Date: October 23rd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14692 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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


There are no maneuvers



Coasting Arc #1 (Orbit 2584)
---------------------------------------

Vector Time (GMT): 2009/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6268645
13                 A    =         6726431
09  meter
 Y    =         -21404
02  meter          E    =           
0001780
 Z    =       -2439129
93                 I    =           51
75843
 XDOT =       2105
469855                 Wp   =          239
46988
 YDOT =       5105
662053  meter/sec      RA   =           17
66165  deg
 ZDOT =       5362
551579                 TA   =           93
03388
                                          MA   =           93
01352
                                          Ha   =            187
985  n
mi
                                          Hp   =            183
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20566421
02                 X    =         6280267
74
 Y    =         -70223
15  feet           Y    =           48760
68  meter
 Z    =       -8002394
77                 Z    =        -2408647
79
 XDOT =       6907
709498                 XDOT =        2022
169959
 YDOT =      16750
859753  feet/sec       YDOT =        5128
740850  meter/sec
 ZDOT =      17593
673161                 ZDOT =        5372
577938

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17941780
11                 X    =        -5468654
58
 Y    =       10148127
49  feet           Y    =         3093149
26  meter
 Z    =       -7882192
71                 Z    =        -2402492
34
 XDOT =     -13391
564961                 XDOT =       -4081
749000
 YDOT =      -9970
284170  feet/sec       YDOT =       -3038
942615  meter/sec
 ZDOT =      17633
386863                 ZDOT =        5374
656316


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   09294
50478377  
00016717  00000-0  10270-3 0  9002
2 25544  51
6446  18
1727 0007299 229
9262 130
1262 15
75135434 25856


Satellite: ISS
Catalog Number: 25544
Epoch time:      09294
50478377   =   yrday
fracday
Element set:     900
Inclination:       51
6446  deg
RA of node:        18
1727  deg
Eccentricity:     
0007299     
Arg of perigee:   229
9262  deg
Mean anomaly:     130
1262  deg
Mean motion:   15
75135434  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2585
Checksum:              322


Coasting Arc #2 (Orbit 2600)
---------------------------------------

Vector Time (GMT): 2009/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1727777
56                 A    =         6718511
75  meter
 Y    =       -4314295
71  meter          E    =           
0005951
 Z    =       -4856584
35                 I    =           51
70258
 XDOT =       7322
303281                 Wp   =           97
34679
 YDOT =       -278
274101  meter/sec      RA   =           12
56391  deg
 ZDOT =      -2360
983429                 TA   =          149
66797
                                          MA   =          149
63352
                                          Ha   =            187
754  n
mi
                                          Hp   =            183
929

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5668561
56                 X    =        -1655812
98
 Y    =      -14154513
48  feet           Y    =        -4333214
26  meter
 Z    =      -15933675
70                 Z    =        -4864803
37
 XDOT =      24023
304729                 XDOT =        7336
340275
 YDOT =       -912
972772  feet/sec       YDOT =        -196
313259  meter/sec
 ZDOT =      -7746
008626                 ZDOT =       -2325
376753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11952534
66                 X    =         3643132
56
 Y    =        9411760
04  feet           Y    =         2868704
46  meter
 Z    =      -15966231
60                 Z    =        -4866507
39
 XDOT =     -19637
104010                 XDOT =       -5985
389302
 YDOT =      12053
835667  feet/sec       YDOT =        3674
009111  meter/sec
 ZDOT =      -7605
604976                 ZDOT =       -2318
188397


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   09295
51985538  
00016717  00000-0  10270-3 0  9017
2 25544  51
6438  12
9513 0007285 233
3394 126
7100 15
75179006 26016


Satellite: ISS
Catalog Number: 25544
Epoch time:      09295
51985538   =   yrday
fracday
Element set:     901
Inclination:       51
6438  deg
RA of node:        12
9513  deg
Eccentricity:     
0007285     
Arg of perigee:   233
3394  deg
Mean anomaly:     126
7100  deg
Mean motion:   15
75179006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2601
Checksum:              307


Coasting Arc #3 (Orbit 2616)
---------------------------------------

Vector Time (GMT): 2009/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6491770
68                 A    =         6727501
42  meter
 Y    =         484645
26  meter          E    =           
0012101
 Z    =        1666079
84                 I    =           51
70363
 XDOT =      -1833
967058                 Wp   =          146
05566
 YDOT =      -4806
583264  meter/sec      RA   =            7
39010  deg
 ZDOT =      -5737
690198                 TA   =           15
52780
                                          MA   =           15
49071
                                          Ha   =            187
496  n
mi
                                          Hp   =            184
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21298460
25                 X    =        -6504801
26
 Y    =        1590043
49  feet           Y    =          411977
56  meter
 Z    =        5466141
22                 Z    =         1634510
55
 XDOT =      -6016
952291                 XDOT =       -1752
209488
 YDOT =     -15769
630130  feet/sec       YDOT =       -4826
634505  meter/sec
 ZDOT =     -18824
442906                 ZDOT =       -5746
401301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17406290
36                 X    =         5305437
30
 Y    =      -12430568
52  feet           Y    =        -3788837
29  meter
 Z    =        5341663
53                 Z    =         1628139
04
 XDOT =      12327
917387                 XDOT =        3757
549220
 YDOT =       9143
971691  feet/sec       YDOT =        2787
082571  meter/sec
 ZDOT =     -18858
953645                 ZDOT =       -5748
209071


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   09296
53490338  
00016717  00000-0  10270-3 0  9020
2 25544  51
6438   7
7298 0007041 237
6312 122
4171 15
75238903 26175


Satellite: ISS
Catalog Number: 25544
Epoch time:      09296
53490338   =   yrday
fracday
Element set:     902
Inclination:       51
6438  deg
RA of node:         7
7298  deg
Eccentricity:     
0007041     
Arg of perigee:   237
6312  deg
Mean anomaly:     122
4171  deg
Mean motion:   15
75238903  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2617
Checksum:              309


Coasting Arc #4 (Orbit 2632)
---------------------------------------

Vector Time (GMT): 2009/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1436093
52                 A    =         6717079
20  meter
 Y    =        4110909
66  meter          E    =           
0006503
 Z    =        5117892
87                 I    =           51
63931
 XDOT =      -7519
423476                 Wp   =          203
63157
 YDOT =        836
369588  meter/sec      RA   =            2
27447  deg
 ZDOT =       1432
935330                 TA   =          232
61031
                                          MA   =          232
66953
                                          Ha   =            187
135  n
mi
                                          Hp   =            184
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4711592
93                 X    =         1365155
66
 Y    =       13487236
40  feet           Y    =         4126572
18  meter
 Z    =       16790987
09                 Z    =         5124697
28
 XDOT =     -24670
024528                 XDOT =       -7535
178100
 YDOT =       2743
994711  feet/sec       YDOT =         752
194851  meter/sec
 ZDOT =       4701
231397                 ZDOT =        1396
367098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11099575
36                 X    =        -3383150
57
 Y    =       -8944143
31  feet           Y    =        -2726174
88  meter
 Z    =       16817955
54                 Z    =         5126112
85
 XDOT =      18769
308914                 XDOT =        5720
885357
 YDOT =     -14691
535497  feet/sec       YDOT =       -4477
980020  meter/sec
 ZDOT =       4557
050203                 ZDOT =        1388
988902


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   09297
54992676  
00016717  00000-0  10270-3 0  9035
2 25544  51
6439   2
5074 0007115 242
1035 117
9408 15
75284467 26332


Satellite: ISS
Catalog Number: 25544
Epoch time:      09297
54992676   =   yrday
fracday
Element set:     903
Inclination:       51
6439  deg
RA of node:         2
5074  deg
Eccentricity:     
0007115     
Arg of perigee:   242
1035  deg
Mean anomaly:     117
9408  deg
Mean motion:   15
75284467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2633
Checksum:              321


Coasting Arc #5 (Orbit 2647)
---------------------------------------

Vector Time (GMT): 2009/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6603475
78                 A    =         6728327
35  meter
 Y    =        -977342
50  meter          E    =           
0005482
 Z    =        -812805
48                 I    =           51
64624
 XDOT =       1422
695416                 Wp   =            2
50464
 YDOT =       4655
772657  meter/sec      RA   =          357
10994  deg
 ZDOT =       5967
041829                 TA   =          348
62898
                                          MA   =          348
64136
                                          Ha   =            186
864  n
mi
                                          Hp   =            184
310

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21664946
78                 X    =         6617862
32
 Y    =       -3206504
28  feet           Y    =         -903418
10  meter
 Z    =       -2666684
63                 Z    =         -780690
37
 XDOT =       4667
635878                 XDOT =        1341
540769
 YDOT =      15274
844674  feet/sec       YDOT =        4671
228284  meter/sec
 ZDOT =      19576
908888                 ZDOT =        5973
756285

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16375228
10                 X    =        -4991169
53
 Y    =       14565807
54  feet           Y    =         4439658
14  meter
 Z    =       -2540069
02                 Z    =         -774213
04
 XDOT =     -11119
154205                 XDOT =       -3389
118202
 YDOT =      -9085
974290  feet/sec       YDOT =       -2769
404964  meter/sec
 ZDOT =      19603
541097                 ZDOT =        5975
159326


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   09298
50149165  
00016717  00000-0  10270-3 0  9040
2 25544  51
6433 357
6117 0006880 247
6599 112
3836 15
75260131 26483


Satellite: ISS
Catalog Number: 25544
Epoch time:      09298
50149165   =   yrday
fracday
Element set:     904
Inclination:       51
6433  deg
RA of node:       357
6117  deg
Eccentricity:     
0006880     
Arg of perigee:   247
6599  deg
Mean anomaly:     112
3836  deg
Mean motion:   15
75260131  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2648
Checksum:              327


Coasting Arc #6 (Orbit 2663)
---------------------------------------

Vector Time (GMT): 2009/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1026543
36                 A    =         6716382
25  meter
 Y    =       -4064672
46  meter          E    =           
0008644
 Z    =       -5254543
41                 I    =           51
57662
 XDOT =       7559
994624                 Wp   =           99
89398
 YDOT =      -1389
686576  meter/sec      RA   =          351
97340  deg
 ZDOT =       -403
966782                 TA   =          166
27672
                                          MA   =          166
25321
                                          Ha   =            186
611  n
mi
                                          Hp   =            184
243

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3367924
42                 X    =         -955489
20
 Y    =      -13335539
56  feet           Y    =        -4075754
63  meter
 Z    =      -17239315
65                 Z    =        -5259357
80
 XDOT =      24803
131969                 XDOT =        7576
934887
 YDOT =      -4559
339161  feet/sec       YDOT =       -1305
051546  meter/sec
 ZDOT =      -1325
350335                 ZDOT =        -367
198630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10202206
44                 X    =         3109632
52
 Y    =        9188845
34  feet           Y    =         2800760
06  meter
 Z    =      -17258436
76                 Z    =        -5260371
52
 XDOT =     -17279
526037                 XDOT =       -5266
799536
 YDOT =      16980
559031  feet/sec       YDOT =        5175
674393  meter/sec
 ZDOT =      -1180
400526                 ZDOT =        -359
786080


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   09299
51647138  
00016717  00000-0  10270-3 0  9056
2 25544  51
6433 352
3891 0006872 250
6925 109
3496 15
75318738 26645


Satellite: ISS
Catalog Number: 25544
Epoch time:      09299
51647138   =   yrday
fracday
Element set:     905
Inclination:       51
6433  deg
RA of node:       352
3891  deg
Eccentricity:     
0006872     
Arg of perigee:   250
6925  deg
Mean anomaly:     109
3496  deg
Mean motion:   15
75318738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2664
Checksum:              345


Coasting Arc #7 (Orbit 2679)
---------------------------------------

Vector Time (GMT): 2009/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6564178
19                 A    =         6728214
55  meter
 Y    =        1439978
37  meter          E    =           
0010468
 Z    =        -119101
74                 I    =           51
58827
 XDOT =       -923
039471                 Wp   =          169
44808
 YDOT =      -4699
198707  meter/sec      RA   =          346
82187  deg
 ZDOT =      -6035
743658                 TA   =           11
84775
                                          MA   =           11
82314
                                          Ha   =            186
187  n
mi
                                          Hp   =            184
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21536017
69                 X    =        -6579213
83
 Y    =        4724338
49  feet           Y    =         1366489
79  meter
 Z    =        -390753
76                 Z    =         -151027
58
 XDOT =      -3028
344722                 XDOT =        -841
102600
 YDOT =     -15417
318592  feet/sec       YDOT =       -4709
062691  meter/sec
 ZDOT =     -19802
308590                 ZDOT =       -6040
028712

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14869447
26                 X    =         4532207
53
 Y    =      -16275895
68  feet           Y    =        -4960893
00  meter
 Z    =        -516602
80                 Z    =         -157460
53
 XDOT =      10082
589882                 XDOT =        3073
173396
 YDOT =       9833
043959  feet/sec       YDOT =        2997
111799  meter/sec
 ZDOT =     -19819
365207                 ZDOT =       -6040
942515


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   09300
53142725  
00016717  00000-0  10270-3 0  9064
2 25544  51
6439 347
1667 0006663 255
3870 104
6556 15
75390153 26807


Satellite: ISS
Catalog Number: 25544
Epoch time:      09300
53142725   =   yrday
fracday
Element set:     906
Inclination:       51
6439  deg
RA of node:       347
1667  deg
Eccentricity:     
0006663     
Arg of perigee:   255
3870  deg
Mean anomaly:     104
6556  deg
Mean motion:   15
75390153  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2680
Checksum:              315


Coasting Arc #8 (Orbit 2695)
---------------------------------------

Vector Time (GMT): 2009/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         582717
09                 A    =         6716210
56  meter
 Y    =        4182872
38  meter          E    =           
0003821
 Z    =        5225504
39                 I    =           51
51851
 XDOT =      -7433
773644                 Wp   =          272
40066
 YDOT =       1890
533307  meter/sec      RA   =          341
66268  deg
 ZDOT =       -684
621622                 TA   =          184
11877
                                          MA   =          184
12191
                                          Ha   =            185
884  n
mi
                                          Hp   =            184
092

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1911801
47                 X    =          510515
16
 Y    =       13723334
59  feet           Y    =         4188985
17  meter
 Z    =       17144043
27                 Z    =         5228159
74
 XDOT =     -24389
021141                 XDOT =       -7451
035588
 YDOT =       6202
537098  feet/sec       YDOT =        1807
307924  meter/sec
 ZDOT =      -2246
133930                 ZDOT =        -720
777543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9566640
14                 X    =        -2915911
91
 Y    =      -10005010
63  feet           Y    =        -3049527
24  meter
 Z    =       17154657
54                 Z    =         5228739
62
 XDOT =      15278
329265                 XDOT =        4656
834760
 YDOT =     -18702
963266  feet/sec       YDOT =       -5700
663204  meter/sec
 ZDOT =      -2388
643443                 ZDOT =        -728
058521


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   09301
54635970  
00016717  00000-0  10270-3 0  9076
2 25544  51
6432 341
9444 0006657 259
2400 100
8015 15
75425411 26961


Satellite: ISS
Catalog Number: 25544
Epoch time:      09301
54635970   =   yrday
fracday
Element set:     907
Inclination:       51
6432  deg
RA of node:       341
9444  deg
Eccentricity:     
0006657     
Arg of perigee:   259
2400  deg
Mean anomaly:     100
8015  deg
Mean motion:   15
75425411  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2696
Checksum:              301


Coasting Arc #9 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2009/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6376829
63                 A    =         6727622
43  meter
 Y    =       -1830569
38  meter          E    =           
0008687
 Z    =        1083772
49                 I    =           51
52877
 XDOT =        410
523374                 Wp   =           36
63165
 YDOT =       4934
231692  meter/sec      RA   =          336
52464  deg
 ZDOT =       5901
421133                 TA   =          335
25179
                                          MA   =          335
29344
                                          Ha   =            185
702  n
mi
                                          Hp   =            183
935

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20921357
07                 X    =         6391560
55
 Y    =       -6005805
07  feet           Y    =        -1759177
50  meter
 Z    =        3555684
01                 Z    =         1114787
66
 XDOT =       1346
861462                 XDOT =         326
648767
 YDOT =      16188
424186  feet/sec       YDOT =        4938
353723  meter/sec
 ZDOT =      19361
617889                 ZDOT =        5903
211525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13021945
00                 X    =        -3969088
84
 Y    =       17416016
46  feet           Y    =         5308401
82  meter
 Z    =        3677918
41                 Z    =         1121029
53
 XDOT =      -9496
733921                 XDOT =       -2894
604499
 YDOT =     -11202
650589  feet/sec       YDOT =       -3414
567900  meter/sec
 ZDOT =      19368
848594                 ZDOT =        5903
625051


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   09302
56127169  
00016717  00000-0  10270-3 0  9086
2 25544  51
6432 336
7212 0006428 265
1338  94
9092 15
75410216 27122


Satellite: ISS
Catalog Number: 25544
Epoch time:      09302
56127169   =   yrday
fracday
Element set:     908
Inclination:       51
6432  deg
RA of node:       336
7212  deg
Eccentricity:     
0006428     
Arg of perigee:   265
1338  deg
Mean anomaly:      94
9092  deg
Mean motion:   15
75410216  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              302


Coasting Arc #10 (Orbit 2726)
---------------------------------------

Vector Time (GMT): 2009/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -148463
25                 A    =         6717052
66  meter
 Y    =       -4471583
82  meter          E    =           
0007207
 Z    =       -5016541
13                 I    =           51
46730
 XDOT =       7133
619810                 Wp   =          117
82717
 YDOT =      -2261
819146  meter/sec      RA   =          331
34223  deg
 ZDOT =       1803
653627                 TA   =          169
60941
                                          MA   =          169
59451
                                          Ha   =            185
493  n
mi
                                          Hp   =            183
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -487084
16                 X    =          -74080
10
 Y    =      -14670550
59  feet           Y    =        -4472828
38  meter
 Z    =      -16458468
27                 Z    =        -5017081
47
 XDOT =      23404
264469                 XDOT =        7149
619621
 YDOT =      -7420
666491  feet/sec       YDOT =       -2181
957252  meter/sec
 ZDOT =       5917
498777                 ZDOT =        1838
348629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9373520
38                 X    =         2857049
01
 Y    =       11292659
47  feet           Y    =         3442002
61  meter
 Z    =      -16460754
57                 Z    =        -5017237
99
 XDOT =     -12963
840918                 XDOT =       -3951
378712
 YDOT =      19592
049255  feet/sec       YDOT =        5971
656613  meter/sec
 ZDOT =       6054
222006                 ZDOT =        1845
326867


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   09303
51272687  
00016717  00000-0  10270-3 0  9099
2 25544  51
6440 331
8247 0006555 268
0218  92
0195 15
75464420 27270


Satellite: ISS
Catalog Number: 25544
Epoch time:      09303
51272687   =   yrday
fracday
Element set:     909
Inclination:       51
6440  deg
RA of node:       331
8247  deg
Eccentricity:     
0006555     
Arg of perigee:   268
0218  deg
Mean anomaly:      92
0195  deg
Mean motion:   15
75464420  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2727
Checksum:              313


Coasting Arc #11 (Orbit 2742)
---------------------------------------

Vector Time (GMT): 2009/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6052921
60                 A    =         6725951
30  meter
 Y    =        2072670
05  meter          E    =           
0005186
 Z    =       -2063423
02                 I    =           51
47152
 XDOT =         58
079194                 Wp   =          205
08719
 YDOT =      -5348
346379  meter/sec      RA   =          326
21724  deg
 ZDOT =      -5542
235427                 TA   =          358
01437
                                          MA   =          358
01643
                                          Ha   =            185
423  n
mi
                                          Hp   =            183
755

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19858666
67                 X    =        -6065624
64
 Y    =        6800098
59  feet           Y    =         2004911
60  meter
 Z    =       -6769760
57                 Z    =        -2092859
96
 XDOT =        190
548537                 XDOT =         144
805022
 YDOT =     -17547
068174  feet/sec       YDOT =       -5347
212225  meter/sec
 ZDOT =     -18183
187096                 ZDOT =       -5541
742383

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11075079
60                 X    =         3375684
26
 Y    =      -17786698
78  feet           Y    =        -5421385
79  meter
 Z    =       -6885753
35                 Z    =        -2098777
62
 XDOT =       9552
340762                 XDOT =        2911
553464
 YDOT =      12986
995626  feet/sec       YDOT =        3958
436267  meter/sec
 ZDOT =     -18181
428851                 ZDOT =       -5541
699514


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   09304
52759140  
00016717  00000-0  10270-3 0  9107
2 25544  51
6433 326
6015 0006454 271
7340  88
3085 15
75513950 27439


Satellite: ISS
Catalog Number: 25544
Epoch time:      09304
52759140   =   yrday
fracday
Element set:     910
Inclination:       51
6433  deg
RA of node:       326
6015  deg
Eccentricity:     
0006454     
Arg of perigee:   271
7340  deg
Mean anomaly:      88
3085  deg
Mean motion:   15
75513950  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2743
Checksum:              300


Coasting Arc #12 (Orbit 2758)
---------------------------------------

Vector Time (GMT): 2009/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -216530
84                 A    =         6718491
99  meter
 Y    =        4894313
22  meter          E    =           
0004464
 Z    =        4598546
07                 I    =           51
42128
 XDOT =      -6701
382917                 Wp   =           14
98211
 YDOT =       2439
988165  meter/sec      RA   =          321
01493  deg
 ZDOT =      -2907
591858                 TA   =          103
91920
                                          MA   =          103
86954
                                          Ha   =            185
516  n
mi
                                          Hp   =            183
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -710403
03                 X    =         -293583
49
 Y    =       16057458
06  feet           Y    =         4891461
12  meter
 Z    =       15087093
39                 Z    =         4597306
85
 XDOT =     -21986
164426                 XDOT =       -6714
044177
 YDOT =       8005
210516  feet/sec       YDOT =        2364
978492  meter/sec
 ZDOT =      -9539
343367                 ZDOT =       -2940
179107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9741148
98                 X    =        -2969102
21
 Y    =      -12790581
37  feet           Y    =        -3898569
20  meter
 Z    =       15082375
92                 Z    =         4597108
18
 XDOT =      10671
981130                 XDOT =        3252
819848
 YDOT =     -19546
513747  feet/sec       YDOT =       -5957
777390  meter/sec
 ZDOT =      -9667
741448                 ZDOT =       -2946
727593


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   09305
54243209  
00016717  00000-0  10270-3 0  9115
2 25544  51
6421 321
3779 0006404 276
6309  83
4126 15
75573959 27593


Satellite: ISS
Catalog Number: 25544
Epoch time:      09305
54243209   =   yrday
fracday
Element set:     911
Inclination:       51
6421  deg
RA of node:       321
3779  deg
Eccentricity:     
0006404     
Arg of perigee:   276
6309  deg
Mean anomaly:      83
4126  deg
Mean motion:   15
75573959  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2759
Checksum:              322


Coasting Arc #13 (Orbit 2774)
---------------------------------------

Vector Time (GMT): 2009/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5627068
19                 A    =         6723674
52  meter
 Y    =       -2126032
74  meter          E    =           
0007349
 Z    =        2994821
79                 I    =           51
41612
 XDOT =       -409
905906                 Wp   =           68
99605
 YDOT =       5892
569754  meter/sec      RA   =          315
89827  deg
 ZDOT =       4946
195707                 TA   =          325
76476
                                          MA   =          325
81211
                                          Ha   =            185
581  n
mi
                                          Hp   =            183
679

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18461509
79                 X    =         5635874
80
 Y    =       -6975173
04  feet           Y    =        -2063058
32  meter
 Z    =        9825530
81                 Z    =         3022180
47
 XDOT =      -1344
835651                 XDOT =        -499
795786
 YDOT =      19332
577932  feet/sec       YDOT =        5887
483319  meter/sec
 ZDOT =      16227
676204                 ZDOT =        4943
985989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9275726
86                 X    =        -2827241
55
 Y    =       17358323
32  feet           Y    =         5290816
95  meter
 Z    =        9933324
80                 Z    =         3027677
40
 XDOT =     -10365
089506                 XDOT =       -3159
279281
 YDOT =     -14833
471869  feet/sec       YDOT =       -4521
242226  meter/sec
 ZDOT =      16219
163723                 ZDOT =        4943
601103


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   09306
55725049  
00016717  00000-0  10270-3 0  9125
2 25544  51
6417 316
1540 0006387 281
0743  78
9702 15
75585794 27755


Satellite: ISS
Catalog Number: 25544
Epoch time:      09306
55725049   =   yrday
fracday
Element set:     912
Inclination:       51
6417  deg
RA of node:       316
1540  deg
Eccentricity:     
0006387     
Arg of perigee:   281
0743  deg
Mean anomaly:      78
9702  deg
Mean motion:   15
75585794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2775
Checksum:              334


Coasting Arc #14 (Orbit 2789)
---------------------------------------

Vector Time (GMT): 2009/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         456518
78                 A    =         6720728
40  meter
 Y    =       -5400803
83  meter          E    =           
0000666
 Z    =       -3974556
11                 I    =           51
38586
 XDOT =       6181
215045                 Wp   =          134
95134
 YDOT =      -2371
886222  meter/sec      RA   =          310
68304  deg
 ZDOT =       3932
938430                 TA   =          175
86460
                                          MA   =          175
86405
                                          Ha   =            185
880  n
mi
                                          Hp   =            183
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1497765
03                 X    =          536185
96
 Y    =      -17719172
66  feet           Y    =        -5395253
19  meter
 Z    =      -13039882
27                 Z    =        -3972144
93
 XDOT =      20279
576920                 XDOT =        6188
172285
 YDOT =      -7781
778942  feet/sec       YDOT =       -2302
725467  meter/sec
 ZDOT =      12903
341306                 ZDOT =        3962
984681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10714380
24                 X    =         3265743
10
 Y    =       14200618
95  feet           Y    =         4328348
66  meter
 Z    =      -13030555
90                 Z    =        -3971713
44
 XDOT =      -8734
784914                 XDOT =       -2662
362442
 YDOT =      18539
389516  feet/sec       YDOT =        5650
805924  meter/sec
 ZDOT =      13021
725719                 ZDOT =        3969
021999


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   09307
50862017  
00016717  00000-0  10270-3 0  9139
2 25544  51
6420 311
2568 0006440 285
2160  74
8292 15
75608171 27905


Satellite: ISS
Catalog Number: 25544
Epoch time:      09307
50862017   =   yrday
fracday
Element set:     913
Inclination:       51
6420  deg
RA of node:       311
2568  deg
Eccentricity:     
0006440     
Arg of perigee:   285
2160  deg
Mean anomaly:      74
8292  deg
Mean motion:   15
75608171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2790
Checksum:              298


Coasting Arc #15 (Orbit 2805)
---------------------------------------

Vector Time (GMT): 2009/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5163744
63                 A    =         6720952
57  meter
 Y    =        1942927
68  meter          E    =           
0003894
 Z    =       -3841530
88                 I    =           51
36745
 XDOT =        611
381297                 Wp   =            3
19352
 YDOT =      -6487
949385  meter/sec      RA   =          305
56743  deg
 ZDOT =      -4099
582705                 TA   =          223
81790
                                          MA   =          223
84881
                                          Ha   =            186
037  n
mi
                                          Hp   =            183
471

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16941419
39                 X    =        -5166424
91
 Y    =        6374434
64  feet           Y    =         1885168
89  meter
 Z    =      -12603447
78                 Z    =        -3866623
59
 XDOT =       2005
844150                 XDOT =         703
800932
 YDOT =     -21285
923178  feet/sec       YDOT =       -6480
595567  meter/sec
 ZDOT =     -13450
074492                 ZDOT =       -4096
388411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7961817
70                 X    =         2426762
03
 Y    =      -16178767
51  feet           Y    =        -4931288
34  meter
 Z    =      -12702320
44                 Z    =        -3871667
27
 XDOT =      11841
437368                 XDOT =        3609
270110
 YDOT =      16386
880012  feet/sec       YDOT =        4994
721028  meter/sec
 ZDOT =     -13437
693975                 ZDOT =       -4095
809124


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   09308
52339211  
00016717  00000-0  10270-3 0  9148
2 25544  51
6409 306
0321 0006400 288
8889  71
1580 15
75651523 28061


Satellite: ISS
Catalog Number: 25544
Epoch time:      09308
52339211   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:       306
0321  deg
Eccentricity:     
0006400     
Arg of perigee:   288
8889  deg
Mean anomaly:      71
1580  deg
Mean motion:   15
75651523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2806
Checksum:              303

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