Date: May 7th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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 3943)
---------------------------------------

Vector Time (GMT): 2009/126/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6333856
08                 A    =         6736094
77  meter
 Y    =        2236065
66  meter          E    =           
0017492
 Z    =         321038
09                 I    =           51
77955
 XDOT =      -1313
539966                 Wp   =           17
05923
 YDOT =      -4597
743962  meter/sec      RA   =          158
39820  deg
 ZDOT =       6042
416529                 TA   =          346
42459
                                          MA   =          346
47158
                                          Ha   =            193
289  n
mi
                                          Hp   =            186
574

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20780367
73                 X    =        -6359948
97
 Y    =        7336173
41  feet           Y    =         2165090
88  meter
 Z    =        1053274
58                 Z    =          290204
32
 XDOT =      -4309
514323                 XDOT =       -1291
383108
 YDOT =     -15084
461818  feet/sec       YDOT =       -4612
308998  meter/sec
 ZDOT =      19824
201211                 ZDOT =        6036
088938

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19858085
94                 X    =         6052744
59
 Y    =        9567589
39  feet           Y    =         2916201
25  meter
 Z    =         932827
25                 Z    =          284325
75
 XDOT =      -6879
626130                 XDOT =       -2096
910044
 YDOT =      12324
781635  feet/sec       YDOT =        3756
593442  meter/sec
 ZDOT =      19799
109251                 ZDOT =        6034
768500


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   09126
81542616  
00010596  00000-0  82463-4 0  9001
2 25544  51
6386 159
0767 0009358 331
6239  28
4412 15
72615019 39446


Satellite: ISS
Catalog Number: 25544
Epoch time:      09126
81542616   =   yrday
fracday
Element set:     900
Inclination:       51
6386  deg
RA of node:       159
0767  deg
Eccentricity:     
0009358     
Arg of perigee:   331
6239  deg
Mean anomaly:      28
4412  deg
Mean motion:   15
72615019  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3944
Checksum:              317


Coasting Arc #2 (Orbit 3958)
---------------------------------------

Vector Time (GMT): 2009/127/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2011018
96                 A    =         6724024
63  meter
 Y    =        3650508
21  meter          E    =           
0014220
 Z    =       -5286272
99                 I    =           51
76646
 XDOT =      -6820
328880                 Wp   =           51
60857
 YDOT =       3551
195199  meter/sec      RA   =          153
28097  deg
 ZDOT =       -133
878065                 TA   =          217
07238
                                          MA   =          217
17069
                                          Ha   =            193
461  n
mi
                                          Hp   =            186
352

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6597831
23                 X    =         1995729
20
 Y    =       11976732
97  feet           Y    =         3672911
36  meter
 Z    =      -17343415
32                 Z    =        -5276540
22
 XDOT =     -22376
407085                 XDOT =       -6858
881666
 YDOT =      11650
902885  feet/sec       YDOT =        3474
710747  meter/sec
 ZDOT =       -439
232498                 ZDOT =        -167
105407

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3542734
89                 X    =         1079825
60
 Y    =      -13257108
96  feet           Y    =        -4040766
81  meter
 Z    =      -17305076
02                 Z    =        -5274587
17
 XDOT =      23198
334207                 XDOT =        7070
852266
 YDOT =       6978
117399  feet/sec       YDOT =        2126
930183  meter/sec
 ZDOT =       -568
960323                 ZDOT =        -173
419107


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   09127
76860376  
00010596  00000-0  82463-4 0  9013
2 25544  51
6389 154
1915 0009406 335
3228  24
7484 15
72628278 39598


Satellite: ISS
Catalog Number: 25544
Epoch time:      09127
76860376   =   yrday
fracday
Element set:     901
Inclination:       51
6389  deg
RA of node:       154
1915  deg
Eccentricity:     
0009406     
Arg of perigee:   335
3228  deg
Mean anomaly:      24
7484  deg
Mean motion:   15
72628278  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3959
Checksum:              341


Coasting Arc #3 (Orbit 3974)
---------------------------------------

Vector Time (GMT): 2009/128/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5468501
06                 A    =         6735914
42  meter
 Y    =       -3895360
08  meter          E    =           
0006966
 Z    =         539889
94                 I    =           51
83283
 XDOT =       3165
383094                 Wp   =           86
58216
 YDOT =       3600
629063  meter/sec      RA   =          148
16042  deg
 ZDOT =      -6016
212212                 TA   =           87
56643
                                          MA   =           87
48668
                                          Ha   =            193
563  n
mi
                                          Hp   =            186
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17941276
45                 X    =         5509030
45
 Y    =      -12780052
74  feet           Y    =        -3833981
53  meter
 Z    =        1771292
47                 Z    =          566554
68
 XDOT =      10385
115139                 XDOT =        3154
111302
 YDOT =      11813
087476  feet/sec       YDOT =        3635
963624  meter/sec
 ZDOT =     -19738
229043                 ZDOT =       -6000
861570

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21819808
76                 X    =        -6650677
71
 Y    =       -2955618
16  feet           Y    =         -900872
42  meter
 Z    =        1875337
95                 Z    =          571603
01
 XDOT =        215
425119                 XDOT =          65
661576
 YDOT =     -14207
330240  feet/sec       YDOT =       -4330
394257  meter/sec
 ZDOT =     -19677
916857                 ZDOT =       -5997
829058


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   09128
78531821  
00010596  00000-0  82463-4 0  9027
2 25544  51
6391 148
9805 0009382 339
4241  20
6543 15
72635754 39759


Satellite: ISS
Catalog Number: 25544
Epoch time:      09128
78531821   =   yrday
fracday
Element set:     902
Inclination:       51
6391  deg
RA of node:       148
9805  deg
Eccentricity:     
0009382     
Arg of perigee:   339
4241  deg
Mean anomaly:      20
6543  deg
Mean motion:   15
72635754  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3975
Checksum:              326


Coasting Arc #4 (Orbit 3990)
---------------------------------------

Vector Time (GMT): 2009/129/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3434800
40                 A    =         6724249
17  meter
 Y    =       -2530111
96  meter          E    =           
0006808
 Z    =        5196298
92                 I    =           51
81825
 XDOT =       5528
140588                 Wp   =            3
26306
 YDOT =      -5245
183173  meter/sec      RA   =          143
06313  deg
 ZDOT =       1106
824159                 TA   =           76
23868
                                          MA   =           76
16291
                                          Ha   =            193
675  n
mi
                                          Hp   =            185
831

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11269030
18                 X    =        -3431496
18
 Y    =       -8300892
25  feet           Y    =        -2568503
91  meter
 Z    =       17048224
81                 Z    =         5179620
11
 XDOT =      18136
944185                 XDOT =        5581
005379
 YDOT =     -17208
606212  feet/sec       YDOT =       -5183
068800  meter/sec
 ZDOT =       3631
312859                 ZDOT =        1133
808351

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2843589
41                 X    =          866726
05
 Y    =       13785378
71  feet           Y    =         4201783
43  meter
 Z    =       16982789
99                 Z    =         5176354
39
 XDOT =     -23974
298264                 XDOT =       -7307
366111
 YDOT =        368
852945  feet/sec       YDOT =         112
426378  meter/sec
 ZDOT =       3736
531852                 ZDOT =        1138
894908


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   09129
80202168  
00010596  00000-0  82463-4 0  9031
2 25544  51
6389 143
7696 0009425 342
4777  17
6059 15
72691993 39916


Satellite: ISS
Catalog Number: 25544
Epoch time:      09129
80202168   =   yrday
fracday
Element set:     903
Inclination:       51
6389  deg
RA of node:       143
7696  deg
Eccentricity:     
0009425     
Arg of perigee:   342
4777  deg
Mean anomaly:      17
6059  deg
Mean motion:   15
72691993  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3991
Checksum:              347


Coasting Arc #5 (Orbit 4005)
---------------------------------------

Vector Time (GMT): 2009/130/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4082138
43                 A    =         6735116
33  meter
 Y    =        5159326
23  meter          E    =           
0016391
 Z    =       -1394959
81                 I    =           51
87776
 XDOT =      -4578
634910                 Wp   =           10
91071
 YDOT =      -2048
875666  meter/sec      RA   =          137
92951  deg
 ZDOT =       5847
653682                 TA   =          333
80176
                                          MA   =          333
88459
                                          Ha   =            193
820  n
mi
                                          Hp   =            185
595

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13392842
62                 X    =        -4132750
91
 Y    =       16926923
33  feet           Y    =         5113394
54  meter
 Z    =       -4576639
81                 Z    =        -1414913
57
 XDOT =     -15021
768077                 XDOT =       -4583
791095
 YDOT =      -6722
033026  feet/sec       YDOT =       -2100
106108  meter/sec
 ZDOT =      19185
215491                 ZDOT =        5825
397518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21207914
47                 X    =         6464172
33
 Y    =       -3923744
67  feet           Y    =        -1195957
37  meter
 Z    =       -4654373
27                 Z    =        -1418652
97
 XDOT =       6666
561252                 XDOT =        2031
967870
 YDOT =      13481
431174  feet/sec       YDOT =        4109
140222  meter/sec
 ZDOT =      19097
984807                 ZDOT =        5821
065769


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   09130
75517578  
00010596  00000-0  82463-4 0  9042
2 25544  51
6390 138
8840 0009528 346
7516  13
3395 15
72660821 40066


Satellite: ISS
Catalog Number: 25544
Epoch time:      09130
75517578   =   yrday
fracday
Element set:     904
Inclination:       51
6390  deg
RA of node:       138
8840  deg
Eccentricity:     
0009528     
Arg of perigee:   346
7516  deg
Mean anomaly:      13
3395  deg
Mean motion:   15
72660821  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4006
Checksum:              318


Coasting Arc #6 (Orbit 4021)
---------------------------------------

Vector Time (GMT): 2009/131/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4422249
40                 A    =         6725224
89  meter
 Y    =         985173
96  meter          E    =           
0016771
 Z    =       -4983354
10                 I    =           51
86686
 XDOT =      -3741
304023                 Wp   =           40
62677
 YDOT =       6396
038985  meter/sec      RA   =          132
85017  deg
 ZDOT =      -2046
993891                 TA   =          209
53866
                                          MA   =          209
63352
                                          Ha   =            193
943  n
mi
                                          Hp   =            185
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14508692
25                 X    =         4435112
93
 Y    =        3232198
04  feet           Y    =         1034698
67  meter
 Z    =      -16349586
94                 Z    =        -4961839
13
 XDOT =     -12274
619499                 XDOT =       -3802
603475
 YDOT =      20984
379873  feet/sec       YDOT =        6353
859047  meter/sec
 ZDOT =      -6715
859224                 ZDOT =       -2065
317533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9060168
05                 X    =        -2761539
22
 Y    =      -11900040
26  feet           Y    =        -3627132
27  meter
 Z    =      -16265320
31                 Z    =        -4957669
63
 XDOT =      22027
302845                 XDOT =        6713
921907
 YDOT =      -7454
971533  feet/sec       YDOT =       -2272
275323  meter/sec
 ZDOT =      -6787
147196                 ZDOT =       -2068
722465


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   09131
77186309  
00010596  00000-0  82463-4 0  9050
2 25544  51
6400 133
6728 0009517 351
1446   8
9547 15
72704782 40228


Satellite: ISS
Catalog Number: 25544
Epoch time:      09131
77186309   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:       133
6728  deg
Eccentricity:     
0009517     
Arg of perigee:   351
1446  deg
Mean anomaly:       8
9547  deg
Mean motion:   15
72704782  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4022
Checksum:              308


Coasting Arc #7 (Orbit 4037)
---------------------------------------

Vector Time (GMT): 2009/132/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2414812
28                 A    =         6733856
58  meter
 Y    =       -5900135
48  meter          E    =           
0013296
 Z    =        2166853
31                 I    =           51
91508
 XDOT =       5354
404084                 Wp   =           68
95448
 YDOT =        151
244243  meter/sec      RA   =          127
70628  deg
 ZDOT =      -5523
557217                 TA   =           86
91261
                                          MA   =           86
76047
                                          Ha   =            194
045  n
mi
                                          Hp   =            185
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7922612
48                 X    =         2470082
82
 Y    =      -19357399
86  feet           Y    =        -5872822
88  meter
 Z    =        7109098
78                 Z    =         2178718
11
 XDOT =      17566
942534                 XDOT =        5379
147619
 YDOT =        496
208146  feet/sec       YDOT =         211
259351  meter/sec
 ZDOT =     -18121
906880                 ZDOT =       -5497
485118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18350826
62                 X    =        -5593331
96
 Y    =       10003346
08  feet           Y    =         3049019
88  meter
 Z    =        7155154
29                 Z    =         2180891
03
 XDOT =     -12641
366582                 XDOT =       -3853
088534
 YDOT =     -10227
015353  feet/sec       YDOT =       -3117
194279  meter/sec
 ZDOT =     -18019
849005                 ZDOT =       -5492
449977


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   09132
78854185  
00010596  00000-0  82463-4 0  9067
2 25544  51
6399 128
4615 0009463 354
7956   5
3106 15
72685810 40386


Satellite: ISS
Catalog Number: 25544
Epoch time:      09132
78854185   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       128
4615  deg
Eccentricity:     
0009463     
Arg of perigee:   354
7956  deg
Mean anomaly:       5
3106  deg
Mean motion:   15
72685810  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4038
Checksum:              333


Coasting Arc #8 (Orbit 4053)
---------------------------------------

Vector Time (GMT): 2009/133/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4802767
30                 A    =         6726582
00  meter
 Y    =         755317
06  meter          E    =           
0009329
 Z    =        4639711
03                 I    =           51
90860
 XDOT =       1722
892198                 Wp   =           50
56059
 YDOT =      -6922
180843  meter/sec      RA   =          122
64062  deg
 ZDOT =       2912
270103                 TA   =           10
74731
                                          MA   =           10
72739
                                          Ha   =            194
289  n
mi
                                          Hp   =            184
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15757110
56                 X    =        -4833395
47
 Y    =        2478074
33  feet           Y    =          701437
90  meter
 Z    =       15222149
06                 Z    =         4616304
71
 XDOT =       5652
533459                 XDOT =        1786
021755
 YDOT =     -22710
567070  feet/sec       YDOT =       -6902
561832  meter/sec
 ZDOT =       9554
691940                 ZDOT =        2920
792486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13975580
81                 X    =         4259757
03
 Y    =        7867025
41  feet           Y    =         2397869
35  meter
 Z    =       15130573
68                 Z    =         4611798
86
 XDOT =     -17885
515542                 XDOT =       -5451
505137
 YDOT =      13345
746886  feet/sec       YDOT =        4067
783651  meter/sec
 ZDOT =       9587
608374                 ZDOT =        2922
303033


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   09133
80521024  
00010596  00000-0  82463-4 0  9075
2 25544  51
6406 123
2501 0009549 358
6196   1
4938 15
72712783 40544


Satellite: ISS
Catalog Number: 25544
Epoch time:      09133
80521024   =   yrday
fracday
Element set:     907
Inclination:       51
6406  deg
RA of node:       123
2501  deg
Eccentricity:     
0009549     
Arg of perigee:   358
6196  deg
Mean anomaly:       1
4938  deg
Mean motion:   15
72712783  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4054
Checksum:              299


Coasting Arc #9 (Orbit 4068)
---------------------------------------

Vector Time (GMT): 2009/134/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -577273
06                 A    =         6732089
25  meter
 Y    =        6039395
17  meter          E    =           
0012318
 Z    =       -2906691
54                 I    =           51
94309
 XDOT =      -5469
955634                 Wp   =           21
39063
 YDOT =       1909
689326  meter/sec      RA   =          117
48955  deg
 ZDOT =       5072
105513                 TA   =          305
32897
                                          MA   =          305
44406
                                          Ha   =            194
252  n
mi
                                          Hp   =            184
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1893940
47                 X    =         -630643
43
 Y    =       19814288
63  feet           Y    =         6032641
68  meter
 Z    =       -9536389
58                 Z    =        -2909624
92
 XDOT =     -17946
048669                 XDOT =       -5515
543057
 YDOT =       6265
384927  feet/sec       YDOT =        1848
265640  meter/sec
 ZDOT =      16640
766119                 ZDOT =        5045
421807

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13464531
77                 X    =         4103989
28
 Y    =      -14652221
21  feet           Y    =        -4465997
02  meter
 Z    =       -9547490
16                 Z    =        -2910075
00
 XDOT =      17082
614529                 XDOT =        5206
780908
 YDOT =       4960
885810  feet/sec       YDOT =        1512
077995  meter/sec
 ZDOT =      16536
423957                 ZDOT =        5040
302022


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   09134
75832818  
00010596  00000-0  82463-4 0  9087
2 25544  51
6413 118
3648 0009619   1
6377 358
4815 15
72736528 40691


Satellite: ISS
Catalog Number: 25544
Epoch time:      09134
75832818   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       118
3648  deg
Eccentricity:     
0009619     
Arg of perigee:     1
6377  deg
Mean anomaly:     358
4815  deg
Mean motion:   15
72736528  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4069
Checksum:              338


Coasting Arc #10 (Orbit 4084)
---------------------------------------

Vector Time (GMT): 2009/135/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4610828
04                 A    =         6728177
92  meter
 Y    =       -2537659
40  meter          E    =           
0014900
 Z    =       -4206783
13                 I    =           51
94263
 XDOT =        340
085527                 Wp   =           34
09881
 YDOT =       6736
497083  meter/sec      RA   =          112
43361  deg
 ZDOT =      -3685
123700                 TA   =          198
36346
                                          MA   =          198
41730
                                          Ha   =            194
322  n
mi
                                          Hp   =            184
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15127388
59                 X    =         4659297
76
 Y    =       -8325654
18  feet           Y    =        -2485827
01  meter
 Z    =      -13801781
91                 Z    =        -4184266
14
 XDOT =       1115
766164                 XDOT =         282
633342
 YDOT =      22101
368382  feet/sec       YDOT =        6739
979240  meter/sec
 ZDOT =     -12090
300854                 ZDOT =       -3683
610463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17185087
99                 X    =        -5238014
82
 Y    =       -2290959
01  feet           Y    =         -698284
31  meter
 Z    =      -13713783
02                 Z    =        -4179961
06
 XDOT =      11959
525869                 XDOT =        3645
263485
 YDOT =     -17262
102264  feet/sec       YDOT =       -5261
488770  meter/sec
 ZDOT =     -12083
953001                 ZDOT =       -3683
188875


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   09135
77497799  
00010596  00000-0  82463-4 0  9096
2 25544  51
6414 113
1537 0009645   4
7530 355
3723 15
72748418 40859


Satellite: ISS
Catalog Number: 25544
Epoch time:      09135
77497799   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:       113
1537  deg
Eccentricity:     
0009645     
Arg of perigee:     4
7530  deg
Mean anomaly:     355
3723  deg
Mean motion:   15
72748418  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4085
Checksum:              335


Coasting Arc #11 (Orbit 4100)
---------------------------------------

Vector Time (GMT): 2009/136/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1137503
95                 A    =         6730291
01  meter
 Y    =       -5620059
25  meter          E    =           
0017083
 Z    =        3521772
03                 I    =           51
96023
 XDOT =       4901
351112                 Wp   =           53
80430
 YDOT =      -3842
131657  meter/sec      RA   =          107
27881  deg
 ZDOT =      -4523
186686                 TA   =           84
55082
                                          MA   =           84
35597
                                          Ha   =            194
433  n
mi
                                          Hp   =            184
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3731968
35                 X    =        -1091683
17
 Y    =      -18438514
59  feet           Y    =        -5632523
57  meter
 Z    =       11554370
17                 Z    =         3516356
85
 XDOT =      16080
548269                 XDOT =        4965
923119
 YDOT =     -12605
418822  feet/sec       YDOT =       -3786
960478  meter/sec
 ZDOT =     -14839
851332                 ZDOT =       -4499
219277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7556871
61                 X    =        -2303334
47
 Y    =       17242322
42  feet           Y    =         5255459
88  meter
 Z    =       11532817
83                 Z    =         3515202
87
 XDOT =     -19220
963039                 XDOT =       -5858
549534
 YDOT =       1494
195384  feet/sec       YDOT =         455
430753  meter/sec
 ZDOT =     -14746
247168                 ZDOT =       -4494
656137


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   09136
79161847  
00010596  00000-0  82463-4 0  9103
2 25544  51
6414 107
9422 0009734   9
1187 351
0151 15
72780096 41014


Satellite: ISS
Catalog Number: 25544
Epoch time:      09136
79161847   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       107
9422  deg
Eccentricity:     
0009734     
Arg of perigee:     9
1187  deg
Mean anomaly:     351
0151  deg
Mean motion:   15
72780096  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4101
Checksum:              297


Coasting Arc #12 (Orbit 4116)
---------------------------------------

Vector Time (GMT): 2009/137/18:03:29
295
Vector Time (MET): N/A
Weight (LBS)     : 657345
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3830948
29                 A    =         6729932
06  meter
 Y    =        4123523
67  meter          E    =           
0016389
 Z    =        3670014
43                 I    =           51
96612
 XDOT =      -2210
430369                 Wp   =           58
80046
 YDOT =      -5950
620238  meter/sec      RA   =          102
22605  deg
 ZDOT =       4372
650974                 TA   =          345
10325
                                          MA   =          345
15147
                                          Ha   =            194
679  n
mi
                                          Hp   =            184
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12568727
97                 X    =        -3894601
88
 Y    =       13528620
95  feet           Y    =         4080327
61  meter
 Z    =       12040729
75                 Z    =         3651249
22
 XDOT =      -7252
068141                 XDOT =       -2164
966934
 YDOT =     -19523
032276  feet/sec       YDOT =       -5975
084662  meter/sec
 ZDOT =      14345
967764                 ZDOT =        4362
022654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18065902
01                 X    =         5506486
93
 Y    =       -4046934
05  feet           Y    =        -1233505
50  meter
 Z    =       11967505
58                 Z    =         3647695
70
 XDOT =      -5245
284970                 XDOT =       -1598
762859
 YDOT =      18941
927813  feet/sec       YDOT =        5773
499597  meter/sec
 ZDOT =      14303
985465                 ZDOT =        4359
854770


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   09137
80824967  
00010596  00000-0  82463-4 0  9116
2 25544  51
6411 102
7302 0009774  12
8519 347
2891 15
72754342 41175


Satellite: ISS
Catalog Number: 25544
Epoch time:      09137
80824967   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       102
7302  deg
Eccentricity:     
0009774     
Arg of perigee:    12
8519  deg
Mean anomaly:     347
2891  deg
Mean motion:   15
72754342  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4117
Checksum:              311

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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