Date: December 18th 2006

SHUTTLE TRAJECTORY DATA

Lift off time (UTC) : 2006/344/01:47:34 973 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 06121

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


353/22:38:38 130 0 3 -0 0 1 5
009/20:51:03 157 -1 3 0 0 193 3
000/00:00:06 314 -0 7 -1 5 176 2

353/23:06:56 004 4 8 -10 0 10 0
009/21:19:21 031 -8 5 0 0 189 4
000/00:00:42 062 -2 1 0 0 174 3

353/23:52:12 667 -8 4 -18 2 18 2
009/22:04:37 694 15 6 -0 0 186 5
000/00:00:13 651 4 1 0 0 166 3

355/18:52:39 169 0 6 2 0 2 0
011/17:05:04 196 1 2 -0 0 187 9
000/00:00:08 392 1 4 0 0 165 8

Coasting Arc #1 (Orbit 129)
---------------------------------------

Vector Time (GMT): 2006/352/04:36:48
000
Vector Time (MET): 008/02:49:13
027
Weight (LBS)     : 237484
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1850925
59                 A    =         6714670
34  meter
 Y    =        3874428
70  meter          E    =           
0025074
 Z    =        5167870
94                 I    =           51
40571
 XDOT =      -6221
940405                 Wp   =          355
44037
 YDOT =       4411
622294  meter/sec      RA   =          318
32522  deg
 ZDOT =      -1054
721938                 TA   =          104
79239
                                          MA   =          104
51445
                                          Ha   =            193
235  n
mi
                                          Hp   =            176
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6072590
53                 X    =         1782341
32
 Y    =       12711380
25  feet           Y    =         3894750
52  meter
 Z    =       16954957
16                 Z    =         5176696
94
 XDOT =     -20413
190304                 XDOT =       -6265
705013
 YDOT =      14473
826423  feet/sec       YDOT =        4341
772721  meter/sec
 ZDOT =      -3460
373811                 ZDOT =       -1085
054078

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -77942
70                 X    =          -23756
94
 Y    =      -14046857
06  feet           Y    =        -4281482
03  meter
 Z    =       16988403
33                 Z    =         5178065
34
 XDOT =      23565
414840                 XDOT =        7182
738443
 YDOT =      -4548
531121  feet/sec       YDOT =       -1386
392286  meter/sec
 ZDOT =      -3573
316311                 ZDOT =       -1089
146811


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 29647U 06055A   06352
23797990  
00014500  00000-0  95600-4 0  9002
2 29647  51
6364 318
6403 0023433 347
7778  12
2815 15
76049418  1306


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06352
23797990   =   yrday
fracday
Element set:     900
Inclination:       51
6364  deg
RA of node:       318
6403  deg
Eccentricity:     
0023433     
Arg of perigee:   347
7778  deg
Mean anomaly:      12
2815  deg
Mean motion:   15
76049418  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             130
Checksum:              315


Coasting Arc #2 (Orbit 145)
---------------------------------------

Vector Time (GMT): 2006/353/04:41:20
487
Vector Time (MET): 009/02:53:45
514
Weight (LBS)     : 237484
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5505966
20                 A    =         6722150
00  meter
 Y    =       -2313620
68  meter          E    =           
0026160
 Z    =        3047893
35                 I    =           51
41041
 XDOT =       -211
298897                 Wp   =           21
55764
 YDOT =       5952
734950  meter/sec      RA   =          313
17584  deg
 ZDOT =       4911
083147                 TA   =           14
00247
                                          MA   =           13
93008
                                          Ha   =            193
281  n
mi
                                          Hp   =            176
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18064193
57                 X    =         5516632
01
 Y    =       -7590619
03  feet           Y    =        -2251966
26  meter
 Z    =        9999650
09                 Z    =         3074667
07
 XDOT =       -693
237850                 XDOT =        -301
731449
 YDOT =      19529
970310  feet/sec       YDOT =        5949
864367  meter/sec
 ZDOT =      16112
477516                 ZDOT =        4909
838128

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19542869
62                 X    =        -5956666
66
 Y    =          36953
12  feet           Y    =           11263
31  meter
 Z    =       10099528
20                 Z    =         3078336
20
 XDOT =       8275
891095                 XDOT =        2522
491606
 YDOT =     -16283
185477  feet/sec       YDOT =       -4963
114933  meter/sec
 ZDOT =      16108
491622                 ZDOT =        4909
868246


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 29647U 06055A   06353
25250071  
00014500  00000-0  95600-4 0  9010
2 29647  51
6361 313
4142 0023355 351
9857   8
0930 15
76068708  1465


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06353
25250071   =   yrday
fracday
Element set:     901
Inclination:       51
6361  deg
RA of node:       313
4142  deg
Eccentricity:     
0023355     
Arg of perigee:   351
9857  deg
Mean anomaly:       8
0930  deg
Mean motion:   15
76068708  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             146
Checksum:              292


Coasting Arc #3 (Orbit 156)
---------------------------------------

Vector Time (GMT): 2006/353/22:38:41
287
Vector Time (MET): 009/20:51:06
314
Weight (LBS)     : 237442
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1448890
71                 A    =         6721915
07  meter
 Y    =       -5745652
22  meter          E    =           
0023825
 Z    =       -3148179
14                 I    =           51
39307
 XDOT =       5908
914205                 Wp   =            4
61279
 YDOT =      -1140
307534  meter/sec      RA   =          309
25520  deg
 ZDOT =       4826
527505                 TA   =          318
48827
                                          MA   =          318
66898
                                          Ha   =            193
298  n
mi
                                          Hp   =            176
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4753578
46                 X    =         1528350
66
 Y    =      -18850565
04  feet           Y    =        -5728998
36  meter
 Z    =      -10328671
72                 Z    =        -3140948
53
 XDOT =      19386
201461                 XDOT =        5897
784374
 YDOT =      -3741
166450  feet/sec       YDOT =       -1074
267633  meter/sec
 ZDOT =      15835
063992                 ZDOT =        4855
205932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15539294
92                 X    =        -4736377
09
 Y    =      -11705350
70  feet           Y    =        -3567790
89  meter
 Z    =      -10302273
94                 Z    =        -3140133
10
 XDOT =       3133
281928                 XDOT =         955
024332
 YDOT =     -18115
792492  feet/sec       YDOT =       -5521
693552  meter/sec
 ZDOT =      15942
204592                 ZDOT =        4859
183959


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 29647U 06055A   06353
94996715  
00014500  00000-0  95600-4 0  9029
2 29647  51
6335 309
8174 0022938 353
9218   6
1664 15
76090725  1578


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06353
94996715   =   yrday
fracday
Element set:     902
Inclination:       51
6335  deg
RA of node:       309
8174  deg
Eccentricity:     
0022938     
Arg of perigee:   353
9218  deg
Mean anomaly:       6
1664  deg
Mean motion:   15
76090725  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             157
Checksum:              334


Coasting Arc #4 (Orbit 157)
---------------------------------------

Vector Time (GMT): 2006/353/23:07:17
035
Vector Time (MET): 009/21:19:42
062
Weight (LBS)     : 237168
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4160013
31                 A    =         6709444
58  meter
 Y    =        1338671
76  meter          E    =           
0019311
 Z    =        5092858
68                 I    =           51
36842
 XDOT =      -3837
245946                 Wp   =          340
12885
 YDOT =       6526
185210  meter/sec      RA   =          309
18867  deg
 ZDOT =       1438
462318                 TA   =           96
15644
                                          MA   =           95
93639
                                          Ha   =            189
400  n
mi
                                          Hp   =            174
288

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13648337
63                 X    =         4119988
40
 Y    =        4391967
71  feet           Y    =         1384984
99  meter
 Z    =       16708853
93                 Z    =         5112971
20
 XDOT =     -12589
389588                 XDOT =       -3916
954235
 YDOT =      21411
368798  feet/sec       YDOT =        6482
811732  meter/sec
 ZDOT =       4719
364560                 ZDOT =        1419
628561

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7855695
39                 X    =         2394415
96
 Y    =      -11888222
53  feet           Y    =        -3623530
23  meter
 Z    =       16784234
12                 Z    =         5115834
56
 XDOT =      16392
945550                 XDOT =        4996
569804
 YDOT =      17307
036057  feet/sec       YDOT =        5275
184590  meter/sec
 ZDOT =       4649
654087                 ZDOT =        1417
214566


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 29647U 06055A   06354
01329714  
00014500  00000-0  95600-4 0  9038
2 29647  51
6332 309
4894 0023148 334
2277  25
7733 15
77973578  1583


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06354
01329714   =   yrday
fracday
Element set:     903
Inclination:       51
6332  deg
RA of node:       309
4894  deg
Eccentricity:     
0023148     
Arg of perigee:   334
2277  deg
Mean anomaly:      25
7733  deg
Mean motion:   15
77973578  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             158
Checksum:              328


Coasting Arc #5 (Orbit 157)
---------------------------------------

Vector Time (GMT): 2006/353/23:52:19
493
Vector Time (MET): 009/22:04:44
520
Weight (LBS)     : 236743
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4317526
74                 A    =         6700052
85  meter
 Y    =       -1061942
93  meter          E    =           
0032643
 Z    =       -5033707
67                 I    =           51
37019
 XDOT =       3607
493498                 Wp   =           31
22681
 YDOT =      -6584
999339  meter/sec      RA   =          309
03044  deg
 ZDOT =      -1682
367696                 TA   =          222
39358
                                          MA   =          222
64623
                                          Ha   =            186
510  n
mi
                                          Hp   =            166
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14165113
98                 X    =        -4280873
12
 Y    =       -3484064
72  feet           Y    =        -1110037
14  meter
 Z    =      -16514788
94                 Z    =        -5054593
52
 XDOT =      11835
608589                 XDOT =        3689
061657
 YDOT =     -21604
328541  feet/sec       YDOT =       -6544
185654  meter/sec
 ZDOT =      -5519
579054                 ZDOT =       -1664
645582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4508617
29                 X    =        -1374226
55
 Y    =       13779372
83  feet           Y    =         4199952
84  meter
 Z    =      -16593030
74                 Z    =        -5057555
77
 XDOT =     -19669
232170                 XDOT =       -5995
181966
 YDOT =     -13092
552467  feet/sec       YDOT =       -3990
609992  meter/sec
 ZDOT =      -5454
033089                 ZDOT =       -1662
389286


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 29647U 06055A   06354
01328444  
00014500  00000-0  95600-4 0  9048
2 29647  51
6346 309
4908 0025132   8
6380 351
5214 15
81393088  1587


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06354
01328444   =   yrday
fracday
Element set:     904
Inclination:       51
6346  deg
RA of node:       309
4908  deg
Eccentricity:     
0025132     
Arg of perigee:     8
6380  deg
Mean anomaly:     351
5214  deg
Mean motion:   15
81393088  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             158
Checksum:              302


Coasting Arc #6 (Orbit 173)
---------------------------------------

Vector Time (GMT): 2006/354/23:53:46
359
Vector Time (MET): 010/22:06:11
386
Weight (LBS)     : 236743
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4580681
92                 A    =         6710080
44  meter
 Y    =        4688067
78  meter          E    =           
0020745
 Z    =       -1498837
19                 I    =           51
38733
 XDOT =      -2603
799832                 Wp   =           29
88199
 YDOT =      -4380
837866  meter/sec      RA   =          303
81312  deg
 ZDOT =      -5761
284885                 TA   =          166
69422
                                          MA   =          166
63943
                                          Ha   =            186
630  n
mi
                                          Hp   =            166
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15028483
99                 X    =        -4625503
72
 Y    =       15380799
80  feet           Y    =         4636573
20  meter
 Z    =       -4917444
85                 Z    =        -1521198
07
 XDOT =      -8542
650367                 XDOT =       -2526
612208
 YDOT =     -14372
827645  feet/sec       YDOT =       -4409
533692  meter/sec
 ZDOT =     -18901
853298                 ZDOT =       -5773
747559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14611778
82                 X    =         4453670
18
 Y    =       15751060
50  feet           Y    =         4800923
24  meter
 Z    =       -5000561
00                 Z    =        -1524170
99
 XDOT =     -13627
939876                 XDOT =       -4153
796074
 YDOT =       6643
317047  feet/sec       YDOT =        2024
883036  meter/sec
 ZDOT =     -18948
969026                 ZDOT =       -5775
645759


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 29647U 06055A   06355
02436505  
00014500  00000-0  95600-4 0  9059
2 29647  51
6344 304
2393 0025148  12
5192 347
6594 15
81430323  1747


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06355
02436505   =   yrday
fracday
Element set:     905
Inclination:       51
6344  deg
RA of node:       304
2393  deg
Eccentricity:     
0025148     
Arg of perigee:    12
5192  deg
Mean anomaly:     347
6594  deg
Mean motion:   15
81430323  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             174
Checksum:              293


Coasting Arc #7 (Orbit 186)
---------------------------------------

Vector Time (GMT): 2006/355/18:52:43
365
Vector Time (MET): 011/17:05:08
392
Weight (LBS)     : 236689
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4445445
67                 A    =         6710353
33  meter
 Y    =       -4578439
51  meter          E    =           
0037245
 Z    =        1993794
87                 I    =           51
37283
 XDOT =       2410
599508                 Wp   =           32
66102
 YDOT =       4779
714435  meter/sec      RA   =          299
69863  deg
 ZDOT =       5584
020749                 TA   =          349
77975
                                          MA   =          349
85527
                                          Ha   =            187
859  n
mi
                                          Hp   =            165
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14584795
51                 X    =         4486646
79
 Y    =      -15021126
99  feet           Y    =        -4528478
16  meter
 Z    =        6541321
76                 Z    =         2015489
93
 XDOT =       7908
791036                 XDOT =        2329
825419
 YDOT =      15681
477805  feet/sec       YDOT =        4806
228932  meter/sec
 ZDOT =      18320
278047                 ZDOT =        5595
536146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10905006
78                 X    =         3323846
07
 Y    =      -17842921
47  feet           Y    =        -5438522
46  meter
 Z    =        6621962
46                 Z    =         2018374
16
 XDOT =       9751
125891                 XDOT =        2972
143172
 YDOT =      12795
421336  feet/sec       YDOT =        3900
044423  meter/sec
 ZDOT =      18363
901746                 ZDOT =        5597
317252


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 29647U 06055A   06355
84586762  
00014500  00000-0  95600-4 0  9061
2 29647  51
6345 299
9774 0027081  15
2323 344
9653 15
81070762  1872


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06355
84586762   =   yrday
fracday
Element set:     906
Inclination:       51
6345  deg
RA of node:       299
9774  deg
Eccentricity:     
0027081     
Arg of perigee:    15
2323  deg
Mean anomaly:     344
9653  deg
Mean motion:   15
81070762  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             187
Checksum:              340


Coasting Arc #8 (Orbit 201)
---------------------------------------

Vector Time (GMT): 2006/356/18:54:28
028
Vector Time (MET): 012/17:06:53
055
Weight (LBS)     : 236689
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          69294
49                 A    =         6708119
34  meter
 Y    =       -5980845
78  meter          E    =           
0030015
 Z    =       -3015237
16                 I    =           51
35125
 XDOT =       5427
520634                 Wp   =           25
70348
 YDOT =      -2402
909313  meter/sec      RA   =          294
43796  deg
 ZDOT =       4935
910961                 TA   =          299
09981
                                          MA   =          299
40001
                                          Ha   =            188
033  n
mi
                                          Hp   =            165
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         227344
14                 X    =          150842
03
 Y    =      -19622197
45  feet           Y    =        -5979613
90  meter
 Z    =       -9892510
38                 Z    =        -3014703
55
 XDOT =      17806
826226                 XDOT =        5430
019830
 YDOT =      -7883
560738  feet/sec       YDOT =       -2342
178464  meter/sec
 ZDOT =      16193
933598                 ZDOT =        4962
283254

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4498213
11                 X    =        -1371055
36
 Y    =      -19101682
56  feet           Y    =        -5822192
85  meter
 Z    =       -9891202
24                 Z    =        -3014838
44
 XDOT =      13874
788800                 XDOT =        4229
035626
 YDOT =     -11627
501815  feet/sec       YDOT =       -3544
062553  meter/sec
 ZDOT =      16292
325348                 ZDOT =        4965
900766


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 29647U 06055A   06356
79395623  
00014500  00000-0  95600-4 0  9071
2 29647  51
6336 295
0563 0027060  18
9856 341
2313 15
81071698  2023


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06356
79395623   =   yrday
fracday
Element set:     907
Inclination:       51
6336  deg
RA of node:       295
0563  deg
Eccentricity:     
0027060     
Arg of perigee:    18
9856  deg
Mean anomaly:     341
2313  deg
Mean motion:   15
81071698  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             202
Checksum:              321


Coasting Arc #9 (Orbit 217)
---------------------------------------

Vector Time (GMT): 2006/357/18:56:29
004
Vector Time (MET): 013/17:08:54
031
Weight (LBS)     : 236689
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4014692
04                 A    =         6699904
77  meter
 Y    =       -1236101
92  meter          E    =           
0035915
 Z    =       -5241949
04                 I    =           51
31212
 XDOT =       2440
681264                 Wp   =           45
51914
 YDOT =      -7294
567539  meter/sec      RA   =          289
24445  deg
 ZDOT =       -124
856785                 TA   =          223
14835
                                          MA   =          223
43036
                                          Ha   =            188
063  n
mi
                                          Hp   =            165
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13171561
81                 X    =        -3975101
54
 Y    =       -4055452
50  feet           Y    =        -1280792
08  meter
 Z    =      -17197995
55                 Z    =        -5261356
22
 XDOT =       8007
484461                 XDOT =        2522
707700
 YDOT =     -23932
308198  feet/sec       YDOT =       -7266
804758  meter/sec
 ZDOT =       -409
635123                 ZDOT =        -112
802005

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13684687
38                 X    =        -4171092
71
 Y    =        -397695
79  feet           Y    =         -121217
68  meter
 Z    =      -17270754
35                 Z    =        -5264125
93
 XDOT =       1264
687859                 XDOT =         385
476859
 YDOT =     -24205
982478  feet/sec       YDOT =       -7377
983459  meter/sec
 ZDOT =       -365
381041                 ZDOT =        -111
368141


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 29647U 06055A   06357
80522843  
00014500  00000-0  95600-4 0  9081
2 29647  51
6325 289
8070 0027014  23
1271 337
1105 15
81117567  2189


Satellite: SHUTTLE
Catalog Number: 29647
Epoch time:      06357
80522843   =   yrday
fracday
Element set:     908
Inclination:       51
6325  deg
RA of node:       289
8070  deg
Eccentricity:     
0027014     
Arg of perigee:    23
1271  deg
Mean anomaly:     337
1105  deg
Mean motion:   15
81117567  rev/day
Decay rate:    1
45000E-04  rev/day^2
Epoch rev:             218
Checksum:              297

SPACE SHUTTLE ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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