Date: June 11th 2008

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2008/152/21:02:11 970 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 69 ET - UTC (sec) : 65 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


163/12:57:23 283 0 0 0 0 0 0
010/15:55:11 313 0 0 0 0 186 2
000/00:00:00 000 0 0 0 0 180 3

163/13:25:14 746 1 2 1 5 1 5
010/16:23:02 776 0 9 0 0 186 3
000/00:00:05 551 -0 3 -0 0 181 3

164/20:20:23 275 -3 3 6 0 6 0
011/23:18:11 304 2 0 -0 0 189 8
000/00:00:22 608 4 6 -0 1 181 4

Coasting Arc #1 (Orbit 155)
---------------------------------------

Vector Time (GMT): 2008/162/15:27:16
000
Vector Time (MET): 009/18:25:04
030
Weight (LBS)     : 212776
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3797384
53                 A    =         6712777
66  meter
 Y    =        1857688
13  meter          E    =           
0006431
 Z    =        5216212
35                 I    =           51
86763
 XDOT =      -4373
881831                 Wp   =          350
22707
 YDOT =      -6271
500319  meter/sec      RA   =           49
54180  deg
 ZDOT =       -944
616305                 TA   =          108
77546
                                          MA   =          108
70568
                                          Ha   =            185
763  n
mi
                                          Hp   =            181
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12458610
66                 X    =        -3843214
65
 Y    =        6094777
32  feet           Y    =         1814966
71  meter
 Z    =       17113557
57                 Z    =         5197653
57
 XDOT =     -14350
006008                 XDOT =       -4298
839078
 YDOT =     -20575
788449  feet/sec       YDOT =       -6319
991870  meter/sec
 ZDOT =      -3099
134860                 ZDOT =        -965
683095

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12781275
37                 X    =         3895732
73
 Y    =        5606908
86  feet           Y    =         1708985
82  meter
 Z    =       17042262
63                 Z    =         5194481
65
 XDOT =      -5962
527142                 XDOT =       -1817
378273
 YDOT =      23320
366764  feet/sec       YDOT =        7108
047790  meter/sec
 ZDOT =      -3180
763293                 ZDOT =        -969
496652


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 32960U 08027A   08162
68986208  
00020000  00000-0  70000-3 0  9005
2 32960  51
6387  49
8946 0006011 317
9181  42
1521 15
76690087  1566


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08162
68986208   =   yrday
fracday
Element set:     900
Inclination:       51
6387  deg
RA of node:        49
8946  deg
Eccentricity:     
0006011     
Arg of perigee:   317
9181  deg
Mean anomaly:      42
1521  deg
Mean motion:   15
76690087  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             156
Checksum:              301


Coasting Arc #2 (Orbit 169)
---------------------------------------

Vector Time (GMT): 2008/163/12:57:23
283
Vector Time (MET): 010/15:55:11
313
Weight (LBS)     : 212702
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5586392
15                 A    =         6720998
52  meter
 Y    =       -2450667
54  meter          E    =           
0011112
 Z    =        2816345
00                 I    =           51
88115
 XDOT =        -71
096065                 Wp   =           73
03673
 YDOT =      -5750
540634  meter/sec      RA   =           44
92442  deg
 ZDOT =      -5125
208220                 TA   =           74
76940
                                          MA   =           74
64656
                                          Ha   =            186
207  n
mi
                                          Hp   =            180
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18328058
24                 X    =        -5572254
54
 Y    =       -8040247
83  feet           Y    =        -2513059
07  meter
 Z    =        9239977
04                 Z    =         2789240
27
 XDOT =       -233
254805                 XDOT =          18
110075
 YDOT =     -18866
603129  feet/sec       YDOT =       -5750
836272  meter/sec
 ZDOT =     -16814
987600                 ZDOT =       -5125
337621

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6793022
48                 X    =        -2070513
25
 Y    =       18876952
85  feet           Y    =         5753695
23  meter
 Z    =        9135424
25                 Z    =         2784477
31
 XDOT =     -17438
721395                 XDOT =       -5315
322281
 YDOT =       1894
187324  feet/sec       YDOT =         577
348296  meter/sec
 ZDOT =     -16815
961019                 ZDOT =       -5125
504919


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 32960U 08027A   08163
57719132  
00020000  00000-0  70000-3 0  9015
2 32960  51
6417  45
3215 0006171 334
1247  25
9608 15
76751669  1706


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08163
57719132   =   yrday
fracday
Element set:     901
Inclination:       51
6417  deg
RA of node:        45
3215  deg
Eccentricity:     
0006171     
Arg of perigee:   334
1247  deg
Mean anomaly:      25
9608  deg
Mean motion:   15
76751669  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             170
Checksum:              281


Coasting Arc #3 (Orbit 169)
---------------------------------------

Vector Time (GMT): 2008/163/13:25:17
522
Vector Time (MET): 010/16:23:05
551
Weight (LBS)     : 212658
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1848139
24                 A    =         6713615
70  meter
 Y    =       -3883912
65  meter          E    =           
0012639
 Z    =       -5164815
51                 I    =           51
85196
 XDOT =       6042
955204                 Wp   =           52
46607
 YDOT =       4590
240291  meter/sec      RA   =           44
85789  deg
 ZDOT =      -1284
061787                 TA   =          205
25475
                                          MA   =          205
31660
                                          Ha   =            186
335  n
mi
                                          Hp   =            181
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6063448
95                 X    =         1916522
22
 Y    =      -12742495
56  feet           Y    =        -3862862
72  meter
 Z    =      -16944932
77                 Z    =        -5155671
59
 XDOT =      19825
968516                 XDOT =        5997
415044
 YDOT =      15059
843474  feet/sec       YDOT =        4657
561605  meter/sec
 ZDOT =      -4212
801138                 ZDOT =       -1254
815082

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13673005
80                 X    =        -4167532
17
 Y    =       -3656015
93  feet           Y    =        -1114353
65  meter
 Z    =      -16910050
64                 Z    =        -5154183
44
 XDOT =      10795
487916                 XDOT =        3290
464717
 YDOT =     -21328
656517  feet/sec       YDOT =       -6500
974506  meter/sec
 ZDOT =      -4099
825237                 ZDOT =       -1249
626732


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 32960U 08027A   08163
57719158  
00020000  00000-0  70000-3 0  9024
2 32960  51
6405  45
3207 0006601 322
9484  37
1224 15
76463967  1700


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08163
57719158   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:        45
3207  deg
Eccentricity:     
0006601     
Arg of perigee:   322
9484  deg
Mean anomaly:      37
1224  deg
Mean motion:   15
76463967  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             170
Checksum:              284


Coasting Arc #4 (Orbit 185)
---------------------------------------

Vector Time (GMT): 2008/164/13:30:11
498
Vector Time (MET): 011/16:27:59
528
Weight (LBS)     : 212658
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4228874
79                 A    =         6724255
20  meter
 Y    =       -5015306
84  meter          E    =           
0001827
 Z    =       -1473601
92                 I    =           51
86592
 XDOT =       4566
991522                 Wp   =          132
86536
 YDOT =      -2143
421804  meter/sec      RA   =           39
70566  deg
 ZDOT =      -5816
880347                 TA   =           63
31339
                                          MA   =           63
29469
                                          Ha   =            186
444  n
mi
                                          Hp   =            181
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13874261
13                 X    =        -4165320
00
 Y    =      -16454418
75  feet           Y    =        -5062240
99  meter
 Z    =       -4834651
97                 Z    =        -1493992
21
 XDOT =      14983
567985                 XDOT =        4618
877713
 YDOT =      -7032
223768  feet/sec       YDOT =       -2092
060227  meter/sec
 ZDOT =     -19084
253108                 ZDOT =       -5794
567995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12904886
02                 X    =        -3933409
26
 Y    =       17202840
37  feet           Y    =         5243425
74  meter
 Z    =       -4913560
64                 Z    =        -1497653
28
 XDOT =      -9002
552193                 XDOT =       -2743
977909
 YDOT =     -12174
523879  feet/sec       YDOT =       -3710
794878  meter/sec
 ZDOT =     -18998
528649                 ZDOT =       -5790
751532


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 32960U 08027A   08164
59144190  
00020000  00000-0  70000-3 0  9036
2 32960  51
6404  40
0935 0006550 325
7023  34
3717 15
76447135  1864


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08164
59144190   =   yrday
fracday
Element set:     903
Inclination:       51
6404  deg
RA of node:        40
0935  deg
Eccentricity:     
0006550     
Arg of perigee:   325
7023  deg
Mean anomaly:      34
3717  deg
Mean motion:   15
76447135  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             186
Checksum:              270


Coasting Arc #5 (Orbit 190)
---------------------------------------

Vector Time (GMT): 2008/164/20:20:34
579
Vector Time (MET): 011/23:18:22
608
Weight (LBS)     : 212511
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4458802
00                 A    =         6727567
48  meter
 Y    =        4841899
65  meter          E    =           
0019382
 Z    =        1329131
36                 I    =           51
86126
 XDOT =      -4379
716056                 Wp   =           30
39735
 YDOT =       2416
367121  meter/sec      RA   =           38
23576  deg
 ZDOT =       5869
371651                 TA   =          344
17835
                                          MA   =          344
23882
                                          Ha   =            189
834  n
mi
                                          Hp   =            181
392

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14628615
48                 X    =         4397871
00
 Y    =       15885497
54  feet           Y    =         4891419
67  meter
 Z    =        4360667
19                 Z    =         1350645
03
 XDOT =     -14369
147166                 XDOT =       -4434
923305
 YDOT =       7927
713653  feet/sec       YDOT =        2367
081167  meter/sec
 ZDOT =      19256
468670                 ZDOT =        5847
961046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20078373
08                 X    =        -6119888
12
 Y    =       -7903901
83  feet           Y    =        -2409109
28  meter
 Z    =        4443884
75                 Z    =         1354496
07
 XDOT =       8980
319081                 XDOT =        2737
201256
 YDOT =     -11995
100123  feet/sec       YDOT =       -3656
106518  meter/sec
 ZDOT =      19174
237416                 ZDOT =        5844
307564


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 32960U 08027A   08164
90843909  
00020000  00000-0  70000-3 0  9046
2 32960  51
6417  38
4562 0009912 347
2398  12
8514 15
75354427  1916


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08164
90843909   =   yrday
fracday
Element set:     904
Inclination:       51
6417  deg
RA of node:        38
4562  deg
Eccentricity:     
0009912     
Arg of perigee:   347
2398  deg
Mean anomaly:      12
8514  deg
Mean motion:   15
75354427  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             191
Checksum:              302


Coasting Arc #6 (Orbit 205)
---------------------------------------

Vector Time (GMT): 2008/165/20:25:51
115
Vector Time (MET): 012/23:23:39
145
Weight (LBS)     : 212511
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5375228
24                 A    =         6721339
38  meter
 Y    =        -278777
59  meter          E    =           
0009104
 Z    =       -4024367
61                 I    =           51
81663
 XDOT =       3230
569664                 Wp   =           33
39317
 YDOT =       5785
165587  meter/sec      RA   =           33
04753  deg
 ZDOT =       3925
844525                 TA   =          276
98265
                                          MA   =          277
08619
                                          Ha   =            190
021  n
mi
                                          Hp   =            181
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17635263
25                 X    =         5397495
92
 Y    =        -914624
65  feet           Y    =         -218543
60  meter
 Z    =      -13203305
81                 Z    =        -3998200
44
 XDOT =      10598
981838                 XDOT =        3146
567694
 YDOT =      18980
202056  feet/sec       YDOT =        5820
821398  meter/sec
 ZDOT =      12880
067340                 ZDOT =        3941
335619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15171251
10                 X    =        -4624197
33
 Y    =        9182681
52  feet           Y    =         2798881
33  meter
 Z    =      -13102588
77                 Z    =        -3993669
06
 XDOT =     -17581
481379                 XDOT =       -5358
835524
 YDOT =     -10638
152049  feet/sec       YDOT =       -3242
508745  meter/sec
 ZDOT =      12940
168010                 ZDOT =        3944
163209


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 32960U 08027A   08165
85996358  
00020000  00000-0  70000-3 0  9059
2 32960  51
6419  33
5611 0009945 350
0987   9
9979 15
75366431  2068


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08165
85996358   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:        33
5611  deg
Eccentricity:     
0009945     
Arg of perigee:   350
0987  deg
Mean anomaly:       9
9979  deg
Mean motion:   15
75366431  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             206
Checksum:              327


Coasting Arc #7 (Orbit 221)
---------------------------------------

Vector Time (GMT): 2008/166/20:26:02
040
Vector Time (MET): 013/23:23:50
070
Weight (LBS)     : 212511
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2691547
92                 A    =         6721855
37  meter
 Y    =       -4838267
40  meter          E    =           
0012661
 Z    =       -3825644
54                 I    =           51
79339
 XDOT =       6456
358870                 Wp   =           23
49636
 YDOT =       -288
800468  meter/sec      RA   =           27
96462  deg
 ZDOT =      -4170
495705                 TA   =          202
84323
                                          MA   =          202
89960
                                          Ha   =            190
036  n
mi
                                          Hp   =            180
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8830537
81                 X    =        -2618661
12
 Y    =      -15873580
71  feet           Y    =        -4867957
65  meter
 Z    =      -12551327
24                 Z    =        -3838544
01
 XDOT =      21182
279758                 XDOT =        6479
368159
 YDOT =       -947
508096  feet/sec       YDOT =        -216
472405  meter/sec
 ZDOT =     -13682
728692                 ZDOT =       -4139
074528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15399928
37                 X    =         4693898
17
 Y    =        9567261
02  feet           Y    =         2916101
16  meter
 Z    =      -12601369
01                 Z    =        -3840897
27
 XDOT =     -17386
588767                 XDOT =       -5299
432256
 YDOT =      10094
948535  feet/sec       YDOT =        3076
940313  meter/sec
 ZDOT =     -13561
783887                 ZDOT =       -4133
631729


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 32960U 08027A   08166
87491192  
00020000  00000-0  70000-3 0  9069
2 32960  51
6418  28
3386 0009920 354
1241   5
9805 15
75379785  2227


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08166
87491192   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:        28
3386  deg
Eccentricity:     
0009920     
Arg of perigee:   354
1241  deg
Mean anomaly:       5
9805  deg
Mean motion:   15
75379785  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             222
Checksum:              306


Coasting Arc #8 (Orbit 237)
---------------------------------------

Vector Time (GMT): 2008/167/20:26:03
569
Vector Time (MET): 014/23:23:51
599
Weight (LBS)     : 212511
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5870945
42                 A    =         6723649
62  meter
 Y    =         320699
62  meter          E    =           
0015730
 Z    =        3261000
50                 I    =           51
77273
 XDOT =      -2942
748847                 Wp   =           52
78611
 YDOT =      -5295
586401  meter/sec      RA   =           22
77773  deg
 ZDOT =      -4752
224331                 TA   =           89
08629
                                          MA   =           88
90607
                                          Ha   =            190
211  n
mi
                                          Hp   =            180
725

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19261631
96                 X    =        -5889936
70
 Y    =        1052164
11  feet           Y    =          254940
54  meter
 Z    =       10698820
54                 Z    =         3232433
09
 XDOT =      -9654
687819                 XDOT =       -2860
228379
 YDOT =     -17373
971131  feet/sec       YDOT =       -5328
031609  meter/sec
 ZDOT =     -15591
287174                 ZDOT =       -4766
320907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16160849
71                 X    =         4925826
99
 Y    =      -10643552
49  feet           Y    =        -3244154
80  meter
 Z    =       10588862
21                 Z    =         3227485
20
 XDOT =      16239
960949                 XDOT =        4949
940097
 YDOT =       9010
353926  feet/sec       YDOT =        2746
355877  meter/sec
 ZDOT =     -15645
968265                 ZDOT =       -4768
891127


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 32960U 08027A   08167
88984506  
00020000  00000-0  70000-3 0  9078
2 32960  51
6416  23
1160 0010044 358
6535   1
4601 15
75412487  2381


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08167
88984506   =   yrday
fracday
Element set:     907
Inclination:       51
6416  deg
RA of node:        23
1160  deg
Eccentricity:     
0010044     
Arg of perigee:   358
6535  deg
Mean anomaly:       1
4601  deg
Mean motion:   15
75412487  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             238
Checksum:              279


Coasting Arc #9 (Orbit 253)
---------------------------------------

Vector Time (GMT): 2008/168/20:31:14
096
Vector Time (MET): 015/23:29:02
125
Weight (LBS)     : 212511
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         149426
27                 A    =         6716459
47  meter
 Y    =        4308811
97  meter          E    =           
0008476
 Z    =        5145505
77                 I    =           51
72176
 XDOT =      -7483
894808                 Wp   =           24
86833
 YDOT =      -1297
085978  meter/sec      RA   =           17
65675  deg
 ZDOT =       1310
277822                 TA   =           52
66359
                                          MA   =           52
58639
                                          Ha   =            190
209  n
mi
                                          Hp   =            180
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         490243
66                 X    =           76237
22
 Y    =       14136522
21  feet           Y    =         4310072
67  meter
 Z    =       16881580
62                 Z    =         5146054
79
 XDOT =     -24553
460657                 XDOT =       -7475
199507
 YDOT =      -4255
531424  feet/sec       YDOT =       -1380
726823  meter/sec
 ZDOT =       4298
811753                 ZDOT =        1273
941632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7935041
95                 X    =        -2418600
79
 Y    =      -11706161
60  feet           Y    =        -3568038
05  meter
 Z    =       16884023
60                 Z    =         5146250
39
 XDOT =      22155
498209                 XDOT =        6752
995854
 YDOT =      -9051
849477  feet/sec       YDOT =       -2759
003721  meter/sec
 ZDOT =       4158
815507                 ZDOT =        1267
606966


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 32960U 08027A   08168
90476031  
00020000  00000-0  70000-3 0  9082
2 32960  51
6417  17
8926 0010066   1
4257 358
6934 15
75468617  2540


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08168
90476031   =   yrday
fracday
Element set:     908
Inclination:       51
6417  deg
RA of node:        17
8926  deg
Eccentricity:     
0010066     
Arg of perigee:     1
4257  deg
Mean anomaly:     358
6934  deg
Mean motion:   15
75468617  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             254
Checksum:              302


Coasting Arc #10 (Orbit 268)
---------------------------------------

Vector Time (GMT): 2008/169/20:31:46
174
Vector Time (MET): 016/23:29:34
203
Weight (LBS)     : 212511
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6611062
78                 A    =         6728076
44  meter
 Y    =        1083803
08  meter          E    =           
0020588
 Z    =        -472552
46                 I    =           51
73157
 XDOT =       -362
385972                 Wp   =           23
88285
 YDOT =       4792
090789  meter/sec      RA   =           12
49995  deg
 ZDOT =       6030
151120                 TA   =          330
97538
                                          MA   =          331
08969
                                          Ha   =            190
490  n
mi
                                          Hp   =            180
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21689838
50                 X    =         6600747
75
 Y    =        3555784
40  feet           Y    =         1157674
20  meter
 Z    =       -1550368
95                 Z    =         -440460
60
 XDOT =      -1188
930355                 XDOT =        -445
238454
 YDOT =      15722
082642  feet/sec       YDOT =        4787
573837  meter/sec
 ZDOT =      19783
960366                 ZDOT =        6028
190419

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20032108
27                 X    =        -6105786
60
 Y    =        9065066
63  feet           Y    =         2763032
31  meter
 Z    =       -1426725
70                 Z    =         -434865
99
 XDOT =      -6968
445045                 XDOT =       -2123
982050
 YDOT =     -12347
666909  feet/sec       YDOT =       -3763
568874  meter/sec
 ZDOT =      19776
773834                 ZDOT =        6027
960665


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 32960U 08027A   08169
85623151  
00020000  00000-0  70000-3 0  9095
2 32960  51
6412  12
9967 0010345   5
1949 354
9320 15
75414652  2699


Satellite: SHUTTLE
Catalog Number: 32960
Epoch time:      08169
85623151   =   yrday
fracday
Element set:     909
Inclination:       51
6412  deg
RA of node:        12
9967  deg
Eccentricity:     
0010345     
Arg of perigee:     5
1949  deg
Mean anomaly:     354
9320  deg
Mean motion:   15
75414652  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             269
Checksum:              294

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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