Date: October 27th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7620 85 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


299/14:46:00 000 0 0 0 0 0 0
N/A 0 0 0 0 188 9
000/00:00:00 000 0 0 0 0 175 2

Coasting Arc #1 (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    =        2356876
87                 A    =         6723086
83  meter
 Y    =        6263722
92  meter          E    =           
0023452
 Z    =        -531471
93                 I    =           51
36294
 XDOT =      -4682
803438                 Wp   =          132
99530
 YDOT =       1268
922161  meter/sec      RA   =          245
74045  deg
 ZDOT =      -5993
181857                 TA   =           52
82147
                                          MA   =           52
60757
                                          Ha   =            189
507  n
mi
                                          Hp   =            174
944

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7732535
67                 X    =         2289241
76
 Y    =       20550272
03  feet           Y    =         6289700
65  meter
 Z    =       -1743674
30                 Z    =         -520186
21
 XDOT =     -15363
528339                 XDOT =       -4667
529940
 YDOT =       4163
130449  feet/sec       YDOT =        1216
641799  meter/sec
 ZDOT =     -19662
670134                 ZDOT =       -6015
894551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13105515
57                 X    =        -3994561
15
 Y    =      -17620984
79  feet           Y    =        -5370876
16  meter
 Z    =       -1700748
41                 Z    =         -518388
11
 XDOT =      12231
770568                 XDOT =        3728
243669
 YDOT =      -7250
358405  feet/sec       YDOT =       -2209
909242  meter/sec
 ZDOT =     -19747
147447                 ZDOT =       -6018
930542


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
48909882  
00020000  00000-0  20000-3 0  9000
2 25544  51
6313 246
4079 0012436 127
4403 232
7895 15
77160426 13403


Satellite: ISS
Catalog Number: 25544
Epoch time:      06296
48909882   =   yrday
fracday
Element set:     900
Inclination:       51
6313  deg
RA of node:       246
4079  deg
Eccentricity:     
0012436     
Arg of perigee:   127
4403  deg
Mean anomaly:     232
7895  deg
Mean motion:   15
77160426  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1340
Checksum:              295


Coasting Arc #2 (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    =        4461117
15                 A    =         6712024
68  meter
 Y    =        -229988
55  meter          E    =           
0014587
 Z    =        4996568
91                 I    =           51
33906
 XDOT =       2374
504157                 Wp   =          110
65519
 YDOT =       7120
784461  meter/sec      RA   =          240
54039  deg
 ZDOT =      -1793
159217                 TA   =          356
65098
                                          MA   =          356
66074
                                          Ha   =            189
264  n
mi
                                          Hp   =            175
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14636211
13                 X    =         4439084
15
 Y    =        -754555
61  feet           Y    =         -180225
13  meter
 Z    =       16392942
62                 Z    =         5018188
18
 XDOT =       7790
367970                 XDOT =        2303
413196
 YDOT =      23362
153744  feet/sec       YDOT =        7146
940019  meter/sec
 ZDOT =      -5883
068297                 ZDOT =       -1781
796096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13690797
27                 X    =        -4172955
01
 Y    =        4970180
32  feet           Y    =         1514910
96  meter
 Z    =       16473493
13                 Z    =         5021120
71
 XDOT =     -13942
709319                 XDOT =       -4249
737800
 YDOT =     -19060
339843  feet/sec       YDOT =       -5809
591584  meter/sec
 ZDOT =      -5839
736278                 ZDOT =       -1779
951617


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
50287818  
00020000  00000-0  20000-3 0  9013
2 25544  51
6314 241
1769 0012385 131
6000 228
6228 15
77201467 13567


Satellite: ISS
Catalog Number: 25544
Epoch time:      06297
50287818   =   yrday
fracday
Element set:     901
Inclination:       51
6314  deg
RA of node:       241
1769  deg
Eccentricity:     
0012385     
Arg of perigee:   131
6000  deg
Mean anomaly:     228
6228  deg
Mean motion:   15
77201467  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1356
Checksum:              282


Coasting Arc #3 (Orbit 1371)
---------------------------------------

Vector Time (GMT): 2006/298/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1664060
25                 A    =         6720082
69  meter
 Y    =       -5989219
31  meter          E    =           
0022796
 Z    =        2543138
93                 I    =           51
38228
 XDOT =       5587
810554                 Wp   =          104
44939
 YDOT =        700
103380  meter/sec      RA   =          235
39749  deg
 ZDOT =       5260
187734                 TA   =          284
53905
                                          MA   =          284
79179
                                          Ha   =            189
232  n
mi
                                          Hp   =            175
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5459515
26                 X    =        -1609318
77
 Y    =      -19649669
65  feet           Y    =        -6007521
77  meter
 Z    =        8343631
66                 Z    =         2535187
44
 XDOT =      18332
711790                 XDOT =        5554
012796
 YDOT =       2296
927101  feet/sec       YDOT =         762
400213  meter/sec
 ZDOT =      17257
833774                 ZDOT =        5287
252056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11298611
05                 X    =         3443816
65
 Y    =       16993074
73  feet           Y    =         5179489
18  meter
 Z    =        8313171
06                 Z    =         2533854
54
 XDOT =     -16817
072945                 XDOT =       -5125
843834
 YDOT =       2617
195106  feet/sec       YDOT =         797
721068  meter/sec
 ZDOT =      17358
815663                 ZDOT =        5290
967014


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   06298
51662640  
00020000  00000-0  20000-3 0  9026
2 25544  51
6317 235
9453 0012423 136
0754 224
1401 15
77275372 13727


Satellite: ISS
Catalog Number: 25544
Epoch time:      06298
51662640   =   yrday
fracday
Element set:     902
Inclination:       51
6317  deg
RA of node:       235
9453  deg
Eccentricity:     
0012423     
Arg of perigee:   136
0754  deg
Mean anomaly:     224
1401  deg
Mean motion:   15
77275372  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1372
Checksum:              275


Coasting Arc #4 (Orbit 1386)
---------------------------------------

Vector Time (GMT): 2006/299/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5265902
10                 A    =         6715962
05  meter
 Y    =       -1384386
15  meter          E    =           
0018649
 Z    =       -3952979
39                 I    =           51
38577
 XDOT =      -1273
003471                 Wp   =          128
22607
 YDOT =      -6466
431446  meter/sec      RA   =          230
17006  deg
 ZDOT =       3961
731265                 TA   =          183
01961
                                          MA   =          183
03089
                                          Ha   =            189
094  n
mi
                                          Hp   =            175
102

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17276581
70                 X    =        -5230826
96
 Y    =       -4541949
31  feet           Y    =        -1443076
06  meter
 Z    =      -12969092
50                 Z    =        -3978476
69
 XDOT =      -4176
520574                 XDOT =       -1219
846203
 YDOT =     -21215
326265  feet/sec       YDOT =       -6480
369866  meter/sec
 ZDOT =      12997
805986                 ZDOT =        3955
675635

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17747098
14                 X    =         5409315
51
 Y    =       -1292503
79  feet           Y    =         -393955
15  meter
 Z    =      -13064336
20                 Z    =        -3982009
67
 XDOT =      10814
424434                 XDOT =        3296
236568
 YDOT =      17391
243288  feet/sec       YDOT =        5300
850954  meter/sec
 ZDOT =      12974
345893                 ZDOT =        3954
580628


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   06299
46699006  
00020000  00000-0  20000-3 0  9038
2 25544  51
6316 231
0402 0012260 139
3180 220
8902 15
77279211 13876


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
46699006   =   yrday
fracday
Element set:     903
Inclination:       51
6316  deg
RA of node:       231
0402  deg
Eccentricity:     
0012260     
Arg of perigee:   139
3180  deg
Mean anomaly:     220
8902  deg
Mean motion:   15
77279211  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1387
Checksum:              276


Coasting Arc #5 (Orbit 1389)
---------------------------------------

Vector Time (GMT): 2006/299/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5042530
63                 A    =         6714155
03  meter
 Y    =         493813
37  meter          E    =           
0017497
 Z    =        4388081
39                 I    =           51
38563
 XDOT =       2218
813173                 Wp   =          110
19076
 YDOT =       6619
832410  meter/sec      RA   =          229
36042  deg
 ZDOT =      -3290
100972                 TA   =           12
89445
                                          MA   =           12
84977
                                          Ha   =            188
862  n
mi
                                          Hp   =            175
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16543735
67                 X    =         5015316
92
 Y    =        1620122
61  feet           Y    =          550049
35  meter
 Z    =       14396592
48                 Z    =         4412512
55
 XDOT =       7279
570777                 XDOT =        2160
607504
 YDOT =      21718
610270  feet/sec       YDOT =        6644
319143  meter/sec
 ZDOT =     -10794
294529                 ZDOT =       -3279
462728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5661312
07                 X    =        -1725567
92
 Y    =       15544669
79  feet           Y    =         4738015
35  meter
 Z    =       14487741
33                 Z    =         4415863
56
 XDOT =     -21727
751488                 XDOT =       -6622
618654
 YDOT =       2123
345539  feet/sec       YDOT =         647
195720  meter/sec
 ZDOT =     -10753
728734                 ZDOT =       -3277
736518


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   06299
65705865  
00020000  00000-0  20000-3 0  9041
2 25544  51
6342 230
0602 0012205 139
9033 220
3035 15
77334890 13909


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
65705865   =   yrday
fracday
Element set:     904
Inclination:       51
6342  deg
RA of node:       230
0602  deg
Eccentricity:     
0012205     
Arg of perigee:   139
9033  deg
Mean anomaly:     220
3035  deg
Mean motion:   15
77334890  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1390
Checksum:              272


Coasting Arc #6 (Orbit 1405)
---------------------------------------

Vector Time (GMT): 2006/300/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1327870
10                 A    =         6716695
26  meter
 Y    =       -5430727
73  meter          E    =           
0021990
 Z    =        3715928
21                 I    =           51
41359
 XDOT =       6281
940680                 Wp   =          120
65757
 YDOT =       1388
788160  meter/sec      RA   =          224
23213  deg
 ZDOT =       4244
861284                 TA   =          284
42753
                                          MA   =          284
67146
                                          Ha   =            188
945  n
mi
                                          Hp   =            175
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4356529
20                 X    =        -1285095
94
 Y    =      -17817348
20  feet           Y    =        -5445337
77  meter
 Z    =       12191365
52                 Z    =         3709580
86
 XDOT =      20610
041600                 XDOT =        6245
322966
 YDOT =       4556
391602  feet/sec       YDOT =        1458
831309  meter/sec
 ZDOT =      13926
710250                 ZDOT =        4275
290731

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18357619
11                 X    =         5595402
31
 Y    =        -172191
07  feet           Y    =          -52483
84  meter
 Z    =       12166955
55                 Z    =         3708488
05
 XDOT =      -9205
279948                 XDOT =       -2805
769328
 YDOT =      17578
264845  feet/sec       YDOT =        5357
855125  meter/sec
 ZDOT =      14040
356602                 ZDOT =        4279
500692


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   06300
67074563  
00020000  00000-0  20000-3 0  9051
2 25544  51
6342 224
8277 0012243 143
7880 216
4116 15
77338986 14067


Satellite: ISS
Catalog Number: 25544
Epoch time:      06300
67074563   =   yrday
fracday
Element set:     905
Inclination:       51
6342  deg
RA of node:       224
8277  deg
Eccentricity:     
0012243     
Arg of perigee:   143
7880  deg
Mean anomaly:     216
4116  deg
Mean motion:   15
77338986  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1406
Checksum:              290


Coasting Arc #7 (Orbit 1420)
---------------------------------------

Vector Time (GMT): 2006/301/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5828470
65                 A    =         6718994
73  meter
 Y    =       -1832347
19  meter          E    =           
0013316
 Z    =       -2815967
99                 I    =           51
44327
 XDOT =       -647
793768                 Wp   =          128
08255
 YDOT =      -5737
864203  meter/sec      RA   =          219
00508  deg
 ZDOT =       5082
622246                 TA   =          199
55489
                                          MA   =          199
60601
                                          Ha   =            188
697  n
mi
                                          Hp   =            175
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19122279
03                 X    =        -5793868
21
 Y    =       -6011637
77  feet           Y    =        -1897330
76  meter
 Z    =       -9238740
14                 Z    =        -2844199
22
 XDOT =      -2125
307639                 XDOT =        -608
274894
 YDOT =     -18825
013791  feet/sec       YDOT =       -5744
887508  meter/sec
 ZDOT =      16675
269836                 ZDOT =        5079
570892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9972769
35                 X    =         3039700
10
 Y    =      -17331597
18  feet           Y    =        -5282670
82  meter
 Z    =       -9344264
23                 Z    =        -2848131
74
 XDOT =      17597
650808                 XDOT =        5363
763966
 YDOT =       1156
354702  feet/sec       YDOT =         352
456913  meter/sec
 ZDOT =      16663
102620                 ZDOT =        5078
913679


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   06301
62104901  
00020000  00000-0  20000-3 0  9068
2 25544  51
6339 219
9221 0012107 148
1104 212
0796 15
77393746 14212


Satellite: ISS
Catalog Number: 25544
Epoch time:      06301
62104901   =   yrday
fracday
Element set:     906
Inclination:       51
6339  deg
RA of node:       219
9221  deg
Eccentricity:     
0012107     
Arg of perigee:   148
1104  deg
Mean anomaly:     212
0796  deg
Mean motion:   15
77393746  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1421
Checksum:              262


Coasting Arc #8 (Orbit 1436)
---------------------------------------

Vector Time (GMT): 2006/302/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -330777
87                 A    =         6711682
38  meter
 Y    =        4532292
68  meter          E    =           
0019427
 Z    =       -4952353
53                 I    =           51
44133
 XDOT =      -6916
278627                 Wp   =          112
33052
 YDOT =      -2700
214016  meter/sec      RA   =          213
86901  deg
 ZDOT =      -2022
797517                 TA   =          138
10129
                                          MA   =          137
95246
                                          Ha   =            188
484  n
mi
                                          Hp   =            175
532

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1085229
22                 X    =         -357376
06
 Y    =       14869726
63  feet           Y    =         4528445
21  meter
 Z    =      -16247879
05                 Z    =        -4954024
90
 XDOT =     -22691
202844                 XDOT =       -6875
743910
 YDOT =      -8858
969868  feet/sec       YDOT =       -2777
328958  meter/sec
 ZDOT =      -6636
474794                 ZDOT =       -2056
298886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14377355
67                 X    =        -4382218
01
 Y    =       -3923763
95  feet           Y    =        -1195963
25  meter
 Z    =      -16253485
36                 Z    =        -4954062
34
 XDOT =      12888
278568                 XDOT =        3928
347308
 YDOT =     -19399
769098  feet/sec       YDOT =       -5913
049621  meter/sec
 ZDOT =      -6761
785796                 ZDOT =       -2060
992311


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   06302
63467847  
00020000  00000-0  20000-3 0  9072
2 25544  51
6334 214
6887 0012043 152
3662 207
8146 15
77450489 14378


Satellite: ISS
Catalog Number: 25544
Epoch time:      06302
63467847   =   yrday
fracday
Element set:     907
Inclination:       51
6334  deg
RA of node:       214
6887  deg
Eccentricity:     
0012043     
Arg of perigee:   152
3662  deg
Mean anomaly:     207
8146  deg
Mean motion:   15
77450489  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1437
Checksum:              302


Coasting Arc #9 (Orbit 1452)
---------------------------------------

Vector Time (GMT): 2006/303/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6082936
97                 A    =         6722218
42  meter
 Y    =        2756580
42  meter          E    =           
0024876
 Z    =         628615
52                 I    =           51
50147
 XDOT =      -1468
471282                 Wp   =          141
90084
 YDOT =       4631
736188  meter/sec      RA   =          208
67205  deg
 ZDOT =      -5994
966867                 TA   =           31
22197
                                          MA   =           31
07445
                                          Ha   =            188
470  n
mi
                                          Hp   =            175
662

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19957142
28                 X    =         6048606
67
 Y    =        9043899
01  feet           Y    =         2824411
23  meter
 Z    =        2062386
88                 Z    =          658083
44
 XDOT =      -4817
819166                 XDOT =       -1491
032049
 YDOT =      15195
984868  feet/sec       YDOT =        4615
188882  meter/sec
 ZDOT =     -19668
526465                 ZDOT =       -6002
155509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12511343
05                 X    =        -3813457
36
 Y    =       17974394
24  feet           Y    =         5478595
37  meter
 Z    =        2172676
52                 Z    =          662231
80
 XDOT =     -12779
359033                 XDOT =       -3895
148633
 YDOT =      -6474
755577  feet/sec       YDOT =       -1973
505500  meter/sec
 ZDOT =     -19694
692747                 ZDOT =       -6002
942349


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   06303
64828118  
00020000  00000-0  20000-3 0  9087
2 25544  51
6336 209
4561 0012265 156
3939 203
7791 15
77443454 14531


Satellite: ISS
Catalog Number: 25544
Epoch time:      06303
64828118   =   yrday
fracday
Element set:     908
Inclination:       51
6336  deg
RA of node:       209
4561  deg
Eccentricity:     
0012265     
Arg of perigee:   156
3939  deg
Mean anomaly:     203
7791  deg
Mean motion:   15
77443454  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1453
Checksum:              300


Coasting Arc #10 (Orbit 1468)
---------------------------------------

Vector Time (GMT): 2006/304/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2271313
50                 A    =         6710145
37  meter
 Y    =       -3542400
36  meter          E    =           
0012173
 Z    =        5220219
03                 I    =           51
48703
 XDOT =       6843
970591                 Wp   =          147
50218
 YDOT =       3504
476010  meter/sec      RA   =          203
50010  deg
 ZDOT =       -609
161463                 TA   =          308
23601
                                          MA   =          308
34552
                                          Ha   =            188
151  n
mi
                                          Hp   =            175
794

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7451815
96                 X    =         2285397
09
 Y    =      -11622048
44  feet           Y    =        -3516922
49  meter
 Z    =       17126702
87                 Z    =         5231287
46
 XDOT =      22453
971755                 XDOT =        6807
233628
 YDOT =      11497
624705  feet/sec       YDOT =        3580
803674  meter/sec
 ZDOT =      -1998
561231                 ZDOT =        -576
002282

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10254345
69                 X    =         3125524
57
 Y    =        9167942
36  feet           Y    =         2794388
83  meter
 Z    =       17167491
06                 Z    =         5232651
28
 XDOT =     -14366
361634                 XDOT =       -4378
867026
 YDOT =      19520
664146  feet/sec       YDOT =        5949
898432  meter/sec
 ZDOT =      -1874
387796                 ZDOT =        -571
313400


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   06304
66185228  
00020000  00000-0  20000-3 0  9099
2 25544  51
6334 204
2226 0012057 160
6554 199
5070 15
77533333 14695


Satellite: ISS
Catalog Number: 25544
Epoch time:      06304
66185228   =   yrday
fracday
Element set:     909
Inclination:       51
6334  deg
RA of node:       204
2226  deg
Eccentricity:     
0012057     
Arg of perigee:   160
6554  deg
Mean anomaly:     199
5070  deg
Mean motion:   15
77533333  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1469
Checksum:              286


Coasting Arc #11 (Orbit 1484)
---------------------------------------

Vector Time (GMT): 2006/305/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5620811
33                 A    =         6720766
70  meter
 Y    =       -3275640
72  meter          E    =           
0016698
 Z    =        1687191
82                 I    =           51
54926
 XDOT =       3781
824243                 Wp   =          109
26804
 YDOT =      -3522
161174  meter/sec      RA   =          198
34859  deg
 ZDOT =       5709
583625                 TA   =          269
42827
                                          MA   =          269
61961
                                          Ha   =            187
984  n
mi
                                          Hp   =            175
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18440982
05                 X    =        -5591961
12
 Y    =      -10746852
74  feet           Y    =        -3338334
39  meter
 Z    =        5535406
22                 Z    =         1659955
62
 XDOT =      12407
559851                 XDOT =        3793
191868
 YDOT =     -11555
646895  feet/sec       YDOT =       -3479
807003  meter/sec
 ZDOT =      18732
229742                 ZDOT =        5727
983745

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13352739
83                 X    =         4069915
10
 Y    =      -16684976
38  feet           Y    =        -5085580
80  meter
 Z    =        5433349
54                 Z    =         1656084
94
 XDOT =       8398
862093                 XDOT =        2559
973166
 YDOT =      12899
451900  feet/sec       YDOT =        3931
752939  meter/sec
 ZDOT =      18800
369283                 ZDOT =        5730
352557


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   06305
67539551  
00020000  00000-0  20000-3 0  9105
2 25544  51
6326 198
9884 0012050 165
2834 194
8684 15
77598578 14859


Satellite: ISS
Catalog Number: 25544
Epoch time:      06305
67539551   =   yrday
fracday
Element set:     910
Inclination:       51
6326  deg
RA of node:       198
9884  deg
Eccentricity:     
0012050     
Arg of perigee:   165
2834  deg
Mean anomaly:     194
8684  deg
Mean motion:   15
77598578  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1485
Checksum:              336


Coasting Arc #12 (Orbit 1499)
---------------------------------------

Vector Time (GMT): 2006/306/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4286222
86                 A    =         6713147
98  meter
 Y    =        2636901
79  meter          E    =           
0019104
 Z    =       -4461183
21                 I    =           51
55058
 XDOT =      -5770
227312                 Wp   =          143
19770
 YDOT =      -3954
665826  meter/sec      RA   =          193
13849  deg
 ZDOT =       3198
432737                 TA   =          158
91163
                                          MA   =          158
83275
                                          Ha   =            187
813  n
mi
                                          Hp   =            175
998

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14062410
97                 X    =        -4293718
39
 Y    =        8651252
58  feet           Y    =         2588928
81  meter
 Z    =      -14636427
85                 Z    =        -4482024
44
 XDOT =     -18931
191968                 XDOT =       -5741
114589
 YDOT =     -12974
625413  feet/sec       YDOT =       -4019
028828  meter/sec
 ZDOT =      10493
545724                 ZDOT =        3170
471187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6754392
01                 X    =        -2058738
68
 Y    =      -14990091
47  feet           Y    =        -4568979
88  meter
 Z    =      -14713801
01                 Z    =        -4484766
55
 XDOT =      14246
957816                 XDOT =        4342
472742
 YDOT =     -16642
324070  feet/sec       YDOT =       -5072
580377  meter/sec
 ZDOT =      10388
682498                 ZDOT =        3166
470425


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   06306
62556870  
00020000  00000-0  20000-3 0  9115
2 25544  51
6318 194
0808 0012008 168
7404 191
4031 15
77618120 15000


Satellite: ISS
Catalog Number: 25544
Epoch time:      06306
62556870   =   yrday
fracday
Element set:     911
Inclination:       51
6318  deg
RA of node:       194
0808  deg
Eccentricity:     
0012008     
Arg of perigee:   168
7404  deg
Mean anomaly:     191
4031  deg
Mean motion:   15
77618120  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1500
Checksum:              267


Coasting Arc #13 (Orbit 1515)
---------------------------------------

Vector Time (GMT): 2006/307/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4240836
56                 A    =         6715711
09  meter
 Y    =        3604750
77  meter          E    =           
0012838
 Z    =       -3755230
88                 I    =           51
58650
 XDOT =      -5908
310087                 Wp   =          145
46573
 YDOT =       2558
194076  meter/sec      RA   =          188
02021  deg
 ZDOT =      -4234
078423                 TA   =           80
07918
                                          MA   =           79
93429
                                          Ha   =            187
688  n
mi
                                          Hp   =            176
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13913505
76                 X    =         4218455
30
 Y    =       11826610
15  feet           Y    =         3652048
94  meter
 Z    =      -12320311
27                 Z    =        -3734682
75
 XDOT =     -19384
219446                 XDOT =       -5915
908071
 YDOT =       8393
025184  feet/sec       YDOT =        2492
081500  meter/sec
 ZDOT =     -13891
333409                 ZDOT =       -4262
800324

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13334964
40                 X    =        -4064497
15
 Y    =       12551032
66  feet           Y    =         3825554
76  meter
 Z    =      -12243150
08                 Z    =        -3731712
14
 XDOT =      -5235
887195                 XDOT =       -1595
898417
 YDOT =     -19161
557104  feet/sec       YDOT =       -5840
442605  meter/sec
 ZDOT =     -13998
121243                 ZDOT =       -4266
627355


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   06307
63905865  
00020000  00000-0  20000-3 0  9120
2 25544  51
6309 188
8474 0011975 172
7869 187
3470 15
77653004 15160


Satellite: ISS
Catalog Number: 25544
Epoch time:      06307
63905865   =   yrday
fracday
Element set:     912
Inclination:       51
6309  deg
RA of node:       188
8474  deg
Eccentricity:     
0011975     
Arg of perigee:   172
7869  deg
Mean anomaly:     187
3470  deg
Mean motion:   15
77653004  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1516
Checksum:              322

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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