Date:
November 15th 2008
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2008/320/00:55:39 000 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 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
320/01:06:52
546 0
0 0
0 0
0
000/00:11:13
546 0
0 0
0 124
3
000/00:00:00
000 0
0 0
0 31
9
320/01:34:32
283 -43
5 97
4 97
4
000/00:38:53
283 -43
0 -0
1 124
3
000/00:01:06
366 -75
8 0
2 85
1
320/04:30:55
000 -29
4 63
5 63
5
000/03:35:16
000 -26
9 0
0 123
8
000/00:00:43
828 -49
4 -0
0 119
9
320/17:57:10
595 -4
1 7
0 7
6
000/17:01:31
595 -3
5 -0
8 123
9
000/00:10:31
355 -5
4 -3
0 122
4
321/02:46:33
346 -1
3 3
0 3
0
001/01:50:54
346 -1
3 -0
0 125
9
000/00:00:13
433 -2
3 0
0 123
2
321/17:09:33
703 -56
8 122
7 122
7
001/16:13:54
703 102
0 0
0 192
1
000/00:01:21
430 37
4 0
1 124
8
321/17:55:12
396 46
3 95
7 95
7
001/16:59:33
396 -79
3 0
0 192
3
000/00:01:03
457 -26
9 0
1 179
0
321/19:26:54
966 4
4 8
9 8
9
001/18:31:15
966 -7
4 0
1 192
4
000/00:00:13
932 -2
5 -0
1 184
2
321/20:43:48
500 0
4 2
5 3
0
001/19:48:09
500 -2
4 -0
0 192
4
000/00:00:13
001 -1
6 1
6 185
7
Coasting Arc #1 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2008/320/01:06:07
160
Vector Time (MET): 000/00:10:28
160
Weight (LBS) : 256958
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4758205
39 A = 6519789
10 meter
Y = 758457
46 meter E =
0127678
Z = 4341247
31 I = 51
43172
XDOT = -3796
725320 Wp = 352
51195
YDOT = 6073
728152 meter/sec RA = 323
13096 deg
ZDOT = 3236
895759 TA = 66
37211
MA = 65
03684
Ha = 124
349 n
mi
Hp = 31
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15610910
08 X = 4728280
98
Y = 2488377
49 feet Y = 811498
60 meter
Z = 14242937
37 Z = 4364290
71
XDOT = -12456
447899 XDOT = -3880
085235
YDOT = 19926
929631 feet/sec YDOT = 6030
804479 meter/sec
ZDOT = 10619
736741 ZDOT = 3218
249037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7584384
28 X = 2311720
33
Y = -13777368
58 feet Y = -4199341
94 meter
Z = 14332307
25 Z = 4368487
25
XDOT = 13527
381577 XDOT = 4123
145905
YDOT = 17956
027882 feet/sec YDOT = 5472
997298 meter/sec
ZDOT = 10547
878429 ZDOT = 3214
993345
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 00126U 08320
09487515
00020000 00000-0 70000-3 0 9005
2 00126 51
6395 323
3439 0350483 169
7501 191
1173 17
96085154 20
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08320
09487515 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 323
3439 deg
Eccentricity:
0350483
Arg of perigee: 169
7501 deg
Mean anomaly: 191
1173 deg
Mean motion: 17
96085154 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 262
Coasting Arc #2 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2008/320/01:06:52
546
Vector Time (MET): 000/00:11:13
546
Weight (LBS) : 256958
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4578835
07 A = 6519158
65 meter
Y = 1032842
10 meter E =
0127644
Z = 4481548
09 I = 51
42965
XDOT = -4105
438132 Wp = 352
05172
YDOT = 6014
484561 meter/sec RA = 323
12630 deg
ZDOT = 2944
246052 TA = 69
98452
MA = 68
61469
Ha = 124
325 n
mi
Hp = 31
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15022424
77 X = 4545174
20
Y = 3388589
56 feet Y = 1083856
51 meter
Z = 14703241
76 Z = 4503711
05
XDOT = -13469
285209 XDOT = -4186
690953
YDOT = 19732
560895 feet/sec YDOT = 5968
120502 meter/sec
ZDOT = 9659
599908 ZDOT = 2924
104673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8189426
76 X = 2496137
28
Y = -12944243
06 feet Y = -3945405
28 meter
Z = 14789217
84 Z = 4507753
60
XDOT = 13129
239429 XDOT = 4001
792178
YDOT = 18748
005881 feet/sec YDOT = 5714
392192 meter/sec
ZDOT = 9581
944135 ZDOT = 2920
576572
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 00126U 08320
09490780
00020000 00000-0 70000-3 0 9014
2 00126 51
6395 323
3441 0347446 169
7174 191
1457 17
95107691 29
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08320
09490780 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 323
3441 deg
Eccentricity:
0347446
Arg of perigee: 169
7174 deg
Mean anomaly: 191
1457 deg
Mean motion: 17
95107691 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 270
Coasting Arc #3 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2008/320/01:35:05
466
Vector Time (MET): 000/00:39:26
466
Weight (LBS) : 254491
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5135273
61 A = 6577926
50 meter
Y = 4149723
33 meter E =
0046479
Z = 279326
84 I = 51
46263
XDOT = -3232
664957 Wp = 349
93300
YDOT = -3600
015938 meter/sec RA = 322
99004 deg
ZDOT = -6052
266698 TA = 186
96930
MA = 187
03415
Ha = 124
344 n
mi
Hp = 85
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16848010
52 X = -5182651
77
Y = 13614577
85 feet Y = 4092032
79 meter
Z = 916426
63 Z = 254264
43
XDOT = -10605
856159 XDOT = -3162
767117
YDOT = -11811
075913 feet/sec YDOT = -3635
773884 meter/sec
ZDOT = -19856
518038 ZDOT = -6067
802081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9655853
22 X = 2943104
06
Y = 19394453
66 feet Y = 5911429
47 meter
Z = 819568
33 Z = 249804
43
XDOT = -12383
203140 XDOT = -3774
400317
YDOT = 6990
732675 feet/sec YDOT = 2130
775319 meter/sec
ZDOT = -19916
981720 ZDOT = -6070
696028
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 00126U 08320
09713556
00020000 00000-0 70000-3 0 9024
2 00126 51
6395 323
3649 0056664 342
3971 17
5256 16
30124981 29
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08320
09713556 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 323
3649 deg
Eccentricity:
0056664
Arg of perigee: 342
3971 deg
Mean anomaly: 17
5256 deg
Mean motion: 16
30124981 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 260
Coasting Arc #4 (Orbit 3)
---------------------------------------
Vector Time (GMT): 2008/320/04:31:16
914
Vector Time (MET): 000/03:35:37
914
Weight (LBS) : 252896
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5005854
15 A = 6610332
88 meter
Y = 4292405
75 meter E =
0004571
Z = 421483
72 I = 51
46270
XDOT = -3449
550244 Wp = 202
50832
YDOT = -3430
710781 meter/sec RA = 322
30587 deg
ZDOT = -6056
361771 TA = 332
81412
MA = 332
83804
Ha = 123
829 n
mi
Hp = 119
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16423406
00 X = -5055528
02
Y = 14082696
02 feet Y = 4236149
60 meter
Z = 1382820
60 Z = 397044
52
XDOT = -11317
422062 XDOT = -3381
509615
YDOT = -11255
612797 feet/sec YDOT = -3468
904439 meter/sec
ZDOT = -19869
953318 ZDOT = -6072
955291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20616096
42 X = 6283786
19
Y = 6578709
01 feet Y = 2005190
51 meter
Z = 1288386
87 Z = 392700
32
XDOT = -3209
150387 XDOT = -978
149038
YDOT = 13943
187661 feet/sec YDOT = 4249
883599 meter/sec
ZDOT = -19934
507264 ZDOT = -6076
037814
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 00126U 08320
22001256
00020000 00000-0 70000-3 0 9037
2 00126 51
6431 322
6843 0012609 291
3546 68
6295 16
17854369 47
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08320
22001256 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 322
6843 deg
Eccentricity:
0012609
Arg of perigee: 291
3546 deg
Mean anomaly: 68
6295 deg
Mean motion: 16
17854369 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4
Checksum: 251
Coasting Arc #5 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2008/320/18:02:26
272
Vector Time (MET): 000/17:06:47
272
Weight (LBS) : 252671
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5592061
16 A = 6609380
97 meter
Y = 1442195
61 meter E =
0006403
Z = -3208088
36 I = 51
43221
XDOT = 1180
099274 Wp = 261
25641
YDOT = -6026
668742 meter/sec RA = 319
24650 deg
ZDOT = -4759
369961 TA = 317
13934
MA = 317
18923
Ha = 123
920 n
mi
Hp = 122
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18346657
35 X = -5592187
75
Y = 4731612
91 feet Y = 1379661
66 meter
Z = -10525224
28 Z = -3235255
32
XDOT = 3871
716779 XDOT = 1270
523426
YDOT = -19772
535242 feet/sec YDOT = -6012
965988 meter/sec
ZDOT = -15614
730843 ZDOT = -4753
418044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17698245
27 X = -5394425
16
Y = -6598059
62 feet Y = -2011088
57 meter
Z = -10630431
15 Z = -3240155
42
XDOT = 14093
513067 XDOT = 4295
702783
YDOT = -12646
063096 feet/sec YDOT = -3854
520032 meter/sec
ZDOT = -15592
074337 ZDOT = -4752
464258
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 00126U 08320
77595007
00020000 00000-0 70000-3 0 9040
2 00126 51
6425 319
6438 0010897 266
6983 93
2956 16
16437751 132
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08320
77595007 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 319
6438 deg
Eccentricity:
0010897
Arg of perigee: 266
6983 deg
Mean anomaly: 93
2956 deg
Mean motion: 16
16437751 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 13
Checksum: 289
Coasting Arc #6 (Orbit 18)
---------------------------------------
Vector Time (GMT): 2008/321/02:46:40
062
Vector Time (MET): 001/01:51:01
062
Weight (LBS) : 252584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4768231
11 A = 6615325
86 meter
Y = 4571512
64 meter E =
0012324
Z = 146190
96 I = 51
43725
XDOT = -3449
590912 Wp = 187
60457
YDOT = -3405
991460 meter/sec RA = 317
21757 deg
ZDOT = -6074
573290 TA = 350
77394
MA = 350
79657
Ha = 125
923 n
mi
Hp = 123
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15643802
86 X = -4819706
30
Y = 14998401
06 feet Y = 4517903
70 meter
Z = 479629
12 Z = 122901
98
XDOT = -11317
555484 XDOT = -3381
738423
YDOT = -11174
512663 feet/sec YDOT = -3444
186622 meter/sec
ZDOT = -19929
702395 ZDOT = -6091
167350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16664294
26 X = 5079276
89
Y = 13858575
03 feet Y = 4224093
67 meter
Z = 389667
96 Z = 118770
79
XDOT = -8832
030575 XDOT = -2692
002919
YDOT = 11174
424344 feet/sec YDOT = 3405
964540 meter/sec
ZDOT = -19994
261727 ZDOT = -6094
250974
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 00126U 08321
14688114
00020000 00000-0 70000-3 0 9055
2 00126 51
6397 317
6111 0011208 253
1648 106
8309 16
16034984 192
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08321
14688114 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 317
6111 deg
Eccentricity:
0011208
Arg of perigee: 253
1648 deg
Mean anomaly: 106
8309 deg
Mean motion: 16
16034984 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 19
Checksum: 254
Coasting Arc #7 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2008/321/17:10:14
418
Vector Time (MET): 001/16:14:35
418
Weight (LBS) : 249533
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4375415
32 A = 6668395
17 meter
Y = 1035590
32 meter E =
0088803
Z = 4844025
77 I = 51
38850
XDOT = -3862
942452 Wp = 68
97414
YDOT = 6438
511215 meter/sec RA = 313
95665 deg
ZDOT = 2113
979177 TA =
73889
MA =
72585
Ha = 192
085 n
mi
Hp = 124
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14355037
12 X = 4339978
21
Y = 3397606
02 feet Y = 1084320
02 meter
Z = 15892472
99 Z = 4865195
92
XDOT = -12673
695710 XDOT = -3944
921319
YDOT = 21123
724459 feet/sec YDOT = 6394
854940 meter/sec
ZDOT = 6935
627222 ZDOT = 2095
014346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7231047
43 X = 2204023
26
Y = 12755597
22 feet Y = 3887906
03 meter
Z = 15974611
35 Z = 4869061
54
XDOT = -23193
944686 XDOT = -7069
514340
YDOT = 4559
005195 feet/sec YDOT = 1389
584784 meter/sec
ZDOT = 6862
556277 ZDOT = 2091
707153
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 00126U 08321
76616429
00020000 00000-0 70000-3 0 9064
2 00126 51
6412 314
2443 0085412 66
1041 294
9052 15
92832385 297
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08321
76616429 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 314
2443 deg
Eccentricity:
0085412
Arg of perigee: 66
1041 deg
Mean anomaly: 294
9052 deg
Mean motion: 15
92832385 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 258
Coasting Arc #8 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2008/321/17:55:44
124
Vector Time (MET): 001/17:00:05
124
Weight (LBS) : 247178
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4390867
10 A = 6718753
57 meter
Y = -1158152
66 meter E =
0023212
Z = -4972640
58 I = 51
38869
XDOT = 3895
218529 Wp = 60
79994
YDOT = -6327
366994 meter/sec RA = 313
78822 deg
ZDOT = -1961
572388 TA = 190
11029
MA = 190
15706
Ha = 192
341 n
mi
Hp = 178
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14405731
95 X = -4353433
54
Y = -3799713
46 feet Y = -1207043
98 meter
Z = -16314437
61 Z = -4993880
96
XDOT = 12779
588350 XDOT = 3975
211786
YDOT = -20759
078063 feet/sec YDOT = -6283
360910 meter/sec
ZDOT = -6435
604946 ZDOT = -1942
455567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9415450
18 X = -2869829
22
Y = -11428744
08 feet Y = -3483481
20 meter
Z = -16396856
91 Z = -4997761
99
XDOT = 21679
775555 XDOT = 6607
995589
YDOT = -8713
256081 feet/sec YDOT = -2655
800453 meter/sec
ZDOT = -6361
937107 ZDOT = -1939
118430
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 00126U 08321
76624524
00020000 00000-0 70000-3 0 9070
2 00126 51
6424 314
2466 0011036 44
0619 316
1422 15
74918117 298
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08321
76624524 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 314
2466 deg
Eccentricity:
0011036
Arg of perigee: 44
0619 deg
Mean anomaly: 316
1422 deg
Mean motion: 15
74918117 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 245
Coasting Arc #9 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2008/321/19:27:01
932
Vector Time (MET): 001/18:31:22
932
Weight (LBS) : 246960
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4414662
35 A = 6723527
77 meter
Y = -1104607
55 meter E =
0016125
Z = -4963652
30 I = 51
38799
XDOT = 3834
669860 Wp = 56
39729
YDOT = -6358
377773 meter/sec RA = 313
46182 deg
ZDOT = -1991
421446 TA = 194
21919
MA = 194
26463
Ha = 192
385 n
mi
Hp = 184
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14483800
36 X = -4377869
45
Y = -3624040
51 feet Y = -1153768
55 meter
Z = -16284948
49 Z = -4985009
82
XDOT = 12580
937862 XDOT = 3915
159385
YDOT = -20860
819466 feet/sec YDOT = -6315
046003 meter/sec
ZDOT = -6533
534927 ZDOT = -1972
597573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13234085
23 X = -4033749
18
Y = -6713210
31 feet Y = -2046186
50 meter
Z = -16367818
59 Z = -4988911
11
XDOT = 16424
895710 XDOT = 5006
308212
YDOT = -16593
380987 feet/sec YDOT = -5057
662525 meter/sec
ZDOT = -6461
004879 ZDOT = -1969
314287
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 00126U 08321
82970482
00020000 00000-0 70000-3 0 9085
2 00126 51
6428 313
9211 0005624 9
2613 350
8652 15
73254509 308
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08321
82970482 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 313
9211 deg
Eccentricity:
0005624
Arg of perigee: 9
2613 deg
Mean anomaly: 350
8652 deg
Mean motion: 15
73254509 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 30
Checksum: 250
Coasting Arc #10 (Orbit 30)
---------------------------------------
Vector Time (GMT): 2008/321/20:43:55
001
Vector Time (MET): 001/19:48:16
001
Weight (LBS) : 246875
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5189921
42 A = 6735125
08 meter
Y = 4114790
45 meter E =
0006434
Z = -1214088
76 I = 51
42027
XDOT = -2193
642264 Wp = 124
50851
YDOT = -4486
501106 meter/sec RA = 313
18278 deg
ZDOT = -5853
986993 TA = 68
82650
MA = 68
75777
Ha = 192
384 n
mi
Hp = 185
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17027301
25 X = -5229650
04
Y = 13499968
65 feet Y = 4056531
75 meter
Z = -3983230
84 Z = -1239397
80
XDOT = -7196
989056 XDOT = -2114
872407
YDOT = -14719
491818 feet/sec YDOT = -4510
590569 meter/sec
ZDOT = -19205
994071 ZDOT = -5864
453060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15363201
30 X = -4682703
76
Y = 15341489
17 feet Y = 4676085
90 meter
Z = -4081056
88 Z = -1243906
14
XDOT = -7591
692289 XDOT = -2313
947810
YDOT = -12700
577401 feet/sec YDOT = -3871
135992 meter/sec
ZDOT = -19246
878106 ZDOT = -5866
448447
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 00126U 08321
89323104
00020000 00000-0 70000-3 0 9096
2 00126 51
6421 313
5954 0003575 356
0291 4
0843 15
72731994 317
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08321
89323104 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 313
5954 deg
Eccentricity:
0003575
Arg of perigee: 356
0291 deg
Mean anomaly: 4
0843 deg
Mean motion: 15
72731994 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 31
Checksum: 250
Coasting Arc #11 (Orbit 46)
---------------------------------------
Vector Time (GMT): 2008/322/20:45:40
580
Vector Time (MET): 002/19:50:01
580
Weight (LBS) : 246875
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2031138
57 A = 6724457
19 meter
Y = 3950981
58 meter E =
0007904
Z = 5046117
09 I = 51
36557
XDOT = -5603
859127 Wp = 31
66074
YDOT = 5013
567193 meter/sec RA = 308
00627 deg
ZDOT = -1662
047347 TA = 74
42230
MA = 74
33506
Ha = 192
326 n
mi
Hp = 185
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6663840
45 X = 1962293
70
Y = 12962538
01 feet Y = 3973309
54 meter
Z = 16555502
25 Z = 5055817
62
XDOT = -18385
364589 XDOT = -5651
431144
YDOT = 16448
711264 feet/sec YDOT = 4950
635771 meter/sec
ZDOT = -5452
911242 ZDOT = -1689
386273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8296182
61 X = 2528676
46
Y = 11931120
97 feet Y = 3636605
67 meter
Z = 16593387
91 Z = 5057664
63
XDOT = -15035
790016 XDOT = -4582
908797
YDOT = 18221
169158 feet/sec YDOT = 5553
812359 meter/sec
ZDOT = -5558
544762 ZDOT = -1694
244444
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 00126U 08322
90985578
00020000 00000-0 70000-3 0 9100
2 00126 51
6419 308
3834 0003720 359
6844
4315 15
72812323 475
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08322
90985578 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 308
3834 deg
Eccentricity:
0003720
Arg of perigee: 359
6844 deg
Mean anomaly:
4315 deg
Mean motion: 15
72812323 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 47
Checksum: 262
Coasting Arc #12 (Orbit 62)
---------------------------------------
Vector Time (GMT): 2008/323/20:46:59
463
Vector Time (MET): 003/19:51:20
463
Weight (LBS) : 246875
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4523316
85 A = 6734428
28 meter
Y = -4733399
39 meter E =
0016213
Z = 1537988
48 I = 51
38122
XDOT = 2631
993017 Wp = 51
19817
YDOT = 4394
691439 meter/sec RA = 302
88414 deg
ZDOT = 5753
857232 TA = 325
82094
MA = 325
92521
Ha = 192
323 n
mi
Hp = 185
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14840278
39 X = 4568438
97
Y = -15529525
57 feet Y = -4682564
87 meter
Z = 5045893
96 Z = 1560072
24
XDOT = 8635
147693 XDOT = 2554
703772
YDOT = 14418
279000 feet/sec YDOT = 4423
691354 meter/sec
ZDOT = 18877
484358 ZDOT = 5766
456154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12120772
93 X = 3694411
59
Y = -17709291
78 feet Y = -5397792
13 meter
Z = 5131171
52 Z = 1563981
08
XDOT = 9443
028469 XDOT = 2878
235077
YDOT = 11975
629627 feet/sec YDOT = 3650
171910 meter/sec
ZDOT = 18926
645285 ZDOT = 5768
841483
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 00126U 08323
92646307
00020000 00000-0 70000-3 0 9118
2 00126 51
6407 303
1712 0003645 2
9738 357
1445 15
72848719 638
Satellite: SHUTTLE
Catalog Number: 00126
Epoch time: 08323
92646307 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 303
1712 deg
Eccentricity:
0003645
Arg of perigee: 2
9738 deg
Mean anomaly: 357
1445 deg
Mean motion: 15
72848719 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 63
Checksum: 263
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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