Date:
May 15th 2009
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2009/131/18:01:55 956 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
139/12:54:58
079 1
0 -0
6 1
0
007/18:53:02
123 -0
0 0
2 305
8
000/00:00:04
246 0
2 -0
8 301
7
139/13:31:38
687 0
6 -6
0 6
0
007/19:29:42
731 5
8 -0
0 305
8
000/00:00:25
462 1
3 0
1 297
9
139/15:03:31
887 87
2 -234
1 234
8
007/21:01:35
931 203
5 -0
1 305
9
000/00:02:27
862 78
4 19
0 160
2
Coasting Arc #1 (Orbit 35)
---------------------------------------
Vector Time (GMT): 2009/133/22:49:06
000
Vector Time (MET): 002/04:47:10
044
Weight (LBS) : 243996
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2032622
93 A = 6945634
26 meter
Y = 5815126
38 meter E =
0009124
Z = 3195367
50 I = 28
26759
XDOT = -6957
238471 Wp = 86
65009
YDOT = 2895
185135 meter/sec RA = 325
45772 deg
ZDOT = -838
871026 TA = 16
87505
MA = 16
84472
Ha = 305
053 n
mi
Hp = 302
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6668710
41 X = 1951923
52
Y = 19078498
61 feet Y = 5837404
76 meter
Z = 10483489
17 Z = 3205046
72
XDOT = -22825
585536 XDOT = -6985
020728
YDOT = 9498
638894 feet/sec YDOT = 2817
229996 meter/sec
ZDOT = -2752
201530 ZDOT = -872
736667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16004656
44 X = -4878219
28
Y = -12308931
85 feet Y = -3751762
43 meter
Z = 10521669
15 Z = 3207004
76
XDOT = 12939
752291 XDOT = 3944
036498
YDOT = -19302
748585 feet/sec YDOT = -5883
477769 meter/sec
ZDOT = -2884
528332 ZDOT = -879
204236
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 34933U 09025A 09133
99805789
00020000 00000-0 70000-3 0 9003
2 34933 28
4709 325
4202 0003111 301
6230 58
4211 15
00543360 360
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09133
99805789 = yrday
fracday
Element set: 900
Inclination: 28
4709 deg
RA of node: 325
4202 deg
Eccentricity:
0003111
Arg of perigee: 301
6230 deg
Mean anomaly: 58
4211 deg
Mean motion: 15
00543360 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 36
Checksum: 254
Coasting Arc #2 (Orbit 50)
---------------------------------------
Vector Time (GMT): 2009/134/22:53:50
136
Vector Time (MET): 003/04:51:54
180
Weight (LBS) : 243996
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -731021
74 A = 6947452
42 meter
Y = 6484341
11 meter E =
0010513
Z = 2365263
86 I = 28
25148
XDOT = -7160
561020 Wp = 108
41101
YDOT = 104
535095 meter/sec RA = 318
85110 deg
ZDOT = -2489
589600 TA = 25
54021
MA = 25
48831
Ha = 305
306 n
mi
Hp = 302
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2398365
30 X = -814966
48
Y = 21274085
01 feet Y = 6475696
79 meter
Z = 7760052
03 Z = 2361509
33
XDOT = -23492
654264 XDOT = -7149
103724
YDOT = 342
962910 feet/sec YDOT = 24
525851 meter/sec
ZDOT = -8167
944883 ZDOT = -2524
347936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10366827
11 X = -3159808
90
Y = -18737396
07 feet Y = -5711158
32 meter
Z = 7745717
57 Z = 2360894
72
XDOT = 17519
997241 XDOT = 5340
095159
YDOT = -13139
665717 feet/sec YDOT = -4004
970110 meter/sec
ZDOT = -8303
921006 ZDOT = -2531
035123
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 34933U 09025A 09134
99574022
00020000 00000-0 70000-3 0 9018
2 34933 28
4707 318
9117 0003145 313
1430 46
9051 15
00558742 518
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09134
99574022 = yrday
fracday
Element set: 901
Inclination: 28
4707 deg
RA of node: 318
9117 deg
Eccentricity:
0003145
Arg of perigee: 313
1430 deg
Mean anomaly: 46
9051 deg
Mean motion: 15
00558742 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 51
Checksum: 267
Coasting Arc #3 (Orbit 65)
---------------------------------------
Vector Time (GMT): 2009/135/22:58:29
086
Vector Time (MET): 004/04:56:33
130
Weight (LBS) : 243996
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3245920
63 A = 6949391
41 meter
Y = 6070279
28 meter E =
0010688
Z = 903092
23 I = 28
23857
XDOT = -6154
872949 Wp = 139
89870
YDOT = -2774
370657 meter/sec RA = 312
27383 deg
ZDOT = -3448
195374 TA = 24
14369
MA = 24
09363
Ha = 305
545 n
mi
Hp = 302
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10649345
89 X = -3317945
34
Y = 19915614
43 feet Y = 6033578
70 meter
Z = 2962901
00 Z = 887149
09
XDOT = -20193
152721 XDOT = -6106
641246
YDOT = -9102
265934 feet/sec YDOT = -2842
928040 meter/sec
ZDOT = -11312
976949 ZDOT = -3477
978975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3722808
96 X = -1134712
17
Y = -22283283
97 feet Y = -6791944
96 meter
Z = 2900861
43 Z = 884182
56
XDOT = 19870
447892 XDOT = 6056
512517
YDOT = -4818
730610 feet/sec YDOT = -1468
749090 meter/sec
ZDOT = -11429
654139 ZDOT = -3483
758582
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 34933U 09025A 09135
99341921
00020000 00000-0 70000-3 0 9020
2 34933 28
4704 312
4032 0003066 323
7276 36
3260 15
00544667 669
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09135
99341921 = yrday
fracday
Element set: 902
Inclination: 28
4704 deg
RA of node: 312
4032 deg
Eccentricity:
0003066
Arg of perigee: 323
7276 deg
Mean anomaly: 36
3260 deg
Mean motion: 15
00544667 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 66
Checksum: 270
Coasting Arc #4 (Orbit 80)
---------------------------------------
Vector Time (GMT): 2009/136/23:03:09
443
Vector Time (MET): 005/05:01:13
487
Weight (LBS) : 243996
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5148228
69 A = 6949458
18 meter
Y = 4589904
11 meter E =
0008100
Z = -805495
98 I = 28
21468
XDOT = -4173
271771 Wp = 176
87490
YDOT = -5287
814807 meter/sec RA = 305
70914 deg
ZDOT = -3474
000474 TA = 17
32783
MA = 17
30020
Ha = 305
738 n
mi
Hp = 302
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16890514
07 X = -5195258
17
Y = 15058740
51 feet Y = 4532070
72 meter
Z = -2642703
34 Z = -830620
07
XDOT = -13691
836518 XDOT = -4096
956218
YDOT = -17348
473775 feet/sec YDOT = -5334
055792 meter/sec
ZDOT = -11397
639349 ZDOT = -3494
089373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3320025
43 X = 1011943
75
Y = -22371963
96 feet Y = -6818974
61 meter
Z = -2740743
02 Z = -835378
47
XDOT = 19943
067388 XDOT = 6078
646940
YDOT = 4359
435973 feet/sec YDOT = 1328
756084 meter/sec
ZDOT = -11476
532306 ZDOT = -3498
047047
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 34933U 09025A 09136
99109708
00020000 00000-0 70000-3 0 9037
2 34933 28
4701 305
8946 0003043 332
7363 27
3221 15
00533385 817
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09136
99109708 = yrday
fracday
Element set: 903
Inclination: 28
4701 deg
RA of node: 305
8946 deg
Eccentricity:
0003043
Arg of perigee: 332
7363 deg
Mean anomaly: 27
3221 deg
Mean motion: 15
00533385 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 81
Checksum: 275
Coasting Arc #5 (Orbit 95)
---------------------------------------
Vector Time (GMT): 2009/137/23:07:44
241
Vector Time (MET): 006/05:05:48
285
Weight (LBS) : 243996
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6147179
77 A = 6947606
26 meter
Y = 2290051
75 meter E =
0004071
Z = -2279867
37 I = 28
17997
XDOT = -1630
720713 Wp = 225
66959
YDOT = -6938
507921 meter/sec RA = 299
12291 deg
ZDOT = -2572
342541 TA = 358
37052
MA = 358
37185
Ha = 305
917 n
mi
Hp = 302
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20167912
65 X = -6161255
38
Y = 7513293
15 feet Y = 2221231
85 meter
Z = -7479879
83 Z = -2309764
63
XDOT = -5350
133572 XDOT = -1540
515883
YDOT = -22764
133599 feet/sec YDOT = -6956
239059 meter/sec
ZDOT = -8439
444032 ZDOT = -2580
045993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9945280
62 X = 3031321
53
Y = -19040064
71 feet Y = -5803411
72 meter
Z = -7596723
38 Z = -2315481
29
XDOT = 17771
155160 XDOT = 5416
648093
YDOT = 12662
233948 feet/sec YDOT = 3859
448907 meter/sec
ZDOT = -8469
977136 ZDOT = -2581
649031
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 34933U 09025A 09137
98877132
00020000 00000-0 70000-3 0 9041
2 34933 28
4697 299
3858 0003087 341
9590 18
1045 15
00536356 961
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09137
98877132 = yrday
fracday
Element set: 904
Inclination: 28
4697 deg
RA of node: 299
3858 deg
Eccentricity:
0003087
Arg of perigee: 341
9590 deg
Mean anomaly: 18
1045 deg
Mean motion: 15
00536356 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 96
Checksum: 323
Coasting Arc #6 (Orbit 110)
---------------------------------------
Vector Time (GMT): 2009/138/23:12:21
900
Vector Time (MET): 007/05:10:25
943
Weight (LBS) : 243996
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6168826
17 A = 6945659
73 meter
Y = -495789
33 meter E =
0002654
Z = -3150891
65 I = 28
14861
XDOT = 1098
976250 Wp = 311
37779
YDOT = -7432
358566 meter/sec RA = 292
49752 deg
ZDOT = -978
377675 TA = 302
72351
MA = 302
74909
Ha = 306
069 n
mi
Hp = 301
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20238930
99 X = -6147517
06
Y = -1626605
42 feet Y = -564653
42 meter
Z = -10337571
04 Z = -3180808
41
XDOT = 3605
565126 XDOT = 1186
757292
YDOT = -24384
378499 feet/sec YDOT = -7419
578305 meter/sec
ZDOT = -3209
900507 ZDOT = -972
826008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15624398
44 X = 4762316
64
Y = -12872607
14 feet Y = -3923570
66 meter
Z = -10454650
01 Z = -3186577
32
XDOT = 13425
893475 XDOT = 4092
212331
YDOT = 18895
449462 feet/sec YDOT = 5759
332996 meter/sec
ZDOT = -3188
604257 ZDOT = -971
886578
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 34933U 09025A 09138
98644229
00020000 00000-0 70000-3 0 9052
2 34933 28
4693 292
8767 0003106 352
5506 7
5192 15
00553859 1111
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09138
98644229 = yrday
fracday
Element set: 905
Inclination: 28
4693 deg
RA of node: 292
8767 deg
Eccentricity:
0003106
Arg of perigee: 352
5506 deg
Mean anomaly: 7
5192 deg
Mean motion: 15
00553859 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 111
Checksum: 304
Coasting Arc #7 (Orbit 119)
---------------------------------------
Vector Time (GMT): 2009/139/12:55:00
202
Vector Time (MET): 007/18:53:04
246
Weight (LBS) : 243963
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4934766
97 A = 6945402
12 meter
Y = 3732270
71 meter E =
0011259
Z = 3140040
40 I = 28
14145
XDOT = -4112
909787 Wp = 79
62639
YDOT = 6291
180337 meter/sec RA = 288
69034 deg
ZDOT = -1005
565963 TA = 26
73128
MA = 26
67329
Ha = 305
831 n
mi
Hp = 301
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16190180
36 X = 4877411
38
Y = 12244982
65 feet Y = 3787133
28 meter
Z = 10301969
81 Z = 3163874
71
XDOT = -13493
798513 XDOT = -4178
068221
YDOT = 20640
355437 feet/sec YDOT = 6244
823117 meter/sec
ZDOT = -3299
100930 ZDOT = -1025
704650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16962740
69 X = 5170243
36
Y = -11063111
76 feet Y = -3372036
46 meter
Z = 10395436
91 Z = 3168529
17
XDOT = 14088
851591 XDOT = 4294
281965
YDOT = 18402
423652 feet/sec YDOT = 5609
058729 meter/sec
ZDOT = -3377
534066 ZDOT = -1029
472383
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 34933U 09025A 09139
58503818
00020000 00000-0 70000-3 0 9068
2 34933 28
4696 288
9661 0003482 347
7269 12
3390 15
00649668 1200
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09139
58503818 = yrday
fracday
Element set: 906
Inclination: 28
4696 deg
RA of node: 288
9661 deg
Eccentricity:
0003482
Arg of perigee: 347
7269 deg
Mean anomaly: 12
3390 deg
Mean motion: 15
00649668 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 120
Checksum: 319
Coasting Arc #8 (Orbit 119)
---------------------------------------
Vector Time (GMT): 2009/139/13:31:51
418
Vector Time (MET): 007/19:29:55
462
Weight (LBS) : 243764
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6193511
76 A = 6942353
06 meter
Y = 1039931
81 meter E =
0003585
Z = -2963646
05 I = 28
14518
XDOT = -513
204780 Wp = 28
84922
YDOT = -7402
994083 meter/sec RA = 288
56943 deg
ZDOT = -1521
436014 TA = 215
93829
MA = 215
96241
Ha = 305
802 n
mi
Hp = 297
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20319920
46 X = -6190283
08
Y = 3411849
77 feet Y = 970690
57 meter
Z = -9723248
20 Z = -2993726
63
XDOT = -1683
742715 XDOT = -422
994148
YDOT = -24288
038330 feet/sec YDOT = -7408
228556 meter/sec
ZDOT = -4991
587972 ZDOT = -1523
710505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -318477
81 X = -97072
04
Y = 20545974
85 feet Y = 6262413
13 meter
Z = -9840880
63 Z = -2999500
42
XDOT = -22687
391594 XDOT = -6915
116958
YDOT = -2752
752045 feet/sec YDOT = -839
038823 meter/sec
ZDOT = -5000
911432 ZDOT = -1524
277804
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 34933U 09025A 09139
58503147
00020000 00000-0 70000-3 0 9074
2 34933 28
4704 288
9680 0006604 33
4993 326
6169 15
01775453 1201
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09139
58503147 = yrday
fracday
Element set: 907
Inclination: 28
4704 deg
RA of node: 288
9680 deg
Eccentricity:
0006604
Arg of perigee: 33
4993 deg
Mean anomaly: 326
6169 deg
Mean motion: 15
01775453 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 120
Checksum: 306
Coasting Arc #9 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2009/139/15:04:45
818
Vector Time (MET): 007/21:02:49
862
Weight (LBS) : 238184
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5985537
15 A = 6815376
32 meter
Y = 2306210
82 meter E =
0189765
Z = -2658968
67 I = 28
14985
XDOT = -1760
346935 Wp = 47
33773
YDOT = -6998
215110 meter/sec RA = 288
14900 deg
ZDOT = -2061
426112 TA = 186
92209
MA = 187
18791
Ha = 305
890 n
mi
Hp = 160
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19637589
08 X = -5997963
76
Y = 7566308
46 feet Y = 2239207
72 meter
Z = -8723650
49 Z = -2688076
86
XDOT = -5775
416452 XDOT = -1671
946707
YDOT = -22960
023327 feet/sec YDOT = -7017
405945 meter/sec
ZDOT = -6763
209028 ZDOT = -2069
763678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11731238
83 X = 3575681
60
Y = 17414485
37 feet Y = 5307935
14 meter
Z = -8837405
80 Z = -2693641
29
XDOT = -19840
440303 XDOT = -6047
366204
YDOT = 9841
484972 feet/sec YDOT = 2999
684619 meter/sec
ZDOT = -6796
231499 ZDOT = -2071
491361
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 34933U 09025A 09139
65109552
00020000 00000-0 70000-3 0 9085
2 34933 28
4708 288
5241 0194396 47
4108 314
2881 15
44221318 1211
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09139
65109552 = yrday
fracday
Element set: 908
Inclination: 28
4708 deg
RA of node: 288
5241 deg
Eccentricity:
0194396
Arg of perigee: 47
4108 deg
Mean anomaly: 314
2881 deg
Mean motion: 15
44221318 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 121
Checksum: 297
Coasting Arc #10 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2009/140/15:08:56
471
Vector Time (MET): 008/21:07:00
515
Weight (LBS) : 238184
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5677328
87 A = 6815194
07 meter
Y = -2172537
07 meter E =
0206470
Z = 2756340
54 I = 28
13568
XDOT = 1952
709782 Wp = 59
53096
YDOT = 7346
662077 meter/sec RA = 281
07192 deg
ZDOT = 1779
235887 TA = 1
60144
MA = 1
53633
Ha = 305
822 n
mi
Hp = 160
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18626407
05 X = 5687810
54
Y = -7127746
29 feet Y = -2108991
44 meter
Z = 9043112
01 Z = 2783946
83
XDOT = 6406
528157 XDOT = 1861
769673
YDOT = 24103
222038 feet/sec YDOT = 7367
989829 meter/sec
ZDOT = 5837
388082 ZDOT = 1788
501908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11657627
49 X = -3553244
86
Y = -16120936
98 feet Y = -4913661
59 meter
Z = 9150999
61 Z = 2789224
68
XDOT = 20483
475603 XDOT = 6243
363364
YDOT = -11497
612043 feet/sec YDOT = -3504
472151 meter/sec
ZDOT = 5874
063546 ZDOT = 1790
414569
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 34933U 09025A 09140
68520347
00020000 00000-0 70000-3 0 9090
2 34933 28
4706 281
3062 0194287 59
1948 302
7785 15
44109315 1376
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09140
68520347 = yrday
fracday
Element set: 909
Inclination: 28
4706 deg
RA of node: 281
3062 deg
Eccentricity:
0194287
Arg of perigee: 59
1948 deg
Mean anomaly: 302
7785 deg
Mean motion: 15
44109315 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 137
Checksum: 307
Coasting Arc #11 (Orbit 151)
---------------------------------------
Vector Time (GMT): 2009/141/15:13:09
720
Vector Time (MET): 009/21:11:13
764
Weight (LBS) : 238184
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5842754
54 A = 6814534
85 meter
Y = 2211972
08 meter E =
0191605
Z = -3033519
73 I = 28
12752
XDOT = -2005
138970 Wp = 70
28804
YDOT = -7106
078882 meter/sec RA = 273
98919 deg
ZDOT = -1333
553195 TA = 177
61009
MA = 177
51720
Ha = 306
127 n
mi
Hp = 159
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19169142
19 X = -5852318
32
Y = 7257126
26 feet Y = 2146581
77 meter
Z = -9952492
56 Z = -3061927
51
XDOT = -6578
539928 XDOT = -1919
050265
YDOT = -23313
907094 feet/sec YDOT = -7128
020059 meter/sec
ZDOT = -4375
174525 ZDOT = -1343
085853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12505309
71 X = 3811618
40
Y = 16171482
95 feet Y = 4929068
00 meter
Z = -10063516
79 Z = -3067359
92
XDOT = -19217
980130 XDOT = -5857
640344
YDOT = 12143
265822 feet/sec YDOT = 3701
267422 meter/sec
ZDOT = -4412
877731 ZDOT = -1345
045132
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 34933U 09025A 09141
65465780
00020000 00000-0 70000-3 0 9109
2 34933 28
4709 274
5374 0194336 70
2017 291
9592 15
44218912 1521
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09141
65465780 = yrday
fracday
Element set: 910
Inclination: 28
4709 deg
RA of node: 274
5374 deg
Eccentricity:
0194336
Arg of perigee: 70
2017 deg
Mean anomaly: 291
9592 deg
Mean motion: 15
44218912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 152
Checksum: 301
Coasting Arc #12 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2009/142/15:17:33
277
Vector Time (MET): 010/21:15:37
321
Weight (LBS) : 238184
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5583204
97 A = 6814398
85 meter
Y = -2036325
64 meter E =
0206329
Z = 3038537
00 I = 28
12387
XDOT = 2175
684208 Wp = 81
55662
YDOT = 7437
259685 meter/sec RA = 266
90609 deg
ZDOT = 946
629742 TA = 353
40357
MA = 353
67105
Ha = 305
976 n
mi
Hp = 159
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18317601
61 X = 5590799
52
Y = -6680858
40 feet Y = -1973848
86 meter
Z = 9968953
40 Z = 3065679
10
XDOT = 7138
071550 XDOT = 2087
759144
YDOT = 24400
458284 feet/sec YDOT = 7461
097737 meter/sec
ZDOT = 3105
740625 ZDOT = 956
986722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12263642
19 X = -3737958
14
Y = -15087911
04 feet Y = -4598795
29 meter
Z = 10075040
96 Z = 3070872
48
XDOT = 19650
741546 XDOT = 5989
546023
YDOT = -13784
811589 feet/sec YDOT = -4201
610572 meter/sec
ZDOT = 3146
684952 ZDOT = 959
109573
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 34933U 09025A 09142
68872829
00020000 00000-0 70000-3 0 9110
2 34933 28
4702 267
3206 0194293 81
9676 280
3086 15
44128976 1687
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09142
68872829 = yrday
fracday
Element set: 911
Inclination: 28
4702 deg
RA of node: 267
3206 deg
Eccentricity:
0194293
Arg of perigee: 81
9676 deg
Mean anomaly: 280
3086 deg
Mean motion: 15
44128976 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 168
Checksum: 328
Coasting Arc #13 (Orbit 182)
---------------------------------------
Vector Time (GMT): 2009/143/15:21:39
654
Vector Time (MET): 011/21:19:43
698
Weight (LBS) : 238184
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5797261
45 A = 6813991
55 meter
Y = 2021660
55 meter E =
0192637
Z = -3241267
79 I = 28
12767
XDOT = -2242
963002 Wp = 93
10128
YDOT = -7144
388572 meter/sec RA = 259
82016 deg
ZDOT = -505
151191 TA = 168
90707
MA = 168
47625
Ha = 306
176 n
mi
Hp = 159
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19019886
65 X = -5803691
26
Y = 6632744
59 feet Y = 1956796
70 meter
Z = -10634080
69 Z = -3269446
90
XDOT = -7358
802501 XDOT = -2160
452549
YDOT = -23439
595052 feet/sec YDOT = -7169
009281 meter/sec
ZDOT = -1657
320180 ZDOT = -515
848363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12992196
05 X = 3960021
35
Y = 15316569
66 feet Y = 4668490
43 meter
Z = -10744235
51 Z = -3274842
98
XDOT = -18125
985226 XDOT = -5524
800297
YDOT = 14321
386957 feet/sec YDOT = 4365
158744 meter/sec
ZDOT = -1699
576611 ZDOT = -518
030951
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 34933U 09025A 09143
65814486
00020000 00000-0 70000-3 0 9124
2 34933 28
4710 260
5513 0194324 92
9673 269
3351 15
44226314 1830
Satellite: SHUTTLE
Catalog Number: 34933
Epoch time: 09143
65814486 = yrday
fracday
Element set: 912
Inclination: 28
4710 deg
RA of node: 260
5513 deg
Eccentricity:
0194324
Arg of perigee: 92
9673 deg
Mean anomaly: 269
3351 deg
Mean motion: 15
44226314 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 183
Checksum: 295
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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