Date: February 6th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9526 06 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 2492)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3769841
88                 A    =         6732045
11  meter
 Y    =       -3058364
71  meter          E    =           
0006456
 Z    =        4658302
08                 I    =           51
29933
 XDOT =       2138
317633                 Wp   =           43
62364
 YDOT =       6856
847021  meter/sec      RA   =          270
70191  deg
 ZDOT =       2773
638277                 TA   =           18
89841
                                          MA   =           18
87446
                                          Ha   =            196
341  n
mi
                                          Hp   =            188
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12368247
63                 X    =         3781131
85
 Y    =      -10034004
96  feet           Y    =        -3016145
24  meter
 Z    =       15283143
30                 Z    =         4676643
08
 XDOT =       7015
477799                 XDOT =        2048
010601
 YDOT =      22496
217259  feet/sec       YDOT =        6880
253867  meter/sec
 ZDOT =       9099
863112                 ZDOT =        2783
807097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15714571
77                 X    =         4789801
47
 Y    =        2127351
99  feet           Y    =          648416
89  meter
 Z    =       15354344
06                 Z    =         4680004
07
 XDOT =     -11535
298225                 XDOT =       -3515
958899
 YDOT =      19296
662703  feet/sec       YDOT =        5881
622792  meter/sec
 ZDOT =       9139
954170                 ZDOT =        2785
858031


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
55259493  
00010596  00000-0  82463-4 0  9008
2 25544  51
6416 271
1653 0008687 342
9361  17
1507 15
70711658 24937


Satellite: ISS
Catalog Number: 25544
Epoch time:      09034
55259493   =   yrday
fracday
Element set:     900
Inclination:       51
6416  deg
RA of node:       271
1653  deg
Eccentricity:     
0008687     
Arg of perigee:   342
9361  deg
Mean anomaly:      17
1507  deg
Mean motion:   15
70711658  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2493
Checksum:              315


Coasting Arc #2 (Orbit 2507)
---------------------------------------

Vector Time (GMT): 2009/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3055943
76                 A    =         6736637
05  meter
 Y    =       -4999205
66  meter          E    =           
0009070
 Z    =       -3317280
26                 I    =           51
31544
 XDOT =       3343
001982                 Wp   =           16
01297
 YDOT =      -5129
772470  meter/sec      RA   =          265
52068  deg
 ZDOT =       4662
648081                 TA   =          304
85159
                                          MA   =          304
93685
                                          Ha   =            196
449  n
mi
                                          Hp   =            188
727

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10026062
22                 X    =        -2983700
15
 Y    =      -16401593
38  feet           Y    =        -5032974
84  meter
 Z    =      -10883465
44                 Z    =        -3331950
72
 XDOT =      10967
854271                 XDOT =        3377
465465
 YDOT =     -16829
962172  feet/sec       YDOT =       -5092
196705  meter/sec
 ZDOT =      15297
401839                 ZDOT =        4678
971545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4869692
56                 X    =         1484282
29
 Y    =      -18562476
08  feet           Y    =        -5657842
71  meter
 Z    =      -10940959
06                 Z    =        -3334804
32
 XDOT =      18308
609686                 XDOT =        5580
464232
 YDOT =      -4228
286111  feet/sec       YDOT =       -1288
781607  meter/sec
 ZDOT =      15360
600162                 ZDOT =        4681
910929


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
50691891  
00010596  00000-0  82463-4 0  9017
2 25544  51
6411 266
2878 0008817 345
0593  15
0307 15
70742902 25080


Satellite: ISS
Catalog Number: 25544
Epoch time:      09035
50691891   =   yrday
fracday
Element set:     901
Inclination:       51
6411  deg
RA of node:       266
2878  deg
Eccentricity:     
0008817     
Arg of perigee:   345
0593  deg
Mean anomaly:      15
0307  deg
Mean motion:   15
70742902  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2508
Checksum:              307


Coasting Arc #3 (Orbit 2523)
---------------------------------------

Vector Time (GMT): 2009/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1780578
71                 A    =         6736553
52  meter
 Y    =        5573876
87  meter          E    =           
0008999
 Z    =       -3349551
39                 I    =           51
31796
 XDOT =      -4465
643431                 Wp   =           19
79814
 YDOT =      -4209
713960  meter/sec      RA   =          260
43767  deg
 ZDOT =      -4626
662884                 TA   =          199
72661
                                          MA   =          199
76144
                                          Ha   =            196
613  n
mi
                                          Hp   =            188
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5841793
68                 X    =        -1826503
16
 Y    =       18286997
60  feet           Y    =         5553708
90  meter
 Z    =      -10989341
84                 Z    =        -3358312
39
 XDOT =     -14651
061124                 XDOT =       -4395
762723
 YDOT =     -13811
397508  feet/sec       YDOT =       -4259
260278  meter/sec
 ZDOT =     -15179
340171                 ZDOT =       -4648
187204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17015171
25                 X    =        -5186224
20
 Y    =        8847747
78  feet           Y    =         2696793
52  meter
 Z    =      -11023056
54                 Z    =        -3359827
63
 XDOT =        110
328653                 XDOT =          33
628174
 YDOT =     -18823
151430  feet/sec       YDOT =       -5737
296556  meter/sec
 ZDOT =     -15263
479581                 ZDOT =       -4652
308576


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
52485242  
00010596  00000-0  82463-4 0  9022
2 25544  51
6403 261
0854 0008771 348
4408  11
6551 15
70752457 25246


Satellite: ISS
Catalog Number: 25544
Epoch time:      09036
52485242   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:       261
0854  deg
Eccentricity:     
0008771     
Arg of perigee:   348
4408  deg
Mean anomaly:      11
6551  deg
Mean motion:   15
70752457  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2524
Checksum:              298


Coasting Arc #4 (Orbit 2539)
---------------------------------------

Vector Time (GMT): 2009/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4395605
73                 A    =         6731869
47  meter
 Y    =        2145386
51  meter          E    =           
0013770
 Z    =        4625911
95                 I    =           51
30900
 XDOT =       -475
632728                 Wp   =           25
92951
 YDOT =       7134
693407  meter/sec      RA   =          255
25589  deg
 ZDOT =      -2841
538769                 TA   =           92
38750
                                          MA   =           92
22983
                                          Ha   =            196
596  n
mi
                                          Hp   =            188
225

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14421278
65                 X    =         4348817
68
 Y    =        7038669
64  feet           Y    =         2194278
75  meter
 Z    =       15176876
46                 Z    =         4647151
81
 XDOT =      -1560
474829                 XDOT =        -541
575352
 YDOT =      23407
786769  feet/sec       YDOT =        7129
006128  meter/sec
 ZDOT =      -9322
633755                 ZDOT =       -2844
008938

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5419779
19                 X    =         1651948
70
 Y    =       15020624
70  feet           Y    =         4578286
41  meter
 Z    =       15259769
15                 Z    =         4651177
64
 XDOT =     -16250
155195                 XDOT =       -4953
047304
 YDOT =      15394
793083  feet/sec       YDOT =        4692
332932  meter/sec
 ZDOT =      -9331
725793                 ZDOT =       -2844
310022


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
54277101  
00010596  00000-0  82463-4 0  9039
2 25544  51
6402 255
8823 0008882 352
1090   7
9930 15
70820797 25404


Satellite: ISS
Catalog Number: 25544
Epoch time:      09037
54277101   =   yrday
fracday
Element set:     903
Inclination:       51
6402  deg
RA of node:       255
8823  deg
Eccentricity:     
0008882     
Arg of perigee:   352
1090  deg
Mean anomaly:       7
9930  deg
Mean motion:   15
70820797  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2540
Checksum:              303


Coasting Arc #5 (Orbit 2555)
---------------------------------------

Vector Time (GMT): 2009/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1041665
20                 A    =         6740229
24  meter
 Y    =       -6470577
02  meter          E    =           
0019332
 Z    =        1520867
74                 I    =           51
34429
 XDOT =       5090
509815                 Wp   =           37
51305
 YDOT =        539
209594  meter/sec      RA   =          250
15758  deg
 ZDOT =       5757
417639                 TA   =          339
31304
                                          MA   =          339
39119
                                          Ha   =            196
703  n
mi
                                          Hp   =            188
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3417536
75                 X    =         -976620
60
 Y    =      -21228927
23  feet           Y    =        -6481861
94  meter
 Z    =        4989723
54                 Z    =         1515965
06
 XDOT =      16701
147686                 XDOT =        5056
134297
 YDOT =       1769
060349  feet/sec       YDOT =         595
942069  meter/sec
 ZDOT =      18889
165483                 ZDOT =        5782
063132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11963610
50                 X    =         3646508
48
 Y    =      -17872158
44  feet           Y    =        -5447433
89  meter
 Z    =        4970133
43                 Z    =         1514896
67
 XDOT =       9620
399534                 XDOT =        2932
297778
 YDOT =      11740
836815  feet/sec       YDOT =        3578
607061  meter/sec
 ZDOT =      18985
216085                 ZDOT =        5786
693863


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
56067720  
00010596  00000-0  82463-4 0  9047
2 25544  51
6387 250
6788 0008800 355
9079   4
2009 15
70829067 25560


Satellite: ISS
Catalog Number: 25544
Epoch time:      09038
56067720   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:       250
6788  deg
Eccentricity:     
0008800     
Arg of perigee:   355
9079  deg
Mean anomaly:       4
2009  deg
Mean motion:   15
70829067  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2556
Checksum:              327


Coasting Arc #6 (Orbit 2570)
---------------------------------------

Vector Time (GMT): 2009/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4075728
44                 A    =         6729235
95  meter
 Y    =        1178158
56  meter          E    =           
0016688
 Z    =       -5235445
69                 I    =           51
31708
 XDOT =      -2805
227583                 Wp   =           62
66346
 YDOT =      -7131
157371  meter/sec      RA   =          245
00392  deg
 ZDOT =        588
055887                 TA   =          212
90952
                                          MA   =          213
01353
                                          Ha   =            196
825  n
mi
                                          Hp   =            187
703

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13371812
47                 X    =        -4063167
90
 Y    =        3865349
60  feet           Y    =         1132651
80  meter
 Z    =      -17176659
08                 Z    =        -5255214
36
 XDOT =      -9203
502570                 XDOT =       -2728
133885
 YDOT =     -23396
185600  feet/sec       YDOT =       -7162
096021  meter/sec
 ZDOT =       1929
317215                 ZDOT =         574
615571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12446138
66                 X    =        -3793583
06
 Y    =       -6015920
73  feet           Y    =        -1833652
64  meter
 Z    =      -17253586
40                 Z    =        -5258893
14
 XDOT =       8382
523429                 XDOT =        2554
993141
 YDOT =     -22639
676057  feet/sec       YDOT =       -6900
573262  meter/sec
 ZDOT =       1876
398168                 ZDOT =         571
926161


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
51495230  
00010596  00000-0  82463-4 0  9055
2 25544  51
6371 245
8000 0008850 359
9693    
1466 15
70838839 25713


Satellite: ISS
Catalog Number: 25544
Epoch time:      09039
51495230   =   yrday
fracday
Element set:     905
Inclination:       51
6371  deg
RA of node:       245
8000  deg
Eccentricity:     
0008850     
Arg of perigee:   359
9693  deg
Mean anomaly:        
1466  deg
Mean motion:   15
70838839  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2571
Checksum:              318


Coasting Arc #7 (Orbit 2586)
---------------------------------------

Vector Time (GMT): 2009/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3707360
89                 A    =         6740967
58  meter
 Y    =        5608230
83  meter          E    =           
0010637
 Z    =         489926
95                 I    =           51
37081
 XDOT =      -3770
503635                 Wp   =           86
87576
 YDOT =       3024
815734  meter/sec      RA   =          239
87159  deg
 ZDOT =      -5980
790784                 TA   =           87
78579
                                          MA   =           87
66399
                                          Ha   =            196
964  n
mi
                                          Hp   =            187
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12163257
51                 X    =         3641993
29
 Y    =       18399707
46  feet           Y    =         5649323
21  meter
 Z    =        1607371
89                 Z    =          507777
92
 XDOT =     -12370
418749                 XDOT =       -3774
994782
 YDOT =       9923
936135  feet/sec       YDOT =        2982
626655  meter/sec
 ZDOT =     -19622
017008                 ZDOT =       -5999
118178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2917045
55                 X    =         -889115
48
 Y    =       21857606
84  feet           Y    =         6662198
56  meter
 Z    =        1677373
24                 Z    =          511263
36
 XDOT =     -14166
658712                 XDOT =       -4317
997575
 YDOT =       -352
230393  feet/sec       YDOT =        -107
359824  meter/sec
 ZDOT =     -19693
184564                 ZDOT =       -6002
482655


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
53283102  
00010596  00000-0  82463-4 0  9063
2 25544  51
6374 240
5971 0008998   3
4327 356
6895 15
70874413 25873


Satellite: ISS
Catalog Number: 25544
Epoch time:      09040
53283102   =   yrday
fracday
Element set:     906
Inclination:       51
6374  deg
RA of node:       240
5971  deg
Eccentricity:     
0008998     
Arg of perigee:     3
4327  deg
Mean anomaly:     356
6895  deg
Mean motion:   15
70874413  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2587
Checksum:              326


Coasting Arc #8 (Orbit 2602)
---------------------------------------

Vector Time (GMT): 2009/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2190552
40                 A    =         6730140
90  meter
 Y    =       -3880847
69  meter          E    =           
0007996
 Z    =        5037118
09                 I    =           51
34875
 XDOT =       5375
817945                 Wp   =           43
56535
 YDOT =       5243
788561  meter/sec      RA   =          234
75746  deg
 ZDOT =       1706
335146                 TA   =           29
97570
                                          MA   =           29
92994
                                          Ha   =            197
049  n
mi
                                          Hp   =            187
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7186851
72                 X    =         2209317
23
 Y    =      -12732439
94  feet           Y    =        -3856246
59  meter
 Z    =       16525978
00                 Z    =         5047805
16
 XDOT =      17637
197982                 XDOT =        5308
492682
 YDOT =      17204
030711  feet/sec       YDOT =        5303
527698  meter/sec
 ZDOT =       5598
212420                 ZDOT =        1732
286372

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13622089
74                 X    =         4152012
95
 Y    =       -5180438
88  feet           Y    =        -1578997
77  meter
 Z    =       16567303
26                 Z    =         5049714
03
 XDOT =       2022
889798                 XDOT =         616
576810
 YDOT =      23504
395954  feet/sec       YDOT =        7164
139887  meter/sec
 ZDOT =       5699
761330                 ZDOT =        1737
287253


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
55069813  
00010596  00000-0  82463-4 0  9078
2 25544  51
6363 235
3922 0008935   7
8437 352
2863 15
70828459 26035


Satellite: ISS
Catalog Number: 25544
Epoch time:      09041
55069813   =   yrday
fracday
Element set:     907
Inclination:       51
6363  deg
RA of node:       235
3922  deg
Eccentricity:     
0008935     
Arg of perigee:     7
8437  deg
Mean anomaly:     352
2863  deg
Mean motion:   15
70828459  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2603
Checksum:              323


Coasting Arc #9 (Orbit 2617)
---------------------------------------

Vector Time (GMT): 2009/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5350586
56                 A    =         6738384
79  meter
 Y    =       -3277663
95  meter          E    =           
0013470
 Z    =       -2441413
06                 I    =           51
39489
 XDOT =        930
677179                 Wp   =           25
48001
 YDOT =      -5473
468002  meter/sec      RA   =          229
58995  deg
 ZDOT =       5331
469019                 TA   =          306
87379
                                          MA   =          306
99719
                                          Ha   =            197
001  n
mi
                                          Hp   =            187
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17554417
85                 X    =        -5301677
88
 Y    =      -10753490
64  feet           Y    =        -3337223
97  meter
 Z    =       -8009885
36                 Z    =        -2467286
57
 XDOT =       3053
402819                 XDOT =         965
914594
 YDOT =     -17957
572184  feet/sec       YDOT =       -5462
863345  meter/sec
 ZDOT =      17491
696257                 ZDOT =        5336
075988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6812780
73                 X    =        -2076535
57
 Y    =      -19384309
00  feet           Y    =        -5908337
38  meter
 Z    =       -8110979
82                 Z    =        -2472226
65
 XDOT =      12198
075292                 XDOT =        3717
973349
 YDOT =     -11582
508049  feet/sec       YDOT =       -3530
348453  meter/sec
 ZDOT =      17509
192737                 ZDOT =        5336
801946


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
50493243  
00010596  00000-0  82463-4 0  9083
2 25544  51
6360 230
5130 0008804  11
1707 348
9648 15
70890852 26188


Satellite: ISS
Catalog Number: 25544
Epoch time:      09042
50493243   =   yrday
fracday
Element set:     908
Inclination:       51
6360  deg
RA of node:       230
5130  deg
Eccentricity:     
0008804     
Arg of perigee:    11
1707  deg
Mean anomaly:     348
9648  deg
Mean motion:   15
70890852  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2618
Checksum:              301


Coasting Arc #10 (Orbit 2633)
---------------------------------------

Vector Time (GMT): 2009/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         678231
69                 A    =         6733583
79  meter
 Y    =        5288371
93  meter          E    =           
0014790
 Z    =       -4128715
83                 I    =           51
39903
 XDOT =      -6380
817510                 Wp   =           41
20683
 YDOT =      -2096
456180  meter/sec      RA   =          224
50725  deg
 ZDOT =      -3730
143091                 TA   =          190
36932
                                          MA   =          190
39986
                                          Ha   =            197
190  n
mi
                                          Hp   =            186
944

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2225169
57                 X    =          639101
97
 Y    =       17350301
59  feet           Y    =         5295737
30  meter
 Z    =      -13545655
60                 Z    =        -4125516
38
 XDOT =     -20934
440650                 XDOT =       -6338
780367
 YDOT =      -6878
137074  feet/sec       YDOT =       -2167
575354  meter/sec
 ZDOT =     -12238
002268                 ZDOT =       -3761
038240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8890795
19                 X    =        -2709914
38
 Y    =       15076066
04  feet           Y    =         4595184
93  meter
 Z    =      -13532742
67                 Z    =        -4124779
97
 XDOT =     -11077
510529                 XDOT =       -3376
425209
 YDOT =     -17636
028865  feet/sec       YDOT =       -5375
461598  meter/sec
 ZDOT =     -12358
573081                 ZDOT =       -3766
893075


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   09043
52277012  
00010596  00000-0  82463-4 0  9091
2 25544  51
6360 225
3094 0008935  15
8372 344
3067 15
70928661 26346


Satellite: ISS
Catalog Number: 25544
Epoch time:      09043
52277012   =   yrday
fracday
Element set:     909
Inclination:       51
6360  deg
RA of node:       225
3094  deg
Eccentricity:     
0008935     
Arg of perigee:    15
8372  deg
Mean anomaly:     344
3067  deg
Mean motion:   15
70928661  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2634
Checksum:              307


Coasting Arc #11 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2009/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5421129
60                 A    =         6733987
64  meter
 Y    =         341176
81  meter          E    =           
0017114
 Z    =        3976330
63                 I    =           51
42249
 XDOT =       2516
285046                 Wp   =           52
10084
 YDOT =       6117
752897  meter/sec      RA   =          219
32709  deg
 ZDOT =      -3933
623154                 TA   =           78
82329
                                          MA   =           78
63094
                                          Ha   =            197
156  n
mi
                                          Hp   =            186
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17785858
26                 X    =         5397595
61
 Y    =        1119346
50  feet           Y    =          401667
64  meter
 Z    =       13045704
16                 Z    =         4002608
87
 XDOT =       8255
528366                 XDOT =        2466
796826
 YDOT =      20071
367772  feet/sec       YDOT =        6145
614566  meter/sec
 ZDOT =     -12905
587775                 ZDOT =       -3921
519742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13449025
40                 X    =         4099262
94
 Y    =       11577141
23  feet           Y    =         3528712
65  meter
 Z    =       13148140
72                 Z    =         4007553
29
 XDOT =      -4621
176547                 XDOT =       -1408
534612
 YDOT =      20051
912334  feet/sec       YDOT =        6111
822879  meter/sec
 ZDOT =     -12857
902225                 ZDOT =       -3919
088598


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   09044
54059290  
00010596  00000-0  82463-4 0  9102
2 25544  51
6361 220
1048 0008814  18
8512 341
2974 15
70924274 26501


Satellite: ISS
Catalog Number: 25544
Epoch time:      09044
54059290   =   yrday
fracday
Element set:     910
Inclination:       51
6361  deg
RA of node:       220
1048  deg
Eccentricity:     
0008814     
Arg of perigee:    18
8512  deg
Mean anomaly:     341
2974  deg
Mean motion:   15
70924274  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2650
Checksum:              293


Coasting Arc #12 (Orbit 2665)
---------------------------------------

Vector Time (GMT): 2009/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3643068
47                 A    =         6737903
43  meter
 Y    =       -5008247
45  meter          E    =           
0020223
 Z    =        2623213
42                 I    =           51
45948
 XDOT =       5521
812031                 Wp   =           56
86448
 YDOT =      -1272
344117  meter/sec      RA   =          214
24804  deg
 ZDOT =       5221
346375                 TA   =          333
04602
                                          MA   =          333
15092
                                          Ha   =            197
288  n
mi
                                          Hp   =            186
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11952324
37                 X    =        -3599537
58
 Y    =      -16431258
03  feet           Y    =        -5048742
87  meter
 Z    =        8606343
24                 Z    =         2605621
54
 XDOT =      18116
181203                 XDOT =        5510
265182
 YDOT =      -4174
357338  feet/sec       YDOT =       -1210
660388  meter/sec
 ZDOT =      17130
401493                 ZDOT =        5248
142973

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          -9063
70                 X    =           -2762
61
 Y    =      -20347650
45  feet           Y    =        -6201963
86  meter
 Z    =        8537357
97                 Z    =         2602186
71
 XDOT =      15530
677895                 XDOT =        4733
750622
 YDOT =       7249
421246  feet/sec       YDOT =        2209
623596  meter/sec
 ZDOT =      17234
727533                 ZDOT =        5253
144952


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   09045
55840124  
00010596  00000-0  82463-4 0  9119
2 25544  51
6361 214
9007 0008817  23
4744 336
6819 15
70962043 26668


Satellite: ISS
Catalog Number: 25544
Epoch time:      09045
55840124   =   yrday
fracday
Element set:     911
Inclination:       51
6361  deg
RA of node:       214
9007  deg
Eccentricity:     
0008817     
Arg of perigee:    23
4744  deg
Mean anomaly:     336
6819  deg
Mean motion:   15
70962043  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2666
Checksum:              307

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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