0 95600-4 0 9020
2 31600 51
6350 90
8923 0009382 343
4840 16
6019 15
78391203 1712
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07170
70615465 = yrday
fracday
Element set: 902
Inclination: 51
6350 deg
RA of node: 90
8923 deg
Eccentricity:
0009382
Arg of perigee: 343
4840 deg
Mean anomaly: 16
6019 deg
Mean motion: 15
78391203 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 171
Checksum: 262
Coasting Arc #4 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2007/170/16:25:07
609
Vector Time (MET): 010/16:47:03
632
Weight (LBS) : 208723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3400865
95 A = 6712321
57 meter
Y = -3863793
57 meter E =
0012513
Z = -4319303
99 I = 51
94708
XDOT = 2705
863524 Wp = 22
98831
YDOT = 6300
794438 meter/sec RA = 90
29335 deg
ZDOT = -3497
927840 TA = 211
72984
MA = 211
80532
Ha = 184
970 n
mi
Hp = 177
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11157696
69 X = 3464758
39
Y = -12676488
09 feet Y = -3825443
48 meter
Z = -14170944
85 Z = -4302628
08
XDOT = 8877
505001 XDOT = 2652
268352
YDOT = 20671
897763 feet/sec YDOT = 6330
723978 meter/sec
ZDOT = -11476
141206 ZDOT = -3484
912285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15760318
48 X = -4803745
07
Y = 6210496
97 feet Y = 1892959
48 meter
Z = -14108341
95 Z = -4300222
63
XDOT = 1846
344149 XDOT = 562
765697
YDOT = -21330
483848 feet/sec YDOT = -6501
531477 meter/sec
ZDOT = -11426
224581 ZDOT = -3482
713252
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 31600U 07024A 07170
70615698
00014500 00000-0 95600-4 0 9039
2 31600 51
6333 90
8920 0009053 338
6238 21
4548 15
78152048 1715
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07170
70615698 = yrday
fracday
Element set: 903
Inclination: 51
6333 deg
RA of node: 90
8920 deg
Eccentricity:
0009053
Arg of perigee: 338
6238 deg
Mean anomaly: 21
4548 deg
Mean motion: 15
78152048 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 171
Checksum: 274
Coasting Arc #5 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2007/171/16:29:13
483
Vector Time (MET): 011/16:51:09
506
Weight (LBS) : 208723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -841953
47 A = 6720261
52 meter
Y = -6658057
77 meter E =
0007003
Z = 346258
69 I = 51
97312
XDOT = 4673
460262 Wp = 89
29158
YDOT = -911
248034 meter/sec RA = 85
10532 deg
ZDOT = -6053
604403 TA = 86
95790
MA = 86
87777
Ha = 185
073 n
mi
Hp = 177
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2762314
53 X = -769195
54
Y = -21844021
55 feet Y = -6667057
25 meter
Z = 1136019
31 Z = 342344
51
XDOT = 15332
874876 XDOT = 4712
700129
YDOT = -2989
658903 feet/sec YDOT = -858
818790 meter/sec
ZDOT = -19860
906833 ZDOT = -6030
805737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6694975
98 X = -2040628
68
Y = 20976273
36 feet Y = 6393568
12 meter
Z = 1120469
19 Z = 341519
01
XDOT = -13735
625669 XDOT = -4186
618704
YDOT = -3309
121188 feet/sec YDOT = -1008
620138 meter/sec
ZDOT = -19774
819880 ZDOT = -6027
365099
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 31600U 07024A 07171
71930453
00014500 00000-0 95600-4 0 9041
2 31600 51
6335 85
6558 0009034 342
8969 17
1891 15
78176310 1871
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07171
71930453 = yrday
fracday
Element set: 904
Inclination: 51
6335 deg
RA of node: 85
6558 deg
Eccentricity:
0009034
Arg of perigee: 342
8969 deg
Mean anomaly: 17
1891 deg
Mean motion: 15
78176310 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 187
Checksum: 292
Coasting Arc #6 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2007/172/16:32:28
676
Vector Time (MET): 012/16:54:24
700
Weight (LBS) : 208723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194682
29 A = 6710237
79 meter
Y = -2073663
94 meter E =
0012999
Z = 4810928
03 I = 51
93499
XDOT = 701
421597 Wp = 17
88744
YDOT = -7254
944350 meter/sec RA = 79
93057 deg
ZDOT = -2501
654063 TA = 96
53780
MA = 96
38980
Ha = 185
205 n
mi
Hp = 177
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13762080
99 X = -4194576
52
Y = -6803359
37 feet Y = -2120524
56 meter
Z = 15783884
61 Z = 4790550
44
XDOT = 2301
251959 XDOT = 794
567417
YDOT = -23802
310859 feet/sec YDOT = -7246
587910 meter/sec
ZDOT = -8207
526454 ZDOT = -2498
021040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10065605
88 X = 3067996
67
Y = 11696046
24 feet Y = 3564954
90 meter
Z = 15706612
16 Z = 4787375
39
XDOT = -10653
280858 XDOT = -3247
120005
YDOT = 20234
211267 feet/sec YDOT = 6167
387594 meter/sec
ZDOT = -8194
608398 ZDOT = -2497
716640
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 31600U 07024A 07172
73244151
00014500 00000-0 95600-4 0 9058
2 31600 51
6328 80
4184 0009019 345
9103 14
1810 15
78197816 2039
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07172
73244151 = yrday
fracday
Element set: 905
Inclination: 51
6328 deg
RA of node: 80
4184 deg
Eccentricity:
0009019
Arg of perigee: 345
9103 deg
Mean anomaly: 14
1810 deg
Mean motion: 15
78197816 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 203
Checksum: 257
Coasting Arc #7 (Orbit 218)
---------------------------------------
Vector Time (GMT): 2007/173/16:35:48
517
Vector Time (MET): 013/16:57:44
541
Weight (LBS) : 208723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2118476
77 A = 6712492
32 meter
Y = 4772707
75 meter E =
0010103
Z = 4207121
87 I = 51
93547
XDOT = -4382
940428 Wp = 53
17310
YDOT = -5179
772504 meter/sec RA = 74
81579 deg
ZDOT = 3669
033919 TA = 359
65971
MA = 359
66039
Ha = 185
333 n
mi
Hp = 177
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6950383
11 X = -2192073
14
Y = 15658490
01 feet Y = 4748629
77 meter
Z = 13802893
28 Z = 4196652
03
XDOT = -14379
725814 XDOT = -4342
575183
YDOT = -16994
004277 feet/sec YDOT = -5228
511255 meter/sec
ZDOT = 12037
512859 ZDOT = 3647
839185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12236088
71 X = 3729559
84
Y = -12035394
30 feet Y = -3668388
18 meter
Z = 13763844
48 Z = 4195219
80
XDOT = 6408
080280 XDOT = 1953
182869
YDOT = 20189
182037 feet/sec YDOT = 6153
662685 meter/sec
ZDOT = 11956
803957 ZDOT = 3644
433846
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 31600U 07024A 07173
74556293
00014500 00000-0 95600-4 0 9064
2 31600 51
6318 75
1810 0009045 349
7341 10
3638 15
78216299 2190
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07173
74556293 = yrday
fracday
Element set: 906
Inclination: 51
6318 deg
RA of node: 75
1810 deg
Eccentricity:
0009045
Arg of perigee: 349
7341 deg
Mean anomaly: 10
3638 deg
Mean motion: 15
78216299 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 219
Checksum: 284
Coasting Arc #8 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2007/174/16:39:17
143
Vector Time (MET): 014/17:01:13
166
Weight (LBS) : 208723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2857009
84 A = 6719889
88 meter
Y = 6024891
30 meter E =
0017976
Z = -741591
01 I = 51
95138
XDOT = -4038
419499 Wp = 18
50232
YDOT = 2648
539475 meter/sec RA = 69
62323 deg
ZDOT = 6015
319176 TA = 333
42873
MA = 333
52077
Ha = 185
326 n
mi
Hp = 176
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9373391
86 X = 2793096
00
Y = 19766703
75 feet Y = 6056451
36 meter
Z = -2433041
38 Z = -727866
26
XDOT = -13249
407804 XDOT = -4096
928208
YDOT = 8689
433974 feet/sec YDOT = 2603
096977 meter/sec
ZDOT = 19735
299133 ZDOT = 5995
558654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2270710
57 X = -692112
58
Y = -21764188
67 feet Y = -6633724
71 meter
Z = -2380484
69 Z = -725571
73
XDOT = 13903
313162 XDOT = 4237
729852
YDOT = -3580
450982 feet/sec YDOT = -1091
321459 meter/sec
ZDOT = 19660
884296 ZDOT = 5992
637534
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 31600U 07024A 07174
69534369
00014500 00000-0 95600-4 0 9070
2 31600 51
6314 70
2710 0008914 353
4148 6
6899 15
78246984 2340
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07174
69534369 = yrday
fracday
Element set: 907
Inclination: 51
6314 deg
RA of node: 70
2710 deg
Eccentricity:
0008914
Arg of perigee: 353
4148 deg
Mean anomaly: 6
6899 deg
Mean motion: 15
78246984 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 234
Checksum: 300
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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