SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2011/189/15:29:03 960 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 99 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 52 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
200/07:50:09
711 2
8 0
0 3
0
010/16:21:05
751 0
6 0
0 214
1
000/00:00:11
501 0
9 3
0 205
2
200/08:18:17
126 -5
3 -7
0 7
0
010/16:49:13
165 -2
7 -0
0 211
3
000/00:00:26
331 -3
6 0
1 203
2
201/05:06:17
359 4
2 -7
0 7
0
011/13:37:13
398 3
2 -0
0 210
5
000/00:00:26
796 4
6 0
1 200
5
Coasting Arc #1 (Orbit 78)
---------------------------------------
Vector Time (GMT): 2011/194/13:08:02
000
Vector Time (MET): 004/21:38:58
040
Weight (LBS) : 216337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5128186
42 A = 6765061
23 meter
Y = 1127466
68 meter E =
0011597
Z = 4271176
69 I = 51
79207
XDOT = -4173
493997 Wp = 10
61696
YDOT = -5345
574493 meter/sec RA = 27
41519 deg
ZDOT = -3587
143877 TA = 115
95764
MA = 115
83811
Ha = 213
113 n
mi
Hp = 206
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16824758
60 X = -5161161
08
Y = 3699037
66 feet Y = 1069935
06 meter
Z = 14013046
88 Z = 4246184
48
XDOT = -13692
565608 XDOT = -4095
983168
YDOT = -17537
974058 feet/sec YDOT = -5391
811025 meter/sec
ZDOT = -11768
844741 ZDOT = -3607
231037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13187201
42 X = 4019458
99
Y = 11211161
19 feet Y = 3417161
93 meter
Z = 13911450
25 Z = 4240210
03
XDOT = -4883
861476 XDOT = -1488
600978
YDOT = 20500
950356 feet/sec YDOT = 6248
689669 meter/sec
ZDOT = -11850
086065 ZDOT = -3611
906233
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 37736U 11031A 11194
58873965
00020000 00000-0 20000-3 0 9008
2 37736 51
6371 27
7786 0011330 319
2320 40
7987 15
59857628 793
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11194
58873965 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 27
7786 deg
Eccentricity:
0011330
Arg of perigee: 319
2320 deg
Mean anomaly: 40
7987 deg
Mean motion: 15
59857628 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 79
Checksum: 327
Coasting Arc #2 (Orbit 94)
---------------------------------------
Vector Time (GMT): 2011/195/13:11:47
663
Vector Time (MET): 005/21:42:43
703
Weight (LBS) : 216337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6238378
47 A = 6772650
11 meter
Y = 2605635
45 meter E =
0017618
Z = 39234
29 I = 51
79055
XDOT = -1865
771089 Wp = 6
59556
YDOT = 4372
310467 meter/sec RA = 22
40749 deg
ZDOT = 6038
443352 TA = 353
82760
MA = 353
84928
Ha = 213
203 n
mi
Hp = 206
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20467120
98 X = 6208587
51
Y = 8548672
73 feet Y = 2675230
22 meter
Z = 128721
43 Z = 69467
76
XDOT = -6121
296225 XDOT = -1943
857479
YDOT = 14344
850613 feet/sec YDOT = 4351
008690 meter/sec
ZDOT = 19811
165853 ZDOT = 6029
190673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6316503
89 X = -1925270
39
Y = -21261185
54 feet Y = -6480409
35 meter
Z = 251363
70 Z = 76615
66
XDOT = 13509
665969 XDOT = 4117
746187
YDOT = -3774
851368 feet/sec YDOT = -1150
574697 meter/sec
ZDOT = 19773
287636 ZDOT = 6026
898072
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 37736U 11031A 11195
61377755
00020000 00000-0 20000-3 0 9010
2 37736 51
6372 22
6227 0011212 323
3647 36
6741 15
59887511 959
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11195
61377755 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 22
6227 deg
Eccentricity:
0011212
Arg of perigee: 323
3647 deg
Mean anomaly: 36
6741 deg
Mean motion: 15
59887511 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 95
Checksum: 295
Coasting Arc #3 (Orbit 109)
---------------------------------------
Vector Time (GMT): 2011/196/13:16:06
474
Vector Time (MET): 006/21:47:02
514
Weight (LBS) : 216337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2514776
85 A = 6764098
58 meter
Y = -4454180
62 meter E =
0013056
Z = -4435553
07 I = 51
73447
XDOT = 6892
005060 Wp = 11
88919
YDOT = -580
192037 meter/sec RA = 17
39509 deg
ZDOT = -3314
102003 TA = 224
66597
MA = 224
77121
Ha = 213
335 n
mi
Hp = 206
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8250580
21 X = -2443235
84
Y = -14613453
48 feet Y = -4481901
73 meter
Z = -14552339
47 Z = -4447596
44
XDOT = 22611
565158 XDOT = 6914
079568
YDOT = -1903
517181 feet/sec YDOT = -502
997537 meter/sec
ZDOT = -10873
038069 ZDOT = -3280
567914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5596093
70 X = -1705689
36
Y = 15776284
92 feet Y = 4808611
64 meter
Z = -14600967
43 Z = -4450374
87
XDOT = -15242
043380 XDOT = -4645
774822
YDOT = -15376
028972 feet/sec YDOT = -4686
613631 meter/sec
ZDOT = -10736
773466 ZDOT = -3272
568552
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 37736U 11031A 11196
57473890
00020000 00000-0 20000-3 0 9024
2 37736 51
6377 17
7904 0011198 327
8063 32
2408 15
59922529 1104
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11196
57473890 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 17
7904 deg
Eccentricity:
0011198
Arg of perigee: 327
8063 deg
Mean anomaly: 32
2408 deg
Mean motion: 15
59922529 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 110
Checksum: 304
Coasting Arc #4 (Orbit 125)
---------------------------------------
Vector Time (GMT): 2011/197/13:19:42
164
Vector Time (MET): 007/21:50:38
203
Weight (LBS) : 216337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3124789
26 A = 6762131
35 meter
Y = 3344971
39 meter E =
0013116
Z = 4981639
77 I = 51
69758
XDOT = -6688
347798 Wp = 358
92286
YDOT = -3138
298548 meter/sec RA = 12
31811 deg
ZDOT = -2075
358666 TA = 111
30580
MA = 111
16573
Ha = 213
588 n
mi
Hp = 206
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10251933
26 X = -3186160
43
Y = 10974315
58 feet Y = 3309684
34 meter
Z = 16343962
49 Z = 4966311
27
XDOT = -21943
398287 XDOT = -6642
676182
YDOT = -10296
255079 feet/sec YDOT = -3212
836105 meter/sec
ZDOT = -6808
919509 ZDOT = -2107
739295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15085586
58 X = 4598086
79
Y = 39678
67 feet Y = 12094
06 meter
Z = 16281472
62 Z = 4962592
86
XDOT = 7478
066515 XDOT = 2279
314674
YDOT = 21918
231473 feet/sec YDOT = 6680
676953 meter/sec
ZDOT = -6940
252366 ZDOT = -2115
388921
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 37736U 11031A 11197
59975339
00020000 00000-0 20000-3 0 9033
2 37736 51
6372 12
6340 0011110 331
3268 28
7275 15
59887362 1262
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11197
59975339 = yrday
fracday
Element set: 903
Inclination: 51
6372 deg
RA of node: 12
6340 deg
Eccentricity:
0011110
Arg of perigee: 331
3268 deg
Mean anomaly: 28
7275 deg
Mean motion: 15
59887362 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 126
Checksum: 301
Coasting Arc #5 (Orbit 140)
---------------------------------------
Vector Time (GMT): 2011/198/13:23:34
789
Vector Time (MET): 008/21:54:30
829
Weight (LBS) : 216337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6607926
67 A = 6771701
35 meter
Y = -272197
27 meter E =
0017030
Z = -1402744
05 I = 51
70198
XDOT = 1429
318249 Wp = 1
41086
YDOT = 4813
825830 meter/sec RA = 7
28346 deg
ZDOT = 5817
143526 TA = 343
25891
MA = 343
31506
Ha = 213
679 n
mi
Hp = 205
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21679549
44 X = 6617293
43
Y = -893035
66 feet Y = -198250
90 meter
Z = -4602178
65 Z = -1370620
81
XDOT = 4689
364335 XDOT = 1347
124952
YDOT = 15793
391832 feet/sec YDOT = 4829
349185 meter/sec
ZDOT = 19085
116556 ZDOT = 5823
887825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16013483
01 X = -4880909
62
Y = -14681722
14 feet Y = -4474988
91 meter
Z = -4471668
82 Z = -1362964
66
XDOT = 6830
846522 XDOT = 2082
042020
YDOT = -13252
886250 feet/sec YDOT = -4039
479729 meter/sec
ZDOT = 19112
198229 ZDOT = 5825
398020
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 37736U 11031A 11198
56069098
00020000 00000-0 20000-3 0 9048
2 37736 51
6389 7
8012 0011173 334
7878 25
2731 15
59938681 1412
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11198
56069098 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 7
8012 deg
Eccentricity:
0011173
Arg of perigee: 334
7878 deg
Mean anomaly: 25
2731 deg
Mean motion: 15
59938681 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 141
Checksum: 316
Coasting Arc #6 (Orbit 156)
---------------------------------------
Vector Time (GMT): 2011/199/13:27:22
911
Vector Time (MET): 009/21:58:18
951
Weight (LBS) : 216337
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5146543
86 A = 6767535
24 meter
Y = -2857209
41 meter E =
0010411
Z = -3350592
18 I = 51
65851
XDOT = 4982
944451 Wp = 3
45389
YDOT = -3494
031206 meter/sec RA = 2
28134 deg
ZDOT = -4664
913334 TA = 215
64830
MA = 215
71787
Ha = 213
765 n
mi
Hp = 205
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16884986
43 X = -5097935
29
Y = -9374046
61 feet Y = -2914489
14 meter
Z = -10992756
51 Z = -3375475
70
XDOT = 16348
242948 XDOT = 5044
305837
YDOT = -11463
356975 feet/sec YDOT = -3437
965418 meter/sec
ZDOT = -15304
833772 ZDOT = -4640
557971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5928163
20 X = 1806904
14
Y = 18319498
32 feet Y = 5583783
09 meter
Z = -11093650
19 Z = -3381344
58
XDOT = -18509
343535 XDOT = -5641
647909
YDOT = -3236
961713 feet/sec YDOT = -986
625930 meter/sec
ZDOT = -15205
673006 ZDOT = -4634
689132
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 37736U 11031A 11199
58567989
00020000 00000-0 20000-3 0 9054
2 37736 51
6390 2
6463 0011259 338
6902 21
3784 15
59967872 1579
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11199
58567989 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 2
6463 deg
Eccentricity:
0011259
Arg of perigee: 338
6902 deg
Mean anomaly: 21
3784 deg
Mean motion: 15
59967872 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 157
Checksum: 339
Coasting Arc #7 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2011/200/07:50:15
462
Vector Time (MET): 010/16:21:11
501
Weight (LBS) : 216261
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6271436
48 A = 6770490
28 meter
Y = -1482061
48 meter E =
0006913
Z = -2089743
99 I = 51
64714
XDOT = 2897
689220 Wp = 353
20379
YDOT = -4455
131819 meter/sec RA = 358
42833 deg
ZDOT = -5527
925980 TA = 209
95958
MA = 209
99915
Ha = 214
134 n
mi
Hp = 205
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20575578
99 X = -6244246
28
Y = -4862406
42 feet Y = -1552040
32 meter
Z = -6856115
46 Z = -2120144
08
XDOT = 9506
854395 XDOT = 2974
145127
YDOT = -14616
574209 feet/sec YDOT = -4422
300215 meter/sec
ZDOT = -18136
240091 ZDOT = -5513
663895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16113418
60 X = -4911369
99
Y = 13625271
86 feet Y = 4152982
86 meter
Z = -6979503
83 Z = -2127352
77
XDOT = -5048
684400 XDOT = -1538
839005
YDOT = -15245
224555 feet/sec YDOT = -4646
744444 meter/sec
ZDOT = -18078
020108 ZDOT = -5510
180529
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 37736U 11031A 11200
35440481
00020000 00000-0 20000-3 0 9060
2 37736 51
6409 358
7851 0012651 336
9388 23
1198 15
59962401 1697
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11200
35440481 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 358
7851 deg
Eccentricity:
0012651
Arg of perigee: 336
9388 deg
Mean anomaly: 23
1198 deg
Mean motion: 15
59962401 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 169
Checksum: 303
Coasting Arc #8 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2011/200/08:18:30
291
Vector Time (MET): 010/16:49:26
331
Weight (LBS) : 216057
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4544649
96 A = 6762304
68 meter
Y = -3191709
11 meter E =
0008213
Z = -3857711
89 I = 51
63099
XDOT = 5678
192696 Wp = 38
79447
YDOT = 3103
312759 meter/sec RA = 358
28403 deg
ZDOT = 4132
768291 TA = 274
51459
MA = 274
60840
Ha = 211
300 n
mi
Hp = 203
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14910268
88 X = 4598742
19
Y = -10471486
58 feet Y = -3140585
35 meter
Z = -12656535
08 Z = -3835503
26
XDOT = 18629
241129 XDOT = 5622
992998
YDOT = 10181
472308 feet/sec YDOT = 3166
500839 meter/sec
ZDOT = 13558
951085 ZDOT = 4160
218540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1773537
30 X = -540574
17
Y = -18196243
18 feet Y = -5546214
92 meter
Z = -12566118
31 Z = -3830152
86
XDOT = 16644
698712 XDOT = 5073
304167
YDOT = -11037
690874 feet/sec YDOT = -3364
288178 meter/sec
ZDOT = 13670
252446 ZDOT = 4166
692945
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 37736U 11031A 11200
35440548
00020000 00000-0 20000-3 0 9075
2 37736 51
6402 358
7838 0007991 353
8892 6
2165 15
61291781 1699
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11200
35440548 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 358
7838 deg
Eccentricity:
0007991
Arg of perigee: 353
8892 deg
Mean anomaly: 6
2165 deg
Mean motion: 15
61291781 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 169
Checksum: 310
Coasting Arc #9 (Orbit 182)
---------------------------------------
Vector Time (GMT): 2011/201/05:06:30
757
Vector Time (MET): 011/13:37:26
796
Weight (LBS) : 215882
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5473942
34 A = 6761551
73 meter
Y = 2815913
54 meter E =
0014353
Z = 2802815
31 I = 51
61597
XDOT = -4471
901502 Wp = 44
52320
YDOT = -3588
450988 meter/sec RA = 353
91922 deg
ZDOT = -5102
620116 TA = 103
56314
MA = 103
40321
Ha = 210
542 n
mi
Hp = 200
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17959128
41 X = -5518638
93
Y = 9238561
49 feet Y = 2754450
49 meter
Z = 9195588
27 Z = 2776114
96
XDOT = -14671
592855 XDOT = -4406
655204
YDOT = -11773
133162 feet/sec YDOT = -3638
093374 meter/sec
ZDOT = -16740
879646 ZDOT = -5124
185994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15364711
73 X = -4683164
14
Y = 13183058
23 feet Y = 4018196
15 meter
Z = 9086955
73 Z = 2769704
11
XDOT = -15952
167207 XDOT = -4862
220565
YDOT = -6933
365716 feet/sec YDOT = -2113
289870 meter/sec
ZDOT = -16828
245066 ZDOT = -5129
249096
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 37736U 11031A 11201
25046353
00020000 00000-0 20000-3 0 9082
2 37736 51
6413 354
2690 0012995 346
1810 13
8990 15
62594567 1838
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11201
25046353 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 354
2690 deg
Eccentricity:
0012995
Arg of perigee: 346
1810 deg
Mean anomaly: 13
8990 deg
Mean motion: 15
62594567 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 183
Checksum: 296
Coasting Arc #10 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2011/202/05:09:20
265
Vector Time (MET): 012/13:40:16
305
Weight (LBS) : 215882
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6219566
35 A = 6762067
18 meter
Y = 796580
40 meter E =
0019661
Z = 2495827
75 I = 51
58844
XDOT = -2752
903467 Wp = 33
49970
YDOT = 4833
665911 meter/sec RA = 348
90089 deg
ZDOT = 5313
662019 TA = 354
66220
MA = 354
68312
Ha = 210
636 n
mi
Hp = 200
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20405401
42 X = 6198072
47
Y = 2613452
77 feet Y = 866011
04 meter
Z = 8188411
24 Z = 2525989
83
XDOT = -9031
835521 XDOT = -2832
562309
YDOT = 15858
483961 feet/sec YDOT = 4802
435526 meter/sec
ZDOT = 17433
274339 ZDOT = 5300
095421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20330387
33 X = 6196702
06
Y = -2804543
51 feet Y = -854824
86 meter
Z = 8310866
85 Z = 2533152
22
XDOT = -4872
062867 XDOT = -1485
004762
YDOT = 16215
181960 feet/sec YDOT = 4942
387461 meter/sec
ZDOT = 17377
862044 ZDOT = 5296
772351
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 37736U 11031A 11202
27370694
00020000 00000-0 20000-3 0 9094
2 37736 51
6419 349
1020 0013200 349
9726 10
1165 15
62600199 1991
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11202
27370694 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 349
1020 deg
Eccentricity:
0013200
Arg of perigee: 349
9726 deg
Mean anomaly: 10
1165 deg
Mean motion: 15
62600199 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 199
Checksum: 281
Coasting Arc #11 (Orbit 213)
---------------------------------------
Vector Time (GMT): 2011/203/05:12:05
989
Vector Time (MET): 013/13:43:02
028
Weight (LBS) : 215882
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1395421
95 A = 6752656
11 meter
Y = -3972812
04 meter E =
0018930
Z = -5290796
31 I = 51
52774
XDOT = 7320
393241 Wp = 44
25952
YDOT = -2289
103667 meter/sec RA = 343
81675 deg
ZDOT = -198
992944 TA = 223
76694
MA = 223
91715
Ha = 210
747 n
mi
Hp = 199
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4578156
00 X = -1325192
03
Y = -13034160
23 feet Y = -3988023
44 meter
Z = -17358255
61 Z = -5297404
90
XDOT = 24017
038193 XDOT = 7346
413034
YDOT = -7510
182635 feet/sec YDOT = -2207
097072 meter/sec
ZDOT = -652
863991 ZDOT = -163
367820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8059928
39 X = -2456666
17
Y = -11178672
65 feet Y = -3407259
42 meter
Z = -17384841
54 Z = -5298899
70
XDOT = 19997
245809 XDOT = 6095
160523
YDOT = -13562
624704 feet/sec YDOT = -4133
888010 meter/sec
ZDOT = -508
027857 ZDOT = -154
846891
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 37736U 11031A 11203
23298994
00020000 00000-0 20000-3 0 9105
2 37736 51
6420 344
2585 0013234 353
0055 7
0915 15
62653026 2146
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11203
23298994 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 344
2585 deg
Eccentricity:
0013234
Arg of perigee: 353
0055 deg
Mean anomaly: 7
0915 deg
Mean motion: 15
62653026 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 214
Checksum: 267
Coasting Arc #12 (Orbit 229)
---------------------------------------
Vector Time (GMT): 2011/204/05:14:32
073
Vector Time (MET): 014/13:45:28
112
Weight (LBS) : 215882
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4465336
12 A = 6761195
83 meter
Y = 4188605
82 meter E =
0016744
Z = 2873009
89 I = 51
52726
XDOT = -5345
178276 Wp = 48
00146
YDOT = -2219
031963 meter/sec RA = 338
72638 deg
ZDOT = -5042
629280 TA = 99
13680
MA = 98
94733
Ha = 210
962 n
mi
Hp = 199
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14650052
89 X = -4525798
49
Y = 13742145
07 feet Y = 4138333
41 meter
Z = 9425885
48 Z = 2851170
97
XDOT = -17536
674133 XDOT = -5295
471400
YDOT = -7280
288591 feet/sec YDOT = -2278
526657 meter/sec
ZDOT = -16544
059316 ZDOT = -5068
475375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9602747
19 X = -2926917
34
Y = 17689744
07 feet Y = 5391833
99 meter
Z = 9336922
35 Z = 2845893
93
XDOT = -17554
830200 XDOT = -5350
712245
YDOT = -689
734363 feet/sec YDOT = -210
231034 meter/sec
ZDOT = -16648
886333 ZDOT = -5074
580554
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 37736U 11031A 11204
25621613
00020000 00000-0 20000-3 0 9117
2 37736 51
6419 339
0918 0013295 357
0730 3
0347 15
62654768 2304
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11204
25621613 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 339
0918 deg
Eccentricity:
0013295
Arg of perigee: 357
0730 deg
Mean anomaly: 3
0347 deg
Mean motion: 15
62654768 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 230
Checksum: 277
Coasting Arc #13 (Orbit 245)
---------------------------------------
Vector Time (GMT): 2011/205/05:17:04
085
Vector Time (MET): 015/13:48:00
124
Weight (LBS) : 215882
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6249669
12 A = 6762245
89 meter
Y = -1021000
08 meter E =
0021853
Z = 2330474
71 I = 51
50270
XDOT = -1142
715988 Wp = 37
09443
YDOT = 5357
752175 meter/sec RA = 333
70162 deg
ZDOT = 5402
521032 TA = 349
09189
MA = 349
13921
Ha = 210
987 n
mi
Hp = 199
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20504163
79 X = 6249300
72
Y = -3349737
80 feet Y = -951114
76 meter
Z = 7645914
42 Z = 2360834
37
XDOT = -3749
068203 XDOT = -1228
786737
YDOT = 17577
927083 feet/sec YDOT = 5344
491858 meter/sec
ZDOT = 17724
806536 ZDOT = 5396
761217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18066759
51 X = 5506748
30
Y = -10165235
16 feet Y = -3098363
68 meter
Z = 7769277
83 Z = 2368075
88
XDOT = 1668
560960 XDOT = 508
577380
YDOT = 16517
141970 feet/sec YDOT = 5034
424873 meter/sec
ZDOT = 17701
071372 ZDOT = 5395
286554
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 37736U 11031A 11205
27943035
00020000 00000-0 20000-3 0 9126
2 37736 51
6414 333
9243 0013419
2647 359
8515 15
62659371 2466
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11205
27943035 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 333
9243 deg
Eccentricity:
0013419
Arg of perigee:
2647 deg
Mean anomaly: 359
8515 deg
Mean motion: 15
62659371 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 246
Checksum: 288
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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