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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