Date: February 1st 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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


035/08:34:45 300 -0 6 1 7 1 7
N/A -1 5 0 0 196 6
000/00:09:26 601 -0 6 0 2 189 6

Coasting Arc #1 (Orbit 2429)
---------------------------------------

Vector Time (GMT): 2009/030/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4527059
97                 A    =         6735198
47  meter
 Y    =        3195005
62  meter          E    =           
0009054
 Z    =       -3837448
09                 I    =           51
33302
 XDOT =      -1041
927053                 Wp   =            9
63848
 YDOT =      -6415
602724  meter/sec      RA   =          291
13229  deg
 ZDOT =      -4104
980578                 TA   =          217
18059
                                          MA   =          217
24332
                                          Ha   =            195
866  n
mi
                                          Hp   =            189
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14852558
97                 X    =        -4543809
31
 Y    =       10482301
90  feet           Y    =         3144287
72  meter
 Z    =      -12590052
79                 Z    =        -3859480
85
 XDOT =      -3418
395843                 XDOT =        -950
168398
 YDOT =     -21048
565368  feet/sec       YDOT =       -6426
741148  meter/sec
 ZDOT =     -13467
784048                 ZDOT =       -4109
819227

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17941448
23                 X    =        -5468553
42
 Y    =       -2533717
03  feet           Y    =         -772276
95  meter
 Z    =      -12675618
47                 Z    =        -3863528
51
 XDOT =      11845
263097                 XDOT =        3610
436192
 YDOT =     -16283
906706  feet/sec       YDOT =       -4963
334764  meter/sec
 ZDOT =     -13487
072401                 ZDOT =       -4110
859668


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
54434781  
00010596  00000-0  82463-4 0  9008
2 25544  51
6427 291
6481 0008559 326
9467  33
1159 15
70676355 24308


Satellite: ISS
Catalog Number: 25544
Epoch time:      09030
54434781   =   yrday
fracday
Element set:     900
Inclination:       51
6427  deg
RA of node:       291
6481  deg
Eccentricity:     
0008559     
Arg of perigee:   326
9467  deg
Mean anomaly:      33
1159  deg
Mean motion:   15
70676355  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2430
Checksum:              316


Coasting Arc #2 (Orbit 2445)
---------------------------------------

Vector Time (GMT): 2009/031/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2235761
52                 A    =         6733497
19  meter
 Y    =        4683490
40  meter          E    =           
0011784
 Z    =        4292367
98                 I    =           51
31785
 XDOT =      -4392
023369                 Wp   =           25
42476
 YDOT =       5282
045723  meter/sec      RA   =          285
94906  deg
 ZDOT =      -3461
662555                 TA   =           99
84477
                                          MA   =           99
71170
                                          Ha   =            195
978  n
mi
                                          Hp   =            189
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7335175
60                 X    =         2162372
53
 Y    =       15365782
15  feet           Y    =         4708081
68  meter
 Z    =       14082572
11                 Z    =         4303050
86
 XDOT =     -14409
525490                 XDOT =       -4433
945756
 YDOT =      17329
546334  feet/sec       YDOT =        5232
697140  meter/sec
 ZDOT =     -11357
160614                 ZDOT =       -3483
100575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5004081
17                 X    =        -1525243
94
 Y    =       16238491
07  feet           Y    =         4949492
08  meter
 Z    =       14124499
24                 Z    =         4305147
37
 XDOT =     -21093
275868                 XDOT =       -6429
230485
 YDOT =       3490
661611  feet/sec       YDOT =        1063
953659  meter/sec
 ZDOT =     -11440
259834                 ZDOT =       -3486
991198


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   09031
56232811  
00010596  00000-0  82463-4 0  9012
2 25544  51
6423 286
4457 0008646 331
2750  28
7934 15
70723126 24467


Satellite: ISS
Catalog Number: 25544
Epoch time:      09031
56232811   =   yrday
fracday
Element set:     901
Inclination:       51
6423  deg
RA of node:       286
4457  deg
Eccentricity:     
0008646     
Arg of perigee:   331
2750  deg
Mean anomaly:      28
7934  deg
Mean motion:   15
70723126  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2446
Checksum:              299


Coasting Arc #3 (Orbit 2461)
---------------------------------------

Vector Time (GMT): 2009/032/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2808549
06                 A    =         6739670
48  meter
 Y    =       -5745379
78  meter          E    =           
0015852
 Z    =        2094222
16                 I    =           51
33137
 XDOT =       3755
122543                 Wp   =           36
77900
 YDOT =       3848
983447  meter/sec      RA   =          280
85867  deg
 ZDOT =       5514
491138                 TA   =          346
71128
                                          MA   =          346
75298
                                          Ha   =            196
120  n
mi
                                          Hp   =            189
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9214399
82                 X    =         2862412
87
 Y    =      -18849671
20  feet           Y    =        -5713671
80  meter
 Z    =        6870807
62                 Z    =         2107996
76
 XDOT =      12319
955851                 XDOT =        3685
015359
 YDOT =      12627
898448  feet/sec       YDOT =        3890
583395  meter/sec
 ZDOT =      18092
162525                 ZDOT =        5532
563063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19349186
18                 X    =         5897631
95
 Y    =       -8067839
57  feet           Y    =        -2459077
50  meter
 Z    =        6924032
39                 Z    =         2110445
07
 XDOT =        219
694963                 XDOT =          66
963025
 YDOT =      16139
851070  feet/sec       YDOT =        4919
426606  meter/sec
 ZDOT =      18162
804073                 ZDOT =        5536
022681


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   09032
58029963  
00010596  00000-0  82463-4 0  9028
2 25544  51
6422 281
2427 0008687 335
1127  24
9615 15
70695730 24623


Satellite: ISS
Catalog Number: 25544
Epoch time:      09032
58029963   =   yrday
fracday
Element set:     902
Inclination:       51
6422  deg
RA of node:       281
2427  deg
Eccentricity:     
0008687     
Arg of perigee:   335
1127  deg
Mean anomaly:      24
9615  deg
Mean motion:   15
70695730  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2462
Checksum:              311


Coasting Arc #4 (Orbit 2476)
---------------------------------------

Vector Time (GMT): 2009/033/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3965413
52                 A    =         6729920
47  meter
 Y    =       -1783332
13  meter          E    =           
0012184
 Z    =       -5145071
88                 I    =           51
29438
 XDOT =       1731
157464                 Wp   =           61
97821
 YDOT =      -7388
918893  meter/sec      RA   =          275
69507  deg
 ZDOT =       1234
699420                 TA   =          219
85217
                                          MA   =          219
94170
                                          Ha   =            196
172  n
mi
                                          Hp   =            189
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13009886
88                 X    =        -3920183
67
 Y    =       -5850827
21  feet           Y    =        -1827422
67  meter
 Z    =      -16880157
08                 Z    =        -5164225
87
 XDOT =       5679
650474                 XDOT =        1807
655018
 YDOT =     -24241
859886  feet/sec       YDOT =       -7369
132395  meter/sec
 ZDOT =       4050
851115                 ZDOT =        1243
294946

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6035069
62                 X    =        -1839489
22
 Y    =      -12827292
84  feet           Y    =        -3909758
86  meter
 Z    =      -16954867
50                 Z    =        -5167843
61
 XDOT =      19090
534450                 XDOT =        5818
794900
 YDOT =     -14345
752112  feet/sec       YDOT =       -4372
585244  meter/sec
 ZDOT =       4083
791208                 ZDOT =        1244
739560


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   09033
53463694  
00010596  00000-0  82463-4 0  9038
2 25544  51
6419 276
3653 0008703 337
9837  22
0950 15
70738392 24771


Satellite: ISS
Catalog Number: 25544
Epoch time:      09033
53463694   =   yrday
fracday
Element set:     903
Inclination:       51
6419  deg
RA of node:       276
3653  deg
Eccentricity:     
0008703     
Arg of perigee:   337
9837  deg
Mean anomaly:      22
0950  deg
Mean motion:   15
70738392  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2477
Checksum:              329


Coasting Arc #5 (Orbit 2492)
---------------------------------------

Vector Time (GMT): 2009/034/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -101365
11                 A    =         6741573
57  meter
 Y    =        6740381
53  meter          E    =           
0005883
 Z    =         -42534
04                 I    =           51
33158
 XDOT =      -4803
647337                 Wp   =           94
70514
 YDOT =       -105
612995  meter/sec      RA   =          270
57227  deg
 ZDOT =      -6003
729031                 TA   =           85
75787
                                          MA   =           85
69064
                                          Ha   =            196
390  n
mi
                                          Hp   =            189
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -332562
69                 X    =         -176523
02
 Y    =       22114112
62  feet           Y    =         6738827
77  meter
 Z    =        -139547
39                 Z    =          -43208
71
 XDOT =     -15759
997824                 XDOT =       -4772
944575
 YDOT =       -346
499327  feet/sec       YDOT =        -159
158216  meter/sec
 ZDOT =     -19697
273725                 ZDOT =       -6026
990366

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14304972
71                 X    =        -4360155
68
 Y    =       16867475
45  feet           Y    =         5141206
52  meter
 Z    =        -141689
68                 Z    =          -43187
01
 XDOT =     -10632
883639                 XDOT =       -3240
902933
 YDOT =      -9164
351914  feet/sec       YDOT =       -2793
294463  meter/sec
 ZDOT =     -19787
862129                 ZDOT =       -6031
340377


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   09034
55258913  
00010596  00000-0  82463-4 0  9048
2 25544  51
6419 271
1633 0008558 341
5519  18
5331 15
70701126 24934


Satellite: ISS
Catalog Number: 25544
Epoch time:      09034
55258913   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:       271
1633  deg
Eccentricity:     
0008558     
Arg of perigee:   341
5519  deg
Mean anomaly:      18
5331  deg
Mean motion:   15
70701126  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2493
Checksum:              302


Coasting Arc #6 (Orbit 2505)
---------------------------------------

Vector Time (GMT): 2009/035/08:39:28
601
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3893266
70                 A    =         6731308
47  meter
 Y    =        2230104
84  meter          E    =           
0014562
 Z    =       -5029229
21                 I    =           51
29439
 XDOT =      -1877
809043                 Wp   =           42
31311
 YDOT =      -7244
035841  meter/sec      RA   =          266
27340  deg
 ZDOT =      -1750
889072                 TA   =          210
67057
                                          MA   =          210
75577
                                          Ha   =            196
553  n
mi
                                          Hp   =            189
568

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12773184
71                 X    =        -3893483
94
 Y    =        7316616
92  feet           Y    =         2186567
19  meter
 Z    =      -16500095
83                 Z    =        -5048142
86
 XDOT =      -6160
790822                 XDOT =       -1788
160071
 YDOT =     -23766
521789  feet/sec       YDOT =       -7264
533224  meter/sec
 ZDOT =      -5744
386718                 ZDOT =       -1759
794084

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5894139
02                 X    =        -1796533
57
 Y    =      -13398340
31  feet           Y    =        -4083814
13  meter
 Z    =      -16573590
30                 Z    =        -5051630
32
 XDOT =      23315
027155                 XDOT =        7106
420277
 YDOT =      -3076
409810  feet/sec       YDOT =        -937
689710  meter/sec
 ZDOT =      -5779
589031                 ZDOT =       -1761
618737


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   09035
37966978  
00010596  00000-0  82463-4 0  9057
2 25544  51
6411 266
9357 0008351 337
2770  22
8021 15
70438493 25066


Satellite: ISS
Catalog Number: 25544
Epoch time:      09035
37966978   =   yrday
fracday
Element set:     905
Inclination:       51
6411  deg
RA of node:       266
9357  deg
Eccentricity:     
0008351     
Arg of perigee:   337
2770  deg
Mean anomaly:      22
8021  deg
Mean motion:   15
70438493  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2506
Checksum:              323


Coasting Arc #7 (Orbit 2521)
---------------------------------------

Vector Time (GMT): 2009/036/08:39:28
601
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2952033
54                 A    =         6739422
83  meter
 Y    =        5478287
23  meter          E    =           
0011653
 Z    =        2585379
61                 I    =           51
32453
 XDOT =      -3547
269310                 Wp   =           65
64779
 YDOT =       4388
826485  meter/sec      RA   =          261
10508  deg
 ZDOT =      -5226
096059                 TA   =           84
91742
                                          MA   =           84
78443
                                          Ha   =            196
713  n
mi
                                          Hp   =            189
491

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9685149
40                 X    =         2877995
93
 Y    =       17973383
29  feet           Y    =         5510884
40  meter
 Z    =        8482216
57                 Z    =         2599540
95
 XDOT =     -11638
022671                 XDOT =       -3570
695252
 YDOT =      14399
037024  feet/sec       YDOT =        4349
028298  meter/sec
 ZDOT =     -17145
984447                 ZDOT =       -5243
384954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18780969
52                 X    =        -5724439
51
 Y    =        7948225
40  feet           Y    =         2422619
10  meter
 Z    =        8537770
22                 Z    =         2602312
36
 XDOT =     -12701
124947                 XDOT =       -3871
302884
 YDOT =     -11440
457940  feet/sec       YDOT =       -3487
051580  meter/sec
 ZDOT =     -17212
999258                 ZDOT =       -5246
522174


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   09036
39781405  
00010596  00000-0  82463-4 0  9061
2 25544  51
6408 261
7349 0008361 340
7672  19
3173 15
70431457 25227


Satellite: ISS
Catalog Number: 25544
Epoch time:      09036
39781405   =   yrday
fracday
Element set:     906
Inclination:       51
6408  deg
RA of node:       261
7349  deg
Eccentricity:     
0008361     
Arg of perigee:   340
7672  deg
Mean anomaly:      19
3173  deg
Mean motion:   15
70431457  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2522
Checksum:              308


Coasting Arc #8 (Orbit 2537)
---------------------------------------

Vector Time (GMT): 2009/037/08:39:28
601
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1938694
54                 A    =         6735681
82  meter
 Y    =       -5130559
62  meter          E    =           
0010738
 Z    =        3897632
73                 I    =           51
31781
 XDOT =       4510
901183                 Wp   =           54
77735
 YDOT =       4766
726490  meter/sec      RA   =          256
02158  deg
 ZDOT =       4029
129328                 TA   =          353
13003
                                          MA   =          353
14474
                                          Ha   =            196
783  n
mi
                                          Hp   =            189
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6360546
39                 X    =         1976987
66
 Y    =      -16832544
69  feet           Y    =        -5108666
22  meter
 Z    =       12787508
97                 Z    =         3907143
29
 XDOT =      14799
544563                 XDOT =        4437
691274
 YDOT =      15638
866438  feet/sec       YDOT =        4816
760342  meter/sec
 ZDOT =      13218
928242                 ZDOT =        4050
865342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16317223
59                 X    =         4973489
75
 Y    =        7523315
39  feet           Y    =         2293106
53  meter
 Z    =       12824173
92                 Z    =         3908808
21
 XDOT =     -16143
899719                 XDOT =       -4920
660634
 YDOT =      12327
004321  feet/sec       YDOT =        3757
270917  meter/sec
 ZDOT =      13303
945806                 ZDOT =        4055
042682


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   09037
41594828  
00010596  00000-0  82463-4 0  9077
2 25544  51
6408 256
5336 0008439 344
8635  15
2273 15
70445830 25388


Satellite: ISS
Catalog Number: 25544
Epoch time:      09037
41594828   =   yrday
fracday
Element set:     907
Inclination:       51
6408  deg
RA of node:       256
5336  deg
Eccentricity:     
0008439     
Arg of perigee:   344
8635  deg
Mean anomaly:      15
2273  deg
Mean motion:   15
70445830  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2538
Checksum:              325


Coasting Arc #9 (Orbit 2552)
---------------------------------------

Vector Time (GMT): 2009/038/08:39:28
601
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4522729
92                 A    =         6734162
66  meter
 Y    =       -2548002
48  meter          E    =           
0008302
 Z    =       -4292060
45                 I    =           51
32155
 XDOT =        566
741313                 Wp   =           50
92435
 YDOT =      -6839
748759  meter/sec      RA   =          250
84023  deg
 ZDOT =       3472
903441                 TA   =          254
36503
                                          MA   =          254
45666
                                          Ha   =            196
867  n
mi
                                          Hp   =            188
985

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14838352
77                 X    =        -4473052
16
 Y    =       -8359588
20  feet           Y    =        -2598300
23  meter
 Z    =      -14081563
14                 Z    =        -4313910
73
 XDOT =       1859
387510                 XDOT =         626
312153
 YDOT =     -22440
120601  feet/sec       YDOT =       -6833
078279  meter/sec
 ZDOT =      11394
040161                 ZDOT =        3475
800834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9192175
90                 X    =         2801775
21
 Y    =      -14253189
00  feet           Y    =        -4344372
01  meter
 Z    =      -14166875
23                 Z    =        -4318063
57
 XDOT =      21260
871211                 XDOT =        6480
313545
 YDOT =       2407
119394  feet/sec       YDOT =         733
689991  meter/sec
 ZDOT =      11404
809741                 ZDOT =        3476
186009


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   09038
37043947  
00010596  00000-0  82463-4 0  9085
2 25544  51
6409 251
6577 0008532 347
9544  12
1412 15
70471011 25537


Satellite: ISS
Catalog Number: 25544
Epoch time:      09038
37043947   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       251
6577  deg
Eccentricity:     
0008532     
Arg of perigee:   347
9544  deg
Mean anomaly:      12
1412  deg
Mean motion:   15
70471011  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2553
Checksum:              302


Coasting Arc #10 (Orbit 2568)
---------------------------------------

Vector Time (GMT): 2009/039/08:39:28
601
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1049673
78                 A    =         6740440
86  meter
 Y    =        6335537
58  meter          E    =           
0004444
 Z    =       -2056940
94                 I    =           51
35321
 XDOT =      -5262
115699                 Wp   =           41
41685
 YDOT =       -921
433932  meter/sec      RA   =          245
75263  deg
 ZDOT =      -5526
929761                 TA   =          161
57282
                                          MA   =          161
55672
                                          Ha   =            197
055  n
mi
                                          Hp   =            188
936

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3443811
62                 X    =          988742
65
 Y    =       20785884
44  feet           Y    =         6346935
03  meter
 Z    =       -6748493
89                 Z    =        -2051989
55
 XDOT =     -17264
159116                 XDOT =       -5224
573055
 YDOT =      -3023
077206  feet/sec       YDOT =        -980
067848  meter/sec
 ZDOT =     -18132
971657                 ZDOT =       -5552
401112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20908917
79                 X    =        -6373038
14
 Y    =        2645107
45  feet           Y    =          806228
75  meter
 Z    =       -6728711
89                 Z    =        -2050911
38
 XDOT =       3902
839685                 XDOT =        1189
585536
 YDOT =     -15499
254121  feet/sec       YDOT =       -4724
172656  meter/sec
 ZDOT =     -18232
278615                 ZDOT =       -5557
198522


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   09039
38855446  
00010596  00000-0  82463-4 0  9093
2 25544  51
6408 246
4563 0008473 350
9755   9
1252 15
70461343 25697


Satellite: ISS
Catalog Number: 25544
Epoch time:      09039
38855446   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       246
4563  deg
Eccentricity:     
0008473     
Arg of perigee:   350
9755  deg
Mean anomaly:       9
1252  deg
Mean motion:   15
70461343  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2569
Checksum:              330


Coasting Arc #11 (Orbit 2584)
---------------------------------------

Vector Time (GMT): 2009/040/08:39:28
601
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4212329
44                 A    =         6730378
45  meter
 Y    =        -941782
65  meter          E    =           
0010958
 Z    =        5163737
55                 I    =           51
33309
 XDOT =       2941
799019                 Wp   =           12
43117
 YDOT =       7024
761153  meter/sec      RA   =          240
59431  deg
 ZDOT =      -1107
588832                 TA   =           88
25324
                                          MA   =           88
12773
                                          Ha   =            197
000  n
mi
                                          Hp   =            188
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13819978
47                 X    =         4197463
89
 Y    =       -3089838
08  feet           Y    =         -894761
07  meter
 Z    =       16941396
15                 Z    =         5184164
23
 XDOT =       9651
571586                 XDOT =        2868
408620
 YDOT =      23047
116645  feet/sec       YDOT =        7057
247717  meter/sec
 ZDOT =      -3633
821627                 ZDOT =       -1093
476293

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2773694
85                 X    =          845422
19
 Y    =       13789310
06  feet           Y    =         4202981
71  meter
 Z    =       17020909
29                 Z    =         5187973
15
 XDOT =     -22257
624598                 XDOT =       -6784
123977
 YDOT =       8938
228603  feet/sec       YDOT =        2724
372078  meter/sec
 ZDOT =      -3578
275670                 ZDOT =       -1090
658424


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   09040
40665757  
00010596  00000-0  82463-4 0  9104
2 25544  51
6405 241
2544 0008647 354
5823   5
5243 15
70538639 25856


Satellite: ISS
Catalog Number: 25544
Epoch time:      09040
40665757   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:       241
2544  deg
Eccentricity:     
0008647     
Arg of perigee:   354
5823  deg
Mean anomaly:       5
5243  deg
Mean motion:   15
70538639  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2585
Checksum:              310


Coasting Arc #12 (Orbit 2599)
---------------------------------------

Vector Time (GMT): 2009/041/08:39:28
601
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3925771
04                 A    =         6742071
21  meter
 Y    =       -5464463
47  meter          E    =           
0018990
 Z    =        -171525
48                 I    =           51
38797
 XDOT =       3819
155305                 Wp   =           24
90588
 YDOT =      -2924
465435  meter/sec      RA   =          235
47242  deg
 ZDOT =       6015
300518                 TA   =          333
22514
                                          MA   =          333
32305
                                          Ha   =            197
207  n
mi
                                          Hp   =            188
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12879826
25                 X    =        -3863541
52
 Y    =      -17928029
77  feet           Y    =        -5508015
79  meter
 Z    =        -562747
64                 Z    =         -190444
98
 XDOT =      12530
037090                 XDOT =        3822
352995
 YDOT =      -9594
702872  feet/sec       YDOT =       -2881
739382  meter/sec
 ZDOT =      19735
237919                 ZDOT =        6033
861232

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18002004
68                 X    =         5487011
03
 Y    =      -12772745
57  feet           Y    =        -3893132
85  meter
 Z    =        -636913
35                 Z    =         -194131
19
 XDOT =       8591
344103                 XDOT =        2618
641683
 YDOT =      11158
322147  feet/sec       YDOT =        3401
056590  meter/sec
 ZDOT =      19807
321511                 ZDOT =        6037
271596


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   09041
36112256  
00010596  00000-0  82463-4 0  9112
2 25544  51
6407 236
3776 0008695 358
3570   1
7561 15
70525378 26009


Satellite: ISS
Catalog Number: 25544
Epoch time:      09041
36112256   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       236
3776  deg
Eccentricity:     
0008695     
Arg of perigee:   358
3570  deg
Mean anomaly:       1
7561  deg
Mean motion:   15
70525378  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2600
Checksum:              301


Coasting Arc #13 (Orbit 2615)
---------------------------------------

Vector Time (GMT): 2009/042/08:39:28
601
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2093110
27                 A    =         6730699
39  meter
 Y    =        3871315
51  meter          E    =           
0018018
 Z    =       -5107020
03                 I    =           51
36742
 XDOT =      -5653
194293                 Wp   =           50
46972
 YDOT =      -4993
690117  meter/sec      RA   =          230
35829  deg
 ZDOT =      -1460
596191                 TA   =          205
40081
                                          MA   =          205
48948
                                          Ha   =            197
344  n
mi
                                          Hp   =            188
112

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6867159
69                 X    =        -2111436
08
 Y    =       12701166
38  feet           Y    =         3847806
43  meter
 Z    =      -16755315
06                 Z    =        -5117232
78
 XDOT =     -18547
225370                 XDOT =       -5589
838744
 YDOT =     -16383
497759  feet/sec       YDOT =       -5056
553252  meter/sec
 ZDOT =      -4791
982254                 ZDOT =       -1487
904551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12777596
24                 X    =        -3894611
33
 Y    =       -6624663
92  feet           Y    =        -2019197
56  meter
 Z    =      -16794789
51                 Z    =        -5119051
84
 XDOT =      15687
640661                 XDOT =        4781
592873
 YDOT =     -17773
621451  feet/sec       YDOT =       -5417
399818  meter/sec
 ZDOT =      -4898
809201                 ZDOT =       -1493
157044


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   09042
37920708  
00010596  00000-0  82463-4 0  9124
2 25544  51
6405 231
1755 0008804   1
8095 358
3097 15
70551080 26162


Satellite: ISS
Catalog Number: 25544
Epoch time:      09042
37920708   =   yrday
fracday
Element set:     912
Inclination:       51
6405  deg
RA of node:       231
1755  deg
Eccentricity:     
0008804     
Arg of perigee:     1
8095  deg
Mean anomaly:     358
3097  deg
Mean motion:   15
70551080  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2616
Checksum:              296

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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