Date: May 2nd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 3860)
---------------------------------------

Vector Time (GMT): 2009/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4470846
59                 A    =         6728794
91  meter
 Y    =       -2874420
95  meter          E    =           
0008931
 Z    =        4129404
60                 I    =           51
60351
 XDOT =       5729
338134                 Wp   =           19
63214
 YDOT =       3511
103214  meter/sec      RA   =          185
26453  deg
 ZDOT =      -3748
438609                 TA   =          108
84903
                                          MA   =          108
75216
                                          Ha   =            192
299  n
mi
                                          Hp   =            187
926

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14668131
86                 X    =         4482596
66
 Y    =       -9430514
93  feet           Y    =        -2824359
86  meter
 Z    =       13547915
34                 Z    =         4151152
36
 XDOT =      18797
041122                 XDOT =        5707
859812
 YDOT =      11519
367500  feet/sec       YDOT =        3575
052129  meter/sec
 ZDOT =     -12298
026932                 ZDOT =       -3720
657451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5464878
24                 X    =         1665694
89
 Y    =      -16489945
35  feet           Y    =        -5026135
34  meter
 Z    =       13632737
15                 Z    =         4155258
28
 XDOT =      20720
676975                 XDOT =        6315
662342
 YDOT =      -3238
734199  feet/sec       YDOT =        -987
166184  meter/sec
 ZDOT =     -12189
132824                 ZDOT =       -3715
247685


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   09121
54096204  
00010596  00000-0  82463-4 0  9003
2 25544  51
6403 186
1014 0009090 309
3540  50
6817 15
72558114 38618


Satellite: ISS
Catalog Number: 25544
Epoch time:      09121
54096204   =   yrday
fracday
Element set:     900
Inclination:       51
6403  deg
RA of node:       186
1014  deg
Eccentricity:     
0009090     
Arg of perigee:   309
3540  deg
Mean anomaly:      50
6817  deg
Mean motion:   15
72558114  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3861
Checksum:              281


Coasting Arc #2 (Orbit 3876)
---------------------------------------

Vector Time (GMT): 2009/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5610122
36                 A    =         6732763
41  meter
 Y    =       -2313128
02  meter          E    =           
0010714
 Z    =        2899946
94                 I    =           51
64560
 XDOT =       4249
091445                 Wp   =           40
26316
 YDOT =      -3978
002774  meter/sec      RA   =          180
18793  deg
 ZDOT =       5044
790884                 TA   =          353
09310
                                          MA   =          353
10785
                                          Ha   =            192
611  n
mi
                                          Hp   =            187
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18405913
27                 X    =        -5597927
05
 Y    =       -7589002
68  feet           Y    =        -2375795
58  meter
 Z    =        9514261
62                 Z    =         2872722
50
 XDOT =      13940
588729                 XDOT =        4268
751640
 YDOT =     -13051
190205  feet/sec       YDOT =       -3930
377179  meter/sec
 ZDOT =      16551
151195                 ZDOT =        5065
480620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19043667
66                 X    =        -5804509
90
 Y    =        5977218
18  feet           Y    =         1821856
10  meter
 Z    =        9407622
65                 Z    =         2867443
38
 XDOT =       2727
485589                 XDOT =         831
337607
 YDOT =     -17499
068162  feet/sec       YDOT =       -5333
715976  meter/sec
 ZDOT =      16631
758772                 ZDOT =        5069
360074


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   09122
55774369  
00010596  00000-0  82463-4 0  9011
2 25544  51
6399 180
8909 0008917 314
2022  45
8407 15
72540059 38770


Satellite: ISS
Catalog Number: 25544
Epoch time:      09122
55774369   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:       180
8909  deg
Eccentricity:     
0008917     
Arg of perigee:   314
2022  deg
Mean anomaly:      45
8407  deg
Mean motion:   15
72540059  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3877
Checksum:              331


Coasting Arc #3 (Orbit 3891)
---------------------------------------

Vector Time (GMT): 2009/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2857110
17                 A    =         6726824
87  meter
 Y    =        3938752
10  meter          E    =           
0005338
 Z    =       -4647011
90                 I    =           51
65574
 XDOT =      -6946
331111                 Wp   =           54
59269
 YDOT =      -1667
609624  meter/sec      RA   =          175
01923  deg
 ZDOT =       2862
682081                 TA   =          243
69210
                                          MA   =          243
74695
                                          Ha   =            192
681  n
mi
                                          Hp   =            187
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9373721
01                 X    =        -2878367
18
 Y    =       12922415
02  feet           Y    =         3906683
42  meter
 Z    =      -15246102
04                 Z    =        -4660943
38
 XDOT =     -22789
800234                 XDOT =       -6941
073792
 YDOT =      -5471
160184  feet/sec       YDOT =       -1745
258188  meter/sec
 ZDOT =       9392
001578                 ZDOT =        2828
949439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1403065
16                 X    =          427654
26
 Y    =       15850290
37  feet           Y    =         4831168
51  meter
 Z    =      -15300287
13                 Z    =        -4663527
52
 XDOT =     -19719
651060                 XDOT =       -6010
549643
 YDOT =      10667
378915  feet/sec       YDOT =        3251
417093  meter/sec
 ZDOT =       9259
949456                 ZDOT =        2822
432594


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   09123
51096402  
00010596  00000-0  82463-4 0  9024
2 25544  51
6399 176
0062 0008992 318
6365  41
4116 15
72562887 38927


Satellite: ISS
Catalog Number: 25544
Epoch time:      09123
51096402   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       176
0062  deg
Eccentricity:     
0008992     
Arg of perigee:   318
6365  deg
Mean anomaly:      41
4116  deg
Mean motion:   15
72562887  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3892
Checksum:              321


Coasting Arc #4 (Orbit 3907)
---------------------------------------

Vector Time (GMT): 2009/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6375032
78                 A    =         6734323
82  meter
 Y    =         553942
50  meter          E    =           
0002474
 Z    =       -2101791
72                 I    =           51
71117
 XDOT =      -2248
463705                 Wp   =          333
03637
 YDOT =       4840
364342  meter/sec      RA   =          169
93799  deg
 ZDOT =      -5539
496780                 TA   =          230
39003
                                          MA   =          230
41188
                                          Ha   =            192
862  n
mi
                                          Hp   =            187
190

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20915461
88                 X    =         6378574
90
 Y    =        1817396
67  feet           Y    =          625251
65  meter
 Z    =       -6895642
12                 Z    =        -2070812
95
 XDOT =      -7376
849426                 XDOT =       -2275
512269
 YDOT =      15880
460441  feet/sec       YDOT =        4815
069484  meter/sec
 ZDOT =     -18174
202034                 ZDOT =       -5550
485596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16845221
56                 X    =         5134423
53
 Y    =      -12595827
53  feet           Y    =        -3839208
23  meter
 Z    =       -6774436
95                 Z    =        -2064848
38
 XDOT =       4228
992466                 XDOT =        1288
996904
 YDOT =      15461
730671  feet/sec       YDOT =        4712
735508  meter/sec
 ZDOT =     -18216
813389                 ZDOT =       -5552
484721


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   09124
52772018  
00010596  00000-0  82463-4 0  9031
2 25544  51
6406 170
7957 0008979 323
1743  36
8802 15
72595317 39088


Satellite: ISS
Catalog Number: 25544
Epoch time:      09124
52772018   =   yrday
fracday
Element set:     903
Inclination:       51
6406  deg
RA of node:       170
7957  deg
Eccentricity:     
0008979     
Arg of perigee:   323
1743  deg
Mean anomaly:      36
8802  deg
Mean motion:   15
72595317  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3908
Checksum:              329


Coasting Arc #5 (Orbit 3923)
---------------------------------------

Vector Time (GMT): 2009/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1042470
90                 A    =         6725208
66  meter
 Y    =       -4376310
69  meter          E    =           
0010767
 Z    =        5002272
07                 I    =           51
70892
 XDOT =       7436
995803                 Wp   =          358
73381
 YDOT =       -444
862638  meter/sec      RA   =          164
78418  deg
 ZDOT =      -1928
580821                 TA   =          109
94402
                                          MA   =          109
82801
                                          Ha   =            192
958  n
mi
                                          Hp   =            186
862

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3420180
11                 X    =         1067029
61
 Y    =      -14357974
72  feet           Y    =        -4364515
89  meter
 Z    =       16411653
79                 Z    =         5007396
09
 XDOT =      24399
592530                 XDOT =        7450
786416
 YDOT =      -1459
523091  feet/sec       YDOT =        -361
620690  meter/sec
 ZDOT =      -6327
364898                 ZDOT =       -1892
417921

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7299692
29                 X    =        -2224946
21
 Y    =      -12802974
34  feet           Y    =        -3902346
58  meter
 Z    =       16431366
07                 Z    =         5008280
38
 XDOT =      16025
846612                 XDOT =        4884
678047
 YDOT =     -17120
369058  feet/sec       YDOT =       -5218
288489  meter/sec
 ZDOT =      -6185
950802                 ZDOT =       -1885
477805


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   09125
54446276  
00010596  00000-0  82463-4 0  9049
2 25544  51
6396 165
5852 0009036 326
8603  33
1992 15
72623966 39242


Satellite: ISS
Catalog Number: 25544
Epoch time:      09125
54446276   =   yrday
fracday
Element set:     904
Inclination:       51
6396  deg
RA of node:       165
5852  deg
Eccentricity:     
0009036     
Arg of perigee:   326
8603  deg
Mean anomaly:      33
1992  deg
Mean motion:   15
72623966  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3924
Checksum:              331


Coasting Arc #6 (Orbit 3939)
---------------------------------------

Vector Time (GMT): 2009/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6468894
92                 A    =         6735570
89  meter
 Y    =        1339323
99  meter          E    =           
0017148
 Z    =        1255372
62                 I    =           51
77137
 XDOT =        112
942336                 Wp   =           26
63038
 YDOT =      -4979
898911  meter/sec      RA   =          159
69348  deg
 ZDOT =       5879
158057                 TA   =          347
11797
                                          MA   =          347
16172
                                          Ha   =            193
342  n
mi
                                          Hp   =            186
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21223408
53                 X    =        -6489489
16
 Y    =        4394107
57  feet           Y    =         1266869
86  meter
 Z    =        4118676
57                 Z    =         1223896
17
 XDOT =        370
545721                 XDOT =         140
059615
 YDOT =     -16338
251020  feet/sec       YDOT =       -4978
484422  meter/sec
 ZDOT =      19288
576301                 ZDOT =        5879
772509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12320397
95                 X    =        -3755257
29
 Y    =       17859096
04  feet           Y    =         5443452
47  meter
 Z    =        3995651
45                 Z    =         1217874
56
 XDOT =      -9801
262878                 XDOT =       -2987
424925
 YDOT =     -11089
412334  feet/sec       YDOT =       -3380
052879  meter/sec
 ZDOT =      19290
609663                 ZDOT =        5879
777825


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
56119608  
00010596  00000-0  82463-4 0  9059
2 25544  51
6394 160
3742 0009134 332
5306  27
5373 15
72584698 39400


Satellite: ISS
Catalog Number: 25544
Epoch time:      09126
56119608   =   yrday
fracday
Element set:     905
Inclination:       51
6394  deg
RA of node:       160
3742  deg
Eccentricity:     
0009134     
Arg of perigee:   332
5306  deg
Mean anomaly:      27
5373  deg
Mean motion:   15
72584698  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3940
Checksum:              319


Coasting Arc #7 (Orbit 3954)
---------------------------------------

Vector Time (GMT): 2009/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         821445
66                 A    =         6724291
41  meter
 Y    =        4166199
92  meter          E    =           
0012461
 Z    =       -5222134
47                 I    =           51
76182
 XDOT =      -7180
361794                 Wp   =           59
18168
 YDOT =       2590
920598  meter/sec      RA   =          154
55787  deg
 ZDOT =        945
461931                 TA   =          219
77607
                                          MA   =          219
86749
                                          Ha   =            193
351  n
mi
                                          Hp   =            186
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2695031
69                 X    =          800166
17
 Y    =       13668634
92  feet           Y    =         4175267
04  meter
 Z    =      -17132987
10                 Z    =        -5218195
32
 XDOT =     -23557
617433                 XDOT =       -7213
393217
 YDOT =       8500
395664  feet/sec       YDOT =        2510
440875  meter/sec
 ZDOT =       3101
909221                 ZDOT =         910
498880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11600439
64                 X    =         3535814
00
 Y    =        7750017
05  feet           Y    =         2362205
20  meter
 Z    =      -17117273
71                 Z    =        -5217345
03
 XDOT =     -10212
822809                 XDOT =       -3112
868392
 YDOT =      21778
897849  feet/sec       YDOT =        6638
208064  meter/sec
 ZDOT =       2965
325387                 ZDOT =         903
831178


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
51436794  
00010596  00000-0  82463-4 0  9064
2 25544  51
6400 155
4891 0009083 334
9298  25
1414 15
72623854 39551


Satellite: ISS
Catalog Number: 25544
Epoch time:      09127
51436794   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       155
4891  deg
Eccentricity:     
0009083     
Arg of perigee:   334
9298  deg
Mean anomaly:      25
1414  deg
Mean motion:   15
72623854  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3955
Checksum:              325


Coasting Arc #8 (Orbit 3970)
---------------------------------------

Vector Time (GMT): 2009/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5948092
08                 A    =         6735926
22  meter
 Y    =       -3134752
61  meter          E    =           
0004518
 Z    =        -411093
68                 I    =           51
82627
 XDOT =       1897
666185                 Wp   =           90
55371
 YDOT =       4383
983018  meter/sec      RA   =          149
45476  deg
 ZDOT =      -6029
201598                 TA   =           93
89865
                                          MA   =           93
84699
                                          Ha   =            193
435  n
mi
                                          Hp   =            186
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19514737
80                 X    =         5984700
39
 Y    =      -10284621
42  feet           Y    =        -3068032
86  meter
 Z    =       -1348732
53                 Z    =         -382108
49
 XDOT =       6225
938926                 XDOT =        1877
792119
 YDOT =      14383
146386  feet/sec       YDOT =        4405
093096  meter/sec
 ZDOT =     -19780
845138                 ZDOT =       -6020
030526

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6279190
37                 X    =         1913897
23
 Y    =      -21153313
49  feet           Y    =        -6447529
95  meter
 Z    =       -1235558
72                 Z    =         -376598
30
 XDOT =      13178
063968                 XDOT =        4016
673897
 YDOT =       5053
195616  feet/sec       YDOT =        1540
214024  meter/sec
 ZDOT =     -19744
653001                 ZDOT =       -6018
170235


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
53107421  
00010596  00000-0  82463-4 0  9070
2 25544  51
6387 150
2777 0009040 339
6397  20
4404 15
72659191 39714


Satellite: ISS
Catalog Number: 25544
Epoch time:      09128
53107421   =   yrday
fracday
Element set:     907
Inclination:       51
6387  deg
RA of node:       150
2777  deg
Eccentricity:     
0009040     
Arg of perigee:   339
6397  deg
Mean anomaly:      20
4404  deg
Mean motion:   15
72659191  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3971
Checksum:              314


Coasting Arc #9 (Orbit 3986)
---------------------------------------

Vector Time (GMT): 2009/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2432632
80                 A    =         6723852
94  meter
 Y    =       -3371188
12  meter          E    =           
0008634
 Z    =        5284757
17                 I    =           51
80986
 XDOT =       6248
529765                 Wp   =          359
07006
 YDOT =      -4498
424530  meter/sec      RA   =          144
33789  deg
 ZDOT =         15
144993                 TA   =           90
83601
                                          MA   =           90
73708
                                          Ha   =            193
608  n
mi
                                          Hp   =            185
826

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7981078
75                 X    =        -2420427
75
 Y    =      -11060328
48  feet           Y    =        -3398323
46  meter
 Z    =       17338442
16                 Z    =         5272968
54
 XDOT =      20500
425738                 XDOT =        6298
293923
 YDOT =     -14758
610663  feet/sec       YDOT =       -4428
271580  meter/sec
 ZDOT =         49
688296                 ZDOT =          45
621482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13590726
21                 X    =        -4142453
35
 Y    =       -1710581
49  feet           Y    =         -521385
24  meter
 Z    =       17292082
95                 Z    =         5270626
88
 XDOT =       3205
943478                 XDOT =         977
171572
 YDOT =     -24048
210658  feet/sec       YDOT =       -7329
894609  meter/sec
 ZDOT =        168
618388                 ZDOT =          51
394885


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
54776738  
00010596  00000-0  82463-4 0  9086
2 25544  51
6379 145
0661 0009101 343
7791  16
3079 15
72682549 39873


Satellite: ISS
Catalog Number: 25544
Epoch time:      09129
54776738   =   yrday
fracday
Element set:     908
Inclination:       51
6379  deg
RA of node:       145
0661  deg
Eccentricity:     
0009101     
Arg of perigee:   343
7791  deg
Mean anomaly:      16
3079  deg
Mean motion:   15
72682549  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3987
Checksum:              349


Coasting Arc #10 (Orbit 4001)
---------------------------------------

Vector Time (GMT): 2009/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4847346
10                 A    =         6735678
36  meter
 Y    =        4639561
01  meter          E    =           
0018042
 Z    =        -442671
07                 I    =           51
87416
 XDOT =      -3580
664199                 Wp   =           17
75000
 YDOT =      -3172
384770  meter/sec      RA   =          139
22268  deg
 ZDOT =       6040
689036                 TA   =          337
44968
                                          MA   =          337
52887
                                          Ha   =            193
571  n
mi
                                          Hp   =            185
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15903366
47                 X    =        -4896715
73
 Y    =       15221656
84  feet           Y    =         4585079
16  meter
 Z    =       -1452332
91                 Z    =         -466339
35
 XDOT =     -11747
585956                 XDOT =       -3574
269059
 YDOT =     -10408
086516  feet/sec       YDOT =       -3212
390732  meter/sec
 ZDOT =      19818
533582                 ZDOT =        6023
309036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         544599
08                 X    =          165993
80
 Y    =       22000970
31  feet           Y    =         6705895
75  meter
 Z    =       -1544632
65                 Z    =         -470804
03
 XDOT =     -14078
313061                 XDOT =       -4291
069821
 YDOT =       1717
594380  feet/sec       YDOT =         523
522767  meter/sec
 ZDOT =      19750
308889                 ZDOT =        6019
894149


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
50090564  
00010596  00000-0  82463-4 0  9091
2 25544  51
6385 140
1814 0009029 347
0444  13
0485 15
72737881 40021


Satellite: ISS
Catalog Number: 25544
Epoch time:      09130
50090564   =   yrday
fracday
Element set:     909
Inclination:       51
6385  deg
RA of node:       140
1814  deg
Eccentricity:     
0009029     
Arg of perigee:   347
0444  deg
Mean anomaly:      13
0485  deg
Mean motion:   15
72737881  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4002
Checksum:              292


Coasting Arc #11 (Orbit 4017)
---------------------------------------

Vector Time (GMT): 2009/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3701365
77                 A    =         6724130
07  meter
 Y    =        2079759
30  meter          E    =           
0016969
 Z    =       -5226860
22                 I    =           51
85575
 XDOT =      -4737
788868                 Wp   =           49
80607
 YDOT =       5976
860256  meter/sec      RA   =          134
12514  deg
 ZDOT =       -968
198992                 TA   =          210
92951
                                          MA   =          211
02956
                                          Ha   =            193
837  n
mi
                                          Hp   =            185
471

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12143588
48                 X    =         3703225
98
 Y    =        6823357
30  feet           Y    =         2121161
16  meter
 Z    =      -17148491
53                 Z    =        -5208873
94
 XDOT =     -15543
926732                 XDOT =       -4799
567592
 YDOT =      19609
121575  feet/sec       YDOT =        5923
534230  meter/sec
 ZDOT =      -3176
505879                 ZDOT =        -991
364878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13210856
60                 X    =         4026669
09
 Y    =       -4681039
56  feet           Y    =        -1426780
86  meter
 Z    =      -17077963
70                 Z    =        -5205363
34
 XDOT =       4118
942896                 XDOT =        1255
453795
 YDOT =      23646
719041  feet/sec       YDOT =        7207
519964  meter/sec
 ZDOT =      -3266
767725                 ZDOT =        -995
710803


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
51757399  
00010596  00000-0  82463-4 0  9101
2 25544  51
6377 134
9696 0009192 350
7960   9
3032 15
72705324 40186


Satellite: ISS
Catalog Number: 25544
Epoch time:      09131
51757399   =   yrday
fracday
Element set:     910
Inclination:       51
6377  deg
RA of node:       134
9696  deg
Eccentricity:     
0009192     
Arg of perigee:   350
7960  deg
Mean anomaly:       9
3032  deg
Mean motion:   15
72705324  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4018
Checksum:              317


Coasting Arc #12 (Orbit 4033)
---------------------------------------

Vector Time (GMT): 2009/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3371388
60                 A    =         6735040
58  meter
 Y    =       -5698358
71  meter          E    =           
0011272
 Z    =        1231975
92                 I    =           51
91245
 XDOT =       4716
977249                 Wp   =           79
55311
 YDOT =       1507
568798  meter/sec      RA   =          128
99587  deg
 ZDOT =      -5887
918756                 TA   =           87
00725
                                          MA   =           86
87826
                                          Ha   =            193
918  n
mi
                                          Hp   =            185
048

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11060986
22                 X    =         3428873
25
 Y    =      -18695402
59  feet           Y    =        -5660336
62  meter
 Z    =        4041915
74                 Z    =         1248493
24
 XDOT =      15475
647141                 XDOT =        4728
371557
 YDOT =       4946
091857  feet/sec       YDOT =        1560
381233  meter/sec
 ZDOT =     -19317
318754                 ZDOT =       -5864
975546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7093815
43                 X    =        -2162194
94
 Y    =      -20518712
26  feet           Y    =        -6254103
50  meter
 Z    =        4106191
29                 Z    =         1251567
11
 XDOT =      12368
322408                 XDOT =        3769
864670
 YDOT =      -8154
402250  feet/sec       YDOT =       -2485
461806  meter/sec
 ZDOT =     -19227
421420                 ZDOT =       -5860
518049


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
53422899  
00010596  00000-0  82463-4 0  9119
2 25544  51
6373 129
7575 0009357 355
0978   5
0091 15
72754621 40340


Satellite: ISS
Catalog Number: 25544
Epoch time:      09132
53422899   =   yrday
fracday
Element set:     911
Inclination:       51
6373  deg
RA of node:       129
7575  deg
Eccentricity:     
0009357     
Arg of perigee:   355
0978  deg
Mean anomaly:       5
0091  deg
Mean motion:   15
72754621  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            4034
Checksum:              319

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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