Date:
May 16th 2010
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/134/18:20:08 955 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 80 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 80 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
134/18:58:56
740 35
3 97
3 97
4
000/00:38:47
785 -48
6 0
4 125
1
000/00:01:05
666 -76
7 3
9 85
2
134/21:55:12
955 12
7 41
2 41
2
000/03:35:04
000 -22
4 0
0 124
6
000/00:00:29
080 -32
1 -0
0 108
1
135/11:14:21
454 2
5 8
0 8
0
000/16:54:12
499 -4
3 -0
0 124
6
000/00:00:12
886 -6
3 -0
0 112
1
135/11:29:37
401 -0
3 -0
0 0
7
000/17:09:28
446 0
4 0
7 124
6
000/00:00:03
019 -0
4 0
0 112
0
135/21:36:25
084 1
0 3
0 3
0
001/03:16:16
129 -1
6 0
0 124
1
000/00:00:13
288 -2
4 -0
0 113
6
136/09:23:16
969 8
2 127
4 127
4
001/15:03:08
014 -84
1 -0
0 185
2
000/00:01:23
752 -95
3 0
0 123
9
136/10:08:39
362 -8
3 105
0 105
0
001/15:48:30
407 68
6 -0
0 185
4
000/00:01:08
698 79
0 0
0 181
5
136/11:40:15
050 -0
9 9
2 9
2
001/17:20:06
095 5
9 -0
1 189
7
000/00:00:14
189 7
0 0
1 184
2
136/12:57:08
513 0
6 2
4 3
0
001/18:36:59
558 2
3 0
1 190
8
000/00:00:13
116 1
9 1
9 184
8
Coasting Arc #1 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2010/134/18:35:08
955
Vector Time (MET): 000/00:14:60
000
Weight (LBS) : 253592
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1581242
49 A = 6517867
99 meter
Y = 3862842
49 meter E =
0130254
Z = 4998008
00 I = 51
84745
XDOT = -6398
412420 Wp = 350
87420
YDOT = -4280
734495 meter/sec RA = 42
09581 deg
ZDOT = 1416
666479 TA = 86
56418
MA = 85
07518
Ha = 125
213 n
mi
Hp = 32
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5187803
43 X = -1648599
87
Y = 12673367
76 feet Y = 3844782
90 meter
Z = 16397664
04 Z = 4990163
01
XDOT = -20992
166732 XDOT = -6356
950973
YDOT = -14044
404512 feet/sec YDOT = -4352
053693 meter/sec
ZDOT = 4647
855902 ZDOT = 1385
682577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10854024
89 X = 3308306
79
Y = -8410777
63 feet Y = -2563605
02 meter
Z = 16366426
13 Z = 4988486
68
XDOT = 10728
001392 XDOT = 3269
894824
YDOT = 21801
046801 feet/sec YDOT = 6644
959065 meter/sec
ZDOT = 4524
449790 ZDOT = 1379
052296
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 00132U 10134
82168589
00020000 00000-0 20000-3 0 9001
2 00132 51
6399 42
3829 0003470 350
1342 9
9820 16
86012558 23
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10134
82168589 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 42
3829 deg
Eccentricity:
0003470
Arg of perigee: 350
1342 deg
Mean anomaly: 9
9820 deg
Mean motion: 16
86012558 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 246
Coasting Arc #2 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2010/134/18:59:29
573
Vector Time (MET): 000/00:39:20
618
Weight (LBS) : 251170
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5081430
93 A = 6578673
01 meter
Y = -4213123
83 meter E =
0047346
Z = 341152
98 I = 51
88896
XDOT = 2816
766042 Wp = 350
62908
YDOT = -3884
185829 meter/sec RA = 41
98631 deg
ZDOT = -6082
800633 TA = 185
60968
MA = 185
66290
Ha = 125
067 n
mi
Hp = 85
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16671361
33 X = -5035598
65
Y = -13822584
74 feet Y = -4269691
19 meter
Z = 1119268
31 Z = 316577
73
XDOT = 9241
358406 XDOT = 2889
540089
YDOT = -12743
391827 feet/sec YDOT = -3852
279459 meter/sec
ZDOT = -19956
694989 ZDOT = -6068
940193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9785520
85 X = 2982626
76
Y = 19324886
84 feet Y = 5890225
51 meter
Z = 1021386
06 Z = 311318
47
XDOT = -12253
905094 XDOT = -3734
990273
YDOT = 7243
594784 feet/sec YDOT = 2207
847690 meter/sec
ZDOT = -19901
499224 ZDOT = -6065
976963
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 00132U 10134
82254028
00020000 00000-0 20000-3 0 9016
2 00132 51
6410 42
3917 0058065 342
8839 17
0394 16
29587372 28
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10134
82254028 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 42
3917 deg
Eccentricity:
0058065
Arg of perigee: 342
8839 deg
Mean anomaly: 17
0394 deg
Mean motion: 16
29587372 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 246
Coasting Arc #3 (Orbit 3)
---------------------------------------
Vector Time (GMT): 2010/134/21:55:27
495
Vector Time (MET): 000/03:35:18
540
Weight (LBS) : 250154
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5232896
62 A = 6599425
99 meter
Y = -3995137
48 meter E =
0014414
Z = 577567
78 I = 51
88898
XDOT = 2494
979767 Wp = 350
81356
YDOT = -4144
347108 meter/sec RA = 41
30640 deg
ZDOT = -6068
368268 TA = 182
80941
MA = 182
81752
Ha = 124
603 n
mi
Hp = 108
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17168296
01 X = -5190639
13
Y = -13107406
43 feet Y = -4053418
64 meter
Z = 1894907
40 Z = 552248
03
XDOT = 8185
629157 XDOT = 2570
616776
YDOT = -13596
939331 feet/sec YDOT = -4116
023123 meter/sec
ZDOT = -19909
344710 ZDOT = -6056
064189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20694625
99 X = 6307722
00
Y = 6217633
46 feet Y = 1895134
68 meter
Z = 1794060
90 Z = 546829
76
XDOT = -2528
876076 XDOT = -770
801428
YDOT = 14141
354232 feet/sec YDOT = 4310
284770 meter/sec
ZDOT = -19860
346747 ZDOT = -6053
433688
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 00132U 10134
94535101
00020000 00000-0 20000-3 0 9024
2 00132 51
6445 41
7107 0026165 331
1490 28
8250 16
21800492 46
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10134
94535101 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 41
7107 deg
Eccentricity:
0026165
Arg of perigee: 331
1490 deg
Mean anomaly: 28
8250 deg
Mean motion: 16
21800492 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4
Checksum: 212
Coasting Arc #4 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2010/135/11:14:27
897
Vector Time (MET): 000/16:54:18
942
Weight (LBS) : 249957
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5369645
02 A = 6603225
83 meter
Y = -3831791
22 meter E =
0008768
Z = 403978
77 I = 51
87576
XDOT = 2485
869301 Wp = 351
70633
YDOT = -4124
637096 meter/sec RA = 38
26645 deg
ZDOT = -6088
253904 TA = 183
83723
MA = 183
84396
Ha = 124
645 n
mi
Hp = 112
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17616945
60 X = -5328360
64
Y = -12571493
50 feet Y = -3891607
00 meter
Z = 1325389
67 Z = 377992
37
XDOT = 8155
739175 XDOT = 2561
383120
YDOT = -13532
273936 feet/sec YDOT = -4096
415616 meter/sec
ZDOT = -19974
586298 ZDOT = -6075
994450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21551882
85 X = -6569013
89
Y = 2044311
52 feet Y = 623106
15 meter
Z = 1221889
81 Z = 372432
01
XDOT = -2463
121277 XDOT = -750
759365
YDOT = -14073
318200 feet/sec YDOT = -4289
547387 meter/sec
ZDOT = -19925
761259 ZDOT = -6073
372032
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 00132U 10135
49991572
00020000 00000-0 20000-3 0 9034
2 00132 51
6448 38
6618 0020752 327
5517 32
4393 16
20422360 138
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10135
49991572 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 38
6618 deg
Eccentricity:
0020752
Arg of perigee: 327
5517 deg
Mean anomaly: 32
4393 deg
Mean motion: 16
20422360 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 13
Checksum: 244
Coasting Arc #5 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2010/135/11:29:38
911
Vector Time (MET): 000/17:09:29
956
Weight (LBS) : 249937
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -716001
38 A = 6594497
39 meter
Y = -4913913
93 meter E =
0021194
Z = -4348818
90 I = 51
84717
XDOT = 6734
088082 Wp = 354
12667
YDOT = 1981
050204 meter/sec RA = 38
23916 deg
ZDOT = -3324
949683 TA = 242
78297
MA = 242
99910
Ha = 124
618 n
mi
Hp = 112
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2349085
89 X = -639873
76
Y = -16121764
86 feet Y = -4921494
46 meter
Z = -14267778
55 Z = -4352113
02
XDOT = 22093
464836 XDOT = 6727
587404
YDOT = 6499
508544 feet/sec YDOT = 2056
318869 meter/sec
ZDOT = -10908
627569 ZDOT = -3292
250451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12954483
47 X = -3948526
56
Y = -9860844
50 feet Y = -3005585
40 meter
Z = -14280900
35 Z = -4352818
43
XDOT = 19597
101654 XDOT = 5973
196584
YDOT = -10029
979162 feet/sec YDOT = -3057
137649 meter/sec
ZDOT = -10778
392699 ZDOT = -3285
254095
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 00132U 10135
49991559
00020000 00000-0 20000-3 0 9040
2 00132 51
6460 38
6637 0020813 327
8153 32
1763 16
20448647 134
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10135
49991559 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 38
6637 deg
Eccentricity:
0020813
Arg of perigee: 327
8153 deg
Mean anomaly: 32
1763 deg
Mean motion: 16
20448647 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 13
Checksum: 256
Coasting Arc #6 (Orbit 19)
---------------------------------------
Vector Time (GMT): 2010/135/21:36:31
728
Vector Time (MET): 001/03:16:22
773
Weight (LBS) : 249850
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5453166
76 A = 6604170
82 meter
Y = -3725140
71 meter E =
0005939
Z = 229058
30 I = 51
86528
XDOT = 2531
995478 Wp = 347
88213
YDOT = -4080
342831 meter/sec RA = 35
89793 deg
ZDOT = -6101
233429 TA = 189
59204
MA = 189
60339
Ha = 124
130 n
mi
Hp = 113
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17890967
05 X = -5412219
01
Y = -12221590
26 feet Y = -3785892
35 meter
Z = 751503
61 Z = 202665
37
XDOT = 8307
071777 XDOT = 2607
073554
YDOT = -13386
951545 feet/sec YDOT = -4051
607940 meter/sec
ZDOT = -20017
170043 ZDOT = -6088
750993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20670614
12 X = 6300403
18
Y = 6505891
66 feet Y = 1982995
78 meter
Z = 646385
26 Z = 197018
23
XDOT = -3705
411405 XDOT = -1129
409396
YDOT = 13748
324607 feet/sec YDOT = 4190
489340 meter/sec
ZDOT = -19967
453490 ZDOT = -6086
079824
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 00132U 10135
93157879
00020000 00000-0 20000-3 0 9059
2 00132 51
6453 36
2866 0018175 324
2012 35
7956 16
20090345 206
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10135
93157879 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 36
2866 deg
Eccentricity:
0018175
Arg of perigee: 324
2012 deg
Mean anomaly: 35
7956 deg
Mean motion: 16
20090345 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 20
Checksum: 247
Coasting Arc #7 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2010/136/09:23:58
845
Vector Time (MET): 001/15:03:49
890
Weight (LBS) : 246733
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5920526
55 A = 6669823
93 meter
Y = -2604901
34 meter E =
0093090
Z = 1352062
20 I = 51
84878
XDOT = 843
043797 Wp = 159
16060
YDOT = -5008
705308 meter/sec RA = 33
19938 deg
ZDOT = -5922
957879 TA = 5
75809
MA = 5
65181
Ha = 185
200 n
mi
Hp = 123
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19424299
70 X = -5897526
20
Y = -8546264
24 feet Y = -2670979
78 meter
Z = 4435899
62 Z = 1323355
43
XDOT = 2765
891721 XDOT = 927
762400
YDOT = -16432
760198 feet/sec YDOT = -4998
803377 meter/sec
ZDOT = -19432
276507 ZDOT = -5918
657236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20952721
68 X = -6386389
57
Y = -3510952
88 feet Y = -1070138
44 meter
Z = 4321564
61 Z = 1317212
89
XDOT = -1497
073483 XDOT = -456
307997
YDOT = -15109
745669 feet/sec YDOT = -4605
450480 meter/sec
ZDOT = -19415
143265 ZDOT = -5917
735667
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 00132U 10136
42560013
00020000 00000-0 20000-3 0 9063
2 00132 51
6449 33
5832 0082562 165
8655 194
4858 15
95913260 280
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10136
42560013 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 33
5832 deg
Eccentricity:
0082562
Arg of perigee: 165
8655 deg
Mean anomaly: 194
4858 deg
Mean motion: 15
95913260 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 28
Checksum: 265
Coasting Arc #8 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2010/136/10:09:13
711
Vector Time (MET): 001/15:49:04
756
Weight (LBS) : 244194
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6022972
80 A = 6724923
13 meter
Y = 2668100
20 meter E =
0007054
Z = -1332219
24 I = 51
84757
XDOT = -885
035441 Wp = 16
16047
YDOT = 4918
232353 meter/sec RA = 33
03413 deg
ZDOT = 5862
744096 TA = 329
23937
MA = 329
28069
Ha = 185
372 n
mi
Hp = 181
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19760409
44 X = 5999161
74
Y = 8753609
59 feet Y = 2735319
72 meter
Z = -4370798
03 Z = -1303016
74
XDOT = -2903
659582 XDOT = -968
446722
YDOT = 16135
932916 feet/sec YDOT = 4907
868163 meter/sec
ZDOT = 19234
724725 ZDOT = 5858
242619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21626320
28 X = 6591702
42
Y = -636345
54 feet Y = -193958
12 meter
Z = -4254488
56 Z = -1296768
11
XDOT = 4191
438630 XDOT = 1277
550494
YDOT = 14282
675784 feet/sec YDOT = 4353
359579 meter/sec
ZDOT = 19216
791462 ZDOT = 5857
278038
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 00132U 10136
42558752
00020000 00000-0 20000-3 0 9071
2 00132 51
6446 33
5841 0003455 263
7272 96
3499 15
76292499 288
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10136
42558752 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 33
5841 deg
Eccentricity:
0003455
Arg of perigee: 263
7272 deg
Mean anomaly: 96
3499 deg
Mean motion: 15
76292499 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 28
Checksum: 281
Coasting Arc #9 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2010/136/11:40:22
144
Vector Time (MET): 001/17:20:13
189
Weight (LBS) : 243973
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6045443
17 A = 6729716
24 meter
Y = 2589168
11 meter E =
0013638
Z = -1385126
90 I = 51
84734
XDOT = -785
538448 Wp = 359
66814
YDOT = 4956
029263 meter/sec RA = 32
70845 deg
ZDOT = 5848
675613 TA = 345
13812
MA = 345
17817
Ha = 189
664 n
mi
Hp = 184
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19834131
14 X = 6022770
09
Y = 8494646
03 feet Y = 2656645
27 meter
Z = -4544379
60 Z = -1355812
49
XDOT = -2577
225878 XDOT = -869
311423
YDOT = 16259
938527 feet/sec YDOT = 4946
775686 meter/sec
ZDOT = 19188
568285 ZDOT = 5844
656628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19538445
78 X = 5955318
27
Y = -9211321
08 feet Y = -2807610
67 meter
Z = -4427624
19 Z = -1349539
85
XDOT = 9701
288105 XDOT = 2956
952615
YDOT = 11383
163013 feet/sec YDOT = 3469
588086 meter/sec
ZDOT = 19172
556354 ZDOT = 5843
795177
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 00132U 10136
48898303
00020000 00000-0 20000-3 0 9087
2 00132 51
6462 33
2575 0008502 321
2217 38
8335 15
74586226 297
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10136
48898303 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 33
2575 deg
Eccentricity:
0008502
Arg of perigee: 321
2217 deg
Mean anomaly: 38
8335 deg
Mean motion: 15
74586226 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 256
Coasting Arc #10 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2010/136/12:57:15
071
Vector Time (MET): 001/18:37:06
116
Weight (LBS) : 243887
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3843297
41 A = 6720795
18 meter
Y = -2251572
07 meter E =
0007590
Z = -5036459
80 I = 51
81211
XDOT = 5416
320480 Wp = 50
66408
YDOT = 5152
835073 meter/sec RA = 32
43300 deg
ZDOT = 1836
110982 TA = 236
96510
MA = 237
03804
Ha = 190
763 n
mi
Hp = 184
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12609243
47 X = 3892655
74
Y = -7387047
49 feet Y = -2208317
35 meter
Z = -16523818
24 Z = -5017669
26
XDOT = 17770
080314 XDOT = 5349
378395
YDOT = 16905
626879 feet/sec YDOT = 5213
029040 meter/sec
ZDOT = 6023
986161 ZDOT = 1862
261899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2006178
08 X = -611483
08
Y = -14560376
28 feet Y = -4438002
69 meter
Z = -16448974
21 Z = -5013647
34
XDOT = 21314
045683 XDOT = 6496
521124
YDOT = -9835
372400 feet/sec YDOT = -2997
821507 meter/sec
ZDOT = 6128
139197 ZDOT = 1867
856827
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 00132U 10136
55244717
00020000 00000-0 20000-3 0 9090
2 00132 51
6466 32
9317 0010574 318
9291 41
1075 15
74156891 309
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10136
55244717 = yrday
fracday
Element set: 909
Inclination: 51
6466 deg
RA of node: 32
9317 deg
Eccentricity:
0010574
Arg of perigee: 318
9291 deg
Mean anomaly: 41
1075 deg
Mean motion: 15
74156891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 30
Checksum: 251
Coasting Arc #11 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2010/137/12:57:31
246
Vector Time (MET): 002/18:37:22
291
Weight (LBS) : 243887
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4997479
41 A = 6730380
54 meter
Y = -4148853
01 meter E =
0003157
Z = -1767839
61 I = 51
81805
XDOT = 4344
042625 Wp = 321
20534
YDOT = -2800
394145 meter/sec RA = 27
33973 deg
ZDOT = -5700
135514 TA = 238
31265
MA = 238
34343
Ha = 190
858 n
mi
Hp = 184
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16395929
81 X = -4942126
86
Y = -13611722
48 feet Y = -4204428
06 meter
Z = -5799998
70 Z = -1791983
64
XDOT = 14252
108349 XDOT = 4402
724681
YDOT = -9187
644832 feet/sec YDOT = -2751
487578 meter/sec
ZDOT = -18701
232001 ZDOT = -5678
889862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18621008
65 X = -5675683
44
Y = 10307221
62 feet Y = 3141641
15 meter
Z = -5896160
39 Z = -1797149
69
XDOT = -2599
023413 XDOT = -792
182336
YDOT = -15359
395209 feet/sec YDOT = -4681
543660 meter/sec
ZDOT = -18616
603130 ZDOT = -5674
340634
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 00132U 10137
56818230
00020000 00000-0 20000-3 0 9101
2 00132 51
6464 27
7150 0010554 321
8995 38
1421 15
74137298 464
Satellite: SHUTTLE
Catalog Number: 00132
Epoch time: 10137
56818230 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 27
7150 deg
Eccentricity:
0010554
Arg of perigee: 321
8995 deg
Mean anomaly: 38
1421 deg
Mean motion: 15
74137298 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 46
Checksum: 247
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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