Date: October 6th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6027 79 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

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


There are no maneuvers



Coasting Arc #1 (Orbit 1039)
---------------------------------------

Vector Time (GMT): 2006/277/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2748041
94                 A    =         6713686
43  meter
 Y    =       -3428943
56  meter          E    =           
0025844
 Z    =       -5098596
25                 I    =           51
53102
 XDOT =       6819
998941                 Wp   =           68
27095
 YDOT =      -3200
745107  meter/sec      RA   =          344
08340  deg
 ZDOT =      -1520
016506                 TA   =          187
07903
                                          MA   =          187
11560
                                          Ha   =            190
547  n
mi
                                          Hp   =            175
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9015885
63                 X    =        -2684726
65
 Y    =      -11249814
82  feet           Y    =        -3459320
04  meter
 Z    =      -16727678
00                 Z    =        -5111792
24
 XDOT =      22375
324611                 XDOT =        6862
667226
 YDOT =     -10501
132241  feet/sec       YDOT =       -3124
241640  meter/sec
 ZDOT =      -4986
930795                 ZDOT =       -1486
780987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8377512
74                 X    =         2553465
88
 Y    =       11661872
56  feet           Y    =         3554538
76  meter
 Z    =      -16777298
57                 Z    =        -5113720
61
 XDOT =     -22026
840060                 XDOT =       -6713
780850
 YDOT =       8811
230853  feet/sec       YDOT =        2685
663164  meter/sec
 ZDOT =      -4863
529098                 ZDOT =       -1482
403669


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

ISS
1 25544U 98067A   06277
47672869  
00020000  00000-0  20000-3 0  9000
2 25544  51
6369 344
4623 0012384  57
4543 302
7816 15
76514597 10406


Satellite: ISS
Catalog Number: 25544
Epoch time:      06277
47672869   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:       344
4623  deg
Eccentricity:     
0012384     
Arg of perigee:    57
4543  deg
Mean anomaly:     302
7816  deg
Mean motion:   15
76514597  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1040
Checksum:              308


Coasting Arc #2 (Orbit 1055)
---------------------------------------

Vector Time (GMT): 2006/278/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6118121
63                 A    =         6724813
49  meter
 Y    =        2747288
89  meter          E    =           
0021081
 Z    =         454607
07                 I    =           51
54141
 XDOT =      -2352
829967                 Wp   =           96
25345
 YDOT =      -4206
620279  meter/sec      RA   =          338
90416  deg
 ZDOT =      -6007
558104                 TA   =           78
79198
                                          MA   =           78
55508
                                          Ha   =            190
588  n
mi
                                          Hp   =            175
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20072577
52                 X    =        -6150595
90
 Y    =        9013414
99  feet           Y    =         2678691
13  meter
 Z    =        1491493
02                 Z    =          424805
87
 XDOT =      -7719
258421                 XDOT =       -2276
432225
 YDOT =     -13801
247634  feet/sec       YDOT =       -4232
504326  meter/sec
 ZDOT =     -19709
836299                 ZDOT =       -6018
802277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20345571
97                 X    =         6201330
34
 Y    =       -8397950
61  feet           Y    =        -2559695
34  meter
 Z    =        1380831
68                 Z    =          420877
50
 XDOT =       6574
364260                 XDOT =        2003
866226
 YDOT =      12542
661989  feet/sec       YDOT =        3823
003374  meter/sec
 ZDOT =     -19752
290117                 ZDOT =       -6020
498028


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

ISS
1 25544U 98067A   06278
49091654  
00020000  00000-0  20000-3 0  9011
2 25544  51
6362 339
2340 0012596  61
4375 298
8056 15
76564270 10561


Satellite: ISS
Catalog Number: 25544
Epoch time:      06278
49091654   =   yrday
fracday
Element set:     901
Inclination:       51
6362  deg
RA of node:       339
2340  deg
Eccentricity:     
0012596     
Arg of perigee:    61
4375  deg
Mean anomaly:     298
8056  deg
Mean motion:   15
76564270  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1056
Checksum:              304


Coasting Arc #3 (Orbit 1071)
---------------------------------------

Vector Time (GMT): 2006/279/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1375775
48                 A    =         6712675
42  meter
 Y    =        3963233
67  meter          E    =           
0015180
 Z    =        5228885
77                 I    =           51
47540
 XDOT =      -7062
513731                 Wp   =           64
73041
 YDOT =       3072
979145  meter/sec      RA   =          333
73945  deg
 ZDOT =       -463
507618                 TA   =           29
71634
                                          MA   =           29
63020
                                          Ha   =            190
438  n
mi
                                          Hp   =            175
467

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4513699
07                 X    =         1305954
44
 Y    =       13002735
14  feet           Y    =         3978228
47  meter
 Z    =       17155137
05                 Z    =         5235399
41
 XDOT =     -23170
976808                 XDOT =       -7094
099636
 YDOT =      10081
952574  feet/sec       YDOT =        2993
825550  meter/sec
 ZDOT =      -1520
694284                 ZDOT =        -497
894828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4246398
43                 X    =        -1294302
24
 Y    =      -13059911
44  feet           Y    =        -3980661
01  meter
 Z    =       17179934
26                 Z    =         5236443
96
 XDOT =      22341
376111                 XDOT =        6809
651439
 YDOT =      -9464
694876  feet/sec       YDOT =       -2884
838998  meter/sec
 ZDOT =      -1648
392146                 ZDOT =        -502
429926


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

ISS
1 25544U 98067A   06279
50508207  
00020000  00000-0  20000-3 0  9022
2 25544  51
6365 334
0051 0012455  64
6063 295
6390 15
76633998 10727


Satellite: ISS
Catalog Number: 25544
Epoch time:      06279
50508207   =   yrday
fracday
Element set:     902
Inclination:       51
6365  deg
RA of node:       334
0051  deg
Eccentricity:     
0012455     
Arg of perigee:    64
6063  deg
Mean anomaly:     295
6390  deg
Mean motion:   15
76633998  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1072
Checksum:              291


Coasting Arc #4 (Orbit 1087)
---------------------------------------

Vector Time (GMT): 2006/280/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6083017
54                 A    =         6724068
30  meter
 Y    =       -2545713
20  meter          E    =           
0026672
 Z    =        1253619
56                 I    =           51
48782
 XDOT =        845
383377                 Wp   =           63
02532
 YDOT =       4945
652517  meter/sec      RA   =          328
58950  deg
 ZDOT =       5857
724417                 TA   =          310
78351
                                          MA   =          311
01464
                                          Ha   =            190
623  n
mi
                                          Hp   =            175
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19957406
62                 X    =         6104941
96
 Y    =       -8352077
44  feet           Y    =        -2477566
84  meter
 Z    =        4112925
08                 Z    =         1283224
95
 XDOT =       2773
567509                 XDOT =         761
561203
 YDOT =      16225
894084  feet/sec       YDOT =        4954
637865  meter/sec
 ZDOT =      19218
255960                 ZDOT =        5861
627365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19901191
31                 X    =        -6065883
11
 Y    =        8430974
63  feet           Y    =         2569761
07  meter
 Z    =        4222875
82                 Z    =         1287132
55
 XDOT =      -2116
906087                 XDOT =        -645
232975
 YDOT =     -14763
763471  feet/sec       YDOT =       -4499
995106  meter/sec
 ZDOT =      19233
456844                 ZDOT =        5862
357646


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

ISS
1 25544U 98067A   06280
51923174  
00020000  00000-0  20000-3 0  9030
2 25544  51
6357 328
7766 0012767  68
1855 292
0666 15
76605098 10889


Satellite: ISS
Catalog Number: 25544
Epoch time:      06280
51923174   =   yrday
fracday
Element set:     903
Inclination:       51
6357  deg
RA of node:       328
7766  deg
Eccentricity:     
0012767     
Arg of perigee:    68
1855  deg
Mean anomaly:     292
0666  deg
Mean motion:   15
76605098  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1088
Checksum:              321


Coasting Arc #5 (Orbit 1102)
---------------------------------------

Vector Time (GMT): 2006/281/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -122396
78                 A    =         6714542
44  meter
 Y    =       -4695377
93  meter          E    =           
0023480
 Z    =       -4818238
22                 I    =           51
43174
 XDOT =       6800
125772                 Wp   =           88
60916
 YDOT =      -2648
944089  meter/sec      RA   =          323
38884  deg
 ZDOT =       2419
360077                 TA   =          205
06624
                                          MA   =          205
18041
                                          Ha   =            190
595  n
mi
                                          Hp   =            175
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -401564
23                 X    =          -46476
59
 Y    =      -15404783
23  feet           Y    =        -4696322
40  meter
 Z    =      -15807868
18                 Z    =        -4818648
18
 XDOT =      22310
123923                 XDOT =        6817
488117
 YDOT =      -8690
761448  feet/sec       YDOT =       -2572
804110  meter/sec
 ZDOT =       7937
533061                 ZDOT =        2452
438228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         640218
54                 X    =          195138
61
 Y    =       15394501
85  feet           Y    =         4692244
16  meter
 Z    =      -15810019
91                 Z    =        -4818894
07
 XDOT =     -20954
527860                 XDOT =       -6386
940092
 YDOT =       9113
354205  feet/sec       YDOT =        2777
750362  meter/sec
 ZDOT =       8060
407232                 ZDOT =        2456
812124


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

ISS
1 25544U 98067A   06281
46997560  
00020000  00000-0  20000-3 0  9046
2 25544  51
6349 323
8741 0012780  71
5677 288
6876 15
76654695 11033


Satellite: ISS
Catalog Number: 25544
Epoch time:      06281
46997560   =   yrday
fracday
Element set:     904
Inclination:       51
6349  deg
RA of node:       323
8741  deg
Eccentricity:     
0012780     
Arg of perigee:    71
5677  deg
Mean anomaly:     288
6876  deg
Mean motion:   15
76654695  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1103
Checksum:              331


Coasting Arc #6 (Orbit 1118)
---------------------------------------

Vector Time (GMT): 2006/282/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5724592
20                 A    =         6720690
25  meter
 Y    =        1974971
24  meter          E    =           
0016784
 Z    =       -2931313
64                 I    =           51
43131
 XDOT =        539
073569                 Wp   =           84
34203
 YDOT =      -5822
798172  meter/sec      RA   =          318
26071  deg
 ZDOT =      -4998
753269                 TA   =          129
52430
                                          MA   =          129
37583
                                          Ha   =            190
583  n
mi
                                          Hp   =            174
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18781470
46                 X    =        -5732010
97
 Y    =        6479564
42  feet           Y    =         1910914
14  meter
 Z    =       -9617170
73                 Z    =        -2959142
48
 XDOT =       1768
614071                 XDOT =         628
428502
 YDOT =     -19103
668542  feet/sec       YDOT =       -5816
270441  meter/sec
 ZDOT =     -16400
109149                 ZDOT =       -4995
917220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18465821
94                 X    =         5628382
53
 Y    =       -7193195
83  feet           Y    =        -2192486
09  meter
 Z    =       -9720582
01                 Z    =        -2962833
40
 XDOT =      -1649
558404                 XDOT =        -502
785401
 YDOT =      17814
183527  feet/sec       YDOT =        5429
763139  meter/sec
 ZDOT =     -16390
313650                 ZDOT =       -4995
767600


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

ISS
1 25544U 98067A   06282
48408402  
00020000  00000-0  20000-3 0  9052
2 25544  51
6351 318
6440 0012899  75
5895 284
6700 15
76694955 11193


Satellite: ISS
Catalog Number: 25544
Epoch time:      06282
48408402   =   yrday
fracday
Element set:     905
Inclination:       51
6351  deg
RA of node:       318
6440  deg
Eccentricity:     
0012899     
Arg of perigee:    75
5895  deg
Mean anomaly:     284
6700  deg
Mean motion:   15
76694955  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1119
Checksum:              317


Coasting Arc #7 (Orbit 1134)
---------------------------------------

Vector Time (GMT): 2006/283/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -971405
60                 A    =         6718139
00  meter
 Y    =        5458167
65  meter          E    =           
0024375
 Z    =        3777262
01                 I    =           51
40248
 XDOT =      -6234
304890                 Wp   =           80
19156
 YDOT =       1796
583400  meter/sec      RA   =          313
03769  deg
 ZDOT =      -4172
482238                 TA   =           53
71713
                                          MA   =           53
49221
                                          Ha   =            190
510  n
mi
                                          Hp   =            174
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3187026
26                 X    =        -1050717
07
 Y    =       17907374
18  feet           Y    =         5446861
38  meter
 Z    =       12392591
91                 Z    =         3772350
20
 XDOT =     -20453
756202                 XDOT =       -6233
661553
 YDOT =       5894
302494  feet/sec       YDOT =        1726
871575  meter/sec
 ZDOT =     -13689
246189                 ZDOT =       -4202
767614

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2255828
87                 X    =          687576
64
 Y    =      -18060394
74  feet           Y    =        -5504808
32  meter
 Z    =       12375011
05                 Z    =         3771903
37
 XDOT =      18702
114728                 XDOT =        5700
404569
 YDOT =      -7181
571894  feet/sec       YDOT =       -2188
943113  meter/sec
 ZDOT =     -13801
837910                 ZDOT =       -4206
800195


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

ISS
1 25544U 98067A   06283
49817026  
00020000  00000-0  20000-3 0  9061
2 25544  51
6349 313
4144 0012815  78
7287 281
5317 15
76753047 11358


Satellite: ISS
Catalog Number: 25544
Epoch time:      06283
49817026   =   yrday
fracday
Element set:     906
Inclination:       51
6349  deg
RA of node:       313
4144  deg
Eccentricity:     
0012815     
Arg of perigee:    78
7287  deg
Mean anomaly:     281
5317  deg
Mean motion:   15
76753047  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1135
Checksum:              301


Coasting Arc #8 (Orbit 1150)
---------------------------------------

Vector Time (GMT): 2006/284/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5100296
32                 A    =         6716436
76  meter
 Y    =       -1060314
84  meter          E    =           
0022434
 Z    =        4221028
26                 I    =           51
37820
 XDOT =      -1579
018815                 Wp   =           93
21933
 YDOT =       6660
394690  meter/sec      RA   =          307
91434  deg
 ZDOT =       3563
544687                 TA   =          320
46765
                                          MA   =          320
63107
                                          Ha   =            190
476  n
mi
                                          Hp   =            174
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16733255
63                 X    =         5091268
46
 Y    =       -3478723
21  feet           Y    =        -1003331
06  meter
 Z    =       13848517
91                 Z    =         4245784
01
 XDOT =      -5180
507923                 XDOT =       -1670
690294
 YDOT =      21851
688614  feet/sec       YDOT =        6642
224590  meter/sec
 ZDOT =      11691
419576                 ZDOT =        3555
651137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16359574
34                 X    =        -4986398
26
 Y    =        4680650
42  feet           Y    =         1426662
25  meter
 Z    =       13940611
40                 Z    =         4249098
36
 XDOT =       3983
707766                 XDOT =        1214
234127
 YDOT =     -20982
102816  feet/sec       YDOT =       -6395
344938  meter/sec
 ZDOT =      11662
884835                 ZDOT =        3554
847298


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

ISS
1 25544U 98067A   06284
51223817  
00020000  00000-0  20000-3 0  9075
2 25544  51
6345 308
1848 0013029  83
0105 277
2541 15
76758788 11518


Satellite: ISS
Catalog Number: 25544
Epoch time:      06284
51223817   =   yrday
fracday
Element set:     907
Inclination:       51
6345  deg
RA of node:       308
1848  deg
Eccentricity:     
0013029     
Arg of perigee:    83
0105  deg
Mean anomaly:     277
2541  deg
Mean motion:   15
76758788  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1151
Checksum:              295


Coasting Arc #9 (Orbit 1165)
---------------------------------------

Vector Time (GMT): 2006/285/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1703323
84                 A    =         6721854
45  meter
 Y    =       -6078438
47  meter          E    =           
0017811
 Z    =       -2315573
45                 I    =           51
38138
 XDOT =       5458
930928                 Wp   =           73
70400
 YDOT =       -513
843267  meter/sec      RA   =          302
69315  deg
 ZDOT =       5403
652444                 TA   =          260
14307
                                          MA   =          260
34420
                                          Ha   =            190
516  n
mi
                                          Hp   =            174
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5588332
80                 X    =         1782415
98
 Y    =      -19942383
42  feet           Y    =        -6058948
68  meter
 Z    =       -7597025
75                 Z    =        -2307106
61
 XDOT =      17909
878372                 XDOT =        5438
020738
 YDOT =      -1685
837489  feet/sec       YDOT =        -452
915520  meter/sec
 ZDOT =      17728
518516                 ZDOT =        5430
121499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3815622
93                 X    =        -1163001
87
 Y    =       20367508
04  feet           Y    =         6208016
45  meter
 Z    =       -7566277
72                 Z    =        -2306201
45
 XDOT =     -16103
015552                 XDOT =       -4908
199140
 YDOT =       3557
799899  feet/sec       YDOT =        1084
417409  meter/sec
 ZDOT =      17827
073215                 ZDOT =        5433
691916


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

ISS
1 25544U 98067A   06285
46290745  
00020000  00000-0  20000-3 0  9085
2 25544  51
6354 303
2821 0013052  86
6120 273
6537 15
76812602 11664


Satellite: ISS
Catalog Number: 25544
Epoch time:      06285
46290745   =   yrday
fracday
Element set:     908
Inclination:       51
6354  deg
RA of node:       303
2821  deg
Eccentricity:     
0013052     
Arg of perigee:    86
6120  deg
Mean anomaly:     273
6537  deg
Mean motion:   15
76812602  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1166
Checksum:              281


Coasting Arc #10 (Orbit 1181)
---------------------------------------

Vector Time (GMT): 2006/286/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4424989
90                 A    =         6712978
62  meter
 Y    =        -277379
15  meter          E    =           
0026565
 Z    =       -5063916
02                 I    =           51
33742
 XDOT =       2284
033348                 Wp   =           83
68357
 YDOT =      -7159
924585  meter/sec      RA   =          297
54964  deg
 ZDOT =      -1608
012907                 TA   =          170
79844
                                          MA   =          170
74967
                                          Ha   =            190
501  n
mi
                                          Hp   =            174
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14517683
40                 X    =        -4396959
50
 Y    =        -910036
57  feet           Y    =         -326705
02  meter
 Z    =      -16613897
69                 Z    =        -5085344
75
 XDOT =       7493
547730                 XDOT =        2371
738376
 YDOT =     -23490
566223  feet/sec       YDOT =       -7133
892848  meter/sec
 ZDOT =      -5275
632898                 ZDOT =       -1596
704045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14440323
75                 X    =         4401410
68
 Y    =        -638434
65  feet           Y    =         -194594
88  meter
 Z    =      -16693781
65                 Z    =        -5088264
65
 XDOT =      -5013
244959                 XDOT =       -1528
037063
 YDOT =      23107
394401  feet/sec       YDOT =        7043
133813  meter/sec
 ZDOT =      -5234
439353                 ZDOT =       -1595
457115


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

ISS
1 25544U 98067A   06286
47693396  
00020000  00000-0  20000-3 0  9097
2 25544  51
6357 298
0518 0012982  90
2717 269
9936 15
76802421 11822


Satellite: ISS
Catalog Number: 25544
Epoch time:      06286
47693396   =   yrday
fracday
Element set:     909
Inclination:       51
6357  deg
RA of node:       298
0518  deg
Eccentricity:     
0012982     
Arg of perigee:    90
2717  deg
Mean anomaly:     269
9936  deg
Mean motion:   15
76802421  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1182
Checksum:              331


Coasting Arc #11 (Orbit 1197)
---------------------------------------

Vector Time (GMT): 2006/287/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2217101
24                 A    =         6724003
38  meter
 Y    =        6324413
76  meter          E    =           
0024831
 Z    =         443817
46                 I    =           51
36192
 XDOT =      -4688
883286                 Wp   =          111
91218
 YDOT =      -1204
702971  meter/sec      RA   =          292
35328  deg
 ZDOT =      -5998
051947                 TA   =           63
23497
                                          MA   =           62
98113
                                          Ha   =            190
464  n
mi
                                          Hp   =            174
642

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7273954
19                 X    =        -2289812
93
 Y    =       20749388
97  feet           Y    =         6299214
35  meter
 Z    =        1456094
03                 Z    =          432870
11
 XDOT =     -15383
475349                 XDOT =       -4645
925985
 YDOT =      -3952
437569  feet/sec       YDOT =       -1256
896456  meter/sec
 ZDOT =     -19678
648119                 ZDOT =       -6020
726361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4651599
56                 X    =         1417807
55
 Y    =      -21492438
87  feet           Y    =        -6550895
37  meter
 Z    =        1416140
86                 Z    =          431639
73
 XDOT =      14079
667363                 XDOT =        4291
482612
 YDOT =       1687
630107  feet/sec       YDOT =         514
389657  meter/sec
 ZDOT =     -19763
301825                 ZDOT =       -6023
854396


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

ISS
1 25544U 98067A   06287
49093909  
00020000  00000-0  20000-3 0  9106
2 25544  51
6345 292
8215 0013118  93
8503 266
4162 15
76850356 11989


Satellite: ISS
Catalog Number: 25544
Epoch time:      06287
49093909   =   yrday
fracday
Element set:     910
Inclination:       51
6345  deg
RA of node:       292
8215  deg
Eccentricity:     
0013118     
Arg of perigee:    93
8503  deg
Mean anomaly:     266
4162  deg
Mean motion:   15
76850356  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1198
Checksum:              307


Coasting Arc #12 (Orbit 1213)
---------------------------------------

Vector Time (GMT): 2006/288/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3794254
25                 A    =         6711965
08  meter
 Y    =        1844709
14  meter          E    =           
0015587
 Z    =        5206837
00                 I    =           51
31138
 XDOT =      -2709
667943                 Wp   =           91
61418
 YDOT =       7203
939052  meter/sec      RA   =          287
17333  deg
 ZDOT =       -576
655250                 TA   =            3
88451
                                          MA   =            3
87242
                                          Ha   =            190
286  n
mi
                                          Hp   =            174
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12448340
72                 X    =         3748050
44
 Y    =        6052195
34  feet           Y    =         1886880
33  meter
 Z    =       17082798
55                 Z    =         5225157
34
 XDOT =      -8889
986691                 XDOT =       -2787
220696
 YDOT =      23634
970643  feet/sec       YDOT =        7173
204416  meter/sec
 ZDOT =      -1891
913550                 ZDOT =        -590
007370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13084212
84                 X    =        -3988068
07
 Y    =       -4248287
52  feet           Y    =        -1294878
04  meter
 Z    =       17151317
41                 Z    =         5227721
55
 XDOT =       5145
795639                 XDOT =        1568
438511
 YDOT =     -23697
319939  feet/sec       YDOT =       -7222
943117  meter/sec
 ZDOT =      -1940
704881                 ZDOT =        -591
526848


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

ISS
1 25544U 98067A   06288
50492231  
00020000  00000-0  20000-3 0  9111
2 25544  51
6337 287
5914 0013091  97
4515 262
8138 15
76894310 12140


Satellite: ISS
Catalog Number: 25544
Epoch time:      06288
50492231   =   yrday
fracday
Element set:     911
Inclination:       51
6337  deg
RA of node:       287
5914  deg
Eccentricity:     
0013091     
Arg of perigee:    97
4515  deg
Mean anomaly:     262
8138  deg
Mean motion:   15
76894310  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1214
Checksum:              293

INTERNATIONAL SPACE STATION 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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