Date: October 13th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4305 56 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 1181)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4389077
46                 A    =         6712764
77  meter
 Y    =        -387754
61  meter          E    =           
0026588
 Z    =       -5087637
69                 I    =           51
33651
 XDOT =       2373
001201                 Wp   =           84
11382
 YDOT =      -7153
238572  meter/sec      RA   =          297
55300  deg
 ZDOT =      -1506
055561                 TA   =          171
37462
                                          MA   =          171
32884
                                          Ha   =            190
386  n
mi
                                          Hp   =            174
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14399860
44                 X    =        -4359700
26
 Y    =       -1272160
81  feet           Y    =         -436671
37  meter
 Z    =      -16691724
70                 Z    =        -5108888
69
 XDOT =       7785
437012                 XDOT =        2460
129557
 YDOT =     -23468
630487  feet/sec       YDOT =       -7126
215174  meter/sec
 ZDOT =      -4941
127169                 ZDOT =       -1494
315890

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14361486
62                 X    =         4377381
12
 Y    =        -265739
98  feet           Y    =          -80997
55  meter
 Z    =      -16770960
96                 Z    =        -5111788
90
 XDOT =      -5276
788183                 XDOT =       -1608
365038
 YDOT =      23122
361378  feet/sec       YDOT =        7047
695748  meter/sec
 ZDOT =      -4898
327464                 ZDOT =       -1493
010211


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
47675535  
00020000  00000-0  20000-3 0  9003
2 25544  51
6353 298
0571 0012827  90
5254 269
7380 15
76840937 11829


Satellite: ISS
Catalog Number: 25544
Epoch time:      06286
47675535   =   yrday
fracday
Element set:     900
Inclination:       51
6353  deg
RA of node:       298
0571  deg
Eccentricity:     
0012827     
Arg of perigee:    90
5254  deg
Mean anomaly:     269
7380  deg
Mean motion:   15
76840937  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1182
Checksum:              314


Coasting Arc #2 (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    =       -2297902
81                 A    =         6723954
71  meter
 Y    =        6302142
55  meter          E    =           
0024467
 Z    =         340442
29                 I    =           51
36150
 XDOT =      -4637
613700                 Wp   =          112
55065
 YDOT =      -1348
476265  meter/sec      RA   =          292
35814  deg
 ZDOT =      -6006
991442                 TA   =           63
72876
                                          MA   =           63
47755
                                          Ha   =            190
362  n
mi
                                          Hp   =            174
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7539051
22                 X    =        -2369857
28
 Y    =       20676320
69  feet           Y    =         6276043
80  meter
 Z    =        1116936
64                 Z    =          329104
24
 XDOT =     -15215
268045                 XDOT =       -4593
009089
 YDOT =      -4424
134729  feet/sec       YDOT =       -1400
087215  meter/sec
 ZDOT =     -19707
977173                 ZDOT =       -6029
412787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4921851
21                 X    =         1500180
25
 Y    =      -21452592
05  feet           Y    =        -6538750
06  meter
 Z    =        1075524
61                 Z    =          327819
90
 XDOT =      13974
022596                 XDOT =        4259
282087
 YDOT =       2156
862767  feet/sec       YDOT =         657
411771  meter/sec
 ZDOT =     -19791
706959                 ZDOT =       -6032
512281


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
49073852  
00020000  00000-0  20000-3 0  9011
2 25544  51
6341 292
8266 0012963  94
0881 266
1765 15
76879414 11982


Satellite: ISS
Catalog Number: 25544
Epoch time:      06287
49073852   =   yrday
fracday
Element set:     901
Inclination:       51
6341  deg
RA of node:       292
8266  deg
Eccentricity:     
0012963     
Arg of perigee:    94
0881  deg
Mean anomaly:     266
1765  deg
Mean motion:   15
76879414  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1198
Checksum:              325


Coasting Arc #3 (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    =        3742915
33                 A    =         6711964
34  meter
 Y    =        1978579
92  meter          E    =           
0015533
 Z    =        5194918
37                 I    =           51
31100
 XDOT =      -2802
792663                 Wp   =           90
79175
 YDOT =       7156
678080  meter/sec      RA   =          287
17583  deg
 ZDOT =       -704
755800                 TA   =            5
93545
                                          MA   =            5
91706
                                          Ha   =            190
200  n
mi
                                          Hp   =            174
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12279905
95                 X    =         3695276
27
 Y    =        6491403
95  feet           Y    =         2020168
99  meter
 Z    =       17043695
42                 Z    =         5212985
81
 XDOT =      -9195
513985                 XDOT =       -2879
187723
 YDOT =      23479
914962  feet/sec       YDOT =        7124
908544  meter/sec
 ZDOT =      -2312
190945                 ZDOT =        -718
557510

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12979653
50                 X    =        -3956198
39
 Y    =       -4706838
14  feet           Y    =        -1434644
26  meter
 Z    =       17111289
81                 Z    =         5215521
13
 XDOT =       5434
405005                 XDOT =        1656
406646
 YDOT =     -23594
227658  feet/sec       YDOT =       -7191
520590  meter/sec
 ZDOT =      -2362
664031                 ZDOT =        -720
139997


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
50470606  
00020000  00000-0  20000-3 0  9023
2 25544  51
6333 287
5964 0012935  97
6398 262
6236 15
76914366 12149


Satellite: ISS
Catalog Number: 25544
Epoch time:      06288
50470606   =   yrday
fracday
Element set:     902
Inclination:       51
6333  deg
RA of node:       287
5964  deg
Eccentricity:     
0012935     
Arg of perigee:    97
6398  deg
Mean anomaly:     262
6236  deg
Mean motion:   15
76914366  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1214
Checksum:              314


Coasting Arc #4 (Orbit 1229)
---------------------------------------

Vector Time (GMT): 2006/289/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2550921
61                 A    =         6722766
08  meter
 Y    =       -6014363
04  meter          E    =           
0025471
 Z    =        1553524
21                 I    =           51
34048
 XDOT =       4016
433622                 Wp   =           80
94526
 YDOT =       3207
171387  meter/sec      RA   =          282
01711  deg
 ZDOT =       5745
260728                 TA   =          296
28824
                                          MA   =          296
54971
                                          Ha   =            190
218  n
mi
                                          Hp   =            174
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8369165
38                 X    =         2610438
67
 Y    =      -19732162
20  feet           Y    =        -5985504
39  meter
 Z    =        5096864
20                 Z    =         1566061
43
 XDOT =      13177
275664                 XDOT =        3952
362452
 YDOT =      10522
215837  feet/sec       YDOT =        3251
727317  meter/sec
 ZDOT =      18849
280604                 ZDOT =        5764
616959

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5116084
14                 X    =        -1559382
45
 Y    =       20802806
38  feet           Y    =         6340695
38  meter
 Z    =        5142772
48                 Z    =         1567517
05
 XDOT =     -13055
271376                 XDOT =       -3979
246715
 YDOT =      -7949
584844  feet/sec       YDOT =       -2423
033460  meter/sec
 ZDOT =      18921
848273                 ZDOT =        5767
379354


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   06289
51865836  
00020000  00000-0  20000-3 0  9039
2 25544  51
6332 282
3667 0012862 101
4547 258
8063 15
76939911 12306


Satellite: ISS
Catalog Number: 25544
Epoch time:      06289
51865836   =   yrday
fracday
Element set:     903
Inclination:       51
6332  deg
RA of node:       282
3667  deg
Eccentricity:     
0012862     
Arg of perigee:   101
4547  deg
Mean anomaly:     258
8063  deg
Mean motion:   15
76939911  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1230
Checksum:              307


Coasting Arc #5 (Orbit 1244)
---------------------------------------

Vector Time (GMT): 2006/290/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3302125
56                 A    =         6714495
45  meter
 Y    =       -3603430
32  meter          E    =           
0023548
 Z    =       -4626452
91                 I    =           51
30750
 XDOT =       3063
033539                 Wp   =          106
86032
 YDOT =      -6451
442897  meter/sec      RA   =          276
79886  deg
 ZDOT =       2843
853086                 TA   =          191
40643
                                          MA   =          191
45989
                                          Ha   =            190
206  n
mi
                                          Hp   =            174
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10833745
26                 X    =        -3239111
40
 Y    =      -11822277
95  feet           Y    =        -3640004
41  meter
 Z    =      -15178651
29                 Z    =        -4642341
55
 XDOT =      10049
322633                 XDOT =        3121
131764
 YDOT =     -21166
151237  feet/sec       YDOT =       -6416
865380  meter/sec
 ZDOT =       9330
226661                 ZDOT =        2858
874865

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12653501
06                 X    =         3856787
12
 Y    =        9757519
74  feet           Y    =         2974092
02  meter
 Z    =      -15238355
11                 Z    =        -4644650
64
 XDOT =      -5426
073230                 XDOT =       -1653
867120
 YDOT =      21666
967020  feet/sec       YDOT =        6604
091548  meter/sec
 ZDOT =       9385
328625                 ZDOT =        2860
648165


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   06290
46922485  
00020000  00000-0  20000-3 0  9040
2 25544  51
6329 277
4626 0012786 104
6711 255
5872 15
76924641 12457


Satellite: ISS
Catalog Number: 25544
Epoch time:      06290
46922485   =   yrday
fracday
Element set:     904
Inclination:       51
6329  deg
RA of node:       277
4626  deg
Eccentricity:     
0012786     
Arg of perigee:   104
6711  deg
Mean anomaly:     255
5872  deg
Mean motion:   15
76924641  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1245
Checksum:              309


Coasting Arc #6 (Orbit 1260)
---------------------------------------

Vector Time (GMT): 2006/291/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2821622
76                 A    =         6718862
10  meter
 Y    =        5109789
26  meter          E    =           
0017509
 Z    =       -3337626
59                 I    =           51
31937
 XDOT =      -3573
947389                 Wp   =          103
86881
 YDOT =      -4990
379095  meter/sec      RA   =          271
66359  deg
 ZDOT =      -4643
186555                 TA   =          115
61512
                                          MA   =          115
43409
                                          Ha   =            190
129  n
mi
                                          Hp   =            174
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9257292
53                 X    =        -2862337
63
 Y    =       16764400
46  feet           Y    =         5078008
47  meter
 Z    =      -10950218
46                 Z    =        -3351433
40
 XDOT =     -11725
549176                 XDOT =       -3495
322595
 YDOT =     -16372
634826  feet/sec       YDOT =       -5029
905610  meter/sec
 ZDOT =     -15233
551690                 ZDOT =       -4660
357749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5807118
78                 X    =         1770009
81
 Y    =      -18218284
10  feet           Y    =        -5552932
99  meter
 Z    =      -11000971
24                 Z    =        -3353096
03
 XDOT =      13239
467896                 XDOT =        4035
389815
 YDOT =      13409
517230  feet/sec       YDOT =        4087
220852  meter/sec
 ZDOT =     -15298
229488                 ZDOT =       -4662
900348


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   06291
48314709  
00020000  00000-0  20000-3 0  9058
2 25544  51
6317 272
2306 0012851 108
6597 251
5964 15
76959617 12618


Satellite: ISS
Catalog Number: 25544
Epoch time:      06291
48314709   =   yrday
fracday
Element set:     905
Inclination:       51
6317  deg
RA of node:       272
2306  deg
Eccentricity:     
0012851     
Arg of perigee:   108
6597  deg
Mean anomaly:     251
5964  deg
Mean motion:   15
76959617  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1261
Checksum:              308


Coasting Arc #7 (Orbit 1276)
---------------------------------------

Vector Time (GMT): 2006/292/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2984349
10                 A    =         6718700
07  meter
 Y    =        4995923
91  meter          E    =           
0024867
 Z    =        3331897
88                 I    =           51
31960
 XDOT =      -3401
520569                 Wp   =          101
17200
 YDOT =       5143
080208  meter/sec      RA   =          266
43012  deg
 ZDOT =      -4640
528146                 TA   =           39
29749
                                          MA   =           39
11728
                                          Ha   =            189
919  n
mi
                                          Hp   =            174
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9791171
59                 X    =         2912076
14
 Y    =       16390826
47  feet           Y    =         5028892
66  meter
 Z    =       10931423
49                 Z    =         3346220
25
 XDOT =     -11159
844386                 XDOT =       -3436
235147
 YDOT =      16873
622730  feet/sec       YDOT =        5104
848139  meter/sec
 ZDOT =     -15224
829875                 ZDOT =       -4657
137659

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12939093
85                 X    =        -3943835
81
 Y    =      -13997183
28  feet           Y    =        -4266341
46  meter
 Z    =       10985488
76                 Z    =         3348376
97
 XDOT =       6286
866255                 XDOT =        1916
236834
 YDOT =     -17871
192657  feet/sec       YDOT =       -5447
139522  meter/sec
 ZDOT =     -15286
019807                 ZDOT =       -4659
178837


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   06292
49705218  
00020000  00000-0  20000-3 0  9060
2 25544  51
6314 266
9994 0012679 111
9369 248
3144 15
77018988 12779


Satellite: ISS
Catalog Number: 25544
Epoch time:      06292
49705218   =   yrday
fracday
Element set:     906
Inclination:       51
6314  deg
RA of node:       266
9994  deg
Eccentricity:     
0012679     
Arg of perigee:   111
9369  deg
Mean anomaly:     248
3144  deg
Mean motion:   15
77018988  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1277
Checksum:              331


Coasting Arc #8 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2006/293/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3145193
21                 A    =         6714274
28  meter
 Y    =       -3744350
59  meter          E    =           
0020872
 Z    =        4589136
99                 I    =           51
30761
 XDOT =       3309
962520                 Wp   =          115
96915
 YDOT =       6341
947340  meter/sec      RA   =          261
29621  deg
 ZDOT =       2886
809929                 TA   =          305
28385
                                          MA   =          305
47892
                                          Ha   =            189
841  n
mi
                                          Hp   =            174
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10318875
35                 X    =         3164535
59
 Y    =      -12284614
79  feet           Y    =        -3709070
88  meter
 Z    =       15056223
73                 Z    =         4604463
88
 XDOT =      10859
457086                 XDOT =        3224
776060
 YDOT =      20806
913844  feet/sec       YDOT =        6378
485039  meter/sec
 ZDOT =       9471
161186                 ZDOT =        2902
682807

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7199879
28                 X    =        -2194523
20
 Y    =       14277431
89  feet           Y    =         4351761
24  meter
 Z    =       15112825
65                 Z    =         4606389
26
 XDOT =     -14181
792513                 XDOT =       -4322
610358
 YDOT =     -17306
898810  feet/sec       YDOT =       -5275
142757  meter/sec
 ZDOT =       9531
193088                 ZDOT =        2905
107653


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   06293
51094217  
00020000  00000-0  20000-3 0  9075
2 25544  51
6311 261
7687 0012619 116
1340 244
1124 15
77033488 12930


Satellite: ISS
Catalog Number: 25544
Epoch time:      06293
51094217   =   yrday
fracday
Element set:     907
Inclination:       51
6311  deg
RA of node:       261
7687  deg
Eccentricity:     
0012619     
Arg of perigee:   116
1340  deg
Mean anomaly:     244
1124  deg
Mean motion:   15
77033488  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1293
Checksum:              277


Coasting Arc #9 (Orbit 1307)
---------------------------------------

Vector Time (GMT): 2006/294/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2772564
71                 A    =         6722364
68  meter
 Y    =       -5919311
50  meter          E    =           
0016052
 Z    =       -1583585
63                 I    =           51
34092
 XDOT =       3895
971501                 Wp   =           89
74193
 YDOT =      -3345
225579  meter/sec      RA   =          256
07718  deg
 ZDOT =       5733
175559                 TA   =          252
70853
                                          MA   =          252
88423
                                          Ha   =            189
901  n
mi
                                          Hp   =            174
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9096340
92                 X    =        -2698475
11
 Y    =      -19420313
33  feet           Y    =        -5949901
68  meter
 Z    =       -5195490
91                 Z    =        -1596874
87
 XDOT =      12782
058729                 XDOT =        3905
237236
 YDOT =     -10975
149538  feet/sec       YDOT =       -3301
606591  meter/sec
 ZDOT =      18809
631099                 ZDOT =        5752
125359

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13503737
21                 X    =         4115939
10
 Y    =       16643779
40  feet           Y    =         5073023
96  meter
 Z    =       -5245836
67                 Z    =        -1598931
02
 XDOT =      -8426
493406                 XDOT =       -2568
395190
 YDOT =      12735
993282  feet/sec       YDOT =        3881
930752  meter/sec
 ZDOT =      18879
790714                 ZDOT =        5754
560210


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   06294
46144940  
00020000  00000-0  20000-3 0  9080
2 25544  51
6312 256
8645 0012826 119
4199 240
8248 15
77056635 13084


Satellite: ISS
Catalog Number: 25544
Epoch time:      06294
46144940   =   yrday
fracday
Element set:     908
Inclination:       51
6312  deg
RA of node:       256
8645  deg
Eccentricity:     
0012826     
Arg of perigee:   119
4199  deg
Mean anomaly:     240
8248  deg
Mean motion:   15
77056635  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1308
Checksum:              306


Coasting Arc #10 (Orbit 1323)
---------------------------------------

Vector Time (GMT): 2006/295/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3724243
30                 A    =         6711549
74  meter
 Y    =        2028296
80  meter          E    =           
0026003
 Z    =       -5223330
76                 I    =           51
31301
 XDOT =      -2975
370067                 Wp   =          102
61960
 YDOT =      -7060
487444  meter/sec      RA   =          250
91509  deg
 ZDOT =       -628
474583                 TA   =          161
41617
                                          MA   =          161
32103
                                          Ha   =            189
791  n
mi
                                          Hp   =            174
788

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12218646
01                 X    =        -3721272
44
 Y    =        6654517
05  feet           Y    =         1986666
69  meter
 Z    =      -17136911
93                 Z    =        -5241416
52
 XDOT =      -9761
712817                 XDOT =       -2893
144470
 YDOT =     -23164
328886  feet/sec       YDOT =       -7093
299956  meter/sec
 ZDOT =      -2061
924486                 ZDOT =        -642
729420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9986543
95                 X    =         3043898
60
 Y    =       -9567745
06  feet           Y    =        -2916248
69  meter
 Z    =      -17204035
93                 Z    =        -5243790
15
 XDOT =      14719
434463                 XDOT =        4486
483624
 YDOT =      19120
280399  feet/sec       YDOT =        5827
861466  meter/sec
 ZDOT =      -2116
026693                 ZDOT =        -644
964936


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   06295
47530754  
00020000  00000-0  20000-3 0  9095
2 25544  51
6317 251
6321 0012646 123
2157 237
0222 15
77056818 13241


Satellite: ISS
Catalog Number: 25544
Epoch time:      06295
47530754   =   yrday
fracday
Element set:     909
Inclination:       51
6317  deg
RA of node:       251
6321  deg
Eccentricity:     
0012646     
Arg of perigee:   123
2157  deg
Mean anomaly:     237
0222  deg
Mean motion:   15
77056818  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1324
Checksum:              278


Coasting Arc #11 (Orbit 1339)
---------------------------------------

Vector Time (GMT): 2006/296/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2377135
83                 A    =         6723267
61  meter
 Y    =        6258285
37  meter          E    =           
0023609
 Z    =        -506595
22                 I    =           51
36420
 XDOT =      -4669
432162                 Wp   =          132
57701
 YDOT =       1303
829627  meter/sec      RA   =          245
73358  deg
 ZDOT =      -5996
035370                 TA   =           52
96640
                                          MA   =           52
75067
                                          Ha   =            189
645  n
mi
                                          Hp   =            174
982

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7799002
08                 X    =         2309439
17
 Y    =       20532432
30  feet           Y    =         6284489
30  meter
 Z    =       -1662057
82                 Z    =         -495211
23
 XDOT =     -15319
659323                 XDOT =       -4654
536136
 YDOT =       4277
656256  feet/sec       YDOT =        1251
696679  meter/sec
 ZDOT =     -19672
032054                 ZDOT =       -6018
684022

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13164057
65                 X    =        -4012404
77
 Y    =      -17585642
65  feet           Y    =        -5360103
88  meter
 Z    =       -1618766
40                 Z    =         -493400
00
 XDOT =      12160
567293                 XDOT =        3706
540911
 YDOT =      -7344
077174  feet/sec       YDOT =       -2238
474723  meter/sec
 ZDOT =     -19756
265865                 ZDOT =       -6021
709836


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   06296
48914873  
00020000  00000-0  20000-3 0  9107
2 25544  51
6324 246
4007 0012542 126
8289 233
4028 15
77100624 13409


Satellite: ISS
Catalog Number: 25544
Epoch time:      06296
48914873   =   yrday
fracday
Element set:     910
Inclination:       51
6324  deg
RA of node:       246
4007  deg
Eccentricity:     
0012542     
Arg of perigee:   126
8289  deg
Mean anomaly:     233
4028  deg
Mean motion:   15
77100624  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1340
Checksum:              278


Coasting Arc #12 (Orbit 1355)
---------------------------------------

Vector Time (GMT): 2006/297/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4441906
34                 A    =         6712189
41  meter
 Y    =        -287340
70  meter          E    =           
0014648
 Z    =        5010867
66                 I    =           51
34009
 XDOT =       2422
362013                 Wp   =          110
61610
 YDOT =       7117
753067  meter/sec      RA   =          240
53485  deg
 ZDOT =      -1740
167437                 TA   =          356
16223
                                          MA   =          356
17345
                                          Ha   =            189
433  n
mi
                                          Hp   =            175
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14573183
53                 X    =         4420446
63
 Y    =        -942718
84  feet           Y    =         -237788
90  meter
 Z    =       16439854
52                 Z    =         5032394
99
 XDOT =       7947
381931                 XDOT =        2351
043959
 YDOT =      23352
208224  feet/sec       YDOT =        7144
442527  meter/sec
 ZDOT =      -5709
210752                 ZDOT =       -1728
572367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13575313
26                 X    =        -4137755
48
 Y    =        5131655
07  feet           Y    =         1564128
46  meter
 Z    =       16520054
47                 Z    =         5035312
60
 XDOT =     -14077
276170                 XDOT =       -4290
753777
 YDOT =     -19013
668777  feet/sec       YDOT =       -5795
366243  meter/sec
 ZDOT =      -5665
014593                 ZDOT =       -1726
696448


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   06297
50297351  
00020000  00000-0  20000-3 0  9117
2 25544  51
6324 241
1702 0012484 130
8932 229
3316 15
77121575 13567


Satellite: ISS
Catalog Number: 25544
Epoch time:      06297
50297351   =   yrday
fracday
Element set:     911
Inclination:       51
6324  deg
RA of node:       241
1702  deg
Eccentricity:     
0012484     
Arg of perigee:   130
8932  deg
Mean anomaly:     229
3316  deg
Mean motion:   15
77121575  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1356
Checksum:              276

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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