Date: September 13th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4800 7 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2454)
---------------------------------------

Vector Time (GMT): 2007/255/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6580155
83                 A    =         6724358
09  meter
 Y    =        1301056
72  meter          E    =           
0019336
 Z    =        -261654
51                 I    =           51
72769
 XDOT =       -702
257521                 Wp   =           22
97388
 YDOT =       4734
505308  meter/sec      RA   =           12
94817  deg
 ZDOT =       6047
744447                 TA   =          334
18019
                                          MA   =          334
27657
                                          Ha   =            187
812  n
mi
                                          Hp   =            178
831

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21588437
77                 X    =         6566389
24
 Y    =        4268558
78  feet           Y    =         1374562
74  meter
 Z    =        -858446
54                 Z    =         -229721
66
 XDOT =      -2303
994491                 XDOT =        -784
526119
 YDOT =      15533
153896  feet/sec       YDOT =        4726
192746  meter/sec
 ZDOT =      19841
681257                 ZDOT =        6044
132686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19510546
27                 X    =        -5946814
50
 Y    =      -10188889
62  feet           Y    =        -3105573
56  meter
 Z    =        -737076
98                 Z    =         -224661
06
 XDOT =       5957
938051                 XDOT =        1815
979518
 YDOT =     -12797
203698  feet/sec       YDOT =       -3900
587687  meter/sec
 ZDOT =      19828
530994                 ZDOT =        6043
736247


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   07255
48168286  
00020000  00000-0  20000-3 0  9001
2 25544  51
6362  13
4392 0009160 357
2628   2
8485 15
76745246 24556


Satellite: ISS
Catalog Number: 25544
Epoch time:      07255
48168286   =   yrday
fracday
Element set:     900
Inclination:       51
6362  deg
RA of node:        13
4392  deg
Eccentricity:     
0009160     
Arg of perigee:   357
2628  deg
Mean anomaly:       2
8485  deg
Mean motion:   15
76745246  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2455
Checksum:              299


Coasting Arc #2 (Orbit 2470)
---------------------------------------

Vector Time (GMT): 2007/256/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1410631
15                 A    =         6712341
15  meter
 Y    =       -3981009
68  meter          E    =           
0016672
 Z    =       -5228814
66                 I    =           51
65930
 XDOT =       7477
963330                 Wp   =           62
48797
 YDOT =       1642
823128  meter/sec      RA   =            7
79215  deg
 ZDOT =        776
063394                 TA   =          214
84464
                                          MA   =          214
95390
                                          Ha   =            187
845  n
mi
                                          Hp   =            178
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4628054
95                 X    =         1480443
31
 Y    =      -13061055
39  feet           Y    =        -3964845
26  meter
 Z    =      -17154903
73                 Z    =        -5221791
91
 XDOT =      24534
000425                 XDOT =        7455
267263
 YDOT =       5389
839660  feet/sec       YDOT =        1726
319098  meter/sec
 ZDOT =       2546
139744                 ZDOT =         812
336252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8024522
13                 X    =        -2445874
35
 Y    =       11336441
09  feet           Y    =         3455347
24  meter
 Z    =      -17128716
55                 Z    =        -5220832
80
 XDOT =     -21379
590367                 XDOT =       -6516
499144
 YDOT =     -11125
034294  feet/sec       YDOT =       -3390
910453  meter/sec
 ZDOT =       2684
017475                 ZDOT =         818
088526


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   07256
49573221  
00020000  00000-0  20000-3 0  9013
2 25544  51
6364   8
2109 0009211   1
2859 358
8328 15
76803588 24717


Satellite: ISS
Catalog Number: 25544
Epoch time:      07256
49573221   =   yrday
fracday
Element set:     901
Inclination:       51
6364  deg
RA of node:         8
2109  deg
Eccentricity:     
0009211     
Arg of perigee:     1
2859  deg
Mean anomaly:     358
8328  deg
Mean motion:   15
76803588  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2471
Checksum:              292


Coasting Arc #3 (Orbit 2486)
---------------------------------------

Vector Time (GMT): 2007/257/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6337897
53                 A    =         6722983
68  meter
 Y    =       -1571155
65  meter          E    =           
0006311
 Z    =       -1613134
61                 I    =           51
66689
 XDOT =       2558
281371                 Wp   =           61
59853
 YDOT =      -4431
735781  meter/sec      RA   =            2
65853  deg
 ZDOT =      -5748
929887                 TA   =          136
20463
                                          MA   =          136
15456
                                          Ha   =            187
941  n
mi
                                          Hp   =            178
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20793627
08                 X    =        -6312021
21
 Y    =       -5154710
13  feet           Y    =        -1641885
02  meter
 Z    =       -5292436
38                 Z    =        -1643861
42
 XDOT =       8393
311585                 XDOT =        2635
575067
 YDOT =     -14539
815556  feet/sec       YDOT =       -4402
695835  meter/sec
 ZDOT =     -18861
318528                 ZDOT =       -5736
313617

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18825556
38                 X    =         5738029
59
 Y    =       10163380
44  feet           Y    =         3097798
36  meter
 Z    =       -5409248
70                 Z    =        -1648739
00
 XDOT =     -11111
336199                 XDOT =       -3386
735273
 YDOT =      10592
067399  feet/sec       YDOT =        3228
462143  meter/sec
 ZDOT =     -18813
952354                 ZDOT =       -5734
492677


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   07257
50976505  
00020000  00000-0  20000-3 0  9029
2 25544  51
6366   2
9806 0009252   4
9679 355
1582 15
76816363 24873


Satellite: ISS
Catalog Number: 25544
Epoch time:      07257
50976505   =   yrday
fracday
Element set:     902
Inclination:       51
6366  deg
RA of node:         2
9806  deg
Eccentricity:     
0009252     
Arg of perigee:     4
9679  deg
Mean anomaly:     355
1582  deg
Mean motion:   15
76816363  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2487
Checksum:              314


Coasting Arc #4 (Orbit 2502)
---------------------------------------

Vector Time (GMT): 2007/258/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3015958
37                 A    =         6714856
32  meter
 Y    =        3808547
49  meter          E    =           
0015634
 Z    =        4633930
59                 I    =           51
61068
 XDOT =      -6884
782641                 Wp   =           34
28203
 YDOT =      -1958
474285  meter/sec      RA   =          357
46458  deg
 ZDOT =      -2853
915427                 TA   =           84
00419
                                          MA   =           83
82604
                                          Ha   =            188
154  n
mi
                                          Hp   =            178
112

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9894876
56                 X    =        -3080833
02
 Y    =       12495234
54  feet           Y    =         3774458
84  meter
 Z    =       15203184
34                 Z    =         4619121
12
 XDOT =     -22587
869558                 XDOT =       -6848
507034
 YDOT =      -6425
440569  feet/sec       YDOT =       -2035
261134  meter/sec
 ZDOT =      -9363
239591                 ZDOT =       -2887
273858

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12610292
87                 X    =         3843617
27
 Y    =       -9834249
96  feet           Y    =        -2997479
39  meter
 Z    =       15147419
71                 Z    =         4616933
53
 XDOT =      19708
076421                 XDOT =        6007
021693
 YDOT =      10565
994923  feet/sec       YDOT =        3220
515253  meter/sec
 ZDOT =      -9490
081264                 ZDOT =       -2892
576769


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   07258
52378166  
00020000  00000-0  20000-3 0  9032
2 25544  51
6370 357
7514 0009374   9
4071 350
7268 15
76821747 25039


Satellite: ISS
Catalog Number: 25544
Epoch time:      07258
52378166   =   yrday
fracday
Element set:     903
Inclination:       51
6370  deg
RA of node:       357
7514  deg
Eccentricity:     
0009374     
Arg of perigee:     9
4071  deg
Mean anomaly:     350
7268  deg
Mean motion:   15
76821747  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2503
Checksum:              303


Coasting Arc #5 (Orbit 2518)
---------------------------------------

Vector Time (GMT): 2007/259/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5543647
91                 A    =         6719210
74  meter
 Y    =        1876985
75  meter          E    =           
0017503
 Z    =        3277642
49                 I    =           51
59749
 XDOT =      -4272
327922                 Wp   =           57
11488
 YDOT =       4352
430214  meter/sec      RA   =          352
35215  deg
 ZDOT =       4724
759726                 TA   =          341
45700
                                          MA   =          341
52070
                                          Ha   =            188
008  n
mi
                                          Hp   =            177
838

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18187821
23                 X    =         5506324
76
 Y    =        6158089
72  feet           Y    =         1938769
38  meter
 Z    =       10753420
23                 Z    =         3304483
14
 XDOT =     -14016
823891                 XDOT =       -4343
632232
 YDOT =      14279
626686  feet/sec       YDOT =        4304
256108  meter/sec
 ZDOT =      15501
180204                 ZDOT =        4703
831152

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16373242
37                 X    =        -4990564
27
 Y    =       -9921177
57  feet           Y    =        -3023974
92  meter
 Z    =       10855511
34                 Z    =         3308759
86
 XDOT =      16127
085899                 XDOT =        4915
535782
 YDOT =      -9709
199440  feet/sec       YDOT =       -2959
363989  meter/sec
 ZDOT =      15422
252259                 ZDOT =        4700
702488


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   07259
53777916  
00020000  00000-0  20000-3 0  9041
2 25544  51
6372 352
5215 0009370  12
8949 347
2454 15
76880604 25192


Satellite: ISS
Catalog Number: 25544
Epoch time:      07259
53777916   =   yrday
fracday
Element set:     904
Inclination:       51
6372  deg
RA of node:       352
5215  deg
Eccentricity:     
0009370     
Arg of perigee:    12
8949  deg
Mean anomaly:     347
2454  deg
Mean motion:   15
76880604  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2519
Checksum:              315


Coasting Arc #6 (Orbit 2533)
---------------------------------------

Vector Time (GMT): 2007/260/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4336324
21                 A    =         6718885
98  meter
 Y    =       -3797695
74  meter          E    =           
0011716
 Z    =       -3449613
29                 I    =           51
56751
 XDOT =       5722
623844                 Wp   =           39
63777
 YDOT =       2406
443535  meter/sec      RA   =          347
14014  deg
 ZDOT =       4561
675160                 TA   =          279
40085
                                          MA   =          279
53328
                                          Ha   =            188
268  n
mi
                                          Hp   =            177
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14226785
45                 X    =         4395226
12
 Y    =      -12459631
69  feet           Y    =        -3748875
23  meter
 Z    =      -11317628
89                 Z    =        -3428404
03
 XDOT =      18775
012613                 XDOT =        5673
129250
 YDOT =       7895
155956  feet/sec       YDOT =        2470
160487  meter/sec
 ZDOT =      14966
125852                 ZDOT =        4589
355739

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16481502
87                 X    =        -5023562
07
 Y    =        9370681
55  feet           Y    =         2856183
74  meter
 Z    =      -11237569
15                 Z    =        -3425211
08
 XDOT =     -16065
164385                 XDOT =       -4896
662105
 YDOT =     -10250
603194  feet/sec       YDOT =       -3124
383854  meter/sec
 ZDOT =      15071
465166                 ZDOT =        4593
782583


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   07260
48838871  
00020000  00000-0  20000-3 0  9056
2 25544  51
6371 347
6195 0009501  15
6057 344
5399 15
76872763 25342


Satellite: ISS
Catalog Number: 25544
Epoch time:      07260
48838871   =   yrday
fracday
Element set:     905
Inclination:       51
6371  deg
RA of node:       347
6195  deg
Eccentricity:     
0009501     
Arg of perigee:    15
6057  deg
Mean anomaly:     344
5399  deg
Mean motion:   15
76872763  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2534
Checksum:              320


Coasting Arc #7 (Orbit 2549)
---------------------------------------

Vector Time (GMT): 2007/261/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4331249
53                 A    =         6714843
52  meter
 Y    =       -2398882
96  meter          E    =           
0017988
 Z    =       -4553252
95                 I    =           51
52592
 XDOT =       5585
673102                 Wp   =           45
60375
 YDOT =      -4337
831832  meter/sec      RA   =          342
02448  deg
 ZDOT =      -3022
908514                 TA   =          194
23640
                                          MA   =          194
28716
                                          Ha   =            188
280  n
mi
                                          Hp   =            177
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14210136
24                 X    =        -4281983
84
 Y    =       -7870350
93  feet           Y    =        -2447041
99  meter
 Z    =      -14938493
94                 Z    =        -4574174
71
 XDOT =      18325
699152                 XDOT =        5648
449142
 YDOT =     -14231
731732  feet/sec       YDOT =       -4275
018689  meter/sec
 ZDOT =      -9917
678852                 ZDOT =       -2995
620535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12458989
32                 X    =         3797499
94
 Y    =       10308096
56  feet           Y    =         3141907
83  meter
 Z    =      -15018179
90                 Z    =        -4577541
23
 XDOT =     -19911
249015                 XDOT =       -6068
948700
 YDOT =       9742
800716  feet/sec       YDOT =        2969
605658  meter/sec
 ZDOT =      -9814
607091                 ZDOT =       -2991
492241


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   07261
50235513  
00020000  00000-0  20000-3 0  9065
2 25544  51
6367 342
3896 0009483  19
7470 340
4060 15
76894179 25503


Satellite: ISS
Catalog Number: 25544
Epoch time:      07261
50235513   =   yrday
fracday
Element set:     906
Inclination:       51
6367  deg
RA of node:       342
3896  deg
Eccentricity:     
0009483     
Arg of perigee:    19
7470  deg
Mean anomaly:     340
4060  deg
Mean motion:   15
76894179  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2550
Checksum:              300


Coasting Arc #8 (Orbit 2565)
---------------------------------------

Vector Time (GMT): 2007/262/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5294629
58                 A    =         6722589
56  meter
 Y    =        3761288
15  meter          E    =           
0016916
 Z    =        1728306
74                 I    =           51
52464
 XDOT =      -4117
645121                 Wp   =           80
43410
 YDOT =      -3157
808863  meter/sec      RA   =          336
81975  deg
 ZDOT =      -5692
081857                 TA   =           80
38907
                                          MA   =           80
19799
                                          Ha   =            188
402  n
mi
                                          Hp   =            177
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17370831
97                 X    =        -5344691
23
 Y    =       12340184
22  feet           Y    =         3701800
69  meter
 Z    =        5670297
71                 Z    =         1702463
66
 XDOT =     -13509
334388                 XDOT =       -4054
376682
 YDOT =     -10360
265300  feet/sec       YDOT =       -3203
500911  meter/sec
 ZDOT =     -18674
809243                 ZDOT =       -5711
931868

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19199365
27                 X    =         5851966
53
 Y    =       -9300982
27  feet           Y    =        -2834939
40  meter
 Z    =        5572641
04                 Z    =         1698540
99
 XDOT =      10833
650283                 XDOT =        3302
096606
 YDOT =      11028
968687  feet/sec       YDOT =        3361
629656  meter/sec
 ZDOT =     -18750
516814                 ZDOT =       -5715
157525


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   07262
51630473  
00020000  00000-0  20000-3 0  9072
2 25544  51
6362 337
1595 0009663  24
2732 335
8886 15
76932939 25666


Satellite: ISS
Catalog Number: 25544
Epoch time:      07262
51630473   =   yrday
fracday
Element set:     907
Inclination:       51
6362  deg
RA of node:       337
1595  deg
Eccentricity:     
0009663     
Arg of perigee:    24
2732  deg
Mean anomaly:     335
8886  deg
Mean motion:   15
76932939  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2566
Checksum:              320


Coasting Arc #9 (Orbit 2581)
---------------------------------------

Vector Time (GMT): 2007/263/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2824309
17                 A    =         6711817
17  meter
 Y    =        3173119
65  meter          E    =           
0009988
 Z    =        5189414
63                 I    =           51
46334
 XDOT =      -6380
930838                 Wp   =           45
86199
 YDOT =       4240
734387  meter/sec      RA   =          331
67432  deg
 ZDOT =        885
554575                 TA   =           35
73057
                                          MA   =           35
66377
                                          Ha   =            188
292  n
mi
                                          Hp   =            176
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9266106
19                 X    =         2763407
62
 Y    =       10410497
53  feet           Y    =         3204362
12  meter
 Z    =       17025638
56                 Z    =         5202987
27
 XDOT =     -20934
812460                 XDOT =       -6432
178999
 YDOT =      13913
170560  feet/sec       YDOT =        4169
092664  meter/sec
 ZDOT =       2905
362779                 ZDOT =         854
431434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7529238
51                 X    =        -2294911
90
 Y    =      -11652479
76  feet           Y    =        -3551675
83  meter
 Z    =       17077524
24                 Z    =         5205229
39
 XDOT =      21928
870473                 XDOT =        6683
919720
 YDOT =     -10111
569864  feet/sec       YDOT =       -3082
006495  meter/sec
 ZDOT =       2787
718005                 ZDOT =         849
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   07263
53023536  
00020000  00000-0  20000-3 0  9082
2 25544  51
6366 331
9287 0009638  27
1954 332
9714 15
76990595 25828


Satellite: ISS
Catalog Number: 25544
Epoch time:      07263
53023536   =   yrday
fracday
Element set:     908
Inclination:       51
6366  deg
RA of node:       331
9287  deg
Eccentricity:     
0009638     
Arg of perigee:    27
1954  deg
Mean anomaly:     332
9714  deg
Mean motion:   15
76990595  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2582
Checksum:              322


Coasting Arc #10 (Orbit 2597)
---------------------------------------

Vector Time (GMT): 2007/264/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5686174
35                 A    =         6723777
87  meter
 Y    =       -3559478
37  meter          E    =           
0022464
 Z    =         213904
64                 I    =           51
47790
 XDOT =       2378
358968                 Wp   =           39
92648
 YDOT =       4181
585080  meter/sec      RA   =          326
49940  deg
 ZDOT =       6029
232150                 TA   =          322
40813
                                          MA   =          322
56495
                                          Ha   =            188
589  n
mi
                                          Hp   =            176
794

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18655427
66                 X    =         5724515
25
 Y    =      -11678078
64  feet           Y    =        -3495677
98  meter
 Z    =         701786
87                 Z    =          241621
23
 XDOT =       7803
014987                 XDOT =        2302
134158
 YDOT =      13719
111155  feet/sec       YDOT =        4207
755055  meter/sec
 ZDOT =      19780
945373                 ZDOT =        6040
601062

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20019415
11                 X    =        -6101917
73
 Y    =        9136052
35  feet           Y    =         2784668
76  meter
 Z    =         806580
87                 Z    =          245845
85
 XDOT =      -5163
397200                 XDOT =       -1573
803467
 YDOT =     -13147
975733  feet/sec       YDOT =       -4007
503003  meter/sec
 ZDOT =      19824
587538                 ZDOT =        6042
534281


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   07264
54415307  
00020000  00000-0  20000-3 0  9096
2 25544  51
6361 326
6988 0009955  31
0720 329
1032 15
76952765 25984


Satellite: ISS
Catalog Number: 25544
Epoch time:      07264
54415307   =   yrday
fracday
Element set:     909
Inclination:       51
6361  deg
RA of node:       326
6988  deg
Eccentricity:     
0009955     
Arg of perigee:    31
0720  deg
Mean anomaly:     329
1032  deg
Mean motion:   15
76952765  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2598
Checksum:              312


Coasting Arc #11 (Orbit 2612)
---------------------------------------

Vector Time (GMT): 2007/265/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1330513
49                 A    =         6712250
76  meter
 Y    =       -4160055
89  meter          E    =           
0020143
 Z    =       -5112310
69                 I    =           51
41522
 XDOT =       6538
492934                 Wp   =           73
75020
 YDOT =      -3802
336454  meter/sec      RA   =          321
31293  deg
 ZDOT =       1402
508768                 TA   =          209
68029
                                          MA   =          209
79473
                                          Ha   =            188
571  n
mi
                                          Hp   =            176
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4365201
74                 X    =        -1259061
61
 Y    =      -13648477
33  feet           Y    =        -4174535
04  meter
 Z    =      -16772672
87                 Z    =        -5118600
67
 XDOT =      21451
748470                 XDOT =        6573
712153
 YDOT =     -12474
857133  feet/sec       YDOT =       -3729
022381  meter/sec
 ZDOT =       4601
406719                 ZDOT =        1434
358325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2689442
05                 X    =          819741
94
 Y    =       14045812
98  feet           Y    =         4281163
79  meter
 Z    =      -16797038
86                 Z    =        -5119737
44
 XDOT =     -21682
084662                 XDOT =       -6608
699405
 YDOT =       9758
757024  feet/sec       YDOT =        2974
469141  meter/sec
 ZDOT =       4721
859680                 ZDOT =        1439
222830


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   07265
49468156  
00020000  00000-0  20000-3 0  9103
2 25544  51
6354 321
7954 0009931  34
5544 325
6265 15
76998891 26138


Satellite: ISS
Catalog Number: 25544
Epoch time:      07265
49468156   =   yrday
fracday
Element set:     910
Inclination:       51
6354  deg
RA of node:       321
7954  deg
Eccentricity:     
0009931     
Arg of perigee:    34
5544  deg
Mean anomaly:     325
6265  deg
Mean motion:   15
76998891  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2613
Checksum:              323


Coasting Arc #12 (Orbit 2628)
---------------------------------------

Vector Time (GMT): 2007/266/11:33:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5623533
83                 A    =         6721328
77  meter
 Y    =        2957126
92  meter          E    =           
0010996
 Z    =       -2208065
76                 I    =           51
42473
 XDOT =       -689
942820                 Wp   =           71
59213
 YDOT =      -5376
414870  meter/sec      RA   =          316
17032  deg
 ZDOT =      -5461
939962                 TA   =          133
23580
                                          MA   =          133
14395
                                          Ha   =            188
635  n
mi
                                          Hp   =            176
287

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18449914
15                 X    =        -5645456
56
 Y    =        9701859
99  feet           Y    =         2894118
71  meter
 Z    =       -7244310
23                 Z    =        -2235438
19
 XDOT =      -2263
591928                 XDOT =        -603
238627
 YDOT =     -17639
156398  feet/sec       YDOT =       -5383
645666  meter/sec
 ZDOT =     -17919
750531                 ZDOT =       -5465
080841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19261002
19                 X    =         5870753
47
 Y    =       -7875793
54  feet           Y    =        -2400541
87  meter
 Z    =       -7347865
04                 Z    =        -2239629
26
 XDOT =       -127
809493                 XDOT =         -38
956333
 YDOT =      16360
991934  feet/sec       YDOT =        4986
830341  meter/sec
 ZDOT =     -17932
313111                 ZDOT =       -5465
769036


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   07266
50856365  
00020000  00000-0  20000-3 0  9110
2 25544  51
6354 316
5644 0010059  39
1485 321
0405 15
77046594 26292


Satellite: ISS
Catalog Number: 25544
Epoch time:      07266
50856365   =   yrday
fracday
Element set:     911
Inclination:       51
6354  deg
RA of node:       316
5644  deg
Eccentricity:     
0010059     
Arg of perigee:    39
1485  deg
Mean anomaly:     321
0405  deg
Mean motion:   15
77046594  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2629
Checksum:              294

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

The following information is a reminder of your current mailing list subscription:

You are subscribed to the following list: [list_name]

using the following email: example@example.com

You may automatically unsubscribe from this list at any time by visiting the following URL:

http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/

If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism

You may also change your subscription by visiting this list's main screen:

http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]

If you're still having trouble, please contact the list owner at:

<mailto:list
admin@aus-city
com>

The following physical address is associated with this mailing list:

http://www aus-city com

Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list