Date: April 14th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9149 32 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 3577)
---------------------------------------

Vector Time (GMT): 2009/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3850409
08                 A    =         6729956
79  meter
 Y    =       -3650863
70  meter          E    =           
0008385
 Z    =        4143044
27                 I    =           51
30425
 XDOT =       2103
010249                 Wp   =          162
87401
 YDOT =       6415
598841  meter/sec      RA   =          277
80839  deg
 ZDOT =       3689
176671                 TA   =          249
17432
                                          MA   =          249
26415
                                          Ha   =            192
789  n
mi
                                          Hp   =            188
769

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12632575
71                 X    =         3870821
07
 Y    =      -11977899
29  feet           Y    =        -3607692
11  meter
 Z    =       13592664
93                 Z    =         4161799
31
 XDOT =       6899
639924                 XDOT =        2013
192076
 YDOT =      21048
552629  feet/sec       YDOT =        6438
613676  meter/sec
 ZDOT =      12103
598001                 ZDOT =        3699
175138

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7415002
61                 X    =         2260092
80
 Y    =      -15686950
72  feet           Y    =        -4781382
58  meter
 Z    =       13665646
48                 Z    =         4165289
05
 XDOT =      12788
836368                 XDOT =        3898
037325
 YDOT =      16651
377595  feet/sec       YDOT =        5075
339891  meter/sec
 ZDOT =      12143
078432                 ZDOT =        3701
210306


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   09103
55435772  
00010596  00000-0  82463-4 0  9001
2 25544  51
6377 278
2280 0009166 234
8722 125
1582 15
72139484 35781


Satellite: ISS
Catalog Number: 25544
Epoch time:      09103
55435772   =   yrday
fracday
Element set:     900
Inclination:       51
6377  deg
RA of node:       278
2280  deg
Eccentricity:     
0009166     
Arg of perigee:   234
8722  deg
Mean anomaly:     125
1582  deg
Mean motion:   15
72139484  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3578
Checksum:              322


Coasting Arc #2 (Orbit 3592)
---------------------------------------

Vector Time (GMT): 2009/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2717127
16                 A    =         6731555
57  meter
 Y    =       -4948276
18  meter          E    =           
0006295
 Z    =       -3670425
99                 I    =           51
30760
 XDOT =       3681
449991                 Wp   =          198
10719
 YDOT =      -5213
277808  meter/sec      RA   =          272
61150  deg
 ZDOT =       4295
104344                 TA   =          117
59532
                                          MA   =          117
53138
                                          Ha   =            192
613  n
mi
                                          Hp   =            188
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8914459
17                 X    =        -2643762
33
 Y    =      -16234501
90  feet           Y    =        -4978250
38  meter
 Z    =      -12042080
02                 Z    =        -3683447
83
 XDOT =      12078
248001                 XDOT =        3718
607096
 YDOT =     -17103
929815  feet/sec       YDOT =       -5171
902037  meter/sec
 ZDOT =      14091
549686                 ZDOT =        4313
079114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14288599
99                 X    =        -4355165
28
 Y    =      -11731455
77  feet           Y    =        -3575747
72  meter
 Z    =      -12093270
09                 Z    =        -3686028
72
 XDOT =       3849
247427                 XDOT =        1173
250616
 YDOT =     -19312
940606  feet/sec       YDOT =       -5886
584297  meter/sec
 ZDOT =      14161
379617                 ZDOT =        4316
388507


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   09104
50783041  
00010596  00000-0  82463-4 0  9013
2 25544  51
6383 273
3443 0009018 237
5316 122
4975 15
72150060 35936


Satellite: ISS
Catalog Number: 25544
Epoch time:      09104
50783041   =   yrday
fracday
Element set:     901
Inclination:       51
6383  deg
RA of node:       273
3443  deg
Eccentricity:     
0009018     
Arg of perigee:   237
5316  deg
Mean anomaly:     122
4975  deg
Mean motion:   15
72150060  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3593
Checksum:              289


Coasting Arc #3 (Orbit 3608)
---------------------------------------

Vector Time (GMT): 2009/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2437443
21                 A    =         6732480
14  meter
 Y    =        5316036
75  meter          E    =           
0005289
 Z    =       -3328225
33                 I    =           51
31126
 XDOT =      -3930
640101                 Wp   =          215
54188
 YDOT =      -4712
391299  meter/sec      RA   =          267
51836  deg
 ZDOT =      -4648
825391                 TA   =            3
77966
                                          MA   =            3
77566
                                          Ha   =            192
219  n
mi
                                          Hp   =            189
211

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7996860
93                 X    =        -2480538
86
 Y    =       17441065
44  feet           Y    =         5288538
96  meter
 Z    =      -10919374
44                 Z    =        -3340171
04
 XDOT =     -12895
800856                 XDOT =       -3855
069936
 YDOT =     -15460
601376  feet/sec       YDOT =       -4755
923352  meter/sec
 ZDOT =     -15252
051809                 ZDOT =       -4667
737111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -482538
62                 X    =         -147077
77
 Y    =       19154500
10  feet           Y    =         5838291
63  meter
 Z    =      -10965654
06                 Z    =        -3342331
36
 XDOT =     -16436
162647                 XDOT =       -5009
742375
 YDOT =      -9187
074683  feet/sec       YDOT =       -2800
220363  meter/sec
 ZDOT =     -15326
233090                 ZDOT =       -4671
435846


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   09105
52485090  
00010596  00000-0  82463-4 0  9020
2 25544  51
6385 268
1360 0008887 242
3239 117
7022 15
72190276 36090


Satellite: ISS
Catalog Number: 25544
Epoch time:      09105
52485090   =   yrday
fracday
Element set:     902
Inclination:       51
6385  deg
RA of node:       268
1360  deg
Eccentricity:     
0008887     
Arg of perigee:   242
3239  deg
Mean anomaly:     117
7022  deg
Mean motion:   15
72190276  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3609
Checksum:              310


Coasting Arc #4 (Orbit 3624)
---------------------------------------

Vector Time (GMT): 2009/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3986112
57                 A    =         6728876
51  meter
 Y    =        3160327
71  meter          E    =           
0000588
 Z    =        4404062
31                 I    =           51
30084
 XDOT =      -1735
170857                 Wp   =          132
68303
 YDOT =       6747
576442  meter/sec      RA   =          262
32319  deg
 ZDOT =      -3271
633728                 TA   =          350
31587
                                          MA   =          350
31701
                                          Ha   =            192
079  n
mi
                                          Hp   =            189
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13077797
16                 X    =         3929082
80
 Y    =       10368529
25  feet           Y    =         3204583
79  meter
 Z    =       14449023
31                 Z    =         4423288
43
 XDOT =      -5692
817772                 XDOT =       -1794
601374
 YDOT =      22137
717984  feet/sec       YDOT =        6727
840522  meter/sec
 ZDOT =     -10733
706458                 ZDOT =       -3280
207434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16088091
60                 X    =         4903650
32
 Y    =        4186469
02  feet           Y    =         1276035
76  meter
 Z    =       14524332
61                 Z    =         4427016
58
 XDOT =       4166
575487                 XDOT =        1269
972208
 YDOT =      21340
555179  feet/sec       YDOT =        6504
601219  meter/sec
 ZDOT =     -10766
714036                 ZDOT =       -3281
694438


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   09106
54185618  
00010596  00000-0  82463-4 0  9037
2 25544  51
6378 262
9266 0008963 245
5807 114
4420 15
72171803 36259


Satellite: ISS
Catalog Number: 25544
Epoch time:      09106
54185618   =   yrday
fracday
Element set:     903
Inclination:       51
6378  deg
RA of node:       262
9266  deg
Eccentricity:     
0008963     
Arg of perigee:   245
5807  deg
Mean anomaly:     114
4420  deg
Mean motion:   15
72171803  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3625
Checksum:              316


Coasting Arc #5 (Orbit 3640)
---------------------------------------

Vector Time (GMT): 2009/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         521143
92                 A    =         6734733
08  meter
 Y    =       -6280143
23  meter          E    =           
0004992
 Z    =        2370404
26                 I    =           51
32735
 XDOT =       4952
932888                 Wp   =           81
74789
 YDOT =       2438
000937  meter/sec      RA   =          257
22245  deg
 ZDOT =       5361
379550                 TA   =          305
05664
                                          MA   =          305
10345
                                          Ha   =            191
880  n
mi
                                          Hp   =            189
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1709789
78                 X    =          579815
80
 Y    =      -20604144
46  feet           Y    =        -6273987
47  meter
 Z    =        7776916
88                 Z    =         2373078
44
 XDOT =      16249
779817                 XDOT =        4899
257996
 YDOT =       7998
690738  feet/sec       YDOT =        2493
087361  meter/sec
 ZDOT =      17589
827921                 ZDOT =        5385
310571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7194813
11                 X    =        -2192979
04
 Y    =      -19378680
87  feet           Y    =        -5906621
93  meter
 Z    =        7786910
71                 Z    =         2373450
38
 XDOT =      16602
083071                 XDOT =        5060
314920
 YDOT =        953
550853  feet/sec       YDOT =         290
642300  meter/sec
 ZDOT =      17683
469791                 ZDOT =        5389
921592


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   09107
55884272  
00010596  00000-0  82463-4 0  9042
2 25544  51
6388 257
7173 0009012 249
5134 110
5061 15
72244940 36411


Satellite: ISS
Catalog Number: 25544
Epoch time:      09107
55884272   =   yrday
fracday
Element set:     904
Inclination:       51
6388  deg
RA of node:       257
7173  deg
Eccentricity:     
0009012     
Arg of perigee:   249
5134  deg
Mean anomaly:     110
5061  deg
Mean motion:   15
72244940  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3641
Checksum:              303


Coasting Arc #6 (Orbit 3655)
---------------------------------------

Vector Time (GMT): 2009/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4478156
74                 A    =         6726582
73  meter
 Y    =       -1057632
11  meter          E    =           
0006975
 Z    =       -4911659
40                 I    =           51
30820
 XDOT =       -597
699976                 Wp   =          148
44221
 YDOT =      -7369
489470  meter/sec      RA   =          252
04013  deg
 ZDOT =       2127
330042                 TA   =          142
33015
                                          MA   =          142
28129
                                          Ha   =            191
562  n
mi
                                          Hp   =            189
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14692115
28                 X    =        -4442137
32
 Y    =       -3469921
62  feet           Y    =        -1107508
10  meter
 Z    =      -16114368
10                 Z    =        -4933326
80
 XDOT =      -1960
957926                 XDOT =        -525
582877
 YDOT =     -24178
115059  feet/sec       YDOT =       -7375
770061  meter/sec
 ZDOT =       6979
429273                 ZDOT =        2124
601623

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14643855
77                 X    =        -4463447
24
 Y    =        3273969
78  feet           Y    =          997905
99  meter
 Z    =      -16199076
42                 Z    =        -4937478
49
 XDOT =     -12149
381875                 XDOT =       -3703
131595
 YDOT =     -19791
614997  feet/sec       YDOT =       -6032
484251  meter/sec
 ZDOT =       6968
233990                 ZDOT =        2123
917720


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   09108
51225470  
00010596  00000-0  82463-4 0  9059
2 25544  51
6391 252
8347 0008904 253
6448 106
3735 15
72251775 36568


Satellite: ISS
Catalog Number: 25544
Epoch time:      09108
51225470   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:       252
8347  deg
Eccentricity:     
0008904     
Arg of perigee:   253
6448  deg
Mean anomaly:     106
3735  deg
Mean motion:   15
72251775  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3656
Checksum:              317


Coasting Arc #7 (Orbit 3671)
---------------------------------------

Vector Time (GMT): 2009/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1567602
88                 A    =         6736287
46  meter
 Y    =        6406890
44  meter          E    =           
0009444
 Z    =       -1336698
50                 I    =           51
35116
 XDOT =      -5046
184497                 Wp   =          200
85513
 YDOT =         20
563843  meter/sec      RA   =          246
92471  deg
 ZDOT =      -5815
409431                 TA   =          353
87802
                                          MA   =          353
88956
                                          Ha   =            191
277  n
mi
                                          Hp   =            190
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5143054
08                 X    =         1502336
90
 Y    =       21019981
76  feet           Y    =         6424055
34  meter
 Z    =       -4385493
76                 Z    =        -1329241
73
 XDOT =     -16555
723414                 XDOT =       -5017
789149
 YDOT =         67
466678  feet/sec       YDOT =         -35
706885  meter/sec
 ZDOT =     -19079
427268                 ZDOT =       -5839
854859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14136223
63                 X    =         4308720
96
 Y    =       16392577
38  feet           Y    =         4996457
58  meter
 Z    =       -4355890
56                 Z    =        -1327675
44
 XDOT =     -13432
086969                 XDOT =       -4094
100108
 YDOT =       6484
583823  feet/sec       YDOT =        1976
501149  meter/sec
 ZDOT =     -19174
912379                 ZDOT =       -5844
513293


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   09109
52921011  
00010596  00000-0  82463-4 0  9066
2 25544  51
6388 247
6245 0008891 258
5398 101
4766 15
72288390 36727


Satellite: ISS
Catalog Number: 25544
Epoch time:      09109
52921011   =   yrday
fracday
Element set:     906
Inclination:       51
6388  deg
RA of node:       247
6245  deg
Eccentricity:     
0008891     
Arg of perigee:   258
5398  deg
Mean anomaly:     101
4766  deg
Mean motion:   15
72288390  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3672
Checksum:              333


Coasting Arc #8 (Orbit 3687)
---------------------------------------

Vector Time (GMT): 2009/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4148229
77                 A    =         6725272
42  meter
 Y    =       -1058349
07  meter          E    =           
0005873
 Z    =        5191769
21                 I    =           51
32777
 XDOT =       2948
943686                 Wp   =          276
42129
 YDOT =       7046
769739  meter/sec      RA   =          241
76042  deg
 ZDOT =       -919
960138                 TA   =          182
38662
                                          MA   =          182
38942
                                          Ha   =            190
959  n
mi
                                          Hp   =            190
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13609677
74                 X    =         4134535
33
 Y    =       -3472273
84  feet           Y    =        -1012037
54  meter
 Z    =       17033363
53                 Z    =         5211888
16
 XDOT =       9675
012094                 XDOT =        2874
395370
 YDOT =      23119
323292  feet/sec       YDOT =        7079
329696  meter/sec
 ZDOT =      -3018
241924                 ZDOT =        -905
815428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10308403
24                 X    =         3142001
31
 Y    =       -9398727
50  feet           Y    =        -2864732
14  meter
 Z    =       17111873
98                 Z    =         5215699
19
 XDOT =      18711
015408                 XDOT =        5703
117496
 YDOT =      15129
829196  feet/sec       YDOT =        4611
571939  meter/sec
 ZDOT =      -2962
456765                 ZDOT =        -902
956822


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   09110
54615058  
00010596  00000-0  82463-4 0  9072
2 25544  51
6397 242
4153 0008824 262
7876  97
2283 15
72281091 36886


Satellite: ISS
Catalog Number: 25544
Epoch time:      09110
54615058   =   yrday
fracday
Element set:     907
Inclination:       51
6397  deg
RA of node:       242
4153  deg
Eccentricity:     
0008824     
Arg of perigee:   262
7876  deg
Mean anomaly:      97
2283  deg
Mean motion:   15
72281091  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3688
Checksum:              328


Coasting Arc #9 (Orbit 3703)
---------------------------------------

Vector Time (GMT): 2009/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3514584
97                 A    =         6736924
28  meter
 Y    =       -5734556
36  meter          E    =           
0008078
 Z    =         274638
93                 I    =           51
38343
 XDOT =       4228
009267                 Wp   =            4
27369
 YDOT =      -2303
419772  meter/sec      RA   =          236
62768  deg
 ZDOT =       6006
696162                 TA   =          358
71948
                                          MA   =          358
72154
                                          Ha   =            190
705  n
mi
                                          Hp   =            190
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11530790
59                 X    =        -3451533
14
 Y    =      -18814161
28  feet           Y    =        -5773505
95  meter
 Z    =         901046
36                 Z    =          257718
34
 XDOT =      13871
421480                 XDOT =        4224
272579
 YDOT =      -7557
151482  feet/sec       YDOT =       -2256
160344  meter/sec
 ZDOT =      19707
008407                 ZDOT =        6027
227014

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19197534
25                 X    =        -5851408
44
 Y    =      -10885860
25  feet           Y    =        -3318010
21  meter
 Z    =         834509
37                 Z    =          254358
46
 XDOT =       7590
894839                 XDOT =        2313
704747
 YDOT =     -11868
968884  feet/sec       YDOT =       -3617
661716  meter/sec
 ZDOT =      19787
034587                 ZDOT =        6031
088142


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   09111
56307248  
00010596  00000-0  82463-4 0  9085
2 25544  51
6407 237
2057 0008857 267
0435  92
9714 15
72323898 37040


Satellite: ISS
Catalog Number: 25544
Epoch time:      09111
56307248   =   yrday
fracday
Element set:     908
Inclination:       51
6407  deg
RA of node:       237
2057  deg
Eccentricity:     
0008857     
Arg of perigee:   267
0435  deg
Mean anomaly:      92
9714  deg
Mean motion:   15
72323898  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3704
Checksum:              325


Coasting Arc #10 (Orbit 3718)
---------------------------------------

Vector Time (GMT): 2009/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3082884
90                 A    =         6724793
88  meter
 Y    =        2865875
16  meter          E    =           
0006155
 Z    =       -5249848
11                 I    =           51
36058
 XDOT =      -4965
755607                 Wp   =           82
23636
 YDOT =      -5870
180362  meter/sec      RA   =          231
48661  deg
 ZDOT =       -287
925281                 TA   =          185
01453
                                          MA   =          185
02070
                                          Ha   =            190
561  n
mi
                                          Hp   =            190
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10114451
78                 X    =        -3089199
33
 Y    =        9402477
55  feet           Y    =         2831365
01  meter
 Z    =      -17223911
11                 Z    =        -5264840
41
 XDOT =     -16291
849103                 XDOT =       -4898
346488
 YDOT =     -19259
121922  feet/sec       YDOT =       -5925
333448  meter/sec
 ZDOT =       -944
636750                 ZDOT =        -311
885245

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3991016
84                 X    =        -1216461
93
 Y    =       13144091
53  feet           Y    =         4006319
10  meter
 Z    =      -17282258
97                 Z    =        -5267632
53
 XDOT =     -22762
741807                 XDOT =       -6938
083703
 YDOT =      -8279
566435  feet/sec       YDOT =       -2523
611849  meter/sec
 ZDOT =      -1038
689059                 ZDOT =        -316
592425


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   09112
51642251  
00010596  00000-0  82463-4 0  9098
2 25544  51
6409 232
3228 0008887 271
4490  88
5654 15
72365068 37196


Satellite: ISS
Catalog Number: 25544
Epoch time:      09112
51642251   =   yrday
fracday
Element set:     909
Inclination:       51
6409  deg
RA of node:       232
3228  deg
Eccentricity:     
0008887     
Arg of perigee:   271
4490  deg
Mean anomaly:      88
5654  deg
Mean motion:   15
72365068  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3719
Checksum:              324


Coasting Arc #11 (Orbit 3734)
---------------------------------------

Vector Time (GMT): 2009/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5041161
45                 A    =         6736546
24  meter
 Y    =        4394285
64  meter          E    =           
0007537
 Z    =         768153
37                 I    =           51
42000
 XDOT =      -2659
116740                 Wp   =          165
08918
 YDOT =       4092
241437  meter/sec      RA   =          226
33536  deg
 ZDOT =      -5953
253129                 TA   =            6
51715
                                          MA   =            6
50736
                                          Ha   =            190
791  n
mi
                                          Hp   =            190
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16539243
61                 X    =         4987917
52
 Y    =       14416947
65  feet           Y    =         4450361
18  meter
 Z    =        2520188
21                 Z    =          792514
30
 XDOT =      -8724
136287                 XDOT =       -2675
758884
 YDOT =      13425
988967  feet/sec       YDOT =        4062
412402  meter/sec
 ZDOT =     -19531
670372                 ZDOT =       -5966
211907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21582819
81                 X    =         6578443
48
 Y    =        3884111
63  feet           Y    =         1183877
23  meter
 Z    =        2615697
45                 Z    =          797264
58
 XDOT =       -210
370333                 XDOT =         -64
120877
 YDOT =      14368
434361  feet/sec       YDOT =        4379
498793  meter/sec
 ZDOT =     -19581
981371                 ZDOT =       -5968
587922


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   09113
53331416  
00010596  00000-0  82463-4 0  9101
2 25544  51
6412 227
1130 0008899 275
0695  84
9451 15
72368831 37358


Satellite: ISS
Catalog Number: 25544
Epoch time:      09113
53331416   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:       227
1130  deg
Eccentricity:     
0008899     
Arg of perigee:   275
0695  deg
Mean anomaly:      84
9451  deg
Mean motion:   15
72368831  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3735
Checksum:              309


Coasting Arc #12 (Orbit 3750)
---------------------------------------

Vector Time (GMT): 2009/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 670564
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1463931
70                 A    =         6725302
02  meter
 Y    =       -4133190
62  meter          E    =           
0005170
 Z    =        5103930
36                 I    =           51
40486
 XDOT =       6379
915455                 Wp   =          256
54419
 YDOT =       4049
970807  meter/sec      RA   =          221
21572  deg
 ZDOT =       1449
818335                 TA   =          179
50596
                                          MA   =          179
50545
                                          Ha   =            190
907  n
mi
                                          Hp   =            189
857

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4802925
53                 X    =         1485246
40
 Y    =      -13560336
69  feet           Y    =        -4116700
86  meter
 Z    =       16745178
33                 Z    =         5111094
11
 XDOT =      20931
481153                 XDOT =        6327
110715
 YDOT =      13287
305796  feet/sec       YDOT =        4121
019513  meter/sec
 ZDOT =       4756
621835                 ZDOT =        1480
684348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3167390
13                 X    =         -965420
51
 Y    =      -13999677
66  feet           Y    =        -4267101
75  meter
 Z    =       16772849
71                 Z    =         5112364
59
 XDOT =      23747
193704                 XDOT =        7238
144641
 YDOT =        470
785471  feet/sec       YDOT =         143
495412  meter/sec
 ZDOT =       4877
522841                 ZDOT =        1486
668962


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   09114
55018810  
00010596  00000-0  82463-4 0  9115
2 25544  51
6421 221
9032 0008950 279
7808  80
2344 15
72432146 37515


Satellite: ISS
Catalog Number: 25544
Epoch time:      09114
55018810   =   yrday
fracday
Element set:     911
Inclination:       51
6421  deg
RA of node:       221
9032  deg
Eccentricity:     
0008950     
Arg of perigee:   279
7808  deg
Mean anomaly:      80
2344  deg
Mean motion:   15
72432146  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3751
Checksum:              290

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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