Date:
May 12th 2009
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2009/131/18:01:49 000 Area (sq ft) : 1301 0 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
131/18:46:17
186 85
5 142
8 142
8
000/00:44:28
186 -107
4 -0
0 296
6
000/00:01:35
740 -39
5 0
0 108
3
131/21:50:27
904 12
6 21
0 21
0
000/03:48:38
904 -16
2 -1
0 296
7
000/00:01:32
213 -4
7 0
0 120
1
132/10:26:49
000 0
0 0
0 0
0
000/16:25:00
000 0
0 0
0 296
5
000/00:00:00
000 0
0 0
0 120
2
132/22:42:02
061 5
3 5
8 6
0
001/04:40:13
061 -0
5 -1
4 297
4
000/00:00:26
122 2
7 -0
1 122
5
133/12:18:38
246 210
4 308
4 308
4
001/18:16:49
246 -221
5 0
1 303
2
000/00:03:18
853 -42
2 0
5 297
1
133/13:03:35
837 -0
8 1
5 1
5
001/19:01:46
837 1
2 -0
0 303
1
000/00:00:06
627 0
3 0
0 298
0
133/14:41:57
797 -4
7 8
6 8
7
001/20:40:08
797 7
2 0
2 303
1
000/00:00:13
595 1
7 -1
4 303
0
133/16:02:00
382 -0
3 1
4 1
6
001/22:00:11
382 1
3 -0
2 304
2
000/00:00:06
763 0
8 0
7 303
2
133/16:14:58
768 -0
1 0
8 0
8
001/22:13:09
768 0
8 0
1 304
6
000/00:00:03
535 0
2 -0
3 303
2
133/16:28:27
000 -0
7 0
6 0
7
001/22:26:38
000 -0
2 -0
2 304
9
000/00:01:00
000 -0
1 0
4 303
2
133/16:54:49
000 0
0 0
0 0
0
001/22:53:00
000 0
0 0
0 304
9
000/00:00:00
000 0
0 0
0 303
2
139/12:54:21
122 0
9 -0
7 1
0
007/18:52:32
122 -0
2 0
0 305
8
000/00:01:04
243 0
4 -0
7 301
9
139/13:27:01
724 2
2 -6
0 6
0
007/19:25:12
724 5
2 -0
0 305
9
000/00:00:25
447 2
0 0
1 298
2
139/15:04:01
103 84
5 -234
8 235
5
007/21:02:12
103 205
8 -0
1 306
0
000/00:02:28
206 77
4 19
1 159
9
Coasting Arc #1 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2009/131/18:12:20
000
Vector Time (MET): 000/00:10:31
000
Weight (LBS) : 255991
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 524657
83 A = 6684321
94 meter
Y = 5741541
08 meter E =
0376430
Z = 3020006
39 I = 28
34523
XDOT = -7786
001098 Wp = 54
98391
YDOT = 1320
749005 meter/sec RA = 340
94273 deg
ZDOT = -697
994841 TA = 47
24646
MA = 44
13918
Ha = 296
543 n
mi
Hp = 28
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1721318
34 X = 445745
10
Y = 18837077
03 feet Y = 5746966
52 meter
Z = 9908157
45 Z = 3022364
23
XDOT = -25544
623024 XDOT = -7796
800477
YDOT = 4333
166028 feet/sec YDOT = 1233
621101 meter/sec
ZDOT = -2290
009322 ZDOT = -735
845858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10291471
68 X = 3136840
57
Y = -15864899
00 feet Y = -4835621
22 meter
Z = 9917690
37 Z = 3022912
02
XDOT = 21625
398405 XDOT = 6591
421434
YDOT = 11560
987947 feet/sec YDOT = 3523
789126 meter/sec
ZDOT = -2437
995852 ZDOT = -743
101136
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 00125U 09131
80320596
00020000 00000-0 70000-3 0 9009
2 00125 28
4705 340
7888 0129208 54
9545 306
3308 16
60555937 20
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09131
80320596 = yrday
fracday
Element set: 900
Inclination: 28
4705 deg
RA of node: 340
7888 deg
Eccentricity:
0129208
Arg of perigee: 54
9545 deg
Mean anomaly: 306
3308 deg
Mean motion: 16
60555937 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 266
Coasting Arc #2 (Orbit 1)
---------------------------------------
Vector Time (GMT): 2009/131/18:47:05
056
Vector Time (MET): 000/00:45:16
056
Weight (LBS) : 252413
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5222869
12 A = 6758544
56 meter
Y = -3612472
15 meter E =
0249974
Z = -2767368
41 I = 28
35405
XDOT = 4787
390731 Wp = 54
21748
YDOT = -5431
482942 meter/sec RA = 340
81827 deg
ZDOT = -1919
556656 TA = 183
04719
MA = 183
20236
Ha = 296
612 n
mi
Hp = 108
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17135397
38 X = -5168642
10
Y = -11851942
74 feet Y = -3670573
78 meter
Z = -9079292
70 Z = -2792610
20
XDOT = 15706
662504 XDOT = 4857
095668
YDOT = -17819
825925 feet/sec YDOT = -5377
557572 meter/sec
ZDOT = -6297
758058 ZDOT = -1896
130520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9094467
28 X = 2771993
63
Y = 18696920
19 feet Y = 5698821
27 meter
Z = -9178223
48 Z = -2797522
52
XDOT = -21087
270221 XDOT = -6427
399963
YDOT = 7169
760678 feet/sec YDOT = 2185
343055 meter/sec
ZDOT = -6206
417580 ZDOT = -1891
716078
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 00125U 09131
80473903
00020000 00000-0 70000-3 0 9011
2 00125 28
4715 340
8083 0254114 54
8021 307
6277 15
63694468 26
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09131
80473903 = yrday
fracday
Element set: 901
Inclination: 28
4715 deg
RA of node: 340
8083 deg
Eccentricity:
0254114
Arg of perigee: 54
8021 deg
Mean anomaly: 307
6277 deg
Mean motion: 15
63694468 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2
Checksum: 254
Coasting Arc #3 (Orbit 3)
---------------------------------------
Vector Time (GMT): 2009/131/21:51:14
010
Vector Time (MET): 000/03:49:25
010
Weight (LBS) : 251695
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5177595
30 A = 6769476
20 meter
Y = -3646579
73 meter E =
0233596
Z = -2807808
90 I = 28
34736
XDOT = 4834
483646 Wp = 55
71575
YDOT = -5422
307138 meter/sec RA = 339
89137 deg
ZDOT = -1850
348501 TA = 182
89352
MA = 183
03105
Ha = 296
676 n
mi
Hp = 120
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16986861
22 X = -5122793
80
Y = -11963844
27 feet Y = -3704171
87 meter
Z = -9211971
45 Z = -2832829
34
XDOT = 15861
166816 XDOT = 4903
746267
YDOT = -17789
721582 feet/sec YDOT = -5367
857628 meter/sec
ZDOT = -6070
697182 ZDOT = -1826
694674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19674843
29 X = 5996892
23
Y = 6539966
50 feet Y = 1993381
79 meter
Z = -9310038
75 Z = -2837699
81
XDOT = -9577
839339 XDOT = -2919
325430
YDOT = 20200
081714 feet/sec YDOT = 6156
984906 meter/sec
ZDOT = -5978
464768 ZDOT = -1822
236061
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 00125U 09131
93241972
00020000 00000-0 70000-3 0 9025
2 00125 28
4706 339
8879 0237561 56
2831 306
0350 15
59865209 44
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09131
93241972 = yrday
fracday
Element set: 902
Inclination: 28
4706 deg
RA of node: 339
8879 deg
Eccentricity:
0237561
Arg of perigee: 56
2831 deg
Mean anomaly: 306
0350 deg
Mean motion: 15
59865209 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4
Checksum: 276
Coasting Arc #4 (Orbit 11)
---------------------------------------
Vector Time (GMT): 2009/132/10:26:49
000
Vector Time (MET): 000/16:25:00
000
Weight (LBS) : 251695
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2002493
91 A = 6770076
03 meter
Y = -6015891
02 meter E =
0237017
Z = -2526780
02 I = 28
33409
XDOT = 7075
219787 Wp = 60
16100
YDOT = 1571
767980 meter/sec RA = 336
06375 deg
ZDOT = 2322
468126 TA = 248
57703
MA = 251
12171
Ha = 296
463 n
mi
Hp = 120
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6569861
92 X = 2081890
58
Y = -19737175
27 feet Y = -5993053
72 meter
Z = -8289960
70 Z = -2516859
68
XDOT = 23212
663343 XDOT = 7045
835900
YDOT = 5156
719094 feet/sec YDOT = 1650
722631 meter/sec
ZDOT = 7619
646084 ZDOT = 2356
768779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2801020
93 X = -853751
18
Y = -20627893
70 feet Y = -6287382
00 meter
Z = -8251478
95 Z = -2515050
79
XDOT = 21553
630663 XDOT = 6569
546626
YDOT = -5425
261486 feet/sec YDOT = -1653
619701 meter/sec
ZDOT = 7753
905584 ZDOT = 2363
390422
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 00125U 09132
44427325
00020000 00000-0 70000-3 0 9031
2 00125 28
4729 336
2351 0236772 62
1945 300
2623 15
59846350 124
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09132
44427325 = yrday
fracday
Element set: 903
Inclination: 28
4729 deg
RA of node: 336
2351 deg
Eccentricity:
0236772
Arg of perigee: 62
1945 deg
Mean anomaly: 300
2623 deg
Mean motion: 15
59846350 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 12
Checksum: 252
Coasting Arc #5 (Orbit 19)
---------------------------------------
Vector Time (GMT): 2009/132/22:42:15
122
Vector Time (MET): 001/04:40:26
122
Weight (LBS) : 251492
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 944739
55 A = 6772602
06 meter
Y = -6216310
65 meter E =
0233970
Z = -2731562
13 I = 28
31108
XDOT = 7296
742894 Wp = 65
47961
YDOT = 392
847487 meter/sec RA = 332
39212 deg
ZDOT = 2009
091737 TA = 237
36311
MA = 239
64228
Ha = 297
368 n
mi
Hp = 122
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3099539
20 X = 1027450
73
Y = -20394719
98 feet Y = -6205283
22 meter
Z = -8961818
00 Z = -2726772
40
XDOT = 23939
445190 XDOT = 7282
047793
YDOT = 1288
869708 feet/sec YDOT = 474
361508 meter/sec
ZDOT = 6591
508323 ZDOT = 2044
504028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7679620
30 X = 2340748
27
Y = 19154755
75 feet Y = 5838369
55 meter
Z = -8943416
14 Z = -2725953
24
XDOT = -19825
853978 XDOT = -6042
920293
YDOT = 10508
509868 feet/sec YDOT = 3202
993808 meter/sec
ZDOT = 6730
056414 ZDOT = 2051
321195
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 00125U 09132
95611183
00020000 00000-0 70000-3 0 9045
2 00125 28
4724 332
5702 0234647 67
2898 295
2507 15
58827124 200
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09132
95611183 = yrday
fracday
Element set: 904
Inclination: 28
4724 deg
RA of node: 332
5702 deg
Eccentricity:
0234647
Arg of perigee: 67
2898 deg
Mean anomaly: 295
2507 deg
Mean motion: 15
58827124 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 20
Checksum: 272
Coasting Arc #6 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2009/133/12:20:17
672
Vector Time (MET): 001/18:18:28
672
Weight (LBS) : 243952
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230278
53 A = 6938574
75 meter
Y = -4438089
42 meter E =
0014613
Z = -3226782
72 I = 28
28071
XDOT = 5706
868152 Wp = 253
25577
YDOT = -4960
703866 meter/sec RA = 328
35612 deg
ZDOT = -661
285803 TA = 6
15729
MA = 6
13935
Ha = 303
151 n
mi
Hp = 297
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13878866
57 X = -4164661
41
Y = -14560660
81 feet Y = -4485027
58 meter
Z = -10586557
48 Z = -3247174
74
XDOT = 18723
320709 XDOT = 5765
127862
YDOT = -16275
275152 feet/sec YDOT = -4896
560510 meter/sec
ZDOT = -2169
572846 ZDOT = -633
420701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19814994
46 X = -6039610
31
Y = 3209559
42 feet Y = 978273
71 meter
Z = -10666569
40 Z = -3251170
35
XDOT = -2653
602655 XDOT = -808
818089
YDOT = -23203
978971 feet/sec YDOT = -7072
572790 meter/sec
ZDOT = -2060
833758 ZDOT = -628
142130
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 00125U 09133
53252913
00020000 00000-0 70000-3 0 9053
2 00125 28
4709 328
4614 0013043 255
6716 104
2581 15
02793285 295
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09133
53252913 = yrday
fracday
Element set: 905
Inclination: 28
4709 deg
RA of node: 328
4614 deg
Eccentricity:
0013043
Arg of perigee: 255
6716 deg
Mean anomaly: 104
2581 deg
Mean motion: 15
02793285 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 255
Coasting Arc #7 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2009/133/13:03:39
150
Vector Time (MET): 001/19:01:50
150
Weight (LBS) : 243908
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5574226
11 A = 6940088
78 meter
Y = 2925997
65 meter E =
0000814
Z = 2919613
34 I = 28
28529
XDOT = -4098
102147 Wp = 85
38167
YDOT = 6157
773072 meter/sec RA = 328
17325 deg
ZDOT = 1652
431393 TA = 337
22296
MA = 337
22657
Ha = 303
124 n
mi
Hp = 297
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18288143
41 X = 5526909
76
Y = 9599729
81 feet Y = 2988066
98 meter
Z = 9578783
92 Z = 2946578
58
XDOT = -13445
217019 XDOT = -4174
682098
YDOT = 20202
667559 feet/sec YDOT = 6111
517321 meter/sec
ZDOT = 5421
362837 ZDOT = 1632
337386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16057883
62 X = 4894442
93
Y = -12912022
37 feet Y = -3935584
42 meter
Z = 9684428
49 Z = 2951813
81
XDOT = 12237
026999 XDOT = 3729
845829
YDOT = 19227
302227 feet/sec YDOT = 5860
481719 meter/sec
ZDOT = 5343
088353 ZDOT = 1628
573330
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 00125U 09133
59895199
00020000 00000-0 70000-3 0 9069
2 00125 28
4707 328
0262 0011679 257
8508 102
0929 15
02546321 305
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09133
59895199 = yrday
fracday
Element set: 906
Inclination: 28
4707 deg
RA of node: 328
0262 deg
Eccentricity:
0011679
Arg of perigee: 257
8508 deg
Mean anomaly: 102
0929 deg
Mean motion: 15
02546321 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 30
Checksum: 271
Coasting Arc #8 (Orbit 30)
---------------------------------------
Vector Time (GMT): 2009/133/14:42:04
595
Vector Time (MET): 001/20:40:15
595
Weight (LBS) : 243698
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4833109
13 A = 6944325
47 meter
Y = 3860946
11 meter E =
0007140
Z = 3144709
44 I = 28
27811
XDOT = -5091
168557 Wp = 77
69816
YDOT = 5519
506635 meter/sec RA = 327
71091 deg
ZDOT = 1047
032432 TA = 355
35044
MA = 355
35707
Ha = 303
141 n
mi
Hp = 303
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15856657
25 X = 4774299
62
Y = 12667146
04 feet Y = 3914663
56 meter
Z = 10317288
20 Z = 3168046
49
XDOT = -16703
308914 XDOT = -5157
596555
YDOT = 18108
617568 feet/sec YDOT = 5462
202672 meter/sec
ZDOT = 3435
145774 ZDOT = 1022
138653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12321358
53 X = 3755550
08
Y = -16067912
47 feet Y = -4897499
72 meter
Z = 10408790
34 Z = 3172599
30
XDOT = 17295
771176 XDOT = 5271
751055
YDOT = 15427
350534 feet/sec YDOT = 4702
256443 meter/sec
ZDOT = 3338
060148 ZDOT = 1017
440733
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 00125U 09133
66544442
00020000 00000-0 70000-3 0 9070
2 00125 28
4699 327
5885 0004860 271
2837 88
7351 15
00996181 310
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09133
66544442 = yrday
fracday
Element set: 907
Inclination: 28
4699 deg
RA of node: 327
5885 deg
Eccentricity:
0004860
Arg of perigee: 271
2837 deg
Mean anomaly: 88
7351 deg
Mean motion: 15
00996181 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 31
Checksum: 287
Coasting Arc #9 (Orbit 31)
---------------------------------------
Vector Time (GMT): 2009/133/16:02:03
763
Vector Time (MET): 001/22:00:14
763
Weight (LBS) : 243654
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6460291
59 A = 6948832
70 meter
Y = -2411513
68 meter E =
0012580
Z = 784013
03 I = 28
30605
XDOT = 1977
047184 Wp = 19
39984
YDOT = 6434
426798 meter/sec RA = 327
34330 deg
ZDOT = 3492
205122 TA = 354
38273
MA = 354
39683
Ha = 304
205 n
mi
Hp = 303
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21195182
37 X = 6482968
77
Y = -7911790
29 feet Y = -2339144
23 meter
Z = 2572221
24 Z = 815452
17
XDOT = 6486
375274 XDOT = 1887
984770
YDOT = 21110
324141 feet/sec YDOT = 6456
036897 meter/sec
ZDOT = 11457
365885 ZDOT = 3501
594136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15063560
15 X = -4591373
13
Y = -16860433
04 feet Y = -5139059
99 meter
Z = 2695080
14 Z = 821460
43
XDOT = 16108
063306 XDOT = 4909
737696
YDOT = -12549
895049 feet/sec YDOT = -3825
208011 meter/sec
ZDOT = 11494
442892 ZDOT = 3503
506193
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 00125U 09133
73194858
00020000 00000-0 70000-3 0 9081
2 00125 28
4714 327
1543 0004239 284
4462 75
5812 15
00740284 323
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09133
73194858 = yrday
fracday
Element set: 908
Inclination: 28
4714 deg
RA of node: 327
1543 deg
Eccentricity:
0004239
Arg of perigee: 284
4462 deg
Mean anomaly: 75
5812 deg
Mean motion: 15
00740284 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 32
Checksum: 261
Coasting Arc #10 (Orbit 31)
---------------------------------------
Vector Time (GMT): 2009/133/16:15:00
535
Vector Time (MET): 001/22:13:11
535
Weight (LBS) : 243631
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5628067
08 A = 6946075
80 meter
Y = 2825470
59 meter E =
0009424
Z = 2915249
76 I = 28
28131
XDOT = -3988
815336 Wp = 63
96179
YDOT = 6230
782272 meter/sec RA = 327
29525 deg
ZDOT = 1661
307112 TA = 358
49280
MA = 358
49564
Ha = 304
615 n
mi
Hp = 303
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18464787
02 X = 5581892
04
Y = 9269916
63 feet Y = 2888148
39 meter
Z = 9564467
73 Z = 2942479
31
XDOT = -13086
664488 XDOT = -4066
262924
YDOT = 20442
199055 feet/sec YDOT = 6185
743779 meter/sec
ZDOT = 5450
482651 ZDOT = 1641
741929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 786642
27 X = 239768
56
Y = -20596333
89 feet Y = -6277762
57 meter
Z = 9671141
67 Z = 2947763
98
XDOT = 22542
178807 XDOT = 6870
856100
YDOT = 3385
169704 feet/sec YDOT = 1031
799726 meter/sec
ZDOT = 5374
280555 ZDOT = 1638
080713
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 00125U 09133
73195472
00020000 00000-0 70000-3 0 9095
2 00125 28
4710 327
1534 0003932 291
4754 68
5571 15
00605010 321
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09133
73195472 = yrday
fracday
Element set: 909
Inclination: 28
4710 deg
RA of node: 327
1534 deg
Eccentricity:
0003932
Arg of perigee: 291
4754 deg
Mean anomaly: 68
5571 deg
Mean motion: 15
00605010 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 32
Checksum: 243
Coasting Arc #11 (Orbit 31)
---------------------------------------
Vector Time (GMT): 2009/133/16:28:57
000
Vector Time (MET): 001/22:27:08
000
Weight (LBS) : 243611
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 547233
78 A = 6946392
36 meter
Y = 6243116
41 meter E =
0009044
Z = 2982119
25 I = 28
27985
XDOT = -7302
818769 Wp = 97
75370
YDOT = 1364
844174 meter/sec RA = 327
17785 deg
ZDOT = -1512
514909 TA = 17
16407
MA = 17
13350
Ha = 304
914 n
mi
Hp = 303
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1795386
40 X = 462894
82
Y = 20482665
40 feet Y = 6248763
98 meter
Z = 9783855
80 Z = 2984573
63
XDOT = -23959
379165 XDOT = -7310
190343
YDOT = 4477
835218 feet/sec YDOT = 1283
138761 meter/sec
ZDOT = -4962
319255 ZDOT = -1548
010018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17262069
33 X = 5261478
73
Y = -11161961
37 feet Y = -3402165
83 meter
Z = 9793794
43 Z = 2985148
54
XDOT = 14386
041655 XDOT = 4384
865496
YDOT = 17758
766585 feet/sec YDOT = 5412
872055 meter/sec
ZDOT = -5101
101654 ZDOT = -1554
815784
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 00125U 09133
73195983
00020000 00000-0 70000-3 0 9104
2 00125 28
4707 327
1545 0003390 290
1622 69
8758 15
00474122 326
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09133
73195983 = yrday
fracday
Element set: 910
Inclination: 28
4707 deg
RA of node: 327
1545 deg
Eccentricity:
0003390
Arg of perigee: 290
1622 deg
Mean anomaly: 69
8758 deg
Mean motion: 15
00474122 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 32
Checksum: 257
Coasting Arc #12 (Orbit 31)
---------------------------------------
Vector Time (GMT): 2009/133/16:54:49
000
Vector Time (MET): 001/22:53:00
000
Weight (LBS) : 200000
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6703054
59 A = 6948584
80 meter
Y = 466967
08 meter E =
0008094
Z = -1748057
85 I = 28
29696
XDOT = 310
843514 Wp = 211
88995
YDOT = -6934
787415 meter/sec RA = 327
11894 deg
ZDOT = -3044
556342 TA =
19139
MA =
19108
Ha = 304
890 n
mi
Hp = 303
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21991648
93 X = -6699286
30
Y = 1532044
22 feet Y = 392030
89 meter
Z = -5735097
95 Z = -1780612
33
XDOT = 1019
827803 XDOT = 403
156387
YDOT = -22751
927213 feet/sec YDOT = -6930
794865 meter/sec
ZDOT = -9988
701909 ZDOT = -3042
822860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13705688
72 X = 4177493
92
Y = 17223739
35 feet Y = 5249795
75 meter
Z = -5862425
29 Z = -1786867
23
XDOT = -18100
839143 XDOT = -5517
135771
YDOT = 11006
061697 feet/sec YDOT = 3354
647605 meter/sec
ZDOT = -9982
295073 ZDOT = -3042
603538
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 00125U 09133
73195927
00020000 00000-0 70000-3 0 9113
2 00125 28
4709 327
1553 0003434 290
0806 69
9569 15
00496715 322
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09133
73195927 = yrday
fracday
Element set: 911
Inclination: 28
4709 deg
RA of node: 327
1553 deg
Eccentricity:
0003434
Arg of perigee: 290
0806 deg
Mean anomaly: 69
9569 deg
Mean motion: 15
00496715 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 32
Checksum: 272
Coasting Arc #13 (Orbit 46)
---------------------------------------
Vector Time (GMT): 2009/134/16:54:49
000
Vector Time (MET): 002/22:53:00
000
Weight (LBS) : 200000
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6547837
55 A = 6947687
34 meter
Y = -163729
84 meter E =
0006340
Z = -2304021
67 I = 28
25985
XDOT = 1077
505145 Wp = 230
39515
YDOT = -7052
075807 meter/sec RA = 320
55843 deg
ZDOT = -2559
553364 TA = 354
10031
MA = 354
10777
Ha = 305
117 n
mi
Hp = 302
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21482406
65 X = -6534327
46
Y = -537171
39 feet Y = -236875
79 meter
Z = -7559126
21 Z = -2335798
44
XDOT = 3535
121867 XDOT = 1168
716473
YDOT = -23136
731651 feet/sec YDOT = -7039
516244 meter/sec
ZDOT = -8397
484789 ZDOT = -2554
098042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12013553
49 X = 3661731
10
Y = 17764060
58 feet Y = 5414485
67 meter
Z = -7683451
16 Z = -2341915
91
XDOT = -19620
757666 XDOT = -5980
406937
YDOT = 9644
050682 feet/sec YDOT = 2939
506648 meter/sec
ZDOT = -8376
526634 ZDOT = -2553
165318
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 00125U 09134
72967321
00020000 00000-0 70000-3 0 9129
2 00125 28
4712 320
6476 0003367 299
3883 60
6525 15
00494004 475
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09134
72967321 = yrday
fracday
Element set: 912
Inclination: 28
4712 deg
RA of node: 320
6476 deg
Eccentricity:
0003367
Arg of perigee: 299
3883 deg
Mean anomaly: 60
6525 deg
Mean motion: 15
00494004 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 47
Checksum: 261
Coasting Arc #14 (Orbit 61)
---------------------------------------
Vector Time (GMT): 2009/135/16:54:49
000
Vector Time (MET): 003/22:53:00
000
Weight (LBS) : 200000
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6320364
02 A = 6946786
84 meter
Y = -833329
68 meter E =
0004835
Z = -2751635
97 I = 28
22534
XDOT = 1788
677258 Wp = 252
65470
YDOT = -7099
860538 meter/sec RA = 313
98542 deg
ZDOT = -1955
807838 TA = 344
26644
MA = 344
28145
Ha = 305
339 n
mi
Hp = 302
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20736102
44 X = -6297208
84
Y = -2734021
25 feet Y = -903877
94 meter
Z = -9027677
07 Z = -2782284
27
XDOT = 5868
363708 XDOT = 1877
437156
YDOT = -23293
505701 feet/sec YDOT = -7079
362033 meter/sec
ZDOT = -6416
692381 ZDOT = -1946
903495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10102289
62 X = 3079177
88
Y = 18254435
09 feet Y = 5563951
82 meter
Z = -9147628
87 Z = -2788197
28
XDOT = -20907
687538 XDOT = -6372
663161
YDOT = 8368
315059 feet/sec YDOT = 2550
662430 meter/sec
ZDOT = -6382
246903 ZDOT = -1945
308856
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 00125U 09135
72738710
00020000 00000-0 70000-3 0 9139
2 00125 28
4714 314
1401 0003302 309
1622 50
8829 15
00492716 626
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09135
72738710 = yrday
fracday
Element set: 913
Inclination: 28
4714 deg
RA of node: 314
1401 deg
Eccentricity:
0003302
Arg of perigee: 309
1622 deg
Mean anomaly: 50
8829 deg
Mean motion: 15
00492716 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 62
Checksum: 232
Coasting Arc #15 (Orbit 76)
---------------------------------------
Vector Time (GMT): 2009/136/16:54:49
000
Vector Time (MET): 004/22:53:00
000
Weight (LBS) : 200000
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6036295
32 A = 6946045
88 meter
Y = -1533844
60 meter E =
0003881
Z = -3070102
96 I = 28
19507
XDOT = 2438
086120 Wp = 279
21036
YDOT = -7063
155023 meter/sec RA = 307
40092 deg
ZDOT = -1261
541826 TA = 330
14734
MA = 330
16947
Ha = 305
552 n
mi
Hp = 302
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19804118
49 X = -6003780
90
Y = -5032298
56 feet Y = -1601163
93 meter
Z = -10072516
29 Z = -3099348
57
XDOT = 7998
970211 XDOT = 2523
014676
YDOT = -23173
080783 feet/sec YDOT = -7035
415957 meter/sec
ZDOT = -4138
916752 ZDOT = -1249
491836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8020139
16 X = 2444538
42
Y = 18731915
20 feet Y = 5709487
75 meter
Z = -10187023
26 Z = -3105004
69
XDOT = -21905
658873 XDOT = -6676
844824
YDOT = 7147
696930 feet/sec YDOT = 2178
618024 meter/sec
ZDOT = -4092
166316 ZDOT = -1247
292293
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 00125U 09136
72510092
00020000 00000-0 70000-3 0 9142
2 00125 28
4715 307
6326 0003237 319
4722 40
5781 15
00493889 773
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09136
72510092 = yrday
fracday
Element set: 914
Inclination: 28
4715 deg
RA of node: 307
6326 deg
Eccentricity:
0003237
Arg of perigee: 319
4722 deg
Mean anomaly: 40
5781 deg
Mean motion: 15
00493889 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 77
Checksum: 262
Coasting Arc #16 (Orbit 91)
---------------------------------------
Vector Time (GMT): 2009/137/16:54:49
000
Vector Time (MET): 005/22:53:00
000
Weight (LBS) : 200000
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5710830
09 A = 6945599
00 meter
Y = -2252710
75 meter E =
0003643
Z = -3244636
21 I = 28
17040
XDOT = 3024
798065 Wp = 305
55354
YDOT = -6928
966040 meter/sec RA = 300
80711 deg
ZDOT = -509
116767 TA = 316
25004
MA = 316
27891
Ha = 305
754 n
mi
Hp = 302
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18736319
20 X = -5669453
50
Y = -7390783
29 feet Y = -2316341
01 meter
Z = -10645131
93 Z = -3272279
26
XDOT = 9923
878165 XDOT = 3104
527334
YDOT = -22732
828216 feet/sec YDOT = -6894
695157 meter/sec
ZDOT = -1670
330600 ZDOT = -494
229018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5828201
37 X = 1776435
78
Y = 19219478
51 feet Y = 5858097
05 meter
Z = -10753412
64 Z = -3277640
17
XDOT = -22577
275321 XDOT = -6881
553518
YDOT = 5936
823768 feet/sec YDOT = 1809
543885 meter/sec
ZDOT = -1612
473934 ZDOT = -491
482055
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 00125U 09137
72281466
00020000 00000-0 70000-3 0 9154
2 00125 28
4714 301
1249 0003170 330
2991 29
7574 15
00497672 920
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09137
72281466 = yrday
fracday
Element set: 915
Inclination: 28
4714 deg
RA of node: 301
1249 deg
Eccentricity:
0003170
Arg of perigee: 330
2991 deg
Mean anomaly: 29
7574 deg
Mean motion: 15
00497672 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 92
Checksum: 261
Coasting Arc #17 (Orbit 106)
---------------------------------------
Vector Time (GMT): 2009/138/16:54:49
000
Vector Time (MET): 006/22:53:00
000
Weight (LBS) : 200000
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5357220
11 A = 6945528
09 meter
Y = -2973480
77 meter E =
0004022
Z = -3267138
70 I = 28
15229
XDOT = 3552
571216 Wp = 324
59793
YDOT = -6687
843735 meter/sec RA = 294
20707 deg
ZDOT = 266
458121 TA = 309
65852
MA = 309
69400
Ha = 305
942 n
mi
Hp = 302
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17576181
47 X = -5307700
66
Y = -9755514
33 feet Y = -3033111
25 meter
Z = -10718958
98 Z = -3293044
23
XDOT = 11655
417374 XDOT = 3625
797358
YDOT = -21941
744536 feet/sec YDOT = -6647
707396 meter/sec
ZDOT = 874
206433 ZDOT = 283
894145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3594503
49 X = 1095604
66
Y = 19722701
26 feet Y = 6011479
35 meter
Z = -10820485
02 Z = -3298083
83
XDOT = -22907
489214 XDOT = -6982
202712
YDOT = 4682
883431 feet/sec YDOT = 1427
342870 meter/sec
ZDOT = 942
043882 ZDOT = 287
134975
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 00125U 09138
72052829
00020000 00000-0 70000-3 0 9165
2 00125 28
4713 294
6171 0003104 341
5384 18
5248 15
00503348 1076
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09138
72052829 = yrday
fracday
Element set: 916
Inclination: 28
4713 deg
RA of node: 294
6171 deg
Eccentricity:
0003104
Arg of perigee: 341
5384 deg
Mean anomaly: 18
5248 deg
Mean motion: 15
00503348 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 107
Checksum: 248
Coasting Arc #18 (Orbit 119)
---------------------------------------
Vector Time (GMT): 2009/139/12:54:53
243
Vector Time (MET): 007/18:53:04
243
Weight (LBS) : 243824
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5022091
97 A = 6945488
46 meter
Y = 3596138
36 meter E =
0010882
Z = 3161076
55 I = 28
14120
XDOT = -3985
156792 Wp = 78
32360
YDOT = 6384
834640 meter/sec RA = 288
69978 deg
ZDOT = -924
129071 TA = 26
67895
MA = 26
62300
Ha = 305
827 n
mi
Hp = 301
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16476679
68 X = 4966149
94
Y = 11798354
20 feet Y = 3651985
35 meter
Z = 10370986
06 Z = 3185338
52
XDOT = -13074
661392 XDOT = -4051
767591
YDOT = 20947
620211 feet/sec YDOT = 6339
897904 meter/sec
ZDOT = -3031
919524 ZDOT = -943
650647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16644402
17 X = 5073213
78
Y = -11474481
46 feet Y = -3497421
95 meter
Z = 10466118
59 Z = 3190072
95
XDOT = 14479
000810 XDOT = 4413
199447
YDOT = 18143
728734 feet/sec YDOT = 5530
208518 meter/sec
ZDOT = -3107
932818 ZDOT = -947
297923
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 00125U 09139
58520809
00020000 00000-0 70000-3 0 9179
2 00125 28
4698 288
9724 0003622 342
0694 17
9922 15
00604212 1202
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09139
58520809 = yrday
fracday
Element set: 917
Inclination: 28
4698 deg
RA of node: 288
9724 deg
Eccentricity:
0003622
Arg of perigee: 342
0694 deg
Mean anomaly: 17
9922 deg
Mean motion: 15
00604212 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 120
Checksum: 268
Coasting Arc #19 (Orbit 119)
---------------------------------------
Vector Time (GMT): 2009/139/13:27:14
447
Vector Time (MET): 007/19:25:25
447
Weight (LBS) : 243626
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5735517
89 A = 6943763
14 meter
Y = 3110814
08 meter E =
0001549
Z = -2377938
60 I = 28
15474
XDOT = -2600
844504 Wp = 10
47311
YDOT = -6676
651529 meter/sec RA = 288
60551 deg
ZDOT = -2459
203644 TA = 216
05207
MA = 216
06251
Ha = 305
870 n
mi
Hp = 298
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18817315
92 X = -5758325
51
Y = 10206082
93 feet Y = 3046548
78 meter
Z = -7801635
83 Z = -2405857
34
XDOT = -8532
954411 XDOT = -2514
045233
YDOT = -21905
024702 feet/sec YDOT = -6705
250227 meter/sec
ZDOT = -8068
253425 ZDOT = -2471
628269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6222037
95 X = 1896477
17
Y = 20440847
28 feet Y = 6230370
25 meter
Z = -7910691
20 Z = -2411178
68
XDOT = -21673
692281 XDOT = -6606
141407
YDOT = 3453
372843 feet/sec YDOT = 1052
588043 meter/sec
ZDOT = -8117
248221 ZDOT = -2474
137258
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 00125U 09139
58519690
00020000 00000-0 70000-3 0 9186
2 00125 28
4703 288
9737 0007230 19
0763 341
0252 15
01725773 1204
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09139
58519690 = yrday
fracday
Element set: 918
Inclination: 28
4703 deg
RA of node: 288
9737 deg
Eccentricity:
0007230
Arg of perigee: 19
0763 deg
Mean anomaly: 341
0252 deg
Mean motion: 15
01725773 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 120
Checksum: 267
Coasting Arc #20 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2009/139/15:05:15
206
Vector Time (MET): 007/21:03:26
206
Weight (LBS) : 238031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6010780
89 A = 6815090
28 meter
Y = 2203655
26 meter E =
0190366
Z = -2688672
58 I = 28
14949
XDOT = -1656
384845 Wp = 47
64722
YDOT = -7036
829861 meter/sec RA = 288
15396 deg
ZDOT = -2015
258483 TA = 187
51353
MA = 187
80287
Ha = 305
951 n
mi
Hp = 159
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19720409
76 X = -6021914
54
Y = 7229840
08 feet Y = 2136377
10 meter
Z = -8821104
25 Z = -2717900
27
XDOT = -5434
333482 XDOT = -1567
784825
YDOT = -23086
712143 feet/sec YDOT = -7054
857017 meter/sec
ZDOT = -6611
740429 ZDOT = -2023
090511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11459100
99 X = 3492733
98
Y = 17544966
73 feet Y = 5347705
86 meter
Z = -8935333
00 Z = -2723489
50
XDOT = -20007
750662 XDOT = -6098
362402
YDOT = 9603
450418 feet/sec YDOT = 2927
131687 meter/sec
ZDOT = -6642
787164 ZDOT = -2024
721528
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 00125U 09139
65127091
00020000 00000-0 70000-3 0 9195
2 00125 28
4710 288
5305 0194879 47
7447 313
9670 15
44297104 1214
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09139
65127091 = yrday
fracday
Element set: 919
Inclination: 28
4710 deg
RA of node: 288
5305 deg
Eccentricity:
0194879
Arg of perigee: 47
7447 deg
Mean anomaly: 313
9670 deg
Mean motion: 15
44297104 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 121
Checksum: 286
Coasting Arc #21 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2009/140/15:05:15
206
Vector Time (MET): 008/21:03:26
206
Weight (LBS) : 238031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025189
14 A = 6816211
60 meter
Y = -3779723
96 meter E =
0208502
Z = 2248522
15 I = 28
14479
XDOT = 3627
734218 Wp = 59
16336
YDOT = 6415
528250 meter/sec RA = 281
10374 deg
ZDOT = 2565
306239 TA = 346
38318
MA = 346
93724
Ha = 305
959 n
mi
Hp = 159
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16486841
02 X = 5056158
05
Y = -12400669
15 feet Y = -3723356
35 meter
Z = 7377041
18 Z = 2273009
95
XDOT = 11902
015151 XDOT = 3543
263055
YDOT = 21048
321030 feet/sec YDOT = 6455
623222 meter/sec
ZDOT = 8416
359052 ZDOT = 2582
725329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15999783
69 X = -4876734
07
Y = -12968419
48 feet Y = -3952774
26 meter
Z = 7472635
21 Z = 2277659
21
XDOT = 16623
527476 XDOT = 5066
851175
YDOT = -15412
026038 feet/sec YDOT = -4697
585536 meter/sec
ZDOT = 8484
880753 ZDOT = 2586
191654
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 00125U 09140
68532907
00020000 00000-0 70000-3 0 9208
2 00125 28
4709 281
3133 0194877 59
5117 302
4737 15
44162144 1374
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09140
68532907 = yrday
fracday
Element set: 920
Inclination: 28
4709 deg
RA of node: 281
3133 deg
Eccentricity:
0194877
Arg of perigee: 59
5117 deg
Mean anomaly: 302
4737 deg
Mean motion: 15
44162144 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 137
Checksum: 269
Coasting Arc #22 (Orbit 151)
---------------------------------------
Vector Time (GMT): 2009/141/15:05:15
206
Vector Time (MET): 009/21:03:26
206
Weight (LBS) : 238031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4135225
01 A = 6816346
63 meter
Y = 5175551
69 meter E =
0190687
Z = -2011451
24 I = 28
14350
XDOT = -4937
924219 Wp = 72
01838
YDOT = -4932
558821 meter/sec RA = 274
04081 deg
ZDOT = -2820
790141 TA = 146
00269
MA = 144
76626
Ha = 306
178 n
mi
Hp = 159
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13567011
20 X = -4183020
08
Y = 16980156
46 feet Y = 5129042
12 meter
Z = -6599249
49 Z = -2031656
28
XDOT = -16200
538777 XDOT = -4868
697322
YDOT = -16182
935763 feet/sec YDOT = -4987
390271 meter/sec
ZDOT = -9254
560830 ZDOT = -2844
611364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19893674
63 X = 6063592
03
Y = 8693991
66 feet Y = 2649928
66 meter
Z = -6678010
12 Z = -2035457
48
XDOT = -10839
675643 XDOT = -3303
933136
YDOT = 18322
066836 feet/sec YDOT = 5584
565972 meter/sec
ZDOT = -9348
046578 ZDOT = -2849
284597
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 00125U 09141
65473390
00020000 00000-0 70000-3 0 9217
2 00125 28
4705 274
5397 0194820 70
5047 291
6654 15
44298735 1529
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09141
65473390 = yrday
fracday
Element set: 921
Inclination: 28
4705 deg
RA of node: 274
5397 deg
Eccentricity:
0194820
Arg of perigee: 70
5047 deg
Mean anomaly: 291
6654 deg
Mean motion: 15
44298735 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 152
Checksum: 283
Coasting Arc #23 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2009/142/15:05:15
206
Vector Time (MET): 010/21:03:26
206
Weight (LBS) : 238031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2240585
10 A = 6817631
69 meter
Y = -6198703
49 meter E =
0206954
Z = 1371661
59 I = 28
15013
XDOT = 6281
230889 Wp = 79
38839
YDOT = 3132
321285 meter/sec RA = 266
98525 deg
ZDOT = 3268
132216 TA = 306
19660
MA = 308
09292
Ha = 306
219 n
mi
Hp = 159
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7351000
97 X = 2303070
07
Y = -20336953
72 feet Y = -6173298
74 meter
Z = 4500202
05 Z = 1382697
71
XDOT = 20607
712890 XDOT = 6229
861522
YDOT = 10276
644637 feet/sec YDOT = 3202
274095 meter/sec
ZDOT = 10722
218556 ZDOT = 3298
522750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21566148
91 X = -6573362
19
Y = -1463821
85 feet Y = -446172
90 meter
Z = 4543035
01 Z = 1384717
07
XDOT = 4138
637421 XDOT = 1261
456686
YDOT = -21003
819669 feet/sec YDOT = -6401
964235 meter/sec
ZDOT = 10841
307974 ZDOT = 3304
430671
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 00125U 09142
68875549
00020000 00000-0 70000-3 0 9224
2 00125 28
4710 267
3291 0194767 82
2294 280
0536 15
44180875 1685
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09142
68875549 = yrday
fracday
Element set: 922
Inclination: 28
4710 deg
RA of node: 267
3291 deg
Eccentricity:
0194767
Arg of perigee: 82
2294 deg
Mean anomaly: 280
0536 deg
Mean motion: 15
44180875 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 168
Checksum: 296
Coasting Arc #24 (Orbit 182)
---------------------------------------
Vector Time (GMT): 2009/143/15:05:15
206
Vector Time (MET): 011/21:03:26
206
Weight (LBS) : 238031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -949169
82 A = 6817612
37 meter
Y = 6687691
29 meter E =
0196098
Z = -1127011
36 I = 28
15654
XDOT = -6676
671649 Wp = 96
14371
YDOT = -1370
030799 meter/sec RA = 259
91391 deg
ZDOT = -3389
841279 TA = 104
26772
MA = 102
08212
Ha = 306
227 n
mi
Hp = 159
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3114074
22 X = -1018407
22
Y = 21941244
39 feet Y = 6676690
15 meter
Z = -3697543
83 Z = -1131789
77
XDOT = -21905
090711 XDOT = -6644
387876
YDOT = -4494
851702 feet/sec YDOT = -1444
512248 meter/sec
ZDOT = -11121
526507 ZDOT = -3422
199105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21892038
75 X = 6672693
41
Y = -3423221
15 feet Y = -1043397
81 meter
Z = -3715870
03 Z = -1132597
19
XDOT = 1802
446527 XDOT = 549
385701
YDOT = 20607
020475 feet/sec YDOT = 6281
019841 meter/sec
ZDOT = -11248
221584 ZDOT = -3428
457939
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 00125U 09143
65812214
00020000 00000-0 70000-3 0 9233
2 00125 28
4706 260
5512 0194655 93
3181 268
9875 15
44257974 1838
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09143
65812214 = yrday
fracday
Element set: 923
Inclination: 28
4706 deg
RA of node: 260
5512 deg
Eccentricity:
0194655
Arg of perigee: 93
3181 deg
Mean anomaly: 268
9875 deg
Mean motion: 15
44257974 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 183
Checksum: 288
Coasting Arc #25 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2009/144/15:05:15
206
Vector Time (MET): 012/21:03:26
206
Weight (LBS) : 238031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1327764
47 A = 6818205
65 meter
Y = -6683973
46 meter E =
0198795
Z = 375729
22 I = 28
16970
XDOT = 6681
354885 Wp = 100
67644
YDOT = -971
569990 meter/sec RA = 252
85492 deg
ZDOT = 3572
340817 TA = 266
02039
MA = 268
29513
Ha = 306
230 n
mi
Hp = 159
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4356182
66 X = -1254749
73
Y = -21929046
80 feet Y = -6698413
12 meter
Z = 1232707
43 Z = 369455
03
XDOT = 21920
455660 XDOT = 6674
368436
YDOT = -3187
565585 feet/sec YDOT = -896
894857 meter/sec
ZDOT = 11720
278270 ZDOT = 3604
782359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19527257
29 X = -5951908
02
Y = 10890659
51 feet Y = 3319473
02 meter
Z = 1207785
87 Z = 368133
13
XDOT = -8953
894782 XDOT = -2729
147130
YDOT = -18391
487432 feet/sec YDOT = -5605
725369 meter/sec
ZDOT = 11847
183143 ZDOT = 3611
021422
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 00125U 09144
69210021
00020000 00000-0 70000-3 0 9247
2 00125 28
4707 253
3437 0194617 105
0172 257
2218 15
44233111 1990
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09144
69210021 = yrday
fracday
Element set: 924
Inclination: 28
4707 deg
RA of node: 253
3437 deg
Eccentricity:
0194617
Arg of perigee: 105
0172 deg
Mean anomaly: 257
2218 deg
Mean motion: 15
44233111 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 199
Checksum: 244
Coasting Arc #26 (Orbit 213)
---------------------------------------
Vector Time (GMT): 2009/145/15:05:15
206
Vector Time (MET): 013/21:03:26
206
Weight (LBS) : 238031
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2593495
01 A = 6818292
87 meter
Y = 6234864
02 meter E =
0204506
Z = -102832
05 I = 28
18461
XDOT = -6249
193352 Wp = 118
47439
YDOT = 2690
772767 meter/sec RA = 245
78583 deg
ZDOT = -3645
382465 TA = 63
37302
MA = 61
29252
Ha = 306
052 n
mi
Hp = 159
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8508841
91 X = 2524082
50
Y = 20455590
63 feet Y = 6263477
91 meter
Z = -337375
50 Z = -90400
10
XDOT = -20502
602862 XDOT = -6261
108721
YDOT = 8827
994643 feet/sec YDOT = 2620
824710 meter/sec
ZDOT = -11959
916225 ZDOT = -3675
769904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16600733
89 X = 5059903
69
Y = -14672350
68 feet Y = -4472132
49 meter
Z = -288376
63 Z = -87897
20
XDOT = 13895
175039 XDOT = 4235
249352
YDOT = 15266
122167 feet/sec YDOT = 4653
114036 meter/sec
ZDOT = -12078
702352 ZDOT = -3681
588477
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 00125U 09145
66142955
00020000 00000-0 70000-3 0 9256
2 00125 28
4710 246
5655 0194722 116
1327 245
9609 15
44225005 2141
Satellite: SHUTTLE
Catalog Number: 00125
Epoch time: 09145
66142955 = yrday
fracday
Element set: 925
Inclination: 28
4710 deg
RA of node: 246
5655 deg
Eccentricity:
0194722
Arg of perigee: 116
1327 deg
Mean anomaly: 245
9609 deg
Mean motion: 15
44225005 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 214
Checksum: 264
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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