Date: January 8th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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


014/18:07:09 671 6 8 9 8 9 8
N/A 5 3 0 0 193 6
000/00:02:19 341 4 8 -0 1 192 9

Coasting Arc #1 (Orbit 2036)
---------------------------------------

Vector Time (GMT): 2009/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3780238
25                 A    =         6725736
74  meter
 Y    =        1742971
67  meter          E    =           
0007039
 Z    =        5278836
74                 I    =           51
90428
 XDOT =      -3676
405083                 Wp   =          143
45136
 YDOT =      -6755
525633  meter/sec      RA   =           59
06444  deg
 ZDOT =       -407
428840                 TA   =          310
37219
                                          MA   =          310
43362
                                          Ha   =            194
826  n
mi
                                          Hp   =            185
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12402356
46                 X    =        -3825091
20
 Y    =        5718411
01  feet           Y    =         1700447
62  meter
 Z    =       17319018
18                 Z    =         5260363
49
 XDOT =     -12061
696467                 XDOT =       -3598
611224
 YDOT =     -22163
798007  feet/sec       YDOT =       -6796
202321  meter/sec
 ZDOT =      -1336
708793                 ZDOT =        -425
100496

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8658397
52                 X    =        -2639079
56
 Y    =      -10678575
95  feet           Y    =        -3254829
95  meter
 Z    =       17247238
30                 Z    =         5256958
23
 XDOT =      17674
467477                 XDOT =        5387
177687
 YDOT =     -16573
546440  feet/sec       YDOT =       -5051
616955  meter/sec
 ZDOT =      -1405
908579                 ZDOT =        -428
520935


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   09005
54697578  
00010596  00000-0  82463-4 0  9005
2 25544  51
6411  59
4499 0006743 165
7805 194
3548 15
72041805 20371


Satellite: ISS
Catalog Number: 25544
Epoch time:      09005
54697578   =   yrday
fracday
Element set:     900
Inclination:       51
6411  deg
RA of node:        59
4499  deg
Eccentricity:     
0006743     
Arg of perigee:   165
7805  deg
Mean anomaly:     194
3548  deg
Mean motion:   15
72041805  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2037
Checksum:              326


Coasting Arc #2 (Orbit 2051)
---------------------------------------

Vector Time (GMT): 2009/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4140150
03                 A    =         6737818
46  meter
 Y    =        5306447
35  meter          E    =           
0009657
 Z    =        -288736
19                 I    =           51
92843
 XDOT =      -3588
406476                 Wp   =           76
68168
 YDOT =       3119
488623  meter/sec      RA   =           53
96394  deg
 ZDOT =       6047
410719                 TA   =          280
19737
                                          MA   =          280
30626
                                          Ha   =            194
662  n
mi
                                          Hp   =            185
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13583169
40                 X    =         4081907
39
 Y    =       17409604
17  feet           Y    =         5352419
29  meter
 Z    =        -947297
21                 Z    =         -268764
14
 XDOT =     -11772
987126                 XDOT =       -3652
399751
 YDOT =      10234
542727  feet/sec       YDOT =        3079
002508  meter/sec
 ZDOT =      19840
586350                 ZDOT =        6029
823077

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13163285
06                 X    =        -4012169
29
 Y    =       17733203
94  feet           Y    =         5405080
56  meter
 Z    =        -869243
80                 Z    =         -264945
51
 XDOT =     -11737
128828                 XDOT =       -3577
476867
 YDOT =      -7773
116898  feet/sec       YDOT =       -2369
246031  meter/sec
 ZDOT =      19772
333134                 ZDOT =        6026
607139


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   09006
50051127  
00010596  00000-0  82463-4 0  9017
2 25544  51
6411  54
5672 0006516 167
4178 192
7148 15
72006144 20522


Satellite: ISS
Catalog Number: 25544
Epoch time:      09006
50051127   =   yrday
fracday
Element set:     901
Inclination:       51
6411  deg
RA of node:        54
5672  deg
Eccentricity:     
0006516     
Arg of perigee:   167
4178  deg
Mean anomaly:     192
7148  deg
Mean motion:   15
72006144  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2052
Checksum:              279


Coasting Arc #3 (Orbit 2067)
---------------------------------------

Vector Time (GMT): 2009/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2338146
48                 A    =         6725991
25  meter
 Y    =       -3554100
54  meter          E    =           
0016074
 Z    =       -5222149
11                 I    =           51
87161
 XDOT =       5589
852268                 Wp   =          106
54740
 YDOT =       5176
009699  meter/sec      RA   =           48
87243  deg
 ZDOT =      -1026
986047                 TA   =          153
71517
                                          MA   =          153
63352
                                          Ha   =            194
563  n
mi
                                          Hp   =            186
074

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7671084
26                 X    =         2403083
55
 Y    =      -11660434
83  feet           Y    =        -3527590
22  meter
 Z    =      -17133035
13                 Z    =        -5210633
13
 XDOT =      18339
410327                 XDOT =        5536
546747
 YDOT =      16981
659116  feet/sec       YDOT =        5238
220761  meter/sec
 ZDOT =      -3369
376794                 ZDOT =        -999
959246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13381844
60                 X    =         4078786
23
 Y    =        4154992
18  feet           Y    =         1266441
62  meter
 Z    =      -17088430
07                 Z    =        -5208553
48
 XDOT =     -10793
871547                 XDOT =       -3289
972047
 YDOT =      21435
566884  feet/sec       YDOT =        6533
560786  meter/sec
 ZDOT =      -3263
879832                 ZDOT =        -994
830573


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   09007
51760095  
00010596  00000-0  82463-4 0  9021
2 25544  51
6420  49
3588 0006660 171
5255 188
6021 15
72049935 20688


Satellite: ISS
Catalog Number: 25544
Epoch time:      09007
51760095   =   yrday
fracday
Element set:     902
Inclination:       51
6420  deg
RA of node:        49
3588  deg
Eccentricity:     
0006660     
Arg of perigee:   171
5255  deg
Mean anomaly:     188
6021  deg
Mean motion:   15
72049935  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2068
Checksum:              309


Coasting Arc #4 (Orbit 2083)
---------------------------------------

Vector Time (GMT): 2009/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5473118
95                 A    =         6736656
07  meter
 Y    =       -3609494
84  meter          E    =           
0018548
 Z    =        1500312
96                 I    =           51
88706
 XDOT =       1569
723267                 Wp   =          135
17940
 YDOT =      -4808
517146  meter/sec      RA   =           43
74626  deg
 ZDOT =      -5811
766332                 TA   =           28
35014
                                          MA   =           28
24933
                                          Ha   =            194
410  n
mi
                                          Hp   =            186
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17956427
00                 X    =        -5439638
44
 Y    =      -11842174
66  feet           Y    =        -3670511
47  meter
 Z    =        4922286
61                 Z    =         1473805
35
 XDOT =       5150
010718                 XDOT =        1651
608657
 YDOT =     -15775
974889  feet/sec       YDOT =       -4790
504800  meter/sec
 ZDOT =     -19067
474841                 ZDOT =       -5803
942520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5917649
76                 X    =         1803699
65
 Y    =      -20704078
73  feet           Y    =        -6310603
20  meter
 Z    =        4818902
56                 Z    =         1468801
50
 XDOT =      15117
468661                 XDOT =        4607
804448
 YDOT =       -133
766921  feet/sec       YDOT =         -40
772157  meter/sec
 ZDOT =     -19037
306139                 ZDOT =       -5802
570911


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   09008
53467539  
00010596  00000-0  82463-4 0  9032
2 25544  51
6415  44
1507 0006550 174
1537 185
9703 15
72100997 20847


Satellite: ISS
Catalog Number: 25544
Epoch time:      09008
53467539   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:        44
1507  deg
Eccentricity:     
0006550     
Arg of perigee:   174
1537  deg
Mean anomaly:     185
9703  deg
Mean motion:   15
72100997  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2084
Checksum:              309


Coasting Arc #5 (Orbit 2099)
---------------------------------------

Vector Time (GMT): 2009/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -305426
32                 A    =         6727324
48  meter
 Y    =        4644158
64  meter          E    =           
0011831
 Z    =        4855866
04                 I    =           51
83308
 XDOT =      -6696
122498                 Wp   =          148
16408
 YDOT =      -2952
871306  meter/sec      RA   =           38
67324  deg
 ZDOT =       2390
479518                 TA   =          278
50729
                                          MA   =          278
64135
                                          Ha   =            194
277  n
mi
                                          Hp   =            186
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1002054
87                 X    =         -380924
05
 Y    =       15236740
94  feet           Y    =         4640320
21  meter
 Z    =       15931319
03                 Z    =         4854199
72
 XDOT =     -21968
905834                 XDOT =       -6674
217734
 YDOT =      -9687
897985  feet/sec       YDOT =       -3027
629164  meter/sec
 ZDOT =       7842
780571                 ZDOT =        2358
002772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14803350
68                 X    =        -4512061
29
 Y    =        3771106
59  feet           Y    =         1149433
29  meter
 Z    =       15925102
14                 Z    =         4853971
13
 XDOT =       2519
738550                 XDOT =         768
016310
 YDOT =     -22866
688415  feet/sec       YDOT =       -6969
766629  meter/sec
 ZDOT =       7716
194739                 ZDOT =        2351
896156


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   09009
55173605  
00010596  00000-0  82463-4 0  9044
2 25544  51
6408  38
9423 0006538 176
9908 183
1294 15
72111907 21002


Satellite: ISS
Catalog Number: 25544
Epoch time:      09009
55173605   =   yrday
fracday
Element set:     904
Inclination:       51
6408  deg
RA of node:        38
9423  deg
Eccentricity:     
0006538     
Arg of perigee:   176
9908  deg
Mean anomaly:     183
1294  deg
Mean motion:   15
72111907  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2100
Checksum:              306


Coasting Arc #6 (Orbit 2114)
---------------------------------------

Vector Time (GMT): 2009/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6016704
60                 A    =         6734460
48  meter
 Y    =        1502578
44  meter          E    =           
0005285
 Z    =       -2634322
74                 I    =           51
83471
 XDOT =        909
664467                 Wp   =          130
58980
 YDOT =       5548
287042  meter/sec      RA   =           33
52510  deg
 ZDOT =       5245
790396                 TA   =          199
59010
                                          MA   =          199
61042
                                          Ha   =            194
097  n
mi
                                          Hp   =            186
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19739844
49                 X    =         6012252
18
 Y    =        4929719
30  feet           Y    =         1569836
26  meter
 Z    =       -8642791
16                 Z    =        -2605104
68
 XDOT =       2984
463476                 XDOT =         822
072361
 YDOT =      18203
041478  feet/sec       YDOT =        5557
968817  meter/sec
 ZDOT =      17210
598411                 ZDOT =        5249
997627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1917711
64                 X    =          584518
51
 Y    =       20303708
24  feet           Y    =         6188570
27  meter
 Z    =       -8528965
09                 Z    =        -2599628
56
 XDOT =     -14733
278697                 XDOT =       -4490
703347
 YDOT =       8623
366227  feet/sec       YDOT =        2628
402026  meter/sec
 ZDOT =      17227
296436                 ZDOT =        5250
879954


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   09010
50521679  
00010596  00000-0  82463-4 0  9050
2 25544  51
6419  34
0596 0006546 180
3274 179
7885 15
72168112 21159


Satellite: ISS
Catalog Number: 25544
Epoch time:      09010
50521679   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:        34
0596  deg
Eccentricity:     
0006546     
Arg of perigee:   180
3274  deg
Mean anomaly:     179
7885  deg
Mean motion:   15
72168112  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2115
Checksum:              309


Coasting Arc #7 (Orbit 2130)
---------------------------------------

Vector Time (GMT): 2009/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1890376
19                 A    =         6729474
40  meter
 Y    =       -4848693
54  meter          E    =           
0008223
 Z    =       -4270777
75                 I    =           51
79198
 XDOT =       6796
811383                 Wp   =          113
95515
 YDOT =        487
518319  meter/sec      RA   =           28
46203  deg
 ZDOT =      -3570
614565                 TA   =          119
88099
                                          MA   =          119
79926
                                          Ha   =            193
941  n
mi
                                          Hp   =            186
379

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6202021
64                 X    =        -1815270
64
 Y    =      -15907787
20  feet           Y    =        -4869412
28  meter
 Z    =      -14011738
01                 Z    =        -4279779
23
 XDOT =      22299
249945                 XDOT =        6808
199703
 YDOT =       1599
469551  feet/sec       YDOT =         563
588379  meter/sec
 ZDOT =     -11714
614716                 ZDOT =       -3537
568714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12782617
62                 X    =         3896141
85
 Y    =      -11275473
06  feet           Y    =        -3436764
19  meter
 Z    =      -14047062
40                 Z    =        -4281544
62
 XDOT =       5463
492759                 XDOT =        1665
272593
 YDOT =      20592
348820  feet/sec       YDOT =        6276
547920  meter/sec
 ZDOT =     -11585
938135                 ZDOT =       -3531
393943


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   09011
52224865  
00010596  00000-0  82463-4 0  9061
2 25544  51
6411  28
8504 0006430 185
0211 175
0888 15
72157029 21311


Satellite: ISS
Catalog Number: 25544
Epoch time:      09011
52224865   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:        28
8504  deg
Eccentricity:     
0006430     
Arg of perigee:   185
0211  deg
Mean anomaly:     175
0888  deg
Mean motion:   15
72157029  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2131
Checksum:              282


Coasting Arc #8 (Orbit 2146)
---------------------------------------

Vector Time (GMT): 2009/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5657657
29                 A    =         6731833
64  meter
 Y    =         632199
41  meter          E    =           
0012507
 Z    =        3578155
72                 I    =           51
77266
 XDOT =      -3408
981389                 Wp   =          116
12859
 YDOT =      -5284
560255  meter/sec      RA   =           23
29993  deg
 ZDOT =      -4449
923553                 TA   =           21
22975
                                          MA   =           21
17790
                                          Ha   =            193
847  n
mi
                                          Hp   =            186
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18561867
75                 X    =        -5681687
73
 Y    =        2074145
04  feet           Y    =          568797
46  meter
 Z    =       11739356
05                 Z    =         3550613
25
 XDOT =     -11184
322142                 XDOT =       -3328
018859
 YDOT =     -17337
796111  feet/sec       YDOT =       -5322
228303  meter/sec
 ZDOT =     -14599
486723                 ZDOT =       -4466
287854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8715560
28                 X    =        -2656502
77
 Y    =      -16594855
36  feet           Y    =        -5058111
91  meter
 Z    =       11632165
63                 Z    =         3545484
08
 XDOT =      10895
484613                 XDOT =        3320
943710
 YDOT =     -16015
856014  feet/sec       YDOT =       -4881
632913  meter/sec
 ZDOT =     -14663
505871                 ZDOT =       -4469
436589


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   09012
53926556  
00010596  00000-0  82463-4 0  9070
2 25544  51
6402  23
6412 0006288 188
9483 171
1568 15
72202349 21471


Satellite: ISS
Catalog Number: 25544
Epoch time:      09012
53926556   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:        23
6412  deg
Eccentricity:     
0006288     
Arg of perigee:   188
9483  deg
Mean anomaly:     171
1568  deg
Mean motion:   15
72202349  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2147
Checksum:              311


Coasting Arc #9 (Orbit 2162)
---------------------------------------

Vector Time (GMT): 2009/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3978854
00                 A    =         6732029
56  meter
 Y    =        4183173
85  meter          E    =           
0012699
 Z    =        3459662
37                 I    =           51
74576
 XDOT =      -5918
106514                 Wp   =          120
58079
 YDOT =       1838
842461  meter/sec      RA   =           18
23796  deg
 ZDOT =       4564
137724                 TA   =          280
30756
                                          MA   =          280
45071
                                          Ha   =            193
584  n
mi
                                          Hp   =            186
659

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13053982
93                 X    =         3914975
36
 Y    =       13724323
65  feet           Y    =         4227310
28  meter
 Z    =       11350598
32                 Z    =         3478836
30
 XDOT =     -19416
359954                 XDOT =       -5960
400096
 YDOT =       6032
947706  feet/sec       YDOT =        1772
425950  meter/sec
 ZDOT =      14974
205132                 ZDOT =        4535
285704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7757316
57                 X    =        -2364430
09
 Y    =       17230255
86  feet           Y    =         5251781
99  meter
 Z    =       11425494
95                 Z    =         3482490
86
 XDOT =     -11736
847915                 XDOT =       -3577
391245
 YDOT =     -15179
607687  feet/sec       YDOT =       -4626
744423  meter/sec
 ZDOT =      14861
987457                 ZDOT =        4529
933777


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   09013
55626847  
00010596  00000-0  82463-4 0  9084
2 25544  51
6399  18
4323 0006325 193
3536 166
7459 15
72205919 21633


Satellite: ISS
Catalog Number: 25544
Epoch time:      09013
55626847   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:        18
4323  deg
Eccentricity:     
0006325     
Arg of perigee:   193
3536  deg
Mean anomaly:     166
7459  deg
Mean motion:   15
72205919  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2163
Checksum:              327


Coasting Arc #10 (Orbit 2177)
---------------------------------------

Vector Time (GMT): 2009/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4519819
13                 A    =         6729243
45  meter
 Y    =       -2469549
55  meter          E    =           
0011073
 Z    =       -4341639
37                 I    =           51
70790
 XDOT =       5536
920297                 Wp   =          144
32173
 YDOT =       4075
271544  meter/sec      RA   =           13
07232  deg
 ZDOT =       3441
696681                 TA   =          160
47461
                                          MA   =          160
43217
                                          Ha   =            193
485  n
mi
                                          Hp   =            186
956

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14828802
93                 X    =         4568188
55
 Y    =       -8102196
68  feet           Y    =        -2418735
64  meter
 Z    =      -14244223
66                 Z    =        -4319565
21
 XDOT =      18165
749007                 XDOT =        5474
219655
 YDOT =      13370
313465  feet/sec       YDOT =        4136
837847  meter/sec
 ZDOT =      11291
655778                 ZDOT =        3468
442355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13344187
46                 X    =         4067308
34
 Y    =       10483716
53  feet           Y    =         3195436
80  meter
 Z    =      -14158433
66                 Z    =        -4315490
58
 XDOT =      -4346
050000                 XDOT =       -1324
676040
 YDOT =      20942
086932  feet/sec       YDOT =        6383
148097  meter/sec
 ZDOT =      11396
025061                 ZDOT =        3473
508439


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   09014
50969510  
00010596  00000-0  82463-4 0  9098
2 25544  51
6401  13
5488 0006222 196
9691 163
1264 15
72198796 21787


Satellite: ISS
Catalog Number: 25544
Epoch time:      09014
50969510   =   yrday
fracday
Element set:     909
Inclination:       51
6401  deg
RA of node:        13
5488  deg
Eccentricity:     
0006222     
Arg of perigee:   196
9691  deg
Mean anomaly:     163
1264  deg
Mean motion:   15
72198796  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2178
Checksum:              325


Coasting Arc #11 (Orbit 2181)
---------------------------------------

Vector Time (GMT): 2009/014/18:08:19
341
Vector Time (MET): N/A
Weight (LBS)     : 639553
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5154193
65                 A    =         6736175
94  meter
 Y    =       -2021418
96  meter          E    =           
0003158
 Z    =       -3837494
83                 I    =           51
70926
 XDOT =       4799
309335                 Wp   =          219
14886
 YDOT =       4347
402374  meter/sec      RA   =           11
76228  deg
 ZDOT =       4151
753425                 TA   =           94
31490
                                          MA   =           94
27882
                                          Ha   =            193
591  n
mi
                                          Hp   =            192
896

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16910084
15                 X    =         5195055
88
 Y    =       -6631951
98  feet           Y    =        -1963553
13  meter
 Z    =      -12590206
12                 Z    =        -3812357
12
 XDOT =      15745
765536                 XDOT =        4730
171228
 YDOT =      14263
131147  feet/sec       YDOT =        4400
684270  meter/sec
 ZDOT =      13621
238272                 ZDOT =        4174
900251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12435955
77                 X    =         3790479
32
 Y    =      -13331631
22  feet           Y    =        -4063481
20  meter
 Z    =      -12492463
19                 Z    =        -3807702
78
 XDOT =      19326
047025                 XDOT =        5890
579133
 YDOT =       5165
941388  feet/sec       YDOT =        1574
578935  meter/sec
 ZDOT =      13711
612829                 ZDOT =        4179
299590


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   09014
76393920  
00010596  00000-0  82463-4 0  9104
2 25544  51
6428  12
2470 0008092 263
8810  96
1430 15
70395973 21826


Satellite: ISS
Catalog Number: 25544
Epoch time:      09014
76393920   =   yrday
fracday
Element set:     910
Inclination:       51
6428  deg
RA of node:        12
2470  deg
Eccentricity:     
0008092     
Arg of perigee:   263
8810  deg
Mean anomaly:      96
1430  deg
Mean motion:   15
70395973  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2182
Checksum:              300


Coasting Arc #12 (Orbit 2197)
---------------------------------------

Vector Time (GMT): 2009/015/18:08:19
341
Vector Time (MET): N/A
Weight (LBS)     : 639553
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5504685
60                 A    =         6739234
76  meter
 Y    =       -2792694
73  meter          E    =           
0005092
 Z    =       -2697059
60                 I    =           51
69130
 XDOT =       4379
537220                 Wp   =          234
06958
 YDOT =      -3614
755932  meter/sec      RA   =            6
70705  deg
 ZDOT =      -5191
799936                 TA   =          336
61139
                                          MA   =          336
63454
                                          Ha   =            192
923  n
mi
                                          Hp   =            192
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18059992
14                 X    =        -5459946
50
 Y    =       -9162384
27  feet           Y    =        -2854001
06  meter
 Z    =       -8848620
74                 Z    =        -2723692
36
 XDOT =      14368
560432                 XDOT =        4444
852929
 YDOT =     -11859
435473  feet/sec       YDOT =       -3565
416004  meter/sec
 ZDOT =     -17033
464357                 ZDOT =       -5170
365987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20205224
25                 X    =        -6158552
35
 Y    =        -113464
59  feet           Y    =          -34584
01  meter
 Z    =       -8952470
59                 Z    =        -2728713
04
 XDOT =       7603
524133                 XDOT =        2317
554156
 YDOT =     -15614
343297  feet/sec       YDOT =       -4759
251837  meter/sec
 ZDOT =     -16950
239172                 ZDOT =       -5166
432900


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   09015
78210326  
00010596  00000-0  82463-4 0  9116
2 25544  51
6434   7
0465 0008214 267
4945  92
5276 15
70393589 21980


Satellite: ISS
Catalog Number: 25544
Epoch time:      09015
78210326   =   yrday
fracday
Element set:     911
Inclination:       51
6434  deg
RA of node:         7
0465  deg
Eccentricity:     
0008214     
Arg of perigee:   267
4945  deg
Mean anomaly:      92
5276  deg
Mean motion:   15
70393589  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2198
Checksum:              316


Coasting Arc #13 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2009/016/18:08:19
341
Vector Time (MET): N/A
Weight (LBS)     : 639553
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2189632
56                 A    =         6731378
18  meter
 Y    =        3916718
03  meter          E    =           
0004999
 Z    =        5021638
11                 I    =           51
63598
 XDOT =      -7272
475747                 Wp   =          314
45425
 YDOT =      -1673
827963  meter/sec      RA   =            1
56257  deg
 ZDOT =      -1863
256531                 TA   =          153
55446
                                          MA   =          153
52894
                                          Ha   =            192
906  n
mi
                                          Hp   =            192
445

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7183833
87                 X    =        -2257661
11
 Y    =       12850124
76  feet           Y    =         3891851
70  meter
 Z    =       16475190
64                 Z    =         5010835
93
 XDOT =     -23859
828566                 XDOT =       -7244
166972
 YDOT =      -5491
561559  feet/sec       YDOT =       -1754
994644  meter/sec
 ZDOT =      -6113
046361                 ZDOT =       -1898
517085

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -489170
47                 X    =         -149099
16
 Y    =       14760420
53  feet           Y    =         4498976
18  meter
 Z    =       16433373
97                 Z    =         5008892
39
 XDOT =     -22577
757987                 XDOT =       -6881
700635
 YDOT =       6219
008841  feet/sec       YDOT =        1895
553895  meter/sec
 ZDOT =      -6250
412687                 ZDOT =       -1905
125787


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   09016
80025213  
00010596  00000-0  82463-4 0  9120
2 25544  51
6433   1
8456 0008231 272
2756  87
7463 15
70471274 22145


Satellite: ISS
Catalog Number: 25544
Epoch time:      09016
80025213   =   yrday
fracday
Element set:     912
Inclination:       51
6433  deg
RA of node:         1
8456  deg
Eccentricity:     
0008231     
Arg of perigee:   272
2756  deg
Mean anomaly:      87
7463  deg
Mean motion:   15
70471274  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2214
Checksum:              285

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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