Date: November 30th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 ET - UTC (sec) : 66 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


332/19:17:48 984 -0 2 1 6 1 7
N/A -1 1 0 1 189 5
000/00:05:37 969 1 2 -0 2 179 4

Coasting Arc #1 (Orbit 3168)
---------------------------------------

Vector Time (GMT): 2009/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 759223
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6250682
37                 A    =         6723897
57  meter
 Y    =       -1055483
17  meter          E    =           
0015836
 Z    =        2233599
88                 I    =           51
61791
 XDOT =       2755
169451                 Wp   =           79
70495
 YDOT =       4677
275776  meter/sec      RA   =          186
62136  deg
 ZDOT =      -5464
571788                 TA   =           75
21130
                                          MA   =           75
03589
                                          Ha   =            188
734  n
mi
                                          Hp   =            179
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20507488
09                 X    =         6251169
72
 Y    =       -3462871
31  feet           Y    =         -985581
72  meter
 Z    =        7328083
58                 Z    =         2263967
55
 XDOT =       9039
269852                 XDOT =        2729
209087
 YDOT =      15345
392965  feet/sec       YDOT =        4707
940771  meter/sec
 ZDOT =     -17928
385132                 ZDOT =       -5451
249735

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5242586
40                 X    =        -1597940
34
 Y    =       20082140
78  feet           Y    =         6121036
51  meter
 Z    =        7447970
47                 Z    =         2270141
40
 XDOT =     -16281
625663                 XDOT =       -4962
639502
 YDOT =       2421
639829  feet/sec       YDOT =         738
115820  meter/sec
 ZDOT =     -17875
560702                 ZDOT =       -5448
470902


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   09331
53624735  
00016717  00000-0  10270-3 0  9008
2 25544  51
6459 187
4857 0007554  17
1100 343
0318 15
76123500 31694


Satellite: ISS
Catalog Number: 25544
Epoch time:      09331
53624735   =   yrday
fracday
Element set:     900
Inclination:       51
6459  deg
RA of node:       187
4857  deg
Eccentricity:     
0007554     
Arg of perigee:    17
1100  deg
Mean anomaly:     343
0318  deg
Mean motion:   15
76123500  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3169
Checksum:              296


Coasting Arc #2 (Orbit 3184)
---------------------------------------

Vector Time (GMT): 2009/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 759223
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1894820
99                 A    =         6715199
33  meter
 Y    =       -4027939
85  meter          E    =           
0008162
 Z    =        5020643
14                 I    =           51
61721
 XDOT =       7394
748450                 Wp   =           62
34410
 YDOT =      -1234
061158  meter/sec      RA   =          181
50289  deg
 ZDOT =       1802
270431                 TA   =           10
31580
                                          MA   =           10
29906
                                          Ha   =            188
883  n
mi
                                          Hp   =            179
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6216604
31                 X    =        -1874029
07
 Y    =      -13215025
75  feet           Y    =        -4049012
87  meter
 Z    =       16471926
31                 Z    =         5011488
14
 XDOT =      24260
985727                 XDOT =        7399
242996
 YDOT =      -4048
757079  feet/sec       YDOT =       -1151
343681  meter/sec
 ZDOT =       5912
960732                 ZDOT =        1838
205943

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14633449
38                 X    =         4460275
37
 Y    =        -583974
42  feet           Y    =         -177995
40  meter
 Z    =       16435588
35                 Z    =         5009567
33
 XDOT =      -5885
481640                 XDOT =       -1793
894804
 YDOT =      22789
785429  feet/sec       YDOT =        6946
326599  meter/sec
 ZDOT =       6054
841561                 ZDOT =        1845
515708


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   09332
55071384  
00016717  00000-0  10270-3 0  9018
2 25544  51
6448 182
2594 0007509  21
0490 339
0982 15
76111411 31857


Satellite: ISS
Catalog Number: 25544
Epoch time:      09332
55071384   =   yrday
fracday
Element set:     901
Inclination:       51
6448  deg
RA of node:       182
2594  deg
Eccentricity:     
0007509     
Arg of perigee:    21
0490  deg
Mean anomaly:     339
0982  deg
Mean motion:   15
76111411  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3185
Checksum:              299


Coasting Arc #3 (Orbit 3189)
---------------------------------------

Vector Time (GMT): 2009/332/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6615104
59                 A    =         6726651
79  meter
 Y    =        -708745
22  meter          E    =           
0020945
 Z    =         908237
85                 I    =           51
66358
 XDOT =       1331
435008                 Wp   =           41
75275
 YDOT =      -4712
660254  meter/sec      RA   =          179
91792  deg
 ZDOT =       5957
051899                 TA   =          328
17718
                                          MA   =          328
30357
                                          Ha   =            189
504  n
mi
                                          Hp   =            179
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21703099
04                 X    =        -6611099
80
 Y    =       -2325279
59  feet           Y    =         -782696
88  meter
 Z    =        2979782
97                 Z    =          876110
46
 XDOT =       4368
225093                 XDOT =        1355
094755
 YDOT =     -15461
483773  feet/sec       YDOT =       -4697
639422  meter/sec
 ZDOT =      19544
133526                 ZDOT =        5963
577386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21581262
71                 X    =        -6577968
87
 Y    =       -3379476
88  feet           Y    =        -1030064
55  meter
 Z    =        2852853
98                 Z    =          869549
89
 XDOT =       4754
786148                 XDOT =        1449
258818
 YDOT =     -13661
971574  feet/sec       YDOT =       -4164
168936  meter/sec
 ZDOT =      19569
700848                 ZDOT =        5964
844819


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   09332
86774207  
00016717  00000-0  10270-3 0  9027
2 25544  51
6460 180
6241 0008257  19
9019 340
2465 15
75831388 31903


Satellite: ISS
Catalog Number: 25544
Epoch time:      09332
86774207   =   yrday
fracday
Element set:     902
Inclination:       51
6460  deg
RA of node:       180
6241  deg
Eccentricity:     
0008257     
Arg of perigee:    19
9019  deg
Mean anomaly:     340
2465  deg
Mean motion:   15
75831388  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3190
Checksum:              314


Coasting Arc #4 (Orbit 3204)
---------------------------------------

Vector Time (GMT): 2009/333/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1576264
10                 A    =         6715655
45  meter
 Y    =        4154739
23  meter          E    =           
0017090
 Z    =       -5048203
46                 I    =           51
65684
 XDOT =      -7456
657827                 Wp   =           74
88840
 YDOT =       -708
290052  meter/sec      RA   =          174
74795  deg
 ZDOT =       1754
640177                 TA   =          211
96598
                                          MA   =          212
06977
                                          Ha   =            189
466  n
mi
                                          Hp   =            179
117

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5171470
14                 X    =        -1598081
98
 Y    =       13631034
21  feet           Y    =         4136990
95  meter
 Z    =      -16562347
30                 Z    =        -5055913
82
 XDOT =     -24464
100481                 XDOT =       -7456
707378
 YDOT =      -2323
786259  feet/sec       YDOT =        -791
675224  meter/sec
 ZDOT =       5756
693494                 ZDOT =        1718
414474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5501051
33                 X    =        -1676720
45
 Y    =       13464163
78  feet           Y    =         4103877
12  meter
 Z    =      -16592627
07                 Z    =        -5057432
73
 XDOT =     -23430
248221                 XDOT =       -7141
539658
 YDOT =      -2692
468131  feet/sec       YDOT =        -820
664286  meter/sec
 ZDOT =       5613
563638                 ZDOT =        1711
014197


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   09333
81896110  
00016717  00000-0  10270-3 0  9032
2 25544  51
6454 175
7272 0008267  23
2481 336
9056 15
75898675 32054


Satellite: ISS
Catalog Number: 25544
Epoch time:      09333
81896110   =   yrday
fracday
Element set:     903
Inclination:       51
6454  deg
RA of node:       175
7272  deg
Eccentricity:     
0008267     
Arg of perigee:    23
2481  deg
Mean anomaly:     336
9056  deg
Mean motion:   15
75898675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3205
Checksum:              330


Coasting Arc #5 (Orbit 3220)
---------------------------------------

Vector Time (GMT): 2009/334/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6347607
40                 A    =         6724780
83  meter
 Y    =         570229
42  meter          E    =           
0008306
 Z    =       -2157591
61                 I    =           51
71641
 XDOT =      -2304
709442                 Wp   =           72
56414
 YDOT =       4846
284143  meter/sec      RA   =          169
63514  deg
 ZDOT =      -5514
528116                 TA   =          131
54745
                                          MA   =          131
47618
                                          Ha   =            189
525  n
mi
                                          Hp   =            179
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20825483
59                 X    =         6351240
71
 Y    =        1870831
42  feet           Y    =          641232
67  meter
 Z    =       -7078712
64                 Z    =        -2126745
14
 XDOT =      -7561
382685                 XDOT =       -2331
940785
 YDOT =      15899
882359  feet/sec       YDOT =        4820
359896  meter/sec
 ZDOT =     -18092
283844                 ZDOT =       -5525
790314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20837691
68                 X    =         6351328
42
 Y    =        2168444
20  feet           Y    =          660941
79  meter
 Z    =       -6956824
32                 Z    =        -2120440
05
 XDOT =      -7523
582396                 XDOT =       -2293
187914
 YDOT =      14271
864765  feet/sec       YDOT =        4350
064381  meter/sec
 ZDOT =     -18136
576240                 ZDOT =       -5528
028438


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   09334
83357172  
00016717  00000-0  10270-3 0  9046
2 25544  51
6444 170
5024 0008226  26
8262 333
3327 15
75910420 32215


Satellite: ISS
Catalog Number: 25544
Epoch time:      09334
83357172   =   yrday
fracday
Element set:     904
Inclination:       51
6444  deg
RA of node:       170
5024  deg
Eccentricity:     
0008226     
Arg of perigee:    26
8262  deg
Mean anomaly:     333
3327  deg
Mean motion:   15
75910420  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3221
Checksum:              285


Coasting Arc #6 (Orbit 3236)
---------------------------------------

Vector Time (GMT): 2009/335/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2414983
36                 A    =         6717651
10  meter
 Y    =       -4358423
55  meter          E    =           
0016253
 Z    =        4500508
21                 I    =           51
72290
 XDOT =       7009
983400                 Wp   =           48
84642
 YDOT =        622
115636  meter/sec      RA   =          164
44807  deg
 ZDOT =      -3141
282880                 TA   =           72
52225
                                          MA   =           72
34467
                                          Ha   =            189
471  n
mi
                                          Hp   =            178
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7923173
74                 X    =         2441677
30
 Y    =      -14299289
87  feet           Y    =        -4331269
17  meter
 Z    =       14765446
90                 Z    =         4512304
73
 XDOT =      22998
633202                 XDOT =        7017
765968
 YDOT =       2041
061798  feet/sec       YDOT =         700
549366  meter/sec
 ZDOT =     -10306
046194                 ZDOT =       -3107
208502

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7794850
84                 X    =         2375870
54
 Y    =      -14321774
36  feet           Y    =        -4365276
83  meter
 Z    =       14811882
88                 Z    =         4514661
90
 XDOT =      22020
030694                 XDOT =        6711
705356
 YDOT =       1405
023569  feet/sec       YDOT =         428
251184  meter/sec
 ZDOT =     -10171
385432                 ZDOT =       -3100
238280


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   09335
84815639  
00016717  00000-0  10270-3 0  9056
2 25544  51
6447 165
2771 0008378  29
6853 330
4785 15
75980786 32378


Satellite: ISS
Catalog Number: 25544
Epoch time:      09335
84815639   =   yrday
fracday
Element set:     905
Inclination:       51
6447  deg
RA of node:       165
2771  deg
Eccentricity:     
0008378     
Arg of perigee:    29
6853  deg
Mean anomaly:     330
4785  deg
Mean motion:   15
75980786  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3237
Checksum:              358


Coasting Arc #7 (Orbit 3252)
---------------------------------------

Vector Time (GMT): 2009/336/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5828568
86                 A    =         6721888
68  meter
 Y    =        -563622
22  meter          E    =           
0018969
 Z    =        3277756
39                 I    =           51
76534
 XDOT =       3176
292990                 Wp   =           67
21303
 YDOT =      -5189
032463  meter/sec      RA   =          159
35384  deg
 ZDOT =       4741
481304                 TA   =          331
23688
                                          MA   =          331
34134
                                          Ha   =            189
643  n
mi
                                          Hp   =            178
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19122601
25                 X    =        -5837756
21
 Y    =       -1849154
27  feet           Y    =         -628852
61  meter
 Z    =       10753793
94                 Z    =         3249418
23
 XDOT =      10420
908761                 XDOT =        3211
047869
 YDOT =     -17024
384721  feet/sec       YDOT =       -5153
319715  meter/sec
 ZDOT =      15556
041023                 ZDOT =        4756
995639

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19218505
97                 X    =        -5857800
62
 Y    =       -1462463
09  feet           Y    =         -445758
75  meter
 Z    =       10641783
87                 Z    =         3243615
73
 XDOT =       9878
417325                 XDOT =        3010
941601
 YDOT =     -15826
989237  feet/sec       YDOT =       -4824
066320  meter/sec
 ZDOT =      15617
149083                 ZDOT =        4760
107041


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   09336
86271731  
00016717  00000-0  10270-3 0  9069
2 25544  51
6442 160
0522 0008338  33
7695 326
3999 15
76003595 32530


Satellite: ISS
Catalog Number: 25544
Epoch time:      09336
86271731   =   yrday
fracday
Element set:     906
Inclination:       51
6442  deg
RA of node:       160
0522  deg
Eccentricity:     
0008338     
Arg of perigee:    33
7695  deg
Mean anomaly:     326
3999  deg
Mean motion:   15
76003595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3253
Checksum:              323


Coasting Arc #8 (Orbit 3267)
---------------------------------------

Vector Time (GMT): 2009/337/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3077069
90                 A    =         6720387
20  meter
 Y    =        4709595
70  meter          E    =           
0012163
 Z    =       -3680771
15                 I    =           51
78813
 XDOT =      -6312
725787                 Wp   =           63
43922
 YDOT =       -742
511261  meter/sec      RA   =          154
16215  deg
 ZDOT =       4343
598565                 TA   =          252
38937
                                          MA   =          252
52225
                                          Ha   =            189
555  n
mi
                                          Hp   =            178
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10095373
70                 X    =        -3111623
98
 Y    =       15451429
45  feet           Y    =         4674993
48  meter
 Z    =      -12076020
84                 Z    =        -3695802
92
 XDOT =     -20711
042609                 XDOT =       -6325
054409
 YDOT =      -2436
060569  feet/sec       YDOT =        -813
173524  meter/sec
 ZDOT =      14250
651461                 ZDOT =        4312
900866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9440963
08                 X    =        -2877605
55
 Y    =       15814466
41  feet           Y    =         4820249
36  meter
 Z    =      -12135254
01                 Z    =        -3698825
42
 XDOT =     -19717
267898                 XDOT =       -6009
823255
 YDOT =       -969
589120  feet/sec       YDOT =        -295
530764  meter/sec
 ZDOT =      14129
290635                 ZDOT =        4306
607786


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   09337
81384634  
00016717  00000-0  10270-3 0  9073
2 25544  51
6436 155
1541 0008457  37
3697 322
8054 15
76048117 32681


Satellite: ISS
Catalog Number: 25544
Epoch time:      09337
81384634   =   yrday
fracday
Element set:     907
Inclination:       51
6436  deg
RA of node:       155
1541  deg
Eccentricity:     
0008457     
Arg of perigee:    37
3697  deg
Mean anomaly:     322
8054  deg
Mean motion:   15
76048117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3268
Checksum:              328


Coasting Arc #9 (Orbit 3283)
---------------------------------------

Vector Time (GMT): 2009/338/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5147135
06                 A    =         6718586
86  meter
 Y    =         820078
66  meter          E    =           
0016292
 Z    =       -4256878
11                 I    =           51
80836
 XDOT =      -3858
719373                 Wp   =           55
33405
 YDOT =       5601
568621  meter/sec      RA   =          149
07303  deg
 ZDOT =      -3587
179270                 TA   =          178
26144
                                          MA   =          178
25577
                                          Ha   =            189
655  n
mi
                                          Hp   =            178
399

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16886926
06                 X    =         5158261
54
 Y    =        2690546
77  feet           Y    =          877699
81  meter
 Z    =      -13966135
54                 Z    =        -4231846
00
 XDOT =     -12659
840461                 XDOT =       -3903
644315
 YDOT =      18377
849806  feet/sec       YDOT =        5558
167498  meter/sec
 ZDOT =     -11768
960859                 ZDOT =       -3606
033340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17089758
49                 X    =         5208958
39
 Y    =        1761411
14  feet           Y    =          536878
11  meter
 Z    =      -13867149
71                 Z    =        -4226707
23
 XDOT =     -11441
995610                 XDOT =       -3487
520262
 YDOT =      17790
259375  feet/sec       YDOT =        5422
471058  meter/sec
 ZDOT =     -11843
281517                 ZDOT =       -3609
832206


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   09338
82835998  
00016717  00000-0  10270-3 0  9080
2 25544  51
6436 149
9282 0008514  40
7670 319
4130 15
76049653 32848


Satellite: ISS
Catalog Number: 25544
Epoch time:      09338
82835998   =   yrday
fracday
Element set:     908
Inclination:       51
6436  deg
RA of node:       149
9282  deg
Eccentricity:     
0008514     
Arg of perigee:    40
7670  deg
Mean anomaly:     319
4130  deg
Mean motion:   15
76049653  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3284
Checksum:              342


Coasting Arc #10 (Orbit 3299)
---------------------------------------

Vector Time (GMT): 2009/339/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3601341
47                 A    =         6723286
47  meter
 Y    =       -5080135
33  meter          E    =           
0019610
 Z    =        2522828
46                 I    =           51
85136
 XDOT =       5444
251936                 Wp   =           81
32863
 YDOT =       1199
433397  meter/sec      RA   =          143
88845  deg
 ZDOT =      -5318
596034                 TA   =           70
15099
                                          MA   =           69
93973
                                          Ha   =            189
603  n
mi
                                          Hp   =            178
007

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11815424
78                 X    =         3645625
30
 Y    =      -16667110
66  feet           Y    =        -5039615
73  meter
 Z    =        8276996
26                 Z    =         2540430
75
 XDOT =      17861
718949                 XDOT =        5456
271882
 YDOT =       3935
148941  feet/sec       YDOT =        1260
382123  meter/sec
 ZDOT =     -17449
462053                 ZDOT =       -5292
118426

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10542022
70                 X    =         3213208
52
 Y    =      -17467366
59  feet           Y    =        -5324053
34  meter
 Z    =        8346398
60                 Z    =         2543982
29
 XDOT =      16925
590307                 XDOT =        5158
919926
 YDOT =       1868
444215  feet/sec       YDOT =         569
501797  meter/sec
 ZDOT =     -17344
733030                 ZDOT =       -5286
674628


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   09339
84284714  
00016717  00000-0  10270-3 0  9098
2 25544  51
6445 144
7025 0008693  43
2019 316
9826 15
76136700 33002


Satellite: ISS
Catalog Number: 25544
Epoch time:      09339
84284714   =   yrday
fracday
Element set:     909
Inclination:       51
6445  deg
RA of node:       144
7025  deg
Eccentricity:     
0008693     
Arg of perigee:    43
2019  deg
Mean anomaly:     316
9826  deg
Mean motion:   15
76136700  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3300
Checksum:              314


Coasting Arc #11 (Orbit 3315)
---------------------------------------

Vector Time (GMT): 2009/340/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4348154
66                 A    =         6715529
15  meter
 Y    =       -1338829
86  meter          E    =           
0011994
 Z    =        4928774
85                 I    =           51
84865
 XDOT =       4305
187147                 Wp   =           78
75752
 YDOT =      -6024
786146  meter/sec      RA   =          138
79157  deg
 ZDOT =       2159
379299                 TA   =          350
37611
                                          MA   =          350
39906
                                          Ha   =            189
787  n
mi
                                          Hp   =            177
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14265599
29                 X    =        -4356803
61
 Y    =       -4392486
41  feet           Y    =        -1387502
35  meter
 Z    =       16170521
15                 Z    =         4907630
33
 XDOT =      14124
629747                 XDOT =        4361
747496
 YDOT =     -19766
358748  feet/sec       YDOT =       -5976
326977  meter/sec
 ZDOT =       7084
577752                 ZDOT =        2180
430709

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14693328
00                 X    =        -4478526
38
 Y    =       -3099351
13  feet           Y    =         -944682
22  meter
 Z    =       16086862
63                 Z    =         4903275
73
 XDOT =      12045
715329                 XDOT =        3671
534032
 YDOT =     -19867
403804  feet/sec       YDOT =       -6055
584679  meter/sec
 ZDOT =       7167
591168                 ZDOT =        2184
681788


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   09340
85731098  
00016717  00000-0  10270-3 0  9105
2 25544  51
6443 139
4771 0008691  47
6316 312
5583 15
76154603 33166


Satellite: ISS
Catalog Number: 25544
Epoch time:      09340
85731098   =   yrday
fracday
Element set:     910
Inclination:       51
6443  deg
RA of node:       139
4771  deg
Eccentricity:     
0008691     
Arg of perigee:    47
6316  deg
Mean anomaly:     312
5583  deg
Mean motion:   15
76154603  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3316
Checksum:              315


Coasting Arc #12 (Orbit 3330)
---------------------------------------

Vector Time (GMT): 2009/341/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3838091
19                 A    =         6725393
40  meter
 Y    =        5383747
42  meter          E    =           
0017976
 Z    =       -1194482
35                 I    =           51
90401
 XDOT =      -4547
024662                 Wp   =           44
06081
 YDOT =      -1944
889623  meter/sec      RA   =          133
62765  deg
 ZDOT =       5909
825898                 TA   =          302
88314
                                          MA   =          303
05599
                                          Ha   =            189
733  n
mi
                                          Hp   =            177
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12592162
70                 X    =        -3892205
34
 Y    =       17663213
31  feet           Y    =         5340525
14  meter
 Z    =       -3918905
36                 Z    =        -1213258
88
 XDOT =     -14918
059915                 XDOT =       -4553
647578
 YDOT =      -6380
871465  feet/sec       YDOT =       -1995
774634  meter/sec
 ZDOT =      19389
192580                 ZDOT =        5887
720137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10627125
68                 X    =        -3239147
91
 Y    =       18895237
23  feet           Y    =         5759268
31  meter
 Z    =       -3992955
66                 Z    =        -1217052
89
 XDOT =     -14244
752572                 XDOT =       -4341
800584
 YDOT =      -3977
213843  feet/sec       YDOT =       -1212
254779  meter/sec
 ZDOT =      19301
702863                 ZDOT =        5883
159033


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   09341
80834862  
00016717  00000-0  10270-3 0  9115
2 25544  51
6444 134
5780 0008869  50
2921 309
9023 15
76157665 33319


Satellite: ISS
Catalog Number: 25544
Epoch time:      09341
80834862   =   yrday
fracday
Element set:     911
Inclination:       51
6444  deg
RA of node:       134
5780  deg
Eccentricity:     
0008869     
Arg of perigee:    50
2921  deg
Mean anomaly:     309
9023  deg
Mean motion:   15
76157665  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3331
Checksum:              318


Coasting Arc #13 (Orbit 3346)
---------------------------------------

Vector Time (GMT): 2009/342/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3588832
23                 A    =         6713938
92  meter
 Y    =        2136918
53  meter          E    =           
0022934
 Z    =       -5275814
57                 I    =           51
88619
 XDOT =      -4461
412275                 Wp   =           74
50959
 YDOT =       6240
591538  meter/sec      RA   =          128
50934  deg
 ZDOT =       -502
965876                 TA   =          190
69612
                                          MA   =          190
74498
                                          Ha   =            189
730  n
mi
                                          Hp   =            177
684

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11774383
96                 X    =         3590299
23
 Y    =        7010887
55  feet           Y    =         2177059
52  meter
 Z    =      -17309102
91                 Z    =        -5258376
20
 XDOT =     -14637
179381                 XDOT =       -4528
420745
 YDOT =      20474
381687  feet/sec       YDOT =        6190
326761  meter/sec
 ZDOT =      -1650
150513                 ZDOT =        -524
801918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12647740
98                 X    =         3855031
45
 Y    =        5496243
77  feet           Y    =         1675255
10  meter
 Z    =      -17240059
69                 Z    =        -5254770
19
 XDOT =     -11596
511674                 XDOT =       -3534
616758
 YDOT =      21196
038456  feet/sec       YDOT =        6460
552521  meter/sec
 ZDOT =      -1736
277295                 ZDOT =        -529
217320


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   09342
82276382  
00016717  00000-0  10270-3 0  9126
2 25544  51
6451 129
3516 0008841  54
4098 305
7889 15
76199297 33475


Satellite: ISS
Catalog Number: 25544
Epoch time:      09342
82276382   =   yrday
fracday
Element set:     912
Inclination:       51
6451  deg
RA of node:       129
3516  deg
Eccentricity:     
0008841     
Arg of perigee:    54
4098  deg
Mean anomaly:     305
7889  deg
Mean motion:   15
76199297  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3347
Checksum:              345


Coasting Arc #14 (Orbit 3362)
---------------------------------------

Vector Time (GMT): 2009/343/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3914197
94                 A    =         6725689
01  meter
 Y    =       -5456355
35  meter          E    =           
0015936
 Z    =        -341165
97                 I    =           51
94393
 XDOT =       3689
887870                 Wp   =          103
89042
 YDOT =       3010
495702  meter/sec      RA   =          123
37485  deg
 ZDOT =      -6051
510466                 TA   =           79
80425
                                          MA   =           79
62456
                                          Ha   =            189
736  n
mi
                                          Hp   =            177
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12841856
77                 X    =         3976578
29
 Y    =      -17901428
31  feet           Y    =        -5412235
67  meter
 Z    =       -1119310
91                 Z    =         -321999
41
 XDOT =      12105
931331                 XDOT =        3685
347202
 YDOT =       9876
954404  feet/sec       YDOT =        3051
733208  meter/sec
 ZDOT =     -19854
036963                 ZDOT =       -6033
595629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10213925
62                 X    =         3113204
53
 Y    =      -19524694
27  feet           Y    =        -5951126
81  meter
 Z    =       -1043702
39                 Z    =         -318120
49
 XDOT =      12061
135758                 XDOT =        3676
234179
 YDOT =       7322
281219  feet/sec       YDOT =        2231
831316  meter/sec
 ZDOT =     -19783
076238                 ZDOT =       -6029
881637


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   09343
83715321  
00016717  00000-0  10270-3 0  9130
2 25544  51
6447 124
1250 0009008  58
0409 302
1630 15
76265311 33634


Satellite: ISS
Catalog Number: 25544
Epoch time:      09343
83715321   =   yrday
fracday
Element set:     913
Inclination:       51
6447  deg
RA of node:       124
1250  deg
Eccentricity:     
0009008     
Arg of perigee:    58
0409  deg
Mean anomaly:     302
1630  deg
Mean motion:   15
76265311  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3363
Checksum:              278


Coasting Arc #15 (Orbit 3378)
---------------------------------------

Vector Time (GMT): 2009/344/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2905438
25                 A    =         6714013
77  meter
 Y    =       -3142998
65  meter          E    =           
0013143
 Z    =        5164339
88                 I    =           51
91959
 XDOT =       4436
922848                 Wp   =           59
62916
 YDOT =      -6181
984104  meter/sec      RA   =          118
22916  deg
 ZDOT =      -1257
272890                 TA   =           42
37384
                                          MA   =           42
27241
                                          Ha   =            189
806  n
mi
                                          Hp   =            177
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9532277
73                 X    =        -2895164
55
 Y    =      -10311675
36  feet           Y    =        -3175431
92  meter
 Z    =       16943372
31                 Z    =         5150249
77
 XDOT =      14556
833492                 XDOT =        4511
828808
 YDOT =     -20282
100080  feet/sec       YDOT =       -6131
948899  meter/sec
 ZDOT =      -4124
911055                 ZDOT =       -1235
536506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11131489
83                 X    =        -3392878
10
 Y    =       -8670289
44  feet           Y    =        -2642704
22  meter
 Z    =       16887535
29                 Z    =         5147320
76
 XDOT =      10581
358799                 XDOT =        3225
198162
 YDOT =     -21509
125034  feet/sec       YDOT =       -6555
981310  meter/sec
 ZDOT =      -4039
150906                 ZDOT =       -1231
133196


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   09344
85151738  
00016717  00000-0  10270-3 0  9140
2 25544  51
6437 118
8986 0009067  61
5506 298
6571 15
76310226 33797


Satellite: ISS
Catalog Number: 25544
Epoch time:      09344
85151738   =   yrday
fracday
Element set:     914
Inclination:       51
6437  deg
RA of node:       118
8986  deg
Eccentricity:     
0009067     
Arg of perigee:    61
5506  deg
Mean anomaly:     298
6571  deg
Mean motion:   15
76310226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3379
Checksum:              341


Coasting Arc #16 (Orbit 3394)
---------------------------------------

Vector Time (GMT): 2009/345/19:20:37
969
Vector Time (MET): N/A
Weight (LBS)     : 759075
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3791039
40                 A    =         6724165
92  meter
 Y    =        5228531
02  meter          E    =           
0023319
 Z    =        1831940
94                 I    =           51
96716
 XDOT =      -3042
476392                 Wp   =           65
40469
 YDOT =      -4217
613147  meter/sec      RA   =          113
12522  deg
 ZDOT =       5694
697370                 TA   =          314
86618
                                          MA   =          315
05534
                                          Ha   =            189
798  n
mi
                                          Hp   =            177
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12437793
29                 X    =        -3858123
38
 Y    =       17153973
15  feet           Y    =         5185762
12  meter
 Z    =        6010304
93                 Z    =         1813361
28
 XDOT =      -9981
877925                 XDOT =       -3022
752466
 YDOT =     -13837
313473  feet/sec       YDOT =       -4251
526155  meter/sec
 ZDOT =      18683
390320                 ZDOT =        5679
964283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9296658
31                 X    =        -2833621
45
 Y    =       19063200
97  feet           Y    =         5810463
65  meter
 Z    =        5936983
68                 Z    =         1809592
63
 XDOT =     -10955
275317                 XDOT =       -3339
167917
 YDOT =     -11191
359488  feet/sec       YDOT =       -3411
126372  meter/sec
 ZDOT =      18624
977446                 ZDOT =        5676
893126


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   09345
86585772  
00016717  00000-0  10270-3 0  9152
2 25544  51
6439 113
6722 0009174  64
4830 295
7282 15
76319363 33957


Satellite: ISS
Catalog Number: 25544
Epoch time:      09345
86585772   =   yrday
fracday
Element set:     915
Inclination:       51
6439  deg
RA of node:       113
6722  deg
Eccentricity:     
0009174     
Arg of perigee:    64
4830  deg
Mean anomaly:     295
7282  deg
Mean motion:   15
76319363  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3395
Checksum:              343

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics 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:

<[program_url]/list/[list]>

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

<mailto:[list_owner_email]>

The following physical address is associated with this mailing list:

[physical_address]

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