Date: February 1st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9902 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 632)
---------------------------------------

Vector Time (GMT): 2008/028/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1525977
94                 A    =         6712472
18  meter
 Y    =       -4565772
75  meter          E    =           
0012572
 Z    =       -4689274
74                 I    =           51
74355
 XDOT =       7166
688300                 Wp   =           43
29085
 YDOT =        454
508405  meter/sec      RA   =           21
33709  deg
 ZDOT =      -2770
099510                 TA   =          199
40594
                                          MA   =          199
45385
                                          Ha   =            185
072  n
mi
                                          Hp   =            178
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5006489
30                 X    =        -1452030
04
 Y    =      -14979569
38  feet           Y    =        -4582423
55  meter
 Z    =      -15384759
65                 Z    =        -4696508
30
 XDOT =      23512
756891                 XDOT =        7174
529717
 YDOT =       1491
169309  feet/sec       YDOT =         534
694287  meter/sec
 ZDOT =      -9088
252984                 ZDOT =       -2735
265203

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9027095
69                 X    =         2751458
77
 Y    =      -12926646
64  feet           Y    =        -3940041
90  meter
 Z    =      -15412871
68                 Z    =        -4697843
29
 XDOT =      12010
324255                 XDOT =        3660
746833
 YDOT =      19082
531522  feet/sec       YDOT =        5816
355608  meter/sec
 ZDOT =      -8954
979085                 ZDOT =       -2729
477625


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   08028
52197361  
00020000  00000-0  20000-3 0  9001
2 25544  51
6382  21
7147 0005757 341
0535  19
0421 15
77551467  6331


Satellite: ISS
Catalog Number: 25544
Epoch time:      08028
52197361   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:        21
7147  deg
Eccentricity:     
0005757     
Arg of perigee:   341
0535  deg
Mean anomaly:      19
0421  deg
Mean motion:   15
77551467  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             633
Checksum:              274


Coasting Arc #2 (Orbit 648)
---------------------------------------

Vector Time (GMT): 2008/029/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6541307
52                 A    =         6721221
49  meter
 Y    =        -842808
75  meter          E    =           
0010480
 Z    =        1280679
15                 I    =           51
74598
 XDOT =       -516
610683                 Wp   =           98
01660
 YDOT =      -4965
743359  meter/sec      RA   =           16
14839  deg
 ZDOT =      -5867
377994                 TA   =           67
93504
                                          MA   =           67
82378
                                          Ha   =            185
140  n
mi
                                          Hp   =            178
526

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21460982
68                 X    =        -6537618
17
 Y    =       -2765120
59  feet           Y    =         -915936
79  meter
 Z    =        4201703
25                 Z    =         1248910
82
 XDOT =      -1694
916940                 XDOT =        -432
542285
 YDOT =     -16291
808922  feet/sec       YDOT =       -4971
050150  meter/sec
 ZDOT =     -19249
927801                 ZDOT =       -5869
683621

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11008337
86                 X    =        -3355341
38
 Y    =      -18655913
24  feet           Y    =        -5686322
36  meter
 Z    =        4080119
90                 Z    =         1243620
55
 XDOT =      10525
407290                 XDOT =        3208
144142
 YDOT =     -10451
812848  feet/sec       YDOT =       -3185
712556  meter/sec
 ZDOT =     -19259
227868                 ZDOT =       -5870
212654


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   08029
53549788  
00020000  00000-0  20000-3 0  9018
2 25544  51
6383  16
4818 0005937 345
0426  15
0563 15
77620249  6496


Satellite: ISS
Catalog Number: 25544
Epoch time:      08029
53549788   =   yrday
fracday
Element set:     901
Inclination:       51
6383  deg
RA of node:        16
4818  deg
Eccentricity:     
0005937     
Arg of perigee:   345
0426  deg
Mean anomaly:      15
0563  deg
Mean motion:   15
77620249  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             649
Checksum:              306


Coasting Arc #3 (Orbit 664)
---------------------------------------

Vector Time (GMT): 2008/030/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -700040
84                 A    =         6709773
10  meter
 Y    =        4101393
41  meter          E    =           
0005773
 Z    =        5262962
68                 I    =           51
67875
 XDOT =      -7579
429432                 Wp   =           11
13521
 YDOT =      -1401
584552  meter/sec      RA   =           11
00337  deg
 ZDOT =         89
635150                 TA   =           78
04791
                                          MA   =           77
98319
                                          Ha   =            185
239  n
mi
                                          Hp   =            178
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2296721
91                 X    =         -771417
43
 Y    =       13456015
12  feet           Y    =         4093165
81  meter
 Z    =       17266937
92                 Z    =         5259388
75
 XDOT =     -24866
894463                 XDOT =       -7563
628807
 YDOT =      -4598
374515  feet/sec       YDOT =       -1486
253703  meter/sec
 ZDOT =        294
078577                 ZDOT =          52
853031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11979907
49                 X    =        -3651475
80
 Y    =        6578700
52  feet           Y    =         2005187
92  meter
 Z    =       17253664
41                 Z    =         5258916
91
 XDOT =     -11543
598430                 XDOT =       -3518
488801
 YDOT =     -21375
234684  feet/sec       YDOT =       -6515
171532  meter/sec
 ZDOT =        153
266407                 ZDOT =          46
715601


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   08030
54899823  
00020000  00000-0  20000-3 0  9020
2 25544  51
6380  11
2489 0005876 348
2774  11
8253 15
77628918  6652


Satellite: ISS
Catalog Number: 25544
Epoch time:      08030
54899823   =   yrday
fracday
Element set:     902
Inclination:       51
6380  deg
RA of node:        11
2489  deg
Eccentricity:     
0005876     
Arg of perigee:   348
2774  deg
Mean anomaly:      11
8253  deg
Mean motion:   15
77628918  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             665
Checksum:              314


Coasting Arc #4 (Orbit 680)
---------------------------------------

Vector Time (GMT): 2008/031/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6427315
63                 A    =         6721025
15  meter
 Y    =        1560757
44  meter          E    =           
0017026
 Z    =        1135388
94                 I    =           51
68882
 XDOT =      -2136
316721                 Wp   =           39
68336
 YDOT =       4473
533714  meter/sec      RA   =            5
85431  deg
 ZDOT =       5908
475305                 TA   =          332
76852
                                          MA   =          332
85770
                                          Ha   =            185
087  n
mi
                                          Hp   =            178
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21086993
55                 X    =         6403869
87
 Y    =        5120595
29  feet           Y    =         1632500
18  meter
 Z    =        3725029
34                 Z    =         1166555
60
 XDOT =      -7008
913128                 XDOT =       -2214
883628
 YDOT =      14676
947882  feet/sec       YDOT =        4449
204531  meter/sec
 ZDOT =      19384
761498                 ZDOT =        5897
906663

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9566761
94                 X    =         2915949
04
 Y    =       19453931
28  feet           Y    =         5929558
25  meter
 Z    =        3844380
35                 Z    =         1171767
13
 XDOT =     -14410
766053                 XDOT =       -4392
401493
 YDOT =       3241
623928  feet/sec       YDOT =         988
046973  meter/sec
 ZDOT =      19344
768716                 ZDOT =        5896
285505


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   08031
56247038  
00020000  00000-0  20000-3 0  9039
2 25544  51
6381   6
0162 0005663 352
1067   8
0008 15
77720304  6812


Satellite: ISS
Catalog Number: 25544
Epoch time:      08031
56247038   =   yrday
fracday
Element set:     903
Inclination:       51
6381  deg
RA of node:         6
0162  deg
Eccentricity:     
0005663     
Arg of perigee:   352
1067  deg
Mean anomaly:       8
0008  deg
Mean motion:   15
77720304  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             681
Checksum:              253


Coasting Arc #5 (Orbit 695)
---------------------------------------

Vector Time (GMT): 2008/032/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2987353
45                 A    =         6711970
59  meter
 Y    =       -3713815
67  meter          E    =           
0010505
 Z    =       -4733675
65                 I    =           51
62897
 XDOT =       6894
034686                 Wp   =           77
27851
 YDOT =       2177
412343  meter/sec      RA   =             
65980  deg
 ZDOT =       2649
616663                 TA   =          218
71811
                                          MA   =          218
79346
                                          Ha   =            185
339  n
mi
                                          Hp   =            178
006

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9801028
39                 X    =         3051654
89
 Y    =      -12184434
61  feet           Y    =        -3680049
49  meter
 Z    =      -15530431
92                 Z    =        -4719007
40
 XDOT =      22618
224036                 XDOT =        6856
302981
 YDOT =       7143
741282  feet/sec       YDOT =        2254
294187  meter/sec
 ZDOT =       8692
968055                 ZDOT =        2683
015912

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15684823
04                 X    =         4780734
06
 Y    =        -485177
82  feet           Y    =         -147882
20  meter
 Z    =      -15474684
12                 Z    =        -4716683
72
 XDOT =       9316
703200                 XDOT =        2839
731135
 YDOT =      20602
847177  feet/sec       YDOT =        6279
747820  meter/sec
 ZDOT =       8820
919162                 ZDOT =        2688
616161


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   08032
51258042  
00020000  00000-0  20000-3 0  9043
2 25544  51
6383   1
1098 0005907 355
7559   4
3555 15
77695463  6963


Satellite: ISS
Catalog Number: 25544
Epoch time:      08032
51258042   =   yrday
fracday
Element set:     904
Inclination:       51
6383  deg
RA of node:         1
1098  deg
Eccentricity:     
0005907     
Arg of perigee:   355
7559  deg
Mean anomaly:       4
3555  deg
Mean motion:   15
77695463  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             696
Checksum:              298


Coasting Arc #6 (Orbit 711)
---------------------------------------

Vector Time (GMT): 2008/033/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5354982
60                 A    =         6716421
63  meter
 Y    =       -2263068
14  meter          E    =           
0007777
 Z    =       -3373897
18                 I    =           51
61638
 XDOT =       4628
929763                 Wp   =           38
60067
 YDOT =      -4043
309332  meter/sec      RA   =          355
54097  deg
 ZDOT =      -4634
610327                 TA   =          181
21662
                                          MA   =          181
21852
                                          Ha   =            185
320  n
mi
                                          Hp   =            177
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17568840
54                 X    =        -5312889
14
 Y    =       -7424764
23  feet           Y    =        -2322714
96  meter
 Z    =      -11069216
48                 Z    =        -3399809
17
 XDOT =      15186
777439                 XDOT =        4696
312331
 YDOT =     -13265
450564  feet/sec       YDOT =       -3991
168861  meter/sec
 ZDOT =     -15205
414459                 ZDOT =       -4611
960061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6139526
86                 X    =        -1871327
79
 Y    =      -17996908
39  feet           Y    =        -5485457
68  meter
 Z    =      -11168542
14                 Z    =        -3404171
64
 XDOT =      18757
318142                 XDOT =        5717
230570
 YDOT =       2984
245038  feet/sec       YDOT =         909
597888  meter/sec
 ZDOT =     -15119
165696                 ZDOT =       -4608
321704


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   08033
52600385  
00020000  00000-0  20000-3 0  9057
2 25544  51
6390 355
8760 0005947 359
8051    
3111 15
77767736  7128


Satellite: ISS
Catalog Number: 25544
Epoch time:      08033
52600385   =   yrday
fracday
Element set:     905
Inclination:       51
6390  deg
RA of node:       355
8760  deg
Eccentricity:     
0005947     
Arg of perigee:   359
8051  deg
Mean anomaly:        
3111  deg
Mean motion:   15
77767736  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             712
Checksum:              287


Coasting Arc #7 (Orbit 727)
---------------------------------------

Vector Time (GMT): 2008/034/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4926233
97                 A    =         6717227
19  meter
 Y    =        3340023
55  meter          E    =           
0014219
 Z    =        3108317
01                 I    =           51
59030
 XDOT =      -5144
930194                 Wp   =           69
99177
 YDOT =      -3037
536174  meter/sec      RA   =          350
32352  deg
 ZDOT =      -4867
284112                 TA   =           73
79636
                                          MA   =           73
63994
                                          Ha   =            185
381  n
mi
                                          Hp   =            177
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16162184
93                 X    =        -4978315
80
 Y    =       10958082
50  feet           Y    =         3284644
13  meter
 Z    =       10197890
45                 Z    =         3084259
67
 XDOT =     -16879
692236                 XDOT =       -5086
937756
 YDOT =      -9965
669862  feet/sec       YDOT =       -3094
745050  meter/sec
 ZDOT =     -15968
779895                 ZDOT =       -4892
137025

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19061028
82                 X    =        -5809801
58
 Y    =       -4453635
09  feet           Y    =        -1357467
98  meter
 Z    =       10106190
11                 Z    =         3080366
75
 XDOT =      -4421
647529                 XDOT =       -1347
718167
 YDOT =     -17699
303679  feet/sec       YDOT =       -5394
747761  meter/sec
 ZDOT =     -16064
133194                 ZDOT =       -4896
347797


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   08034
53940106  
00020000  00000-0  20000-3 0  9068
2 25544  51
6391 350
6426 0005958   3
0437 357
0763 15
77806658  7288


Satellite: ISS
Catalog Number: 25544
Epoch time:      08034
53940106   =   yrday
fracday
Element set:     906
Inclination:       51
6391  deg
RA of node:       350
6426  deg
Eccentricity:     
0005958     
Arg of perigee:     3
0437  deg
Mean anomaly:     357
0763  deg
Mean motion:   15
77806658  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             728
Checksum:              298


Coasting Arc #8 (Orbit 743)
---------------------------------------

Vector Time (GMT): 2008/035/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3448787
13                 A    =         6710744
66  meter
 Y    =        3079436
54  meter          E    =           
0006477
 Z    =        4857852
53                 I    =           51
54158
 XDOT =      -6431
675088                 Wp   =           69
24415
 YDOT =       3584
108492  meter/sec      RA   =          345
19755  deg
 ZDOT =       2293
920274                 TA   =          358
43009
                                          MA   =          358
43213
                                          Ha   =            185
171  n
mi
                                          Hp   =            177
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11314918
41                 X    =         3390498
13
 Y    =       10103138
25  feet           Y    =         3117676
57  meter
 Z    =       15937836
38                 Z    =         4874464
94
 XDOT =     -21101
296219                 XDOT =       -6482
418282
 YDOT =      11758
886130  feet/sec       YDOT =        3511
901952  meter/sec
 ZDOT =       7525
985152                 ZDOT =        2262
553035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         474579
69                 X    =          144651
89
 Y    =       15094252
97  feet           Y    =         4600728
31  meter
 Z    =       16001678
38                 Z    =         4877311
57
 XDOT =     -22019
699924                 XDOT =       -6711
604537
 YDOT =      -7159
925379  feet/sec       YDOT =       -2182
345256  meter/sec
 ZDOT =       7406
345235                 ZDOT =        2257
454028


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   08035
55277021  
00020000  00000-0  20000-3 0  9071
2 25544  51
6399 345
4094 0005804   5
4515 354
6712 15
77879195  7443


Satellite: ISS
Catalog Number: 25544
Epoch time:      08035
55277021   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       345
4094  deg
Eccentricity:     
0005804     
Arg of perigee:     5
4515  deg
Mean anomaly:     354
6712  deg
Mean motion:   15
77879195  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             744
Checksum:              306


Coasting Arc #9 (Orbit 758)
---------------------------------------

Vector Time (GMT): 2008/036/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6035502
02                 A    =         6720939
91  meter
 Y    =       -2837761
18  meter          E    =           
0016012
 Z    =        -758554
31                 I    =           51
54766
 XDOT =       2661
828699                 Wp   =           28
75515
 YDOT =       4081
386138  meter/sec      RA   =          339
99993  deg
 ZDOT =       5976
295655                 TA   =          322
94782
                                          MA   =          323
05827
                                          Ha   =            185
407  n
mi
                                          Hp   =            177
150

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19801515
82                 X    =         6070470
55
 Y    =       -9310240
09  feet           Y    =        -2770073
20  meter
 Z    =       -2488695
23                 Z    =         -729149
94
 XDOT =       8733
033791                 XDOT =        2586
961288
 YDOT =      13390
374468  feet/sec       YDOT =        4110
733279  meter/sec
 ZDOT =      19607
269208                 ZDOT =        5989
044814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20565772
25                 X    =         6268447
38
 Y    =        7508362
42  feet           Y    =         2288548
87  meter
 Z    =       -2376490
88                 Z    =         -724354
42
 XDOT =      -2884
949292                 XDOT =        -879
332544
 YDOT =      14052
030708  feet/sec       YDOT =        4283
058960  meter/sec
 ZDOT =      19656
436075                 ZDOT =        5991
281716


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   08036
50278219  
00020000  00000-0  20000-3 0  9088
2 25544  51
6397 340
5024 0005898   9
9906 350
1375 15
77875874  7598


Satellite: ISS
Catalog Number: 25544
Epoch time:      08036
50278219   =   yrday
fracday
Element set:     908
Inclination:       51
6397  deg
RA of node:       340
5024  deg
Eccentricity:     
0005898     
Arg of perigee:     9
9906  deg
Mean anomaly:     350
1375  deg
Mean motion:   15
77875874  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             759
Checksum:              328


Coasting Arc #10 (Orbit 774)
---------------------------------------

Vector Time (GMT): 2008/037/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1128723
70                 A    =         6709112
53  meter
 Y    =       -4067538
89  meter          E    =           
0016729
 Z    =       -5228136
35                 I    =           51
48189
 XDOT =       7141
982812                 Wp   =           74
45946
 YDOT =      -2794
911518  meter/sec      RA   =          334
82739  deg
 ZDOT =        638
654722                 TA   =          201
59371
                                          MA   =          201
66434
                                          Ha   =            185
382  n
mi
                                          Hp   =            176
937

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3703161
74                 X    =        -1057759
43
 Y    =      -13344943
85  feet           Y    =        -4079763
97  meter
 Z    =      -17152678
31                 Z    =        -5233447
28
 XDOT =      23431
702140                 XDOT =        7169
602770
 YDOT =      -9169
657211  feet/sec       YDOT =       -2714
891390  meter/sec
 ZDOT =       2095
323890                 ZDOT =         673
416365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6726406
87                 X    =         2050208
81
 Y    =      -12076639
22  feet           Y    =        -3680959
63  meter
 Z    =      -17173396
35                 Z    =        -5234451
21
 XDOT =      22295
380557                 XDOT =        6795
631994
 YDOT =       9278
101533  feet/sec       YDOT =        2827
965347  meter/sec
 ZDOT =       2228
024924                 ZDOT =         679
101997


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   08037
51610098  
00020000  00000-0  20000-3 0  9096
2 25544  51
6405 335
2682 0005890  13
3881 346
7439 15
77916592  7755


Satellite: ISS
Catalog Number: 25544
Epoch time:      08037
51610098   =   yrday
fracday
Element set:     909
Inclination:       51
6405  deg
RA of node:       335
2682  deg
Eccentricity:     
0005890     
Arg of perigee:    13
3881  deg
Mean anomaly:     346
7439  deg
Mean motion:   15
77916592  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             775
Checksum:              313


Coasting Arc #11 (Orbit 790)
---------------------------------------

Vector Time (GMT): 2008/038/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6173632
02                 A    =         6719341
02  meter
 Y    =        1899958
02  meter          E    =           
0006201
 Z    =       -1856506
00                 I    =           51
49181
 XDOT =         77
277078                 Wp   =           89
00843
 YDOT =      -5243
164451  meter/sec      RA   =          329
67438  deg
 ZDOT =      -5638
929800                 TA   =          111
66253
                                          MA   =          111
59647
                                          Ha   =            185
394  n
mi
                                          Hp   =            176
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20254698
24                 X    =        -6185400
53
 Y    =        6233458
08  feet           Y    =         1830855
16  meter
 Z    =       -6090898
95                 Z    =        -1886525
13
 XDOT =        253
533720                 XDOT =         163
293243
 YDOT =     -17201
983108  feet/sec       YDOT =       -5241
819328  meter/sec
 ZDOT =     -18500
425852                 ZDOT =       -5638
345497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18998310
63                 X    =        -5790685
08
 Y    =       -9314679
95  feet           Y    =        -2839114
45  meter
 Z    =       -6205544
37                 Z    =        -1891449
93
 XDOT =      11368
677078                 XDOT =        3465
172773
 YDOT =     -10898
086672  feet/sec       YDOT =       -3321
736818  meter/sec
 ZDOT =     -18498
716159                 ZDOT =       -5638
408685


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   08038
52939294  
00020000  00000-0  20000-3 0  9102
2 25544  51
6411 330
0343 0005882  17
5132 342
6235 15
77968508  7916


Satellite: ISS
Catalog Number: 25544
Epoch time:      08038
52939294   =   yrday
fracday
Element set:     910
Inclination:       51
6411  deg
RA of node:       330
0343  deg
Eccentricity:     
0005882     
Arg of perigee:    17
5132  deg
Mean anomaly:     342
6235  deg
Mean motion:   15
77968508  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             791
Checksum:              290


Coasting Arc #12 (Orbit 806)
---------------------------------------

Vector Time (GMT): 2008/039/12:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1174341
47                 A    =         6712829
29  meter
 Y    =        5031963
15  meter          E    =           
0014277
 Z    =        4280501
24                 I    =           51
44502
 XDOT =      -6734
398641                 Wp   =           53
21270
 YDOT =       1402
740938  meter/sec      RA   =          324
45452  deg
 ZDOT =      -3480
145735                 TA   =           72
12374
                                          MA   =           71
96809
                                          Ha   =            185
437  n
mi
                                          Hp   =            176
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3852826
35                 X    =        -1251315
68
 Y    =       16509065
45  feet           Y    =         5018400
70  meter
 Z    =       14043639
25                 Z    =         4274609
39
 XDOT =     -22094
483730                 XDOT =       -6732
678364
 YDOT =       4602
168431  feet/sec       YDOT =        1327
442605  meter/sec
 ZDOT =     -11417
800967                 ZDOT =       -3512
856345

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14013645
25                 X    =        -4271359
07
 Y    =        9572327
36  feet           Y    =         2917645
38  meter
 Z    =       14021612
32                 Z    =         4273787
44
 XDOT =     -18699
670031                 XDOT =       -5699
659426
 YDOT =     -10388
883909  feet/sec       YDOT =       -3166
531816  meter/sec
 ZDOT =     -11542
789065                 ZDOT =       -3518
242107


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   08039
54265831  
00020000  00000-0  20000-3 0  9115
2 25544  51
6407 324
8005 0005840  21
4608 338
6801 15
78001574  8077


Satellite: ISS
Catalog Number: 25544
Epoch time:      08039
54265831   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       324
8005  deg
Eccentricity:     
0005840     
Arg of perigee:    21
4608  deg
Mean anomaly:     338
6801  deg
Mean motion:   15
78001574  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             807
Checksum:              274

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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