Date: October 19th 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 8
000/00:00:00 000 0 0 0 0 175 1

Coasting Arc #1 (Orbit 1259)
---------------------------------------

Vector Time (GMT): 2006/291/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1072234
18                 A    =         6722473
26  meter
 Y    =       -6443223
00  meter          E    =           
0017207
 Z    =       -1598310
25                 I    =           51
33319
 XDOT =       4656
390186                 Wp   =           82
65398
 YDOT =      -2182
241683  meter/sec      RA   =          271
84362  deg
 ZDOT =       5728
280507                 TA   =          259
62317
                                          MA   =          259
81717
                                          Ha   =            190
077  n
mi
                                          Hp   =            174
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3517828
67                 X    =         -992341
07
 Y    =      -21139183
08  feet           Y    =        -6454766
71  meter
 Z    =       -5243800
03                 Z    =        -1603324
80
 XDOT =      15276
870688                 XDOT =        4652
618928
 YDOT =      -7159
585573  feet/sec       YDOT =       -2130
192105  meter/sec
 ZDOT =      18793
571217                 ZDOT =        5750
892504

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2015968
69                 X    =          614467
26
 Y    =       21330035
14  feet           Y    =         6501394
71  meter
 Z    =       -5263372
46                 Z    =        -1604275
93
 XDOT =     -14077
040656                 XDOT =       -4290
681992
 YDOT =       5944
436909  feet/sec       YDOT =        1811
864370  meter/sec
 ZDOT =      18877
540640                 ZDOT =        5753
874387


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
41979277  
00020000  00000-0  20000-3 0  9003
2 25544  51
6328 272
5626 0012894 108
9552 251
3011 15
77015876 12600


Satellite: ISS
Catalog Number: 25544
Epoch time:      06291
41979277   =   yrday
fracday
Element set:     900
Inclination:       51
6328  deg
RA of node:       272
5626  deg
Eccentricity:     
0012894     
Arg of perigee:   108
9552  deg
Mean anomaly:     251
3011  deg
Mean motion:   15
77015876  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1260
Checksum:              295


Coasting Arc #2 (Orbit 1275)
---------------------------------------

Vector Time (GMT): 2006/292/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4131364
65                 A    =         6711736
48  meter
 Y    =         988379
97  meter          E    =           
0026733
 Z    =       -5218847
69                 I    =           51
29623
 XDOT =       -978
273925                 Wp   =           97
55321
 YDOT =      -7594
406084  meter/sec      RA   =          266
68167  deg
 ZDOT =       -670
249590                 TA   =          166
06826
                                          MA   =          165
99436
                                          Ha   =            190
009  n
mi
                                          Hp   =            174
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13554345
96                 X    =        -4116757
13
 Y    =        3242716
43  feet           Y    =          942262
12  meter
 Z    =      -17122203
71                 Z    =        -5238882
79
 XDOT =      -3209
560121                 XDOT =        -890
023506
 YDOT =     -24916
030460  feet/sec       YDOT =       -7604
852294  meter/sec
 ZDOT =      -2198
981593                 ZDOT =        -674
787304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13610312
31                 X    =         4148423
19
 Y    =       -2537149
65  feet           Y    =         -773323
21  meter
 Z    =      -17196733
25                 Z    =        -5241564
30
 XDOT =       1709
699456                 XDOT =         521
116394
 YDOT =      24056
285098  feet/sec       YDOT =        7332
355698  meter/sec
 ZDOT =      -2216
940206                 ZDOT =        -675
723375


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
43369393  
00020000  00000-0  20000-3 0  9019
2 25544  51
6319 267
3306 0012696 112
5547 247
6962 15
76996379 12767


Satellite: ISS
Catalog Number: 25544
Epoch time:      06292
43369393   =   yrday
fracday
Element set:     901
Inclination:       51
6319  deg
RA of node:       267
3306  deg
Eccentricity:     
0012696     
Arg of perigee:   112
5547  deg
Mean anomaly:     247
6962  deg
Mean motion:   15
76996379  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1276
Checksum:              328


Coasting Arc #3 (Orbit 1291)
---------------------------------------

Vector Time (GMT): 2006/293/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         628123
67                 A    =         6723417
88  meter
 Y    =        6670051
61  meter          E    =           
0023615
 Z    =        -456192
14                 I    =           51
33844
 XDOT =      -4842
837804                 Wp   =          126
57260
 YDOT =         61
421213  meter/sec      RA   =          261
49739  deg
 ZDOT =      -5997
989019                 TA   =           58
41856
                                          MA   =           58
18824
                                          Ha   =            189
915  n
mi
                                          Hp   =            174
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2060773
19                 X    =          555707
69
 Y    =       21883371
41  feet           Y    =         6676670
71  meter
 Z    =       -1496693
38                 Z    =         -453316
93
 XDOT =     -15888
575472                 XDOT =       -4814
026891
 YDOT =        201
513165  feet/sec       YDOT =           7
426662  meter/sec
 ZDOT =     -19678
441665                 ZDOT =       -6021
446070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1303529
08                 X    =         -397315
66
 Y    =      -21942293
49  feet           Y    =        -6688011
06  meter
 Z    =       -1485055
52                 Z    =         -452644
92
 XDOT =      14177
061292                 XDOT =        4321
168282
 YDOT =        444
508943  feet/sec       YDOT =         135
486326  meter/sec
 ZDOT =     -19765
852246                 ZDOT =       -6024
631764


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
44756693  
00020000  00000-0  20000-3 0  9025
2 25544  51
6311 262
0986 0012781 116
0577 244
1905 15
77053097 12921


Satellite: ISS
Catalog Number: 25544
Epoch time:      06293
44756693   =   yrday
fracday
Element set:     902
Inclination:       51
6311  deg
RA of node:       262
0986  deg
Eccentricity:     
0012781     
Arg of perigee:   116
0577  deg
Mean anomaly:     244
1905  deg
Mean motion:   15
77053097  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1292
Checksum:              298


Coasting Arc #4 (Orbit 1307)
---------------------------------------

Vector Time (GMT): 2006/294/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4351276
23                 A    =         6712161
86  meter
 Y    =         855450
99  meter          E    =           
0015435
 Z    =        5024841
04                 I    =           51
30621
 XDOT =        454
571743                 Wp   =          102
45339
 YDOT =       7520
805625  meter/sec      RA   =          256
29653  deg
 ZDOT =      -1672
995375                 TA   =            3
67679
                                          MA   =            3
66546
                                          Ha   =            189
622  n
mi
                                          Hp   =            174
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14275840
64                 X    =         4316976
63
 Y    =        2806597
73  feet           Y    =          903917
83  meter
 Z    =       16485698
96                 Z    =         5045896
75
 XDOT =       1491
377110                 XDOT =         378
566593
 YDOT =      24674
559138  feet/sec       YDOT =        7525
463854  meter/sec
 ZDOT =      -5488
829971                 ZDOT =       -1670
971982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14132637
70                 X    =        -4307627
97
 Y    =       -3057416
41  feet           Y    =         -931900
52  meter
 Z    =       16564288
20                 Z    =         5048795
04
 XDOT =      -1306
983105                 XDOT =        -398
368450
 YDOT =     -23667
145837  feet/sec       YDOT =       -7213
746051  meter/sec
 ZDOT =      -5480
248385                 ZDOT =       -1670
379708


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
46141015  
00020000  00000-0  20000-3 0  9035
2 25544  51
6308 256
8670 0012598 120
0161 240
2255 15
77109561 13089


Satellite: ISS
Catalog Number: 25544
Epoch time:      06294
46141015   =   yrday
fracday
Element set:     903
Inclination:       51
6308  deg
RA of node:       256
8670  deg
Eccentricity:     
0012598     
Arg of perigee:   120
0161  deg
Mean anomaly:     240
2255  deg
Mean motion:   15
77109561  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1308
Checksum:              266


Coasting Arc #5 (Orbit 1323)
---------------------------------------

Vector Time (GMT): 2006/295/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -97702
53                 A    =         6720586
58  meter
 Y    =       -6265200
00  meter          E    =           
0024060
 Z    =        2414940
47                 I    =           51
34346
 XDOT =       5191
388921                 Wp   =           98
17698
 YDOT =       1994
679142  meter/sec      RA   =          251
15043  deg
 ZDOT =       5336
279845                 TA   =          289
24366
                                          MA   =          289
50381
                                          Ha   =            189
576  n
mi
                                          Hp   =            174
767

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -320546
35                 X    =          -39368
63
 Y    =      -20555118
13  feet           Y    =        -6265966
33  meter
 Z    =        7923033
04                 Z    =         2414607
71
 XDOT =      17032
115881                 XDOT =        5142
774839
 YDOT =       6544
222906  feet/sec       YDOT =        2052
460483  meter/sec
 ZDOT =      17507
479807                 ZDOT =        5361
382220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         353494
04                 X    =          107744
98
 Y    =       20555389
54  feet           Y    =         6265282
73  meter
 Z    =        7920927
14                 Z    =         2414298
59
 XDOT =     -15432
844391                 XDOT =       -4703
930970
 YDOT =      -6578
702420  feet/sec       YDOT =       -2005
188498  meter/sec
 ZDOT =      17601
309867                 ZDOT =        5364
879247


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
47522359  
00020000  00000-0  20000-3 0  9042
2 25544  51
6309 251
6361 0012603 124
6518 235
5836 15
77188893 13248


Satellite: ISS
Catalog Number: 25544
Epoch time:      06295
47522359   =   yrday
fracday
Element set:     904
Inclination:       51
6309  deg
RA of node:       251
6361  deg
Eccentricity:     
0012603     
Arg of perigee:   124
6518  deg
Mean anomaly:     235
5836  deg
Mean motion:   15
77188893  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1324
Checksum:              302


Coasting Arc #6 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2006/296/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4708949
06                 A    =         6715896
56  meter
 Y    =       -2564059
81  meter          E    =           
0019923
 Z    =       -4066016
28                 I    =           51
33796
 XDOT =        351
813347                 Wp   =          120
61017
 YDOT =      -6672
561898  meter/sec      RA   =          245
92105  deg
 ZDOT =       3804
161631                 TA   =          188
69067
                                          MA   =          188
72522
                                          Ha   =            189
552  n
mi
                                          Hp   =            174
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15449307
94                 X    =        -4660174
80
 Y    =       -8412269
71  feet           Y    =        -2616445
22  meter
 Z    =      -13339948
42                 Z    =        -4088774
58
 XDOT =       1154
243264                 XDOT =         407
920195
 YDOT =     -21891
607276  feet/sec       YDOT =       -6668
313978  meter/sec
 ZDOT =      12480
845245                 ZDOT =        3806
007151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15513572
63                 X    =         4728536
94
 Y    =        8154553
23  feet           Y    =         2485507
82  meter
 Z    =      -13425123
73                 Z    =        -4091977
71
 XDOT =       -125
451273                 XDOT =         -38
237548
 YDOT =      20775
522157  feet/sec       YDOT =        6332
379153  meter/sec
 ZDOT =      12486
804135                 ZDOT =        3805
977900


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
42564981  
00020000  00000-0  20000-3 0  9056
2 25544  51
6308 246
7307 0012554 127
1554 233
0759 15
77166960 13399


Satellite: ISS
Catalog Number: 25544
Epoch time:      06296
42564981   =   yrday
fracday
Element set:     905
Inclination:       51
6308  deg
RA of node:       246
7307  deg
Eccentricity:     
0012554     
Arg of perigee:   127
1554  deg
Mean anomaly:     233
0759  deg
Mean motion:   15
77166960  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1339
Checksum:              307


Coasting Arc #7 (Orbit 1354)
---------------------------------------

Vector Time (GMT): 2006/297/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -817580
02                 A    =         6715641
76  meter
 Y    =        5261354
66  meter          E    =           
0017657
 Z    =       -4103032
26                 I    =           51
35060
 XDOT =      -5554
520007                 Wp   =          108
94336
 YDOT =      -3778
245600  meter/sec      RA   =          240
79019  deg
 ZDOT =      -3756
874603                 TA   =          122
46085
                                          MA   =          122
29002
                                          Ha   =            189
385  n
mi
                                          Hp   =            174
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2682349
15                 X    =         -856420
03
 Y    =       17261662
25  feet           Y    =         5251994
91  meter
 Z    =      -13461391
92                 Z    =        -4107098
46
 XDOT =     -18223
490835                 XDOT =       -5493
607514
 YDOT =     -12395
818897  feet/sec       YDOT =       -3840
018694  meter/sec
 ZDOT =     -12325
704079                 ZDOT =       -3783
711406

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2021780
33                 X    =          616238
64
 Y    =      -17340230
40  feet           Y    =        -5285302
23  meter
 Z    =      -13475825
28                 Z    =        -4107431
55
 XDOT =      17300
154133                 XDOT =        5273
086980
 YDOT =      11626
180943  feet/sec       YDOT =        3543
659952  meter/sec
 ZDOT =     -12426
252237                 ZDOT =       -3787
521682


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
43940760  
00020000  00000-0  20000-3 0  9062
2 25544  51
6310 241
4980 0012561 131
1939 229
0311 15
77230549 13553


Satellite: ISS
Catalog Number: 25544
Epoch time:      06297
43940760   =   yrday
fracday
Element set:     906
Inclination:       51
6310  deg
RA of node:       241
4980  deg
Eccentricity:     
0012561     
Arg of perigee:   131
1939  deg
Mean anomaly:     229
0311  deg
Mean motion:   15
77230549  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1355
Checksum:              277


Coasting Arc #8 (Orbit 1370)
---------------------------------------

Vector Time (GMT): 2006/298/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4937122
51                 A    =         6720375
65  meter
 Y    =        3883451
49  meter          E    =           
0025525
 Z    =        2348342
22                 I    =           51
38217
 XDOT =      -1587
349098                 Wp   =          119
93239
 YDOT =       5294
172383  meter/sec      RA   =          235
56358  deg
 ZDOT =      -5386
813031                 TA   =           33
43999
                                          MA   =           33
27906
                                          Ha   =            189
123  n
mi
                                          Hp   =            174
997

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16197908
49                 X    =         4881922
11
 Y    =       12740982
58  feet           Y    =         3938352
41  meter
 Z    =        7704534
83                 Z    =         2372193
53
 XDOT =      -5207
838247                 XDOT =       -1620
262346
 YDOT =      17369
331965  feet/sec       YDOT =        5276
237928  meter/sec
 ZDOT =     -17673
271098                 ZDOT =       -5394
604366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16784593
64                 X    =        -5115944
14
 Y    =      -11899415
75  feet           Y    =        -3626941
92  meter
 Z    =        7793975
53                 Z    =         2375603
74
 XDOT =       3348
914225                 XDOT =        1020
749056
 YDOT =     -16383
817182  feet/sec       YDOT =       -4993
787477  meter/sec
 ZDOT =     -17701
589052                 ZDOT =       -5395
444343


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
45313498  
00020000  00000-0  20000-3 0  9078
2 25544  51
6309 236
2662 0012387 135
1173 225
0996 15
77289158 13713


Satellite: ISS
Catalog Number: 25544
Epoch time:      06298
45313498   =   yrday
fracday
Element set:     907
Inclination:       51
6309  deg
RA of node:       236
2662  deg
Eccentricity:     
0012387     
Arg of perigee:   135
1173  deg
Mean anomaly:     225
0996  deg
Mean motion:   15
77289158  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1371
Checksum:              313


Coasting Arc #9 (Orbit 1386)
---------------------------------------

Vector Time (GMT): 2006/299/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2032460
96                 A    =         6711378
72  meter
 Y    =       -3895250
86  meter          E    =           
0017074
 Z    =        5065858
43                 I    =           51
36975
 XDOT =       5693
945806                 Wp   =          135
79552
 YDOT =       4974
368888  meter/sec      RA   =          230
41886  deg
 ZDOT =       1525
281556                 TA   =          299
45586
                                          MA   =          299
62611
                                          Ha   =            188
971  n
mi
                                          Hp   =            175
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6668178
99                 X    =         2051257
46
 Y    =      -12779694
43  feet           Y    =        -3872417
92  meter
 Z    =       16620270
43                 Z    =         5075777
84
 XDOT =      18680
924559                 XDOT =        5630
488794
 YDOT =      16320
107901  feet/sec       YDOT =        5037
686861  meter/sec
 ZDOT =       5004
204579                 ZDOT =        1552
789594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5688997
18                 X    =        -1734006
34
 Y    =       13198775
53  feet           Y    =         4022986
78  meter
 Z    =       16656717
13                 Z    =         5076967
38
 XDOT =     -18760
599395                 XDOT =       -5718
230696
 YDOT =     -14594
467978  feet/sec       YDOT =       -4448
393840  meter/sec
 ZDOT =       5107
434982                 ZDOT =        1556
746183


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
46683221  
00020000  00000-0  20000-3 0  9085
2 25544  51
6312 231
0349 0012319 139
6025 220
6057 15
77348882 13878


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
46683221   =   yrday
fracday
Element set:     908
Inclination:       51
6312  deg
RA of node:       231
0349  deg
Eccentricity:     
0012319     
Arg of perigee:   139
6025  deg
Mean anomaly:     220
6057  deg
Mean motion:   15
77348882  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1387
Checksum:              295


Coasting Arc #10 (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    =        5072639
39                 A    =         6714232
76  meter
 Y    =         585194
53  meter          E    =           
0017811
 Z    =        4341771
67                 I    =           51
38646
 XDOT =       2126
660721                 Wp   =          110
17959
 YDOT =       6609
801077  meter/sec      RA   =          229
35398  deg
 ZDOT =      -3370
473581                 TA   =           13
82241
                                          MA   =           13
77371
                                          Ha   =            188
823  n
mi
                                          Hp   =            175
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16642517
69                 X    =         5044626
57
 Y    =        1919929
55  feet           Y    =          641762
73  meter
 Z    =       14244657
72                 Z    =         4366347
17
 XDOT =       6977
233337                 XDOT =        2068
964518
 YDOT =      21685
699073  feet/sec       YDOT =        6633
260163  meter/sec
 ZDOT =     -11057
984190                 ZDOT =       -3360
281788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5976472
65                 X    =        -1821628
86
 Y    =       15566644
97  feet           Y    =         4744713
39  meter
 Z    =       14336357
18                 Z    =         4369721
67
 XDOT =     -21619
489417                 XDOT =       -6589
620374
 YDOT =       1863
072168  feet/sec       YDOT =         567
864397  meter/sec
 ZDOT =     -11019
084166                 ZDOT =       -3358
616854


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
65689710  
00020000  00000-0  20000-3 0  9096
2 25544  51
6343 230
0547 0012242 139
8123 220
3949 15
77370174 13907


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
65689710   =   yrday
fracday
Element set:     909
Inclination:       51
6343  deg
RA of node:       230
0547  deg
Eccentricity:     
0012242     
Arg of perigee:   139
8123  deg
Mean anomaly:     220
3949  deg
Mean motion:   15
77370174  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1390
Checksum:              295


Coasting Arc #11 (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    =       -1228272
77                 A    =         6716368
43  meter
 Y    =       -5407525
80  meter          E    =           
0021961
 Z    =        3782747
31                 I    =           51
41309
 XDOT =       6308
880540                 Wp   =          121
50077
 YDOT =       1501
691963  meter/sec      RA   =          224
22575  deg
 ZDOT =       4166
173936                 TA   =          284
63097
                                          MA   =          284
87436
                                          Ha   =            188
900  n
mi
                                          Hp   =            175
233

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4029766
29                 X    =        -1186090
06
 Y    =      -17741226
38  feet           Y    =        -5421025
40  meter
 Z    =       12410588
29                 Z    =         3776882
38
 XDOT =      20698
426969                 XDOT =        6271
380576
 YDOT =       4926
810901  feet/sec       YDOT =        1572
031440  meter/sec
 ZDOT =      13668
549658                 ZDOT =        4196
732123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18208094
10                 X    =         5549827
08
 Y    =         126836
57  feet           Y    =           38659
79  meter
 Z    =       12387980
19                 Z    =         3775856
36
 XDOT =      -9564
625166                 XDOT =       -2915
297751
 YDOT =      17590
647015  feet/sec       YDOT =        5361
629210  meter/sec
 ZDOT =      13782
691488                 ZDOT =        4200
964365


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
67056027  
00020000  00000-0  20000-3 0  9102
2 25544  51
6343 224
8221 0012276 143
7246 216
4754 15
77376231 14062


Satellite: ISS
Catalog Number: 25544
Epoch time:      06300
67056027   =   yrday
fracday
Element set:     910
Inclination:       51
6343  deg
RA of node:       224
8221  deg
Eccentricity:     
0012276     
Arg of perigee:   143
7246  deg
Mean anomaly:     216
4754  deg
Mean motion:   15
77376231  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1406
Checksum:              266


Coasting Arc #12 (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    =       -5838965
49                 A    =         6719111
01  meter
 Y    =       -1934258
41  meter          E    =           
0013094
 Z    =       -2724218
33                 I    =           51
44427
 XDOT =       -511
373807                 Wp   =          126
97048
 YDOT =      -5693
592677  meter/sec      RA   =          218
99892  deg
 ZDOT =       5147
904382                 TA   =          201
84212
                                          MA   =          201
89800
                                          Ha   =            188
653  n
mi
                                          Hp   =            175
295

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19156710
92                 X    =        -5803668
40
 Y    =       -6345992
16  feet           Y    =        -1999355
46  meter
 Z    =       -8937724
18                 Z    =        -2752498
86
 XDOT =      -1677
735586                 XDOT =        -472
677255
 YDOT =     -18679
766000  feet/sec       YDOT =       -5699
095059  meter/sec
 ZDOT =      16889
450071                 ZDOT =        5145
513772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10307064
18                 X    =         3141593
16
 Y    =      -17294930
28  feet           Y    =        -5271494
75  meter
 Z    =       -9043446
14                 Z    =        -2756442
38
 XDOT =      17362
467204                 XDOT =        5292
080004
 YDOT =       1536
671735  feet/sec       YDOT =         468
377545  meter/sec
 ZDOT =      16879
752804                 ZDOT =        5144
948655


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
62084136  
00020000  00000-0  20000-3 0  9111
2 25544  51
6341 219
9163 0012140 148
0298 212
1606 15
77431350 14215


Satellite: ISS
Catalog Number: 25544
Epoch time:      06301
62084136   =   yrday
fracday
Element set:     911
Inclination:       51
6341  deg
RA of node:       219
9163  deg
Eccentricity:     
0012140     
Arg of perigee:   148
0298  deg
Mean anomaly:     212
1606  deg
Mean motion:   15
77431350  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1421
Checksum:              248


Coasting Arc #13 (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    =        -468350
08                 A    =         6711402
12  meter
 Y    =        4477151
95  meter          E    =           
0019799
 Z    =       -4991401
23                 I    =           51
44100
 XDOT =      -6906
137783                 Wp   =          112
32832
 YDOT =      -2817
336709  meter/sec      RA   =          213
86118  deg
 ZDOT =      -1892
430085                 TA   =          139
41492
                                          MA   =          139
26715
                                          Ha   =            188
438  n
mi
                                          Hp   =            175
455

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1536581
61                 X    =         -494131
76
 Y    =       14688818
73  feet           Y    =         4471770
64  meter
 Z    =      -16375988
29                 Z    =        -4993738
95
 XDOT =     -22657
932359                 XDOT =       -6864
927448
 YDOT =      -9243
230671  feet/sec       YDOT =       -2894
334478  meter/sec
 ZDOT =      -6208
760123                 ZDOT =       -1925
880553

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14110698
02                 X    =        -4300940
76
 Y    =       -4329590
83  feet           Y    =        -1319659
29  meter
 Z    =      -16384087
27                 Z    =        -4993869
80
 XDOT =      13229
194793                 XDOT =        4032
258573
 YDOT =     -19312
736936  feet/sec       YDOT =       -5886
522218  meter/sec
 ZDOT =      -6333
897502                 ZDOT =       -1930
571959


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
63444695  
00020000  00000-0  20000-3 0  9124
2 25544  51
6336 214
6828 0012076 152
2726 207
9086 15
77488845 14372


Satellite: ISS
Catalog Number: 25544
Epoch time:      06302
63444695   =   yrday
fracday
Element set:     912
Inclination:       51
6336  deg
RA of node:       214
6828  deg
Eccentricity:     
0012076     
Arg of perigee:   152
2726  deg
Mean anomaly:     207
9086  deg
Mean motion:   15
77488845  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1437
Checksum:              308

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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