Date: January 21st 2009

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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 2256)
---------------------------------------

Vector Time (GMT): 2009/019/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -859769
88                 A    =         6730277
74  meter
 Y    =       -4099237
52  meter          E    =           
0007386
 Z    =       -5274263
00                 I    =           51
54805
 XDOT =       7514
656335                 Wp   =           73
91166
 YDOT =      -1633
687561  meter/sec      RA   =          347
45781  deg
 ZDOT =         46
809239                 TA   =          196
52163
                                          MA   =          196
54571
                                          Ha   =            194
186  n
mi
                                          Hp   =            192
517

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2820767
31                 X    =         -788246
44
 Y    =      -13448942
00  feet           Y    =        -4108451
62  meter
 Z    =      -17304012
48                 Z    =        -5278266
34
 XDOT =      24654
384302                 XDOT =        7532
138605
 YDOT =      -5359
867325  feet/sec       YDOT =       -1549
556570  meter/sec
 ZDOT =        153
573620                 ZDOT =          83
357444

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9320903
81                 X    =         2841011
48
 Y    =      -10069934
11  feet           Y    =        -3069315
92  meter
 Z    =      -17319838
23                 Z    =        -5279086
69
 XDOT =      18026
440118                 XDOT =        5494
458948
 YDOT =      16188
538540  feet/sec       YDOT =        4934
266547  meter/sec
 ZDOT =        295
751854                 ZDOT =          90
145165


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   09019
53659256  
00010596  00000-0  82463-4 0  9000
2 25544  51
6402 347
8788 0008205 285
4453  74
5802 15
70436401 22574


Satellite: ISS
Catalog Number: 25544
Epoch time:      09019
53659256   =   yrday
fracday
Element set:     900
Inclination:       51
6402  deg
RA of node:       347
8788  deg
Eccentricity:     
0008205     
Arg of perigee:   285
4453  deg
Mean anomaly:      74
5802  deg
Mean motion:   15
70436401  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2257
Checksum:              314


Coasting Arc #2 (Orbit 2272)
---------------------------------------

Vector Time (GMT): 2009/020/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6012909
38                 A    =         6741765
21  meter
 Y    =        2833750
32  meter          E    =           
0006114
 Z    =        1102802
67                 I    =           51
55894
 XDOT =      -2953
133016                 Wp   =          142
07414
 YDOT =      -3968
175123  meter/sec      RA   =          342
33371  deg
 ZDOT =      -5892
517982                 TA   =           25
86443
                                          MA   =           25
83388
                                          Ha   =            194
413  n
mi
                                          Hp   =            192
339

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19727392
98                 X    =        -6049507
11
 Y    =        9297081
10  feet           Y    =         2766305
74  meter
 Z    =        3618119
01                 Z    =         1073503
65
 XDOT =      -9688
756614                 XDOT =       -2879
916266
 YDOT =     -13018
947254  feet/sec       YDOT =       -4000
788818  meter/sec
 ZDOT =     -19332
408077                 ZDOT =       -5906
686696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19266862
87                 X    =        -5872539
80
 Y    =      -10256944
62  feet           Y    =        -3126316
72  meter
 Z    =        3504228
57                 Z    =         1068088
87
 XDOT =       3950
687251                 XDOT =        1204
169474
 YDOT =     -14059
291224  feet/sec       YDOT =       -4285
271965  meter/sec
 ZDOT =     -19387
797626                 ZDOT =       -5909
400716


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   09020
55471930  
00010596  00000-0  82463-4 0  9016
2 25544  51
6407 342
6779 0008220 289
5526  70
4748 15
70463187 22738


Satellite: ISS
Catalog Number: 25544
Epoch time:      09020
55471930   =   yrday
fracday
Element set:     901
Inclination:       51
6407  deg
RA of node:       342
6779  deg
Eccentricity:     
0008220     
Arg of perigee:   289
5526  deg
Mean anomaly:      70
4748  deg
Mean motion:   15
70463187  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2273
Checksum:              314


Coasting Arc #3 (Orbit 2288)
---------------------------------------

Vector Time (GMT): 2009/021/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4051655
34                 A    =         6732032
98  meter
 Y    =        2436098
65  meter          E    =           
0001646
 Z    =        4794217
33                 I    =           51
49983
 XDOT =      -5686
253868                 Wp   =          254
37347
 YDOT =       4540
124786  meter/sec      RA   =          337
24746  deg
 ZDOT =       2498
816024                 TA   =          171
10761
                                          MA   =          171
10469
                                          Ha   =            194
422  n
mi
                                          Hp   =            192
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13292832
49                 X    =         4000824
24
 Y    =        7992449
63  feet           Y    =         2481121
88  meter
 Z    =       15729059
47                 Z    =         4813776
80
 XDOT =     -18655
688542                 XDOT =       -5748
738307
 YDOT =      14895
422525  feet/sec       YDOT =        4476
188161  meter/sec
 ZDOT =       8198
215302                 ZDOT =        2471
041292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1761664
60                 X    =          536955
37
 Y    =       15331976
72  feet           Y    =         4673186
51  meter
 Z    =       15805346
76                 Z    =         4817469
69
 XDOT =     -22109
377416                 XDOT =       -6738
938236
 YDOT =      -5798
820768  feet/sec       YDOT =       -1767
480570  meter/sec
 ZDOT =       8090
355880                 ZDOT =        2465
940472


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   09021
57282938  
00010596  00000-0  82463-4 0  9028
2 25544  51
6412 337
4771 0008330 292
5420  67
4859 15
70524866 22895


Satellite: ISS
Catalog Number: 25544
Epoch time:      09021
57282938   =   yrday
fracday
Element set:     902
Inclination:       51
6412  deg
RA of node:       337
4771  deg
Eccentricity:     
0008330     
Arg of perigee:   292
5420  deg
Mean anomaly:      67
4859  deg
Mean motion:   15
70524866  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2289
Checksum:              323


Coasting Arc #4 (Orbit 2303)
---------------------------------------

Vector Time (GMT): 2009/022/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3576721
38                 A    =         6737871
97  meter
 Y    =       -4746371
57  meter          E    =           
0005610
 Z    =       -3166573
13                 I    =           51
49207
 XDOT =       5879
262377                 Wp   =          327
71233
 YDOT =       1219
440359  meter/sec      RA   =          332
08399  deg
 ZDOT =       4813
696132                 TA   =          355
35220
                                          MA   =          355
35741
                                          Ha   =            194
810  n
mi
                                          Hp   =            191
863

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11734650
20                 X    =         3644912
63
 Y    =      -15572085
20  feet           Y    =        -4705992
97  meter
 Z    =      -10389019
45                 Z    =        -3149032
60
 XDOT =      19288
918560                 XDOT =        5841
805778
 YDOT =       4000
788578  feet/sec       YDOT =        1284
975720  meter/sec
 ZDOT =      15792
966311                 ZDOT =        4842
166249

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19527058
20                 X    =         5951847
34
 Y    =        -542469
06  feet           Y    =         -165344
57  meter
 Z    =      -10321012
71                 Z    =        -3145844
67
 XDOT =       8850
700816                 XDOT =        2697
693609
 YDOT =      16055
095526  feet/sec       YDOT =        4893
593116  meter/sec
 ZDOT =      15903
875408                 ZDOT =        4847
501224


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   09022
52729673  
00010596  00000-0  82463-4 0  9037
2 25544  51
6409 332
6006 0008337 297
2478  62
7834 15
70497843 23044


Satellite: ISS
Catalog Number: 25544
Epoch time:      09022
52729673   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:       332
6006  deg
Eccentricity:     
0008337     
Arg of perigee:   297
2478  deg
Mean anomaly:      62
7834  deg
Mean motion:   15
70497843  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2304
Checksum:              321


Coasting Arc #5 (Orbit 2319)
---------------------------------------

Vector Time (GMT): 2009/023/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5772829
82                 A    =         6736793
27  meter
 Y    =         478442
15  meter          E    =           
0005057
 Z    =       -3442336
25                 I    =           51
46470
 XDOT =       2240
591448                 Wp   =          336
30648
 YDOT =      -5778
023329  meter/sec      RA   =          327
01382  deg
 ZDOT =      -4553
695958                 TA   =          244
46862
                                          MA   =          244
52092
                                          Ha   =            194
870  n
mi
                                          Hp   =            191
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18939730
37                 X    =        -5761028
90
 Y    =        1569692
10  feet           Y    =          413953
37  meter
 Z    =      -11293754
08                 Z    =        -3470351
34
 XDOT =       7351
021811                 XDOT =        2327
156292
 YDOT =     -18956
769452  feet/sec       YDOT =       -5752
483244  meter/sec
 ZDOT =     -14939
947370                 ZDOT =       -4542
601747

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13267953
10                 X    =        -4044072
10
 Y    =      -13515319
94  feet           Y    =        -4119469
52  meter
 Z    =      -11402795
65                 Z    =        -3475572
11
 XDOT =      18348
541811                 XDOT =        5592
635544
 YDOT =      -5425
282890  feet/sec       YDOT =       -1653
626225  meter/sec
 ZDOT =     -14897
100035                 ZDOT =       -4540
636091


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   09023
54537940  
00010596  00000-0  82463-4 0  9045
2 25544  51
6419 327
3992 0008281 301
4272  58
6079 15
70547465 23207


Satellite: ISS
Catalog Number: 25544
Epoch time:      09023
54537940   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:       327
3992  deg
Eccentricity:     
0008281     
Arg of perigee:   301
4272  deg
Mean anomaly:      58
6079  deg
Mean motion:   15
70547465  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2320
Checksum:              312


Coasting Arc #6 (Orbit 2335)
---------------------------------------

Vector Time (GMT): 2009/024/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -264783
95                 A    =         6732773
61  meter
 Y    =        4893635
60  meter          E    =           
0008326
 Z    =        4619902
39                 I    =           51
42709
 XDOT =      -6728
427995                 Wp   =            4
35543
 YDOT =       2364
095021  meter/sec      RA   =          321
84416  deg
 ZDOT =      -2881
290041                 TA   =          114
31709
                                          MA   =          114
23012
                                          Ha   =            195
044  n
mi
                                          Hp   =            191
313

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -868713
76                 X    =         -341927
81
 Y    =       16055234
91  feet           Y    =         4890242
86  meter
 Z    =       15157160
06                 Z    =         4618429
19
 XDOT =     -22074
894997                 XDOT =       -6740
367190
 YDOT =       7756
217260  feet/sec       YDOT =        2288
787357  meter/sec
 ZDOT =      -9453
051315                 ZDOT =       -2914
004707

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12795161
42                 X    =        -3899965
20
 Y    =        9745455
12  feet           Y    =         2970414
72  meter
 Z    =       15151722
06                 Z    =         4618244
88
 XDOT =     -19529
296960                 XDOT =       -5952
529714
 YDOT =     -10702
376836  feet/sec       YDOT =       -3262
084460  meter/sec
 ZDOT =      -9580
279385                 ZDOT =       -2920
069157


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   09024
56344749  
00010596  00000-0  82463-4 0  9052
2 25544  51
6420 322
1984 0008266 304
9897  55
0488 15
70553297 23369


Satellite: ISS
Catalog Number: 25544
Epoch time:      09024
56344749   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:       322
1984  deg
Eccentricity:     
0008266     
Arg of perigee:   304
9897  deg
Mean anomaly:      55
0488  deg
Mean motion:   15
70553297  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2336
Checksum:              331


Coasting Arc #7 (Orbit 2351)
---------------------------------------

Vector Time (GMT): 2009/025/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5518110
57                 A    =         6740944
95  meter
 Y    =       -3555883
01  meter          E    =           
0013192
 Z    =        1492802
29                 I    =           51
43263
 XDOT =       1561
614425                 Wp   =           26
36677
 YDOT =       4850
073646  meter/sec      RA   =          316
75547  deg
 ZDOT =       5772
634646                 TA   =          350
10851
                                          MA   =          350
13445
                                          Ha   =            195
128  n
mi
                                          Hp   =            191
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18104037
31                 X    =         5550211
36
 Y    =      -11666282
84  feet           Y    =        -3493996
93  meter
 Z    =        4897645
31                 Z    =         1519686
22
 XDOT =       5123
406906                 XDOT =        1479
222399
 YDOT =      15912
315111  feet/sec       YDOT =        4867
075384  meter/sec
 ZDOT =      18939
090045                 ZDOT =        5780
021024

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20733650
32                 X    =         6319616
62
 Y    =        5739338
80  feet           Y    =         1749350
47  meter
 Z    =        5002098
18                 Z    =         1524639
52
 XDOT =      -8129
759793                 XDOT =       -2477
950785
 YDOT =      12815
547567  feet/sec       YDOT =        3906
178898  meter/sec
 ZDOT =      18968
151051                 ZDOT =        5781
492440


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   09025
58150037  
00010596  00000-0  82463-4 0  9061
2 25544  51
6421 316
9964 0008330 309
0769  50
9651 15
70572843 23527


Satellite: ISS
Catalog Number: 25544
Epoch time:      09025
58150037   =   yrday
fracday
Element set:     906
Inclination:       51
6421  deg
RA of node:       316
9964  deg
Eccentricity:     
0008330     
Arg of perigee:   309
0769  deg
Mean anomaly:      50
9651  deg
Mean motion:   15
70572843  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2352
Checksum:              308


Coasting Arc #8 (Orbit 2366)
---------------------------------------

Vector Time (GMT): 2009/026/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2791686
15                 A    =         6729858
29  meter
 Y    =       -3169469
71  meter          E    =           
0009902
 Z    =       -5246667
46                 I    =           51
37565
 XDOT =       5367
995032                 Wp   =           61
80246
 YDOT =      -5486
343980  meter/sec      RA   =          311
61116  deg
 ZDOT =        463
282629                 TA   =          212
58982
                                          MA   =          212
65097
                                          Ha   =            195
243  n
mi
                                          Hp   =            190
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9159075
29                 X    =        -2730550
51
 Y    =      -10398522
66  feet           Y    =        -3200345
82  meter
 Z    =      -17213475
92                 Z    =        -5260080
78
 XDOT =      17611
532257                 XDOT =        5426
694799
 YDOT =     -17999
816208  feet/sec       YDOT =       -5425
987765  meter/sec
 ZDOT =       1519
956132                 ZDOT =         489
501848

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1504505
12                 X    =          458573
16
 Y    =      -13709364
46  feet           Y    =        -4178614
29  meter
 Z    =      -17265905
06                 Z    =        -5262647
86
 XDOT =      24165
565552                 XDOT =        7365
664380
 YDOT =        631
303620  feet/sec       YDOT =         192
421343  meter/sec
 ZDOT =       1621
694726                 ZDOT =         494
292553


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   09026
53591083  
00010596  00000-0  82463-4 0  9078
2 25544  51
6426 312
1202 0008315 312
6517  47
3943 15
70609936 23673


Satellite: ISS
Catalog Number: 25544
Epoch time:      09026
53591083   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:       312
1202  deg
Eccentricity:     
0008315     
Arg of perigee:   312
6517  deg
Mean anomaly:      47
3943  deg
Mean motion:   15
70609936  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2367
Checksum:              301


Coasting Arc #9 (Orbit 2382)
---------------------------------------

Vector Time (GMT): 2009/027/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3535247
45                 A    =         6741643
39  meter
 Y    =        5697389
74  meter          E    =           
0005246
 Z    =         682513
91                 I    =           51
39670
 XDOT =      -4420
396135                 Wp   =          115
15337
 YDOT =      -2024
907483  meter/sec      RA   =          306
48117  deg
 ZDOT =      -5959
735488                 TA   =           57
40114
                                          MA   =           57
35050
                                          Ha   =            195
450  n
mi
                                          Hp   =            190
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11598580
87                 X    =        -3602009
29
 Y    =       18692223
57  feet           Y    =         5657483
24  meter
 Z    =        2239218
88                 Z    =          665178
22
 XDOT =     -14502
611992                 XDOT =       -4368
474261
 YDOT =      -6643
397255  feet/sec       YDOT =       -2074
048390  meter/sec
 ZDOT =     -19552
937952                 ZDOT =       -5981
083121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21539108
46                 X    =        -6565120
26
 Y    =        4504356
24  feet           Y    =         1372927
78  meter
 Z    =        2172091
77                 Z    =          662053
57
 XDOT =      -4799
370342                 XDOT =       -1462
848080
 YDOT =     -13426
114642  feet/sec       YDOT =       -4092
279743  meter/sec
 ZDOT =     -19636
192188                 ZDOT =       -5985
111379


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   09027
55393509  
00010596  00000-0  82463-4 0  9085
2 25544  51
6426 306
9187 0008277 316
1125  43
9379 15
70611498 23836


Satellite: ISS
Catalog Number: 25544
Epoch time:      09027
55393509   =   yrday
fracday
Element set:     908
Inclination:       51
6426  deg
RA of node:       306
9187  deg
Eccentricity:     
0008277     
Arg of perigee:   316
1125  deg
Mean anomaly:      43
9379  deg
Mean motion:   15
70611498  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2383
Checksum:              331


Coasting Arc #10 (Orbit 2398)
---------------------------------------

Vector Time (GMT): 2009/028/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4546090
58                 A    =         6730919
18  meter
 Y    =         165972
88  meter          E    =           
0003126
 Z    =        4960478
51                 I    =           51
34445
 XDOT =      -2422
927796                 Wp   =          349
69399
 YDOT =       7028
522561  meter/sec      RA   =          301
37463  deg
 ZDOT =       1988
577895                 TA   =           81
00081
                                          MA   =           80
96542
                                          Ha   =            195
443  n
mi
                                          Hp   =            190
316

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14914995
33                 X    =         4519800
29
 Y    =         544530
44  feet           Y    =          216662
83  meter
 Z    =       16274535
78                 Z    =         4982498
98
 XDOT =      -7949
238177                 XDOT =       -2511
001718
 YDOT =      23059
457220  feet/sec       YDOT =        7000
935499  meter/sec
 ZDOT =       6524
205691                 ZDOT =        1976
593800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10027307
37                 X    =         3056323
29
 Y    =       10927404
59  feet           Y    =         3330672
92  meter
 Z    =       16360288
80                 Z    =         4986616
03
 XDOT =     -21221
762626                 XDOT =       -6468
393248
 YDOT =       9790
713594  feet/sec       YDOT =        2984
209503  meter/sec
 ZDOT =       6478
014814                 ZDOT =        1974
498915


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   09028
57194326  
00010596  00000-0  82463-4 0  9095
2 25544  51
6424 301
7168 0008339 319
9937  40
0610 15
70659740 23992


Satellite: ISS
Catalog Number: 25544
Epoch time:      09028
57194326   =   yrday
fracday
Element set:     909
Inclination:       51
6424  deg
RA of node:       301
7168  deg
Eccentricity:     
0008339     
Arg of perigee:   319
9937  deg
Mean anomaly:      40
0610  deg
Mean motion:   15
70659740  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2399
Checksum:              327


Coasting Arc #11 (Orbit 2413)
---------------------------------------

Vector Time (GMT): 2009/029/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         588726
96                 A    =         6738421
38  meter
 Y    =       -6128722
06  meter          E    =           
0009434
 Z    =       -2724177
24                 I    =           51
35584
 XDOT =       5449
788351                 Wp   =          354
23955
 YDOT =      -1759
444280  meter/sec      RA   =          296
20493  deg
 ZDOT =       5143
779960                 TA   =          334
55869
                                          MA   =          334
60510
                                          Ha   =            195
666  n
mi
                                          Hp   =            190
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1931518
90                 X    =          670448
85
 Y    =      -20107355
83  feet           Y    =        -6121681
65  meter
 Z    =       -8937589
37                 Z    =        -2721118
76
 XDOT =      17879
883040                 XDOT =        5444
070726
 YDOT =      -5772
454987  feet/sec       YDOT =       -1698
533542  meter/sec
 ZDOT =      16875
918504                 ZDOT =        5170
240541

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15478290
70                 X    =         4717783
00
 Y    =      -12987080
56  feet           Y    =        -3958462
16  meter
 Z    =       -8926101
23                 Z    =        -2720675
65
 XDOT =      15801
020515                 XDOT =        4816
151053
 YDOT =       7179
746396  feet/sec       YDOT =        2188
386701  meter/sec
 ZDOT =      16978
827773                 ZDOT =        5175
146705


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   09029
52631344  
00010596  00000-0  82463-4 0  9109
2 25544  51
6427 296
8401 0008409 323
7233  36
3357 15
70683041 24144


Satellite: ISS
Catalog Number: 25544
Epoch time:      09029
52631344   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:       296
8401  deg
Eccentricity:     
0008409     
Arg of perigee:   323
7233  deg
Mean anomaly:      36
3357  deg
Mean motion:   15
70683041  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2414
Checksum:              293


Coasting Arc #12 (Orbit 2429)
---------------------------------------

Vector Time (GMT): 2009/030/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4531296
50                 A    =         6735077
53  meter
 Y    =        3165702
96  meter          E    =           
0009115
 Z    =       -3856559
00                 I    =           51
33287
 XDOT =      -1015
482113                 Wp   =           10
19730
 YDOT =      -6434
777430  meter/sec      RA   =          291
12237  deg
 ZDOT =      -4081
552610                 TA   =          216
92748
                                          MA   =          216
99027
                                          Ha   =            195
829  n
mi
                                          Hp   =            189
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14866458
34                 X    =        -4547625
02
 Y    =       10386164
58  feet           Y    =         3114940
04  meter
 Z    =      -12652752
62                 Z    =        -3878611
32
 XDOT =      -3331
634230                 XDOT =        -923
624816
 YDOT =     -21111
474507  feet/sec       YDOT =       -6445
619579  meter/sec
 ZDOT =     -13390
920638                 ZDOT =       -4086
262552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17885251
71                 X    =        -5451424
72
 Y    =       -2612885
94  feet           Y    =         -796407
64  meter
 Z    =      -12738396
49                 Z    =        -3882663
25
 XDOT =      11945
433068                 XDOT =        3640
967999
 YDOT =     -16274
435400  feet/sec       YDOT =       -4960
447910  meter/sec
 ZDOT =     -13409
709196                 ZDOT =       -4087
279363


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   09030
54429355  
00010596  00000-0  82463-4 0  9111
2 25544  51
6426 291
6382 0008526 327
0308  33
0321 15
70696248 24300


Satellite: ISS
Catalog Number: 25544
Epoch time:      09030
54429355   =   yrday
fracday
Element set:     911
Inclination:       51
6426  deg
RA of node:       291
6382  deg
Eccentricity:     
0008526     
Arg of perigee:   327
0308  deg
Mean anomaly:      33
0321  deg
Mean motion:   15
70696248  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2430
Checksum:              291

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

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