Date: February 2nd 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 650)
---------------------------------------

Vector Time (GMT): 2008/029/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6135645
04                 A    =         6721357
68  meter
 Y    =       -2542349
39  meter          E    =           
0004733
 Z    =       -1028283
61                 I    =           51
74494
 XDOT =       2692
383959                 Wp   =          114
18339
 YDOT =      -4107
660920  meter/sec      RA   =           15
49500  deg
 ZDOT =      -5932
485663                 TA   =           77
05223
                                          MA   =           76
99937
                                          Ha   =            185
068  n
mi
                                          Hp   =            178
498

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20130069
03                 X    =        -6101764
93
 Y    =       -8341041
30  feet           Y    =        -2610772
19  meter
 Z    =       -3373633
89                 Z    =        -1058007
99
 XDOT =       8833
280706                 XDOT =        2766
934932
 YDOT =     -13476
577821  feet/sec       YDOT =       -4077
136107  meter/sec
 ZDOT =     -19463
535641                 ZDOT =       -5919
225288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19344728
36                 X    =        -5896273
20
 Y    =       -9989616
26  feet           Y    =        -3044835
04  meter
 Z    =       -3487564
56                 Z    =        -1063009
68
 XDOT =       9307
945696                 XDOT =        2837
061848
 YDOT =     -11272
886926  feet/sec       YDOT =       -3435
975935  meter/sec
 ZDOT =     -19413
218184                 ZDOT =       -5917
148902


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
66217475  
00020000  00000-0  20000-3 0  9006
2 25544  51
6402  15
8285 0005895 343
9524  16
1453 15
77634465  6516


Satellite: ISS
Catalog Number: 25544
Epoch time:      08029
66217475   =   yrday
fracday
Element set:     900
Inclination:       51
6402  deg
RA of node:        15
8285  deg
Eccentricity:     
0005895     
Arg of perigee:   343
9524  deg
Mean anomaly:      16
1453  deg
Mean motion:   15
77634465  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             651
Checksum:              294


Coasting Arc #2 (Orbit 666)
---------------------------------------

Vector Time (GMT): 2008/030/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3432823
05                 A    =         6711823
54  meter
 Y    =        3218851
28  meter          E    =           
0010703
 Z    =        4785080
78                 I    =           51
68443
 XDOT =      -6537
646996                 Wp   =           28
35643
 YDOT =      -3211
507584  meter/sec      RA   =           10
30746  deg
 ZDOT =      -2518
238878                 TA   =           86
31557
                                          MA   =           86
19318
                                          Ha   =            185
198  n
mi
                                          Hp   =            178
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11262542
81                 X    =        -3491806
38
 Y    =       10560535
71  feet           Y    =         3180133
46  meter
 Z    =       15699083
92                 Z    =         4768261
22
 XDOT =     -21448
973083                 XDOT =       -6489
016531
 YDOT =     -10536
442205  feet/sec       YDOT =       -3284
343235  meter/sec
 ZDOT =      -8261
938577                 ZDOT =       -2549
880432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12026123
10                 X    =        -3665562
32
 Y    =        9785096
03  feet           Y    =         2982497
27  meter
 Z    =       15635065
72                 Z    =         4765568
03
 XDOT =     -19943
041684                 XDOT =       -6078
639105
 YDOT =     -11054
561776  feet/sec       YDOT =       -3369
430429  meter/sec
 ZDOT =      -8383
264369                 ZDOT =       -2555
218980


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
67565231  
00020000  00000-0  20000-3 0  9016
2 25544  51
6402  10
5960 0005877 348
0684  12
0341 15
77672232  6673


Satellite: ISS
Catalog Number: 25544
Epoch time:      08030
67565231   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:        10
5960  deg
Eccentricity:     
0005877     
Arg of perigee:   348
0684  deg
Mean anomaly:      12
0341  deg
Mean motion:   15
77672232  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             667
Checksum:              271


Coasting Arc #3 (Orbit 682)
---------------------------------------

Vector Time (GMT): 2008/031/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5027999
32                 A    =         6716962
47  meter
 Y    =        3032546
95  meter          E    =           
0013473
 Z    =        3244920
19                 I    =           51
67348
 XDOT =      -5079
916352                 Wp   =           62
13369
 YDOT =       3318
056724  meter/sec      RA   =            5
19179  deg
 ZDOT =       4761
675913                 TA   =          335
93201
                                          MA   =          335
99491
                                          Ha   =            185
111  n
mi
                                          Hp   =            178
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16496060
75                 X    =         4977952
19
 Y    =        9949301
02  feet           Y    =         3088492
85  meter
 Z    =       10646063
60                 Z    =         3269224
53
 XDOT =     -16666
392232                 XDOT =       -5139
772886
 YDOT =      10886
012874  feet/sec       YDOT =        3260
915216  meter/sec
 ZDOT =      15622
296304                 ZDOT =        4736
852828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15927241
46                 X    =         4854623
20
 Y    =       10744183
87  feet           Y    =         3274827
24  meter
 Z    =       10739309
74                 Z    =         3273341
61
 XDOT =     -16485
345410                 XDOT =       -5024
733281
 YDOT =       8888
896173  feet/sec       YDOT =        2709
335554  meter/sec
 ZDOT =      15527
674166                 ZDOT =        4732
835086


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
68910409  
00020000  00000-0  20000-3 0  9020
2 25544  51
6403   5
3625 0005872 352
1037   8
0034 15
77708985  6834


Satellite: ISS
Catalog Number: 25544
Epoch time:      08031
68910409   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:         5
3625  deg
Eccentricity:     
0005872     
Arg of perigee:   352
1037  deg
Mean anomaly:       8
0034  deg
Mean motion:   15
77708985  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             683
Checksum:              276


Coasting Arc #4 (Orbit 697)
---------------------------------------

Vector Time (GMT): 2008/032/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5268085
24                 A    =         6716924
82  meter
 Y    =       -2585352
43  meter          E    =           
0007611
 Z    =       -3264603
58                 I    =           51
64472
 XDOT =       4773
996733                 Wp   =           32
45035
 YDOT =       3752
049072  meter/sec      RA   =          359
97819  deg
 ZDOT =       4743
800582                 TA   =          289
23740
                                          MA   =          289
31974
                                          Ha   =            185
255  n
mi
                                          Hp   =            177
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17283744
22                 X    =         5312462
13
 Y    =       -8482127
39  feet           Y    =        -2526193
32  meter
 Z    =      -10710641
68                 Z    =        -3238904
02
 XDOT =      15662
718941                 XDOT =        4708
641755
 YDOT =      12309
872285  feet/sec       YDOT =        3805
068829  meter/sec
 ZDOT =      15563
650202                 ZDOT =        4766
833859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17605923
86                 X    =         5366285
59
 Y    =       -7924420
56  feet           Y    =        -2415363
39  meter
 Z    =      -10612593
87                 Z    =        -3234718
61
 XDOT =      14595
781768                 XDOT =        4448
794283
 YDOT =      11516
671667  feet/sec       YDOT =        3510
281524  meter/sec
 ZDOT =      15652
104667                 ZDOT =        4770
761503


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
63919120  
00020000  00000-0  20000-3 0  9036
2 25544  51
6406    
4562 0005848 355
3649   4
7461 15
77758373  6989


Satellite: ISS
Catalog Number: 25544
Epoch time:      08032
63919120   =   yrday
fracday
Element set:     903
Inclination:       51
6406  deg
RA of node:          
4562  deg
Eccentricity:     
0005848     
Arg of perigee:   355
3649  deg
Mean anomaly:       4
7461  deg
Mean motion:   15
77758373  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             698
Checksum:              297


Coasting Arc #5 (Orbit 713)
---------------------------------------

Vector Time (GMT): 2008/033/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3106298
95                 A    =         6711252
37  meter
 Y    =       -3537662
98  meter          E    =           
0014793
 Z    =       -4796350
65                 I    =           51
59776
 XDOT =       6804
415055                 Wp   =           49
68199
 YDOT =      -2593
598867  meter/sec      RA   =          354
85759  deg
 ZDOT =      -2489
446618                 TA   =          195
91503
                                          MA   =          195
96156
                                          Ha   =            185
226  n
mi
                                          Hp   =            177
535

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10191269
53                 X    =        -3043210
03
 Y    =      -11606505
85  feet           Y    =        -3572046
23  meter
 Z    =      -15736058
55                 Z    =        -4811287
83
 XDOT =      22324
196375                 XDOT =        6845
004417
 YDOT =      -8509
182634  feet/sec       YDOT =       -2517
280870  meter/sec
 ZDOT =      -8167
475781                 ZDOT =       -2456
293009

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9930173
34                 X    =        -3026716
84
 Y    =      -11753833
13  feet           Y    =        -3582568
34  meter
 Z    =      -15793528
91                 Z    =        -4813867
61
 XDOT =      21635
732286                 XDOT =        6594
571201
 YDOT =      -7455
100873  feet/sec       YDOT =       -2272
314746  meter/sec
 ZDOT =      -8040
914344                 ZDOT =       -2450
870692


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
65259218  
00020000  00000-0  20000-3 0  9045
2 25544  51
6413 355
2226 0005872 359
8852    
2310 15
77812715  7141


Satellite: ISS
Catalog Number: 25544
Epoch time:      08033
65259218   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:       355
2226  deg
Eccentricity:     
0005872     
Arg of perigee:   359
8852  deg
Mean anomaly:        
2310  deg
Mean motion:   15
77812715  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             714
Checksum:              278


Coasting Arc #6 (Orbit 729)
---------------------------------------

Vector Time (GMT): 2008/034/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6369691
31                 A    =         6720975
52  meter
 Y    =        1918347
80  meter          E    =           
0011664
 Z    =         938807
36                 I    =           51
60150
 XDOT =      -2204
438649                 Wp   =          100
30027
 YDOT =      -4383
252952  meter/sec      RA   =          349
66126  deg
 ZDOT =      -5939
973150                 TA   =           69
42859
                                          MA   =           69
30349
                                          Ha   =            185
277  n
mi
                                          Hp   =            177
539

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20897937
37                 X    =        -6395229
62
 Y    =        6293792
00  feet           Y    =         1846975
42  meter
 Z    =        3080076
65                 Z    =          907802
23
 XDOT =      -7232
410267                 XDOT =       -2126
405945
 YDOT =     -14380
751156  feet/sec       YDOT =       -4407
467443  meter/sec
 ZDOT =     -19488
100885                 ZDOT =       -5950
492897

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20899293
60                 X    =        -6370104
69
 Y    =        6345907
90  feet           Y    =         1934232
73  meter
 Z    =        2961664
40                 Z    =          902715
31
 XDOT =      -6694
989057                 XDOT =       -2040
632665
 YDOT =     -12838
944064  feet/sec       YDOT =       -3913
310151  meter/sec
 ZDOT =     -19528
758758                 ZDOT =       -5952
365669


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
66596732  
00020000  00000-0  20000-3 0  9053
2 25544  51
6413 349
9886 0005756   3
3479 356
7724 15
77819508  7303


Satellite: ISS
Catalog Number: 25544
Epoch time:      08034
66596732   =   yrday
fracday
Element set:     905
Inclination:       51
6413  deg
RA of node:       349
9886  deg
Eccentricity:     
0005756     
Arg of perigee:     3
3479  deg
Mean anomaly:     356
7724  deg
Mean motion:   15
77819508  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             730
Checksum:              328


Coasting Arc #7 (Orbit 745)
---------------------------------------

Vector Time (GMT): 2008/035/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         681946
00                 A    =         6709018
29  meter
 Y    =        4131054
06  meter          E    =           
0007333
 Z    =        5239980
37                 I    =           51
53379
 XDOT =      -7497
775454                 Wp   =           24
05795
 YDOT =       1751
467268  meter/sec      RA   =          344
49655  deg
 ZDOT =       -398
237077                 TA   =           69
76399
                                          MA   =           69
68515
                                          Ha   =            185
189  n
mi
                                          Hp   =            177
270

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2237355
65                 X    =          610247
05
 Y    =       13553326
97  feet           Y    =         4138278
70  meter
 Z    =       17191536
65                 Z    =         5243119
32
 XDOT =     -24599
000833                 XDOT =       -7514
868872
 YDOT =       5746
283688  feet/sec       YDOT =        1667
527332  meter/sec
 ZDOT =      -1306
552091                 ZDOT =        -434
701683

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2406439
21                 X    =          733482
67
 Y    =       13508545
04  feet           Y    =         4117404
53  meter
 Z    =       17203942
16                 Z    =         5243761
57
 XDOT =     -23488
211861                 XDOT =       -7159
206975
 YDOT =       6053
981485  feet/sec       YDOT =        1845
253557  meter/sec
 ZDOT =      -1445
867310                 ZDOT =        -440
700356


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
67931346  
00020000  00000-0  20000-3 0  9060
2 25544  51
6415 344
7547 0005804   5
5373 354
5855 15
77916925  7462


Satellite: ISS
Catalog Number: 25544
Epoch time:      08035
67931346   =   yrday
fracday
Element set:     906
Inclination:       51
6415  deg
RA of node:       344
7547  deg
Eccentricity:     
0005804     
Arg of perigee:     5
5373  deg
Mean anomaly:     354
5855  deg
Mean motion:   15
77916925  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             746
Checksum:              314


Coasting Arc #8 (Orbit 761)
---------------------------------------

Vector Time (GMT): 2008/036/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6426132
51                 A    =         6719901
07  meter
 Y    =       -1049042
33  meter          E    =           
0018258
 Z    =        1618405
50                 I    =           51
54315
 XDOT =       -620
119509                 Wp   =           48
35927
 YDOT =       5110
083200  meter/sec      RA   =          339
34315  deg
 ZDOT =       5745
096214                 TA   =          329
58178
                                          MA   =          329
68759
                                          Ha   =            185
293  n
mi
                                          Hp   =            177
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21083111
90                 X    =         6429523
78
 Y    =       -3441739
93  feet           Y    =         -977162
79  meter
 Z    =        5309729
34                 Z    =         1649630
89
 XDOT =      -2034
512824                 XDOT =        -705
122948
 YDOT =      16765
364831  feet/sec       YDOT =        5102
673085  meter/sec
 ZDOT =      18848
740859                 ZDOT =        5741
877571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20911404
07                 X    =         6373795
96
 Y    =       -4216010
01  feet           Y    =        -1285039
85  meter
 Z    =        5429074
14                 Z    =         1654781
80
 XDOT =      -1828
781299                 XDOT =        -557
412540
 YDOT =      15308
043133  feet/sec       YDOT =        4665
891547  meter/sec
 ZDOT =      18836
926957                 ZDOT =        5741
495336


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
69263653  
00020000  00000-0  20000-3 0  9073
2 25544  51
6419 339
5206 0005893  10
3428 349
7858 15
77906146  7624


Satellite: ISS
Catalog Number: 25544
Epoch time:      08036
69263653   =   yrday
fracday
Element set:     907
Inclination:       51
6419  deg
RA of node:       339
5206  deg
Eccentricity:     
0005893     
Arg of perigee:    10
3428  deg
Mean anomaly:     349
7858  deg
Mean motion:   15
77906146  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             762
Checksum:              319


Coasting Arc #9 (Orbit 776)
---------------------------------------

Vector Time (GMT): 2008/037/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1694135
07                 A    =         6712355
10  meter
 Y    =       -4747627
93  meter          E    =           
0010452
 Z    =       -4439778
32                 I    =           51
49155
 XDOT =       6970
759754                 Wp   =           76
86198
 YDOT =       -524
523341  meter/sec      RA   =          334
12968  deg
 ZDOT =       3229
495141                 TA   =          225
50391
                                          MA   =          225
58939
                                          Ha   =            185
296  n
mi
                                          Hp   =            176
974

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5558185
91                 X    =         1768664
81
 Y    =      -15576207
12  feet           Y    =        -4728266
30  meter
 Z    =      -14566201
85                 Z    =        -4431367
59
 XDOT =      22869
946698                 XDOT =        6960
419176
 YDOT =      -1720
877103  feet/sec       YDOT =        -446
630246  meter/sec
 ZDOT =      10595
456500                 ZDOT =        3263
332877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4790114
49                 X    =         1460026
90
 Y    =      -15858407
62  feet           Y    =        -4833642
64  meter
 Z    =      -14534497
11                 Z    =        -4430114
72
 XDOT =      21526
716728                 XDOT =        6561
343259
 YDOT =      -3301
051688  feet/sec       YDOT =       -1006
160555  meter/sec
 ZDOT =      10724
847525                 ZDOT =        3268
933526


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
64259988  
00020000  00000-0  20000-3 0  9086
2 25544  51
6423 334
6138 0005818  12
7164 347
4147 15
77961925  7777


Satellite: ISS
Catalog Number: 25544
Epoch time:      08037
64259988   =   yrday
fracday
Element set:     908
Inclination:       51
6423  deg
RA of node:       334
6138  deg
Eccentricity:     
0005818     
Arg of perigee:    12
7164  deg
Mean anomaly:     347
4147  deg
Mean motion:   15
77961925  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             777
Checksum:              325


Coasting Arc #10 (Orbit 792)
---------------------------------------

Vector Time (GMT): 2008/038/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5502343
60                 A    =         6714263
91  meter
 Y    =        -271153
54  meter          E    =           
0010796
 Z    =       -3850897
23                 I    =           51
47279
 XDOT =       3150
508415                 Wp   =           46
32059
 YDOT =      -5701
120403  meter/sec      RA   =          329
00265  deg
 ZDOT =      -4099
968330                 TA   =          180
76262
                                          MA   =          180
76427
                                          Ha   =            185
276  n
mi
                                          Hp   =            176
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18052308
41                 X    =        -5480196
20
 Y    =        -889611
36  feet           Y    =         -332560
04  meter
 Z    =      -12634177
27                 Z    =        -3877572
99
 XDOT =      10336
313697                 XDOT =        3233
941350
 YDOT =     -18704
463265  feet/sec       YDOT =       -5665
423122  meter/sec
 ZDOT =     -13451
339664                 ZDOT =       -4084
460995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17998129
74                 X    =        -5485829
95
 Y    =         393613
41  feet           Y    =          119973
37  meter
 Z    =      -12736250
51                 Z    =        -3882009
15
 XDOT =       9082
076832                 XDOT =        2768
217018
 YDOT =     -18086
262133  feet/sec       YDOT =       -5512
692698  meter/sec
 ZDOT =     -13392
590124                 ZDOT =       -4082
061470


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
65586882  
00020000  00000-0  20000-3 0  9095
2 25544  51
6422 329
3795 0005743  15
4278 344
7061 15
77994063  7931


Satellite: ISS
Catalog Number: 25544
Epoch time:      08038
65586882   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:       329
3795  deg
Eccentricity:     
0005743     
Arg of perigee:    15
4278  deg
Mean anomaly:     344
7061  deg
Mean motion:   15
77994063  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             793
Checksum:              328


Coasting Arc #11 (Orbit 808)
---------------------------------------

Vector Time (GMT): 2008/039/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3617819
32                 A    =         6718094
77  meter
 Y    =        5088618
74  meter          E    =           
0015601
 Z    =        2469635
77                 I    =           51
46136
 XDOT =      -5434
030589                 Wp   =           83
12304
 YDOT =      -1268
536040  meter/sec      RA   =          323
77630  deg
 ZDOT =      -5316
171081                 TA   =           68
82696
                                          MA   =           68
66033
                                          Ha   =            185
354  n
mi
                                          Hp   =            176
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11869485
97                 X    =        -3686448
86
 Y    =       16694943
38  feet           Y    =         5047778
56  meter
 Z    =        8102479
56                 Z    =         2451894
09
 XDOT =     -17828
184348                 XDOT =       -5393
617492
 YDOT =      -4161
863648  feet/sec       YDOT =       -1329
076626  meter/sec
 ZDOT =     -17441
506171                 ZDOT =       -5342
470661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10392931
65                 X    =        -3167765
57
 Y    =       17682750
81  feet           Y    =         5389702
45  meter
 Z    =        8035129
26                 Z    =         2449107
40
 XDOT =     -16738
101674                 XDOT =       -5101
773390
 YDOT =      -1820
639369  feet/sec       YDOT =        -554
930880  meter/sec
 ZDOT =     -17542
241199                 ZDOT =       -5346
875117


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
66911191  
00020000  00000-0  20000-3 0  9104
2 25544  51
6421 324
1452 0005790  21
0310 339
1093 15
78038459  8095


Satellite: ISS
Catalog Number: 25544
Epoch time:      08039
66911191   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:       324
1452  deg
Eccentricity:     
0005790     
Arg of perigee:    21
0310  deg
Mean anomaly:     339
1093  deg
Mean motion:   15
78038459  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             809
Checksum:              271


Coasting Arc #12 (Orbit 824)
---------------------------------------

Vector Time (GMT): 2008/040/15:10:49
916
Vector Time (MET): N/A
Weight (LBS)     : 539961
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3845949
03                 A    =         6709098
11  meter
 Y    =        2036812
58  meter          E    =           
0006473
 Z    =        5100498
83                 I    =           51
40841
 XDOT =      -4902
337419                 Wp   =           64
72463
 YDOT =       5790
950615  meter/sec      RA   =          318
62825  deg
 ZDOT =       1385
357074                 TA   =           11
99751
                                          MA   =           11
98210
                                          Ha   =            185
213  n
mi
                                          Hp   =            176
445

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12617943
02                 X    =         3798110
53
 Y    =        6682455
97  feet           Y    =         2079552
89  meter
 Z    =       16733920
06                 Z    =         5119065
74
 XDOT =     -16083
784184                 XDOT =       -4973
458027
 YDOT =      18999
181807  feet/sec       YDOT =        5735
732283  meter/sec
 ZDOT =       4545
134758                 ZDOT =        1361
369110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13158088
50                 X    =         4010585
37
 Y    =        5323842
45  feet           Y    =         1622707
18  meter
 Z    =       16805153
77                 Z    =         5122210
87
 XDOT =     -13626
554151                 XDOT =       -4153
373705
 YDOT =      19633
299309  feet/sec       YDOT =        5984
229629  meter/sec
 ZDOT =       4453
970453                 ZDOT =        1357
570194


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   08040
68232682  
00020000  00000-0  20000-3 0  9110
2 25544  51
6417 318
9102 0005758  23
8678 336
2753 15
78079226  8250


Satellite: ISS
Catalog Number: 25544
Epoch time:      08040
68232682   =   yrday
fracday
Element set:     911
Inclination:       51
6417  deg
RA of node:       318
9102  deg
Eccentricity:     
0005758     
Arg of perigee:    23
8678  deg
Mean anomaly:     336
2753  deg
Mean motion:   15
78079226  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             825
Checksum:              302

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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