Date:
September 15th 2006
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/252/15:14:54 972 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 16339
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
260/14:04:57
861 0
4 0
4 1
6
007/22:50:02
889 -1
1 -0
0 189
6
000/00:00:05
778 -1
0 -1
5 180
4
260/14:32:56
832 -0
3 1
0 1
0
007/23:18:01
861 0
7 0
0 190
2
000/00:00:03
721 0
7 -0
0 180
6
260/16:14:54
972 -0
0 0
0 0
0
008/01:00:00
001 0
0 0
0 190
2
000/00:00:00
043 0
0 0
0 180
5
261/17:19:54
969 -0
9 -1
5 1
5
009/02:04:59
997 0
3 0
0 190
2
000/00:00:05
639 1
2 -0
0 179
6
Coasting Arc #1 (Orbit 79)
---------------------------------------
Vector Time (GMT): 2006/257/13:48:30
000
Vector Time (MET): 004/22:33:35
028
Weight (LBS) : 209983
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2506725
00 A = 6721559
12 meter
Y = 5071731
17 meter E =
0012637
Z = 3613750
28 I = 51
94613
XDOT = -3801
806192 Wp = 41
04140
YDOT = -5036
023333 meter/sec RA = 86
29934 deg
ZDOT = 4431
311422 TA = 2
08693
MA = 2
08166
Ha = 189
401 n
mi
Hp = 180
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8224163
38 X = -2580866
53
Y = 16639537
97 feet Y = 5043254
54 meter
Z = 11856136
08 Z = 3601392
78
XDOT = -12473
117427 XDOT = -3766
676142
YDOT = -16522
386264 feet/sec YDOT = -5078
386134 meter/sec
ZDOT = 14538
423300 ZDOT = 4412
927301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2163561
95 X = 659453
68
Y = -18463557
91 feet Y = -5627692
45 meter
Z = 11810803
49 Z = 3599932
91
XDOT = 16060
993307 XDOT = 4895
390760
YDOT = 11136
364300 feet/sec YDOT = 3394
363839 meter/sec
ZDOT = 14469
257765 ZDOT = 4410
229767
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 29391U 06036A 06257
63118200
00014500 00000-0 95600-4 0 9006
2 29391 51
6296 86
6955 0011031 340
5597 19
5145 15
75743805 801
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06257
63118200 = yrday
fracday
Element set: 900
Inclination: 51
6296 deg
RA of node: 86
6955 deg
Eccentricity:
0011031
Arg of perigee: 340
5597 deg
Mean anomaly: 19
5145 deg
Mean motion: 15
75743805 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 80
Checksum: 295
Coasting Arc #2 (Orbit 94)
---------------------------------------
Vector Time (GMT): 2006/258/13:53:16
349
Vector Time (MET): 005/22:38:21
377
Weight (LBS) : 209983
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2476914
33 A = 6725557
79 meter
Y = 5927813
23 meter E =
0016073
Z = -1956886
84 I = 51
95767
XDOT = -3922
126162 Wp = 5
17086
YDOT = 3495
192053 meter/sec RA = 81
11120 deg
ZDOT = 5642
459540 TA = 333
11470
MA = 333
19790
Ha = 189
531 n
mi
Hp = 180
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8126359
35 X = 2419879
83
Y = 19448206
13 feet Y = 5955221
83 meter
Z = -6420232
41 Z = -1944992
27
XDOT = -12867
867987 XDOT = -3988
369445
YDOT = 11467
165529 feet/sec YDOT = 3450
914878 meter/sec
ZDOT = 18512
006366 ZDOT = 5623
245190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14847573
55 X = -4525540
42
Y = -14979895
60 feet Y = -4565872
18 meter
Z = -6375116
47 Z = -1943135
50
XDOT = 6642
766074 XDOT = 2024
715099
YDOT = -14405
134167 feet/sec YDOT = -4390
684894 meter/sec
ZDOT = 18440
910433 ZDOT = 5620
789500
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 29391U 06036A 06258
58247286
00014500 00000-0 95600-4 0 9019
2 29391 51
6308 81
7968 0011026 344
6751 15
4078 15
75748097 950
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06258
58247286 = yrday
fracday
Element set: 901
Inclination: 51
6308 deg
RA of node: 81
7968 deg
Eccentricity:
0011026
Arg of perigee: 344
6751 deg
Mean anomaly: 15
4078 deg
Mean motion: 15
75748097 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 95
Checksum: 327
Coasting Arc #3 (Orbit 110)
---------------------------------------
Vector Time (GMT): 2006/259/13:58:04
449
Vector Time (MET): 006/22:43:09
477
Weight (LBS) : 209983
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4121143
98 A = 6715051
40 meter
Y = -576244
85 meter E =
0016261
Z = -5280656
50 I = 51
91728
XDOT = 1554
117365 Wp = 51
95758
YDOT = 7525
860249 meter/sec RA = 75
98142 deg
ZDOT = 402
247820 TA = 221
78808
MA = 221
91236
Ha = 189
620 n
mi
Hp = 180
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13520813
59 X = 4152939
95
Y = -1890567
10 feet Y = -529932
66 meter
Z = -17324988
53 Z = -5260558
92
XDOT = 5098
810253 XDOT = 1467
802754
YDOT = 24691
142549 feet/sec YDOT = 7542
774627 meter/sec
ZDOT = 1319
710695 ZDOT = 409
588303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11648541
52 X = -3550475
45
Y = 7299587
64 feet Y = 2224914
31 meter
Z = -17250199
20 Z = -5257860
72
XDOT = -14222
263677 XDOT = -4334
945969
YDOT = -19592
632536 feet/sec YDOT = -5971
834397 meter/sec
ZDOT = 1348
080784 ZDOT = 410
895023
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 29391U 06036A 06259
59716685
00014500 00000-0 95600-4 0 9026
2 29391 51
6312 76
5722 0011032 348
9002 11
1917 15
75792616 1118
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06259
59716685 = yrday
fracday
Element set: 902
Inclination: 51
6312 deg
RA of node: 76
5722 deg
Eccentricity:
0011032
Arg of perigee: 348
9002 deg
Mean anomaly: 11
1917 deg
Mean motion: 15
75792616 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 111
Checksum: 292
Coasting Arc #4 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2006/260/14:02:58
746
Vector Time (MET): 007/22:48:03
774
Weight (LBS) : 209983
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 37917
23 A = 6723984
06 meter
Y = -6190772
75 meter E =
0008512
Z = -2638173
29 I = 51
93947
XDOT = 5141
529880 Wp = 17
10760
YDOT = 2271
352994 meter/sec RA = 70
85978 deg
ZDOT = -5252
399819 TA = 192
75362
MA = 192
77517
Ha = 189
700 n
mi
Hp = 180
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 124400
36 X = 120029
89
Y = -20310934
23 feet Y = -6189888
63 meter
Z = -8655424
17 Z = -2637789
77
XDOT = 16868
536352 XDOT = 5141
236399
YDOT = 7451
945519 feet/sec YDOT = 2328
908155 meter/sec
ZDOT = -17232
282872 ZDOT = -5227
423160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8871823
53 X = 2704131
81
Y = 18271573
69 feet Y = 5569175
66 meter
Z = -8654838
80 Z = -2637994
87
XDOT = -17175
556446 XDOT = -5235
109605
YDOT = 215
584265 feet/sec YDOT = 65
710084 meter/sec
ZDOT = -17138
925365 ZDOT = -5223
944451
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 29391U 06036A 06260
61184379
00014500 00000-0 95600-4 0 9031
2 29391 51
6311 71
3452 0011166 352
3560 7
7432 15
75815258 1274
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
61184379 = yrday
fracday
Element set: 903
Inclination: 51
6311 deg
RA of node: 71
3452 deg
Eccentricity:
0011166
Arg of perigee: 352
3560 deg
Mean anomaly: 7
7432 deg
Mean motion: 15
75815258 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 127
Checksum: 283
Coasting Arc #5 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2006/260/14:05:00
749
Vector Time (MET): 007/22:50:05
778
Weight (LBS) : 209945
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 662797
70 A = 6722654
05 meter
Y = -5854385
21 meter E =
0010451
Z = -3251183
46 I = 51
93437
XDOT = 5085
647863 Wp = 18
65182
YDOT = 3233
701590 meter/sec RA = 70
85541 deg
ZDOT = -4780
648977 TA = 199
20294
MA = 199
24237
Ha = 189
643 n
mi
Hp = 180
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2174533
13 X = 744076
15
Y = -19207300
56 feet Y = -5846510
54 meter
Z = -10666612
41 Z = -3247766
32
XDOT = 16685
196401 XDOT = 5072
294304
YDOT = 10609
257185 feet/sec YDOT = 3290
558070 meter/sec
ZDOT = -15684
543889 ZDOT = -4755
975492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6696532
90 X = 2041103
23
Y = 18140007
05 feet Y = 5529074
15 meter
Z = -10654679
76 Z = -3247546
39
XDOT = -18433
816086 XDOT = -5618
627143
YDOT = -2363
770178 feet/sec YDOT = -720
477150 meter/sec
ZDOT = -15592
184723 ZDOT = -4752
497904
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 29391U 06036A 06260
61184680
00014500 00000-0 95600-4 0 9047
2 29391 51
6313 71
3454 0010506 353
3041 6
7981 15
75735585 1272
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
61184680 = yrday
fracday
Element set: 904
Inclination: 51
6313 deg
RA of node: 71
3454 deg
Eccentricity:
0010506
Arg of perigee: 353
3041 deg
Mean anomaly: 6
7981 deg
Mean motion: 15
75735585 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 127
Checksum: 287
Coasting Arc #6 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2006/260/14:32:58
693
Vector Time (MET): 007/23:18:03
721
Weight (LBS) : 209921
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3954024
65 A = 6724427
13 meter
Y = 4650830
97 meter E =
0013663
Z = -2803854
20 I = 51
93912
XDOT = -2456
859209 Wp = 10
03647
YDOT = 5182
318092 meter/sec RA = 70
70771 deg
ZDOT = 5148
246653 TA = 317
95030
MA = 318
05508
Ha = 190
189 n
mi
Hp = 180
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12972521
82 X = 3915289
11
Y = 15258631
78 feet Y = 4694877
42 meter
Z = -9198996
73 Z = -2784739
72
XDOT = -8060
561709 XDOT = -2539
696439
YDOT = 17002
355946 feet/sec YDOT = 5154
351094 meter/sec
ZDOT = 16890
573010 ZDOT = 5136
110238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19320235
37 X = -5888807
74
Y = -5399747
47 feet Y = -1645843
03 meter
Z = -9127153
97 Z = -2781956
53
XDOT = -3110
659097 XDOT = -948
128893
YDOT = -17250
533041 feet/sec YDOT = -5257
962471 meter/sec
ZDOT = 16846
065957 ZDOT = 5134
680904
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 29391U 06036A 06260
61184671
00014500 00000-0 95600-4 0 9058
2 29391 51
6322 71
3457 0011213 351
4044 8
6926 15
75536357 1279
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
61184671 = yrday
fracday
Element set: 905
Inclination: 51
6322 deg
RA of node: 71
3457 deg
Eccentricity:
0011213
Arg of perigee: 351
4044 deg
Mean anomaly: 8
6926 deg
Mean motion: 15
75536357 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 127
Checksum: 285
Coasting Arc #7 (Orbit 128)
---------------------------------------
Vector Time (GMT): 2006/260/16:14:54
994
Vector Time (MET): 008/01:00:00
022
Weight (LBS) : 209920
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1555101
32 A = 6727457
18 meter
Y = 6468291
41 meter E =
0021305
Z = 903770
15 I = 51
95018
XDOT = -4855
836520 Wp = 26
35084
YDOT = 326
514659 meter/sec RA = 70
37778 deg
ZDOT = 5983
866835 TA = 343
49198
MA = 343
56124
Ha = 190
169 n
mi
Hp = 180
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5102038
45 X = 1478188
84
Y = 21221428
50 feet Y = 6485269
43 meter
Z = 2965125
18 Z = 911138
07
XDOT = -15931
222178 XDOT = -4888
198273
YDOT = 1071
242321 feet/sec YDOT = 271
974901 meter/sec
ZDOT = 19632
109038 ZDOT = 5960
198799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20861566
52 X = -6358605
48
Y = -6403597
51 feet Y = -1951816
52 meter
Z = 2993454
98 Z = 912405
08
XDOT = 6760
957930 XDOT = 2060
739977
YDOT = -12837
064383 feet/sec YDOT = -3912
737224 meter/sec
ZDOT = 19543
980272 ZDOT = 5957
005187
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 29391U 06036A 06260
73870124
00014500 00000-0 95600-4 0 9067
2 29391 51
6337 70
6935 0011304 351
8456 8
2523 15
75536393 1291
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06260
73870124 = yrday
fracday
Element set: 906
Inclination: 51
6337 deg
RA of node: 70
6935 deg
Eccentricity:
0011304
Arg of perigee: 351
8456 deg
Mean anomaly: 8
2523 deg
Mean motion: 15
75536393 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 129
Checksum: 296
Coasting Arc #8 (Orbit 143)
---------------------------------------
Vector Time (GMT): 2006/261/16:14:58
228
Vector Time (MET): 009/01:00:03
257
Weight (LBS) : 209920
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4389942
23 A = 6716478
44 meter
Y = -14406
80 meter E =
0014928
Z = -5091759
40 I = 51
90282
XDOT = 1926
457151 Wp = 55
89205
YDOT = 7265
842505 meter/sec RA = 65
22858 deg
ZDOT = 1651
977673 TA = 229
87057
MA = 230
00146
Ha = 190
269 n
mi
Hp = 180
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14402697
59 X = 4414511
26
Y = -47266
41 feet Y = 34873
78 meter
Z = -16705247
39 Z = -5070373
58
XDOT = 6320
397477 XDOT = 1836
954567
YDOT = 23838
065962 feet/sec YDOT = 7286
907204 meter/sec
ZDOT = 5419
874255 ZDOT = 1661
118906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7105687
93 X = -2165813
68
Y = 12633473
03 feet Y = 3850682
58 meter
Z = -16625576
10 Z = -5067475
59
XDOT = -22919
286587 XDOT = -6985
798552
YDOT = -5762
659031 feet/sec YDOT = -1756
458473 meter/sec
ZDOT = 5454
921171 ZDOT = 1662
659973
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 29391U 06036A 06261
69010570
00014500 00000-0 95600-4 0 9075
2 29391 51
6337 65
7965 0011328 355
3884 4
7174 15
75589685 1441
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06261
69010570 = yrday
fracday
Element set: 907
Inclination: 51
6337 deg
RA of node: 65
7965 deg
Eccentricity:
0011328
Arg of perigee: 355
3884 deg
Mean anomaly: 4
7174 deg
Mean motion: 15
75589685 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 144
Checksum: 324
Coasting Arc #9 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2006/261/17:19:57
789
Vector Time (MET): 009/02:05:02
817
Weight (LBS) : 209883
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2698818
66 A = 6726909
55 meter
Y = -6161630
14 meter E =
0008229
Z = -199806
56 I = 51
93915
XDOT = 4416
984700 Wp = 61
51948
YDOT = -1744
288031 meter/sec RA = 65
01371 deg
ZDOT = -6054
149750 TA = 120
64158
MA = 120
56043
Ha = 190
236 n
mi
Hp = 179
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8854391
93 X = -2628673
50
Y = -20215321
97 feet Y = -6191449
36 meter
Z = -655533
32 Z = -212746
90
XDOT = 14491
419621 XDOT = 4465
591178
YDOT = -5722
729761 feet/sec YDOT = -1694
570188 meter/sec
ZDOT = -19862
696029 ZDOT = -6032
574167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21705666
08 X = 6615887
02
Y = -3982065
40 feet Y = -1213733
53 meter
Z = -704583
39 Z = -214757
02
XDOT = 1933
572975 XDOT = 589
353043
YDOT = 13940
798934 feet/sec YDOT = 4249
155515 meter/sec
ZDOT = -19782
553638 ZDOT = -6029
722349
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 29391U 06036A 06261
75352685
00014500 00000-0 95600-4 0 9089
2 29391 51
6329 65
4708 0012527 356
0617 4
0446 15
75842044 1455
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06261
75352685 = yrday
fracday
Element set: 908
Inclination: 51
6329 deg
RA of node: 65
4708 deg
Eccentricity:
0012527
Arg of perigee: 356
0617 deg
Mean anomaly: 4
0446 deg
Mean motion: 15
75842044 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 145
Checksum: 302
Coasting Arc #10 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2006/262/17:25:05
785
Vector Time (MET): 010/02:10:10
813
Weight (LBS) : 209883
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4779758
25 A = 6717657
60 meter
Y = -1034709
49 meter E =
0017934
Z = 4606918
17 I = 51
89575
XDOT = -1365
704499 Wp = 24
49844
YDOT = -6976
356977 meter/sec RA = 59
83983 deg
ZDOT = -2963
751524 TA = 94
88062
MA = 94
67583
Ha = 190
411 n
mi
Hp = 179
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15681621
54 X = -4790199
19
Y = -3394716
19 feet Y = -1088274
69 meter
Z = 15114560
93 Z = 4583672
94
XDOT = -4480
657805 XDOT = -1273
111851
YDOT = -22888
310293 feet/sec YDOT = -6991
127115 meter/sec
ZDOT = -9723
594239 ZDOT = -2970
161011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6334497
18 X = 1930754
74
Y = -14829906
49 feet Y = -4520155
50 meter
Z = 15027818
31 Z = 4580479
02
XDOT = 22230
972840 XDOT = 6776
000522
YDOT = -449
832816 feet/sec YDOT = -137
109042 meter/sec
ZDOT = -9748
425913 ZDOT = -2971
320218
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 29391U 06036A 06262
76816343
00014500 00000-0 95600-4 0 9098
2 29391 51
6336 60
2443 0012729 359
4829
6320 15
75891766 1614
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06262
76816343 = yrday
fracday
Element set: 909
Inclination: 51
6336 deg
RA of node: 60
2443 deg
Eccentricity:
0012729
Arg of perigee: 359
4829 deg
Mean anomaly:
6320 deg
Mean motion: 15
75891766 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 161
Checksum: 310
Coasting Arc #11 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2006/263/17:29:58
203
Vector Time (MET): 011/02:15:03
232
Weight (LBS) : 209883
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -583188
27 A = 6718531
49 meter
Y = 5079525
01 meter E =
0013573
Z = 4344694
16 I = 51
88315
XDOT = -5872
921970 Wp = 45
44501
YDOT = -3620
773992 meter/sec RA = 54
73707 deg
ZDOT = 3447
632519 TA = 9
94646
MA = 9
91962
Ha = 190
499 n
mi
Hp = 178
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1913347
36 X = -661110
98
Y = 16665108
31 feet Y = 5072560
54 meter
Z = 14254245
93 Z = 4341671
58
XDOT = -19268
116699 XDOT = -5848
701482
YDOT = -11879
179765 feet/sec YDOT = -3686
382537 meter/sec
ZDOT = 11311
130311 ZDOT = 3419
160937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16166456
73 X = -4927536
01
Y = -4509272
35 feet Y = -1374426
21 meter
Z = 14243679
30 Z = 4341473
45
XDOT = 14358
596501 XDOT = 4376
500213
YDOT = -16114
312738 feet/sec YDOT = -4911
642523 meter/sec
ZDOT = 11204
564270 ZDOT = 3415
151189
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 29391U 06036A 06263
78279111
00014500 00000-0 95600-4 0 9109
2 29391 51
6332 55
0183 0012699 3
4293 356
6956 15
75899669 1776
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06263
78279111 = yrday
fracday
Element set: 910
Inclination: 51
6332 deg
RA of node: 55
0183 deg
Eccentricity:
0012699
Arg of perigee: 3
4293 deg
Mean anomaly: 356
6956 deg
Mean motion: 15
75899669 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 177
Checksum: 333
Coasting Arc #12 (Orbit 191)
---------------------------------------
Vector Time (GMT): 2006/264/17:35:15
522
Vector Time (MET): 012/02:20:20
551
Weight (LBS) : 209883
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4701712
25 A = 6726718
74 meter
Y = 4749644
92 meter E =
0022979
Z = -633633
15 I = 51
89240
XDOT = -3002
256626 Wp = 21
98465
YDOT = 3763
823956 meter/sec RA = 49
55506 deg
ZDOT = 6026
235292 TA = 331
12587
MA = 331
25284
Ha = 190
784 n
mi
Hp = 178
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15425565
11 X = 4651272
49
Y = 15582824
55 feet Y = 4801995
74 meter
Z = -2078848
93 Z = -610914
95
XDOT = -9849
923313 XDOT = -3073
439917
YDOT = 12348
503794 feet/sec YDOT = 3729
817136 meter/sec
ZDOT = 19771
113163 ZDOT = 6011
477241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17220165
73 X = -5248706
51
Y = 13586231
30 feet Y = 4141083
30 meter
Z = -1993565
64 Z = -607638
81
XDOT = -10159
116075 XDOT = -3096
498580
YDOT = -10028
716036 feet/sec YDOT = -3056
752648 meter/sec
ZDOT = 19716
646702 ZDOT = 6009
633915
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 29391U 06036A 06264
73398647
00014500 00000-0 95600-4 0 9112
2 29391 51
6328 50
1193 0013066 7
1561 352
9787 15
75865110 1928
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06264
73398647 = yrday
fracday
Element set: 911
Inclination: 51
6328 deg
RA of node: 50
1193 deg
Eccentricity:
0013066
Arg of perigee: 7
1561 deg
Mean anomaly: 352
9787 deg
Mean motion: 15
75865110 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 192
Checksum: 308
Coasting Arc #13 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2006/265/17:40:25
082
Vector Time (MET): 013/02:25:30
111
Weight (LBS) : 209883
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4409359
64 A = 6716105
43 meter
Y = -1125740
65 meter E =
0017412
Z = -4948744
13 I = 51
83779
XDOT = 3971
973958 Wp = 57
27894
YDOT = 6236
339321 meter/sec RA = 44
39072 deg
ZDOT = 2135
020270 TA = 233
30192
MA = 233
46203
Ha = 190
801 n
mi
Hp = 178
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14466403
01 X = 4445673
18
Y = -3693374
82 feet Y = -1076177
20 meter
Z = -16236037
16 Z = -4927235
07
XDOT = 13031
410624 XDOT = 3891
496715
YDOT = 20460
430843 feet/sec YDOT = 6280
353113 meter/sec
ZDOT = 7004
659680 ZDOT = 2154
120445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2622698
34 X = 799398
46
Y = 14786136
79 feet Y = 4506814
49 meter
Z = -16156062
28 Z = -4924367
78
XDOT = -20274
486643 XDOT = -6179
663529
YDOT = 11275
869220 feet/sec YDOT = 3436
884938 meter/sec
ZDOT = 7076
662447 ZDOT = 2156
966714
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 29391U 06036A 06265
74857301
00014500 00000-0 95600-4 0 9122
2 29391 51
6328 44
8929 0013038 11
2261 348
9192 15
75939097 2086
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06265
74857301 = yrday
fracday
Element set: 912
Inclination: 51
6328 deg
RA of node: 44
8929 deg
Eccentricity:
0013038
Arg of perigee: 11
2261 deg
Mean anomaly: 348
9192 deg
Mean motion: 15
75939097 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 208
Checksum: 316
SPACE SHUTTLE ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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