Date:
September 8th 2009
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
251/20:41:49
374 0
0 0
0 0
0
010/16:42:12
416 0
0 0
0 193
1
000/00:00:00
000 0
0 0
0 180
9
251/21:09:47
299 1
6 -5
0 5
0
010/17:10:10
341 -3
0 0
0 191
9
000/00:00:20
683 3
7 0
1 179
5
253/00:09:11
337 2
1 -0
1 17
0
011/20:09:34
379 -12
1 0
0 192
5
000/00:00:12
758 11
7 -17
0 179
4
Coasting Arc #1 (Orbit 112)
---------------------------------------
Vector Time (GMT): 2009/248/05:03:12
000
Vector Time (MET): 007/01:03:35
042
Weight (LBS) : 217155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1679645
05 A = 6726282
51 meter
Y = 5350333
53 meter E =
0014431
Z = -3730778
34 I = 51
31626
XDOT = -4664
496400 Wp = 64
76302
YDOT = -4409
587041 meter/sec RA = 255
24179 deg
ZDOT = -4230
515881 TA = 160
43774
MA = 160
38231
Ha = 193
172 n
mi
Hp = 181
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5510646
50 X = -1721225
20
Y = 17553587
69 feet Y = 5331317
98 meter
Z = -12240086
42 Z = -3739039
42
XDOT = -15303
465878 XDOT = -4594
289972
YDOT = -14467
149084 feet/sec YDOT = -4461
355957 meter/sec
ZDOT = -13879
645280 ZDOT = -4253
005035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12357759
64 X = 3766645
14
Y = 13601199
47 feet Y = 4145645
60 meter
Z = -12272266
73 Z = -3740586
90
XDOT = -19202
202164 XDOT = -5852
831220
YDOT = 4862
962971 feet/sec YDOT = 1482
231113 meter/sec
ZDOT = -13968
385104 ZDOT = -4257
563780
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 09248
23439748
00020000 00000-0 20000-3 0 9003
2 00128 51
6396 255
9247 0008700 56
2971 303
9020 15
73938842 1134
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09248
23439748 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 255
9247 deg
Eccentricity:
0008700
Arg of perigee: 56
2971 deg
Mean anomaly: 303
9020 deg
Mean motion: 15
73938842 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 113
Checksum: 279
Coasting Arc #2 (Orbit 128)
---------------------------------------
Vector Time (GMT): 2009/249/05:03:59
729
Vector Time (MET): 008/01:04:22
771
Weight (LBS) : 217155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4333278
67 A = 6727012
92 meter
Y = 3784356
50 meter E =
0020547
Z = 3473692
84 I = 51
32778
XDOT = -1640
167781 Wp = 76
52386
YDOT = 6034
637826 meter/sec RA = 250
02917 deg
ZDOT = -4501
274597 TA = 62
02021
MA = 61
81243
Ha = 193
201 n
mi
Hp = 180
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14216793
55 X = 4273764
71
Y = 12415867
79 feet Y = 3832481
29 meter
Z = 11396630
05 Z = 3494599
05
XDOT = -5381
127892 XDOT = -1685
659851
YDOT = 19798
680530 feet/sec YDOT = 6016
041782 meter/sec
ZDOT = -14767
961276 ZDOT = -4509
353520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17756939
90 X = 5412315
28
Y = -6251022
65 feet Y = -1905311
70 meter
Z = 11479110
12 Z = 3498832
77
XDOT = 14208
315026 XDOT = 4330
694420
YDOT = 13022
202599 feet/sec YDOT = 3969
167352 meter/sec
ZDOT = -14799
377884 ZDOT = -4510
850379
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 09249
25025957
00020000 00000-0 20000-3 0 9010
2 00128 51
6397 250
7082 0008850 60
4751 299
7293 15
73944766 1297
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09249
25025957 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 250
7082 deg
Eccentricity:
0008850
Arg of perigee: 60
4751 deg
Mean anomaly: 299
7293 deg
Mean motion: 15
73944766 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 129
Checksum: 299
Coasting Arc #3 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2009/250/05:05:07
923
Vector Time (MET): 009/01:05:30
965
Weight (LBS) : 217155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1313735
18 A = 6724499
21 meter
Y = -5086759
58 meter E =
0017679
Z = 4181495
87 I = 51
33189
XDOT = 5237
368532 Wp = 86
62989
YDOT = 4343
784036 meter/sec RA = 244
91822 deg
ZDOT = 3626
578579 TA = 326
27133
MA = 326
38369
Ha = 193
120 n
mi
Hp = 180
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4310154
79 X = 1350205
51
Y = -16688843
76 feet Y = -5071864
38 meter
Z = 13718818
47 Z = 4187967
00
XDOT = 17182
967624 XDOT = 5170
788980
YDOT = 14251
259961 feet/sec YDOT = 4401
979381 meter/sec
ZDOT = 11898
223686 ZDOT = 3651
859791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12735047
54 X = -3881642
49
Y = -11585461
91 feet Y = -3531248
79 meter
Z = 13743964
39 Z = 4189160
35
XDOT = 19782
998124 XDOT = 6029
857828
YDOT = -7465
539609 feet/sec YDOT = -2275
496473 meter/sec
ZDOT = 11997
955067 ZDOT = 3656
976704
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 09250
26610896
00020000 00000-0 20000-3 0 9026
2 00128 51
6403 245
4910 0008782 63
7849 296
4216 15
74009962 1452
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09250
26610896 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 245
4910 deg
Eccentricity:
0008782
Arg of perigee: 63
7849 deg
Mean anomaly: 296
4216 deg
Mean motion: 15
74009962 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 145
Checksum: 280
Coasting Arc #4 (Orbit 159)
---------------------------------------
Vector Time (GMT): 2009/251/05:06:06
881
Vector Time (MET): 010/01:06:29
923
Weight (LBS) : 233520
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4825253
40 A = 6728596
91 meter
Y = -3710695
18 meter E =
0013368
Z = -2870649
18 I = 51
35955
XDOT = 1363
539125 Wp = 65
97723
YDOT = -5653
277187 meter/sec RA = 239
70991 deg
ZDOT = 5039
467231 TA = 260
92314
MA = 261
07443
Ha = 193
194 n
mi
Hp = 180
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15830883
85 X = -4769455
92
Y = -12174196
79 feet Y = -3764342
20 meter
Z = -9418140
35 Z = -2893954
70
XDOT = 4473
553561 XDOT = 1402
172664
YDOT = -18547
497334 feet/sec YDOT = -5637
812967 meter/sec
ZDOT = 16533
685140 ZDOT = 5046
185553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17985322
81 X = -5481926
39
Y = 8579985
98 feet Y = 2615179
73 meter
Z = -9510064
29 Z = -2898667
59
XDOT = -13947
569977 XDOT = -4251
219329
YDOT = -10967
743707 feet/sec YDOT = -3342
968282 meter/sec
ZDOT = 16559
767418 ZDOT = 5047
417109
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 09251
21846129
00020000 00000-0 20000-3 0 9033
2 00128 51
6405 240
6011 0008777 66
0425 294
1657 15
73972092 1606
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09251
21846129 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 240
6011 deg
Eccentricity:
0008777
Arg of perigee: 66
0425 deg
Mean anomaly: 294
1657 deg
Mean motion: 15
73972092 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 160
Checksum: 261
Coasting Arc #5 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2009/251/20:41:49
374
Vector Time (MET): 010/16:42:12
416
Weight (LBS) : 233438
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 420617
39 A = 6724865
71 meter
Y = -5297861
81 meter E =
0017767
Z = 4104051
00 I = 51
35607
XDOT = 5834
935874 Wp = 83
44577
YDOT = 3373
507417 meter/sec RA = 236
41037 deg
ZDOT = 3744
957331 TA = 328
04860
MA = 328
15621
Ha = 193
136 n
mi
Hp = 180
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1379978
33 X = 459890
79
Y = -17381436
38 feet Y = -5292938
43 meter
Z = 13464734
25 Z = 4106190
04
XDOT = 19143
490401 XDOT = 5778
586548
YDOT = 11067
937720 feet/sec YDOT = 3438
442220 meter/sec
ZDOT = 12286
605416 ZDOT = 3773
166702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15990687
38 X = 4873961
51
Y = -6935325
33 feet Y = -2113887
16 meter
Z = 13472821
48 Z = 4106515
99
XDOT = -1428
946643 XDOT = -435
542937
YDOT = 20865
173508 feet/sec YDOT = 6359
704885 meter/sec
ZDOT = 12397
806122 ZDOT = 3778
851306
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 09251
91684748
00020000 00000-0 20000-3 0 9048
2 00128 51
6394 237
0158 0008823 58
1567 302
0454 15
73986478 1715
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09251
91684748 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 237
0158 deg
Eccentricity:
0008823
Arg of perigee: 58
1567 deg
Mean anomaly: 302
0454 deg
Mean motion: 15
73986478 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 171
Checksum: 295
Coasting Arc #6 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2009/251/21:09:57
640
Vector Time (MET): 010/17:10:20
683
Weight (LBS) : 233303
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4608786
50 A = 6728294
86 meter
Y = 4638926
60 meter E =
0018841
Z = 1573295
69 I = 51
37748
XDOT = -2523
757412 Wp = 84
01904
YDOT = 4473
461646 meter/sec RA = 236
26912 deg
ZDOT = -5736
369613 TA = 78
55884
MA = 78
34729
Ha = 191
898 n
mi
Hp = 179
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15120690
62 X = 4548927
82
Y = 15219575
47 feet Y = 4690130
15 meter
Z = 5161731
28 Z = 1595539
79
XDOT = -8280
044002 XDOT = -2545
726319
YDOT = 14676
711438 feet/sec YDOT = 4445
116393 meter/sec
ZDOT = -18820
110278 ZDOT = -5748
683734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3891678
14 X = -1186183
50
Y = 21076323
29 feet Y = 6424063
34 meter
Z = 5249539
99 Z = 1600059
79
XDOT = -15177
964609 XDOT = -4626
243613
YDOT = 1945
834423 feet/sec YDOT = 593
090332 meter/sec
ZDOT = -18868
283091 ZDOT = -5751
052686
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 09251
91682239
00020000 00000-0 20000-3 0 9052
2 00128 51
6394 237
0156 0010433 36
2891 323
8978 15
74974887 1714
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09251
91682239 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 237
0156 deg
Eccentricity:
0010433
Arg of perigee: 36
2891 deg
Mean anomaly: 323
8978 deg
Mean motion: 15
74974887 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 171
Checksum: 298
Coasting Arc #7 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2009/252/21:10:22
505
Vector Time (MET): 011/17:10:45
547
Weight (LBS) : 233303
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2295835
44 A = 6717998
14 meter
Y = -3677196
01 meter E =
0011575
Z = 5122327
18 I = 51
35900
XDOT = 5524
746087 Wp = 62
27310
YDOT = 5225
772821 meter/sec RA = 231
13049 deg
ZDOT = 1278
376414 TA = 15
49077
MA = 15
45538
Ha = 191
947 n
mi
Hp = 179
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7532268
52 X = 2311900
24
Y = -12064291
36 feet Y = -3651432
67 meter
Z = 16805535
36 Z = 5133519
59
XDOT = 18125
807372 XDOT = 5459
689790
YDOT = 17144
923953 feet/sec YDOT = 5287
190065 meter/sec
ZDOT = 4194
148340 ZDOT = 1305
057765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14132067
21 X = 4307454
09
Y = -1045176
41 feet Y = -318569
77 meter
Z = 16849347
06 Z = 5135680
99
XDOT = -3362
373897 XDOT = -1024
851564
YDOT = 23683
841705 feet/sec YDOT = 7218
834952 meter/sec
ZDOT = 4299
459489 ZDOT = 1310
475252
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 09252
93203963
00020000 00000-0 20000-3 0 9069
2 00128 51
6384 231
7936 0010382 40
6976 319
4962 15
74932709 1874
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09252
93203963 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 231
7936 deg
Eccentricity:
0010382
Arg of perigee: 40
6976 deg
Mean anomaly: 319
4962 deg
Mean motion: 15
74932709 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 187
Checksum: 295
Coasting Arc #8 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2009/253/00:09:17
716
Vector Time (MET): 011/20:09:40
758
Weight (LBS) : 232914
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 910622
67 A = 6719817
59 meter
Y = -4745588
45 meter E =
0014393
Z = 4656203
54 I = 51
36653
XDOT = 6064
934206 Wp = 48
33447
YDOT = 3876
969234 meter/sec RA = 230
49573 deg
ZDOT = 2769
216355 TA = 14
32166
MA = 14
28090
Ha = 192
493 n
mi
Hp = 179
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2987607
20 X = 941001
74
Y = -15569515
92 feet Y = -4735235
37 meter
Z = 15276258
33 Z = 4660701
29
XDOT = 19898
078103 XDOT = 6007
678006
YDOT = 12719
715336 feet/sec YDOT = 3944
470823 meter/sec
ZDOT = 9085
355495 ZDOT = 2798
540958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5370020
92 X = 1636782
38
Y = -14898539
67 feet Y = -4541074
89 meter
Z = 15293661
51 Z = 4661508
03
XDOT = 16448
755540 XDOT = 5013
580689
YDOT = 15360
487952 feet/sec YDOT = 4681
876728 meter/sec
ZDOT = 9200
984738 ZDOT = 2804
460148
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
05894702
00020000 00000-0 20000-3 0 9071
2 00128 51
6367 231
1370 0013739 15
5051 344
6531 15
75006727 1892
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09253
05894702 = yrday
fracday
Element set: 907
Inclination: 51
6367 deg
RA of node: 231
1370 deg
Eccentricity:
0013739
Arg of perigee: 15
5051 deg
Mean anomaly: 344
6531 deg
Mean motion: 15
75006727 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 189
Checksum: 265
Coasting Arc #9 (Orbit 203)
---------------------------------------
Vector Time (GMT): 2009/254/00:14:35
190
Vector Time (MET): 012/20:14:58
232
Weight (LBS) : 232914
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4867674
74 A = 6729299
34 meter
Y = -4618636
86 meter E =
0024905
Z = -263615
55 I = 51
41985
XDOT = 3149
027062 Wp = 30
69055
YDOT = -3647
117829 meter/sec RA = 225
29211 deg
ZDOT = 6021
821270 TA = 326
43106
MA = 326
58862
Ha = 192
622 n
mi
Hp = 179
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15970061
49 X = -4814385
96
Y = -15153008
06 feet Y = -4672772
11 meter
Z = -864880
43 Z = -287133
48
XDOT = 10331
453614 XDOT = 3160
322541
YDOT = -11965
609675 feet/sec YDOT = -3611
840387 meter/sec
ZDOT = 19756
631462 ZDOT = 6037
146822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14009975
74 X = -4270240
61
Y = -16976686
79 feet Y = -5174494
13 meter
Z = -957716
33 Z = -291911
94
XDOT = 10353
367478 XDOT = 3155
706407
YDOT = -9616
901489 feet/sec YDOT = -2931
231574 meter/sec
ZDOT = 19816
714103 ZDOT = 6040
134459
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
01069119
00020000 00000-0 20000-3 0 9085
2 00128 51
6380 226
2424 0013748 19
8970 340
2727 15
75001033 2041
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09254
01069119 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 226
2424 deg
Eccentricity:
0013748
Arg of perigee: 19
8970 deg
Mean anomaly: 340
2727 deg
Mean motion: 15
75001033 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 204
Checksum: 248
Coasting Arc #10 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2009/255/00:15:04
274
Vector Time (MET): 013/20:15:27
317
Weight (LBS) : 232914
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2966770
12 A = 6717179
86 meter
Y = 2983691
04 meter E =
0023853
Z = -5253293
56 I = 51
40132
XDOT = -5707
185700 Wp = 60
02377
YDOT = -5141
182315 meter/sec RA = 220
13221 deg
ZDOT = 315
880251 TA = 212
91545
MA = 213
06420
Ha = 192
713 n
mi
Hp = 178
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9733497
77 X = -2974394
10
Y = 9789012
61 feet Y = 2950472
31 meter
Z = -17235215
08 Z = -5267724
68
XDOT = -18724
362534 XDOT = -5650
806437
YDOT = -16867
396045 feet/sec YDOT = -5204
688191 meter/sec
ZDOT = 1036
352530 ZDOT = 288
291502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10581323
34 X = -3225187
35
Y = 8754814
47 feet Y = 2668467
45 meter
Z = -17291824
81 Z = -5270548
20
XDOT = -16272
962238 XDOT = -4959
998890
YDOT = -17918
772604 feet/sec YDOT = -5461
641890 meter/sec
ZDOT = 927
450747 ZDOT = 282
686988
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
02587254
00020000 00000-0 20000-3 0 9093
2 00128 51
6380 221
0221 0013780 23
9626 336
2177 15
75036651 2205
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09255
02587254 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 221
0221 deg
Eccentricity:
0013780
Arg of perigee: 23
9626 deg
Mean anomaly: 336
2177 deg
Mean motion: 15
75036651 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 220
Checksum: 250
Coasting Arc #11 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2009/256/00:15:08
127
Vector Time (MET): 014/20:15:31
169
Weight (LBS) : 232914
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5157500
61 A = 6728960
31 meter
Y = 4273498
43 meter E =
0013884
Z = -683777
56 I = 51
46443
XDOT = -3534
988618 Wp = 73
34157
YDOT = 3326
839132 meter/sec RA = 214
98137 deg
ZDOT = -5967
042556 TA = 114
11849
MA = 113
97321
Ha = 192
799 n
mi
Hp = 178
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16920933
75 X = 5112651
96
Y = 14020664
15 feet Y = 4330921
88 meter
Z = -2243364
70 Z = -658831
32
XDOT = -11597
731685 XDOT = -3542
940372
YDOT = 10914
826547 feet/sec YDOT = 3287
264419 meter/sec
ZDOT = -19576
911274 ZDOT = -5984
234802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15686520
90 X = 4781251
57
Y = 15403316
62 feet Y = 4694930
91 meter
Z = -2144902
43 Z = -653766
26
XDOT = -11242
595631 XDOT = -3426
743148
YDOT = 8759
721767 feet/sec YDOT = 2669
963195 meter/sec
ZDOT = -19644
372695 ZDOT = -5987
604797
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
04104058
00020000 00000-0 20000-3 0 9105
2 00128 51
6374 215
7989 0013834 27
3237 332
8652 15
75062356 2363
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09256
04104058 = yrday
fracday
Element set: 910
Inclination: 51
6374 deg
RA of node: 215
7989 deg
Eccentricity:
0013834
Arg of perigee: 27
3237 deg
Mean anomaly: 332
8652 deg
Mean motion: 15
75062356 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 236
Checksum: 270
Coasting Arc #12 (Orbit 251)
---------------------------------------
Vector Time (GMT): 2009/257/00:15:20
553
Vector Time (MET): 015/20:15:43
595
Weight (LBS) : 232914
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3275362
73 A = 6717649
26 meter
Y = -2833283
41 meter E =
0017695
Z = 5128758
67 I = 51
45231
XDOT = 6030
595970 Wp = 37
11391
YDOT = 4628
484994 meter/sec RA = 209
80712 deg
ZDOT = -1278
186178 TA = 65
21817
MA = 65
03418
Ha = 192
830 n
mi
Hp = 178
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10745940
73 X = 3281887
11
Y = -9295549
25 feet Y = -2796619
89 meter
Z = 16826636
06 Z = 5144686
16
XDOT = 19785
419848 XDOT = 5984
600411
YDOT = 15185
318222 feet/sec YDOT = 4695
665487 meter/sec
ZDOT = -4193
524205 ZDOT = -1249
001422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11242786
19 X = 3426801
23
Y = -8565882
60 feet Y = -2610881
02 meter
Z = 16889155
49 Z = 5147814
59
XDOT = 18130
133215 XDOT = 5526
064604
YDOT = 15650
386049 feet/sec YDOT = 4770
237668 meter/sec
ZDOT = -4078
337248 ZDOT = -1243
077193
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 09257
05619779
00020000 00000-0 20000-3 0 9119
2 00128 51
6383 210
5774 0013838 31
5250 328
6740 15
75040496 2524
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09257
05619779 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 210
5774 deg
Eccentricity:
0013838
Arg of perigee: 31
5250 deg
Mean anomaly: 328
6740 deg
Mean motion: 15
75040496 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 252
Checksum: 275
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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