Date: June 27th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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 741)
---------------------------------------

Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2607367
25                 A    =         6731043
22  meter
 Y    =       -5979252
36  meter          E    =           
0008090
 Z    =       -1670475
95                 I    =           51
33084
 XDOT =       3967
158519                 Wp   =           98
58760
 YDOT =      -3315
104750  meter/sec      RA   =          258
26546  deg
 ZDOT =       5696
173972                 TA   =          242
88589
                                          MA   =          242
96843
                                          Ha   =            192
393  n
mi
                                          Hp   =            182
161

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8554354
48                 X    =        -2532197
69
 Y    =      -19616969
68  feet           Y    =        -6007988
92  meter
 Z    =       -5480564
15                 Z    =        -1682960
67
 XDOT =      13015
611939                 XDOT =        3976
263136
 YDOT =     -10876
327921  feet/sec       YDOT =       -3270
691602  meter/sec
 ZDOT =      18688
234817                 ZDOT =        5715
467790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18978081
89                 X    =        -5784519
36
 Y    =        9863702
03  feet           Y    =         3006456
38  meter
 Z    =       -5529814
96                 Z    =        -1685487
60
 XDOT =     -11026
525144                 XDOT =       -3360
884864
 YDOT =     -10736
748123  feet/sec       YDOT =       -3272
560828  meter/sec
 ZDOT =      18763
710279                 ZDOT =        5719
178893


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   09177
50329257  
00010596  00000-0  82463-4 0  9007
2 25544  51
6408 259
0793 0008034 156
0578 204
0960 15
73961083  7425


Satellite: ISS
Catalog Number: 25544
Epoch time:      09177
50329257   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       259
0793  deg
Eccentricity:     
0008034     
Arg of perigee:   156
0578  deg
Mean anomaly:     204
0960  deg
Mean motion:   15
73961083  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             742
Checksum:              312


Coasting Arc #2 (Orbit 757)
---------------------------------------

Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3224737
62                 A    =         6721279
59  meter
 Y    =        3154193
40  meter          E    =           
0016181
 Z    =       -4994896
73                 I    =           51
30445
 XDOT =      -3548
812632                 Wp   =          105
93485
 YDOT =      -6563
570850  meter/sec      RA   =          253
13779  deg
 ZDOT =      -1863
029151                 TA   =          146
03470
                                          MA   =          145
93100
                                          Ha   =            192
235  n
mi
                                          Hp   =            182
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10579847
83                 X    =        -3235504
62
 Y    =       10348403
53  feet           Y    =         3118072
94  meter
 Z    =      -16387456
48                 Z    =        -5010588
09
 XDOT =     -11643
086062                 XDOT =       -3466
103748
 YDOT =     -21534
025097  feet/sec       YDOT =       -6602
793057  meter/sec
 ZDOT =      -6112
300363                 ZDOT =       -1880
069056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11216940
09                 X    =         3418923
34
 Y    =        9549247
32  feet           Y    =         2910610
58  meter
 Z    =      -16448814
43                 Z    =        -5013598
64
 XDOT =     -19752
052421                 XDOT =       -6020
425578
 YDOT =      12610
131212  feet/sec       YDOT =        3843
567993  meter/sec
 ZDOT =      -6179
453293                 ZDOT =       -1883
497364


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   09178
51912051  
00010596  00000-0  82463-4 0  9010
2 25544  51
6398 253
8623 0008105 160
1699 199
9780 15
73996256  7585


Satellite: ISS
Catalog Number: 25544
Epoch time:      09178
51912051   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:       253
8623  deg
Eccentricity:     
0008105     
Arg of perigee:   160
1699  deg
Mean anomaly:     199
9780  deg
Mean motion:   15
73996256  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             758
Checksum:              345


Coasting Arc #3 (Orbit 773)
---------------------------------------

Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3584623
62                 A    =         6730905
41  meter
 Y    =        5454746
98  meter          E    =           
0020478
 Z    =        1593570
67                 I    =           51
34741
 XDOT =      -3368
989320                 Wp   =          133
06504
 YDOT =       3898
671056  meter/sec      RA   =          247
94904  deg
 ZDOT =      -5734
269152                 TA   =           29
25464
                                          MA   =           29
14012
                                          Ha   =            192
039  n
mi
                                          Hp   =            182
297

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11760576
18                 X    =         3515620
06
 Y    =       17896151
50  feet           Y    =         5494446
32  meter
 Z    =        5228250
23                 Z    =         1610817
72
 XDOT =     -11053
114568                 XDOT =       -3384
478661
 YDOT =      12790
915539  feet/sec       YDOT =        3860
911138  meter/sec
 ZDOT =     -18813
219003                 ZDOT =       -5750
672755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16583395
59                 X    =         5054618
98
 Y    =      -13522559
03  feet           Y    =        -4121675
99  meter
 Z    =        5296166
45                 Z    =         1614271
53
 XDOT =      12870
376789                 XDOT =        3922
890845
 YDOT =       8349
020621  feet/sec       YDOT =        2544
781485  meter/sec
 ZDOT =     -18877
328837                 ZDOT =       -5753
809829


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   09179
53493290  
00010596  00000-0  82463-4 0  9023
2 25544  51
6399 248
6453 0007976 162
5748 197
5691 15
74050708  7742


Satellite: ISS
Catalog Number: 25544
Epoch time:      09179
53493290   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       248
6453  deg
Eccentricity:     
0007976     
Arg of perigee:   162
5748  deg
Mean anomaly:     197
5691  deg
Mean motion:   15
74050708  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             774
Checksum:              355


Coasting Arc #4 (Orbit 789)
---------------------------------------

Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2642220
03                 A    =         6720979
12  meter
 Y    =       -3622787
58  meter          E    =           
0012581
 Z    =        5004115
76                 I    =           51
32654
 XDOT =       4637
461999                 Wp   =          150
17732
 YDOT =       5882
406682  meter/sec      RA   =          242
82142  deg
 ZDOT =       1797
305605                 TA   =          282
36362
                                          MA   =          282
50441
                                          Ha   =            191
884  n
mi
                                          Hp   =            182
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8668700
88                 X    =         2658225
24
 Y    =      -11885786
03  feet           Y    =        -3593151
86  meter
 Z    =       16417702
63                 Z    =         5016990
07
 XDOT =      15214
770338                 XDOT =        4562
608293
 YDOT =      19299
234521  feet/sec       YDOT =        5933
846742  meter/sec
 ZDOT =       5896
671933                 ZDOT =        1819
653266

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12834032
12                 X    =        -3911812
99
 Y    =       -7074758
67  feet           Y    =        -2156386
44  meter
 Z    =       16467988
75                 Z    =         5019442
97
 XDOT =      16808
501221                 XDOT =        5123
231172
 YDOT =     -16464
412384  feet/sec       YDOT =       -5018
352895  meter/sec
 ZDOT =       5984
618351                 ZDOT =        1824
111673


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   09180
55072927  
00010596  00000-0  82463-4 0  9038
2 25544  51
6399 243
4280 0007947 167
1954 192
9413 15
74078874  7904


Satellite: ISS
Catalog Number: 25544
Epoch time:      09180
55072927   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       243
4280  deg
Eccentricity:     
0007947     
Arg of perigee:   167
1954  deg
Mean anomaly:     192
9413  deg
Mean motion:   15
74078874  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             790
Checksum:              342


Coasting Arc #5 (Orbit 804)
---------------------------------------

Vector Time (GMT): 2009/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4479774
73                 A    =         6730946
72  meter
 Y    =       -4788590
42  meter          E    =           
0006402
 Z    =       -1527449
38                 I    =           51
37424
 XDOT =       2688
523962                 Wp   =          100
25800
 YDOT =      -4343
796024  meter/sec      RA   =          237
63493  deg
 ZDOT =       5752
202912                 TA   =          242
86078
                                          MA   =          242
92608
                                          Ha   =            191
822  n
mi
                                          Hp   =            182
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14697423
66                 X    =        -4418474
87
 Y    =      -15710598
48  feet           Y    =        -4838342
92  meter
 Z    =       -5011316
87                 Z    =        -1549063
91
 XDOT =       8820
616674                 XDOT =        2708
954014
 YDOT =     -14251
299290  feet/sec       YDOT =       -4313
617925  meter/sec
 ZDOT =      18872
056798                 ZDOT =        5765
312817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13538743
24                 X    =        -4126608
94
 Y    =       16693719
04  feet           Y    =         5088245
56  meter
 Z    =       -5096335
90                 Z    =        -1553363
18
 XDOT =     -14098
363885                 XDOT =       -4297
181312
 YDOT =      -5675
952315  feet/sec       YDOT =       -1730
030266  meter/sec
 ZDOT =      18923
229028                 ZDOT =        5767
800208


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   09181
50302643  
00010596  00000-0  82463-4 0  9046
2 25544  51
6394 238
5368 0007740 169
9758 190
1561 15
74060388  8056


Satellite: ISS
Catalog Number: 25544
Epoch time:      09181
50302643   =   yrday
fracday
Element set:     904
Inclination:       51
6394  deg
RA of node:       238
5368  deg
Eccentricity:     
0007740     
Arg of perigee:   169
9758  deg
Mean anomaly:     190
1561  deg
Mean motion:   15
74060388  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             805
Checksum:              322


Coasting Arc #6 (Orbit 820)
---------------------------------------

Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2068622
23                 A    =         6720795
96  meter
 Y    =        3936775
94  meter          E    =           
0014895
 Z    =       -5049952
88                 I    =           51
35743
 XDOT =      -5556
378362                 Wp   =          108
83886
 YDOT =      -5050
070739  meter/sec      RA   =          232
50723  deg
 ZDOT =      -1669
548277                 TA   =          145
07518
                                          MA   =          144
97737
                                          Ha   =            191
676  n
mi
                                          Hp   =            182
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6786818
33                 X    =        -2087958
35
 Y    =       12915931
56  feet           Y    =         3913536
05  meter
 Z    =      -16568086
87                 Z    =        -5060048
65
 XDOT =     -18229
587802                 XDOT =       -5491
384262
 YDOT =     -16568
473553  feet/sec       YDOT =       -5111
841756  meter/sec
 ZDOT =      -5477
520594                 ZDOT =       -1696
384146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13795932
68                 X    =         4205000
28
 Y    =        4609562
72  feet           Y    =         1404994
72  meter
 Z    =      -16607464
18                 Z    =        -5061955
08
 XDOT =     -13214
408017                 XDOT =       -4027
751564
 YDOT =      19537
789433  feet/sec       YDOT =        5955
118219  meter/sec
 ZDOT =      -5583
036861                 ZDOT =       -1701
709635


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   09182
51879537  
00010596  00000-0  82463-4 0  9050
2 25544  51
6396 233
3190 0007806 173
3889 186
7378 15
74090202  8214


Satellite: ISS
Catalog Number: 25544
Epoch time:      09182
51879537   =   yrday
fracday
Element set:     905
Inclination:       51
6396  deg
RA of node:       233
3190  deg
Eccentricity:     
0007806     
Arg of perigee:   173
3889  deg
Mean anomaly:     186
7378  deg
Mean motion:   15
74090202  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             821
Checksum:              334


Coasting Arc #7 (Orbit 836)
---------------------------------------

Vector Time (GMT): 2009/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5209943
70                 A    =         6730861
07  meter
 Y    =        4006609
14  meter          E    =           
0019241
 Z    =        1396808
44                 I    =           51
41130
 XDOT =      -2013
037175                 Wp   =          138
84810
 YDOT =       4652
943245  meter/sec      RA   =          227
32533  deg
 ZDOT =      -5807
185156                 TA   =           25
72808
                                          MA   =           25
63249
                                          Ha   =            191
413  n
mi
                                          Hp   =            182
795

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17092991
13                 X    =         5157968
44
 Y    =       13145043
11  feet           Y    =         4064578
93  meter
 Z    =        4582704
86                 Z    =         1421992
86
 XDOT =      -6604
452674                 XDOT =       -2036
707234
 YDOT =      15265
561827  feet/sec       YDOT =        4630
300932  meter/sec
 ZDOT =     -19052
444739                 ZDOT =       -5817
021219

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10017044
36                 X    =         3053195
12
 Y    =      -19071031
02  feet           Y    =        -5812850
25  meter
 Z    =        4681696
92                 Z    =         1426981
22
 XDOT =      14763
316746                 XDOT =        4499
858944
 YDOT =       3043
502140  feet/sec       YDOT =         927
659452  meter/sec
 ZDOT =     -19090
767791                 ZDOT =       -5818
866023


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   09183
53454838  
00010596  00000-0  82463-4 0  9067
2 25544  51
6397 228
1018 0007616 176
5639 183
5577 15
74153309  8374


Satellite: ISS
Catalog Number: 25544
Epoch time:      09183
53454838   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:       228
1018  deg
Eccentricity:     
0007616     
Arg of perigee:   176
5639  deg
Mean anomaly:     183
5577  deg
Mean motion:   15
74153309  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             837
Checksum:              341


Coasting Arc #8 (Orbit 852)
---------------------------------------

Vector Time (GMT): 2009/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1445532
03                 A    =         6720460
03  meter
 Y    =       -4159504
74  meter          E    =           
0011243
 Z    =        5075733
26                 I    =           51
39651
 XDOT =       6341
094076                 Wp   =          159
28693
 YDOT =       4093
110938  meter/sec      RA   =          222
19878  deg
 ZDOT =       1536
956391                 TA   =          275
85514
                                          MA   =          275
98329
                                          Ha   =            191
362  n
mi
                                          Hp   =            182
920

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4742559
17                 X    =         1467279
88
 Y    =      -13646669
08  feet           Y    =        -4143219
30  meter
 Z    =       16652668
19                 Z    =         5082807
71
 XDOT =      20804
114422                 XDOT =        6287
386667
 YDOT =      13428
841661  feet/sec       YDOT =        4163
720178  meter/sec
 ZDOT =       5042
507844                 ZDOT =        1567
631767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14277966
77                 X    =        -4351924
27
 Y    =       -1986386
74  feet           Y    =         -605450
68  meter
 Z    =       16680189
89                 Z    =         5084121
88
 XDOT =       9121
393409                 XDOT =        2780
200711
 YDOT =     -21894
646172  feet/sec       YDOT =       -6673
488153  meter/sec
 ZDOT =       5163
053472                 ZDOT =        1573
698698


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   09184
55028767  
00010596  00000-0  82463-4 0  9079
2 25544  51
6389 222
8846 0007647 179
7780 180
3388 15
74161915  8536


Satellite: ISS
Catalog Number: 25544
Epoch time:      09184
55028767   =   yrday
fracday
Element set:     907
Inclination:       51
6389  deg
RA of node:       222
8846  deg
Eccentricity:     
0007647     
Arg of perigee:   179
7780  deg
Mean anomaly:     180
3388  deg
Mean motion:   15
74161915  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             853
Checksum:              355


Coasting Arc #9 (Orbit 867)
---------------------------------------

Vector Time (GMT): 2009/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5825568
98                 A    =         6730891
32  meter
 Y    =       -3125465
82  meter          E    =           
0005002
 Z    =       -1270534
36                 I    =           51
45538
 XDOT =       1322
248187                 Wp   =           95
59115
 YDOT =      -4831
004660  meter/sec      RA   =          217
02138  deg
 ZDOT =       5840
620493                 TA   =          250
44528
                                          MA   =          250
49930
                                          Ha   =            191
213  n
mi
                                          Hp   =            183
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19112759
13                 X    =        -5784014
51
 Y    =      -10254152
94  feet           Y    =        -3190378
14  meter
 Z    =       -4168419
81                 Z    =        -1298734
59
 XDOT =       4338
084602                 XDOT =        1347
798428
 YDOT =     -15849
752821  feet/sec       YDOT =       -4816
076805  meter/sec
 ZDOT =      19162
140725                 ZDOT =        5847
105065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6110204
79                 X    =        -1862390
42
 Y    =       20788810
14  feet           Y    =         6336429
33  meter
 Z    =       -4279218
19                 Z    =        -1304305
70
 XDOT =     -14863
873664                 XDOT =       -4530
508693
 YDOT =       -431
839663  feet/sec       YDOT =        -131
624729  meter/sec
 ZDOT =      19187
313989                 ZDOT =        5848
293304


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   09185
50253013  
00010596  00000-0  82463-4 0  9080
2 25544  51
6393 217
9931 0007587 183
3810 176
7304 15
74188601  8683


Satellite: ISS
Catalog Number: 25544
Epoch time:      09185
50253013   =   yrday
fracday
Element set:     908
Inclination:       51
6393  deg
RA of node:       217
9931  deg
Eccentricity:     
0007587     
Arg of perigee:   183
3810  deg
Mean anomaly:     176
7304  deg
Mean motion:   15
74188601  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             868
Checksum:              323


Coasting Arc #10 (Orbit 883)
---------------------------------------

Vector Time (GMT): 2009/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -886817
99                 A    =         6720200
26  meter
 Y    =        4262924
66  meter          E    =           
0013756
 Z    =       -5128825
63                 I    =           51
44378
 XDOT =      -6932
471305                 Wp   =          111
34769
 YDOT =      -3051
268208  meter/sec      RA   =          211
89448  deg
 ZDOT =      -1345
254250                 TA   =          145
77481
                                          MA   =          145
68608
                                          Ha   =            191
063  n
mi
                                          Hp   =            183
230

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2909507
85                 X    =         -909506
09
 Y    =       13985973
29  feet           Y    =         4252881
92  meter
 Z    =      -16826855
74                 Z    =        -5133188
02
 XDOT =     -22744
328428                 XDOT =       -6891
301309
 YDOT =     -10010
722467  feet/sec       YDOT =       -3128
560691  meter/sec
 ZDOT =      -4413
563813                 ZDOT =       -1378
832600

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14260708
53                 X    =         4346663
96
 Y    =        -369489
64  feet           Y    =         -112620
44  meter
 Z    =      -16843735
59                 Z    =        -5133970
61
 XDOT =      -4733
907685                 XDOT =       -1442
895063
 YDOT =      23335
936001  feet/sec       YDOT =        7112
793293  meter/sec
 ZDOT =      -4545
474526                 ZDOT =       -1385
460636


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   09186
51824072  
00010596  00000-0  82463-4 0  9092
2 25544  51
6393 212
7751 0007566 187
4975 172
6076 15
74186104  8845


Satellite: ISS
Catalog Number: 25544
Epoch time:      09186
51824072   =   yrday
fracday
Element set:     909
Inclination:       51
6393  deg
RA of node:       212
7751  deg
Eccentricity:     
0007566     
Arg of perigee:   187
4975  deg
Mean anomaly:     172
6076  deg
Mean motion:   15
74186104  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             884
Checksum:              337


Coasting Arc #11 (Orbit 899)
---------------------------------------

Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6260938
72                 A    =         6731008
99  meter
 Y    =        2185971
59  meter          E    =           
0018072
 Z    =        1085083
50                 I    =           51
50517
 XDOT =       -685
715882                 Wp   =          145
63190
 YDOT =       4910
135013  meter/sec      RA   =          206
72335  deg
 ZDOT =      -5902
297478                 TA   =           22
46154
                                          MA   =           22
38252
                                          Ha   =            190
874  n
mi
                                          Hp   =            183
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20541137
54                 X    =         6230758
41
 Y    =        7171822
80  feet           Y    =         2255816
10  meter
 Z    =        3559985
23                 Z    =         1115425
95
 XDOT =      -2249
724021                 XDOT =        -711
898891
 YDOT =      16109
366839  feet/sec       YDOT =        4902
321705  meter/sec
 ZDOT =     -19364
493037                 ZDOT =       -5905
691280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2056162
04                 X    =          626718
19
 Y    =      -21639842
33  feet           Y    =        -6595823
94  meter
 Z    =        3679169
79                 Z    =         1121410
95
 XDOT =      14574
648111                 XDOT =        4442
352744
 YDOT =      -1927
450722  feet/sec       YDOT =        -587
486980  meter/sec
 ZDOT =     -19377
535536                 ZDOT =       -5906
272831


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   09187
53393673  
00010596  00000-0  82463-4 0  9105
2 25544  51
6379 207
5571 0007467 190
3651 169
7359 15
74220376  9005


Satellite: ISS
Catalog Number: 25544
Epoch time:      09187
53393673   =   yrday
fracday
Element set:     910
Inclination:       51
6379  deg
RA of node:       207
5571  deg
Eccentricity:     
0007467     
Arg of perigee:   190
3651  deg
Mean anomaly:     169
7359  deg
Mean motion:   15
74220376  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             900
Checksum:              330


Coasting Arc #12 (Orbit 915)
---------------------------------------

Vector Time (GMT): 2009/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         319600
56                 A    =         6719877
03  meter
 Y    =       -4290639
94  meter          E    =           
0009552
 Z    =        5162237
07                 I    =           51
49428
 XDOT =       7365
591235                 Wp   =          171
50104
 YDOT =       1936
710593  meter/sec      RA   =          201
59639  deg
 ZDOT =       1144
133342                 TA   =          267
50062
                                          MA   =          267
60998
                                          Ha   =            190
748  n
mi
                                          Hp   =            183
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1048558
28                 X    =          342478
61
 Y    =      -14076902
70  feet           Y    =        -4286939
03  meter
 Z    =       16936473
34                 Z    =         5163844
44
 XDOT =      24165
325574                 XDOT =        7337
829266
 YDOT =       6354
037378  feet/sec       YDOT =        2018
921501  meter/sec
 ZDOT =       3753
718315                 ZDOT =        1179
847829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13851222
91                 X    =        -4221852
74
 Y    =        2682689
95  feet           Y    =          817683
90  meter
 Z    =       16942537
94                 Z    =         5164085
56
 XDOT =        161
818075                 XDOT =          49
322149
 YDOT =     -23955
185929  feet/sec       YDOT =       -7301
540671  meter/sec
 ZDOT =       3893
988701                 ZDOT =        1186
887756


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   09188
54961781  
00010596  00000-0  82463-4 0  9119
2 25544  51
6372 202
3387 0007395 194
4658 165
6295 15
74241960  9161


Satellite: ISS
Catalog Number: 25544
Epoch time:      09188
54961781   =   yrday
fracday
Element set:     911
Inclination:       51
6372  deg
RA of node:       202
3387  deg
Eccentricity:     
0007395     
Arg of perigee:   194
4658  deg
Mean anomaly:     165
6295  deg
Mean motion:   15
74241960  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             916
Checksum:              340


Coasting Arc #13 (Orbit 930)
---------------------------------------

Vector Time (GMT): 2009/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6563230
19                 A    =         6730895
84  meter
 Y    =       -1193518
16  meter          E    =           
0003998
 Z    =        -896952
41                 I    =           51
56104
 XDOT =         80
890913                 Wp   =           80
29227
 YDOT =      -4891
599995  meter/sec      RA   =          196
43279  deg
 ZDOT =       5940
135110                 TA   =          269
91227
                                          MA   =          269
95809
                                          Ha   =            190
539  n
mi
                                          Hp   =            183
565

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21532907
46                 X    =        -6545039
12
 Y    =       -3915742
00  feet           Y    =        -1266810
17  meter
 Z    =       -2942757
24                 Z    =         -928792
09
 XDOT =        265
390134                 XDOT =         106
727972
 YDOT =     -16048
556415  feet/sec       YDOT =       -4890
551992  meter/sec
 ZDOT =      19488
632252                 ZDOT =        5940
589982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2093504
80                 X    =          638100
26
 Y    =       21768436
47  feet           Y    =         6635019
44  meter
 Z    =       -3067795
74                 Z    =         -935064
14
 XDOT =     -13895
301356                 XDOT =       -4235
287853
 YDOT =       4072
809999  feet/sec       YDOT =        1241
392488  meter/sec
 ZDOT =      19490
135291                 ZDOT =        5940
593237


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   09189
50180528  
00010596  00000-0  82463-4 0  9129
2 25544  51
6378 197
4473 0007503 197
9571 162
1329 15
74313514  9312


Satellite: ISS
Catalog Number: 25544
Epoch time:      09189
50180528   =   yrday
fracday
Element set:     912
Inclination:       51
6378  deg
RA of node:       197
4473  deg
Eccentricity:     
0007503     
Arg of perigee:   197
9571  deg
Mean anomaly:     162
1329  deg
Mean motion:   15
74313514  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             931
Checksum:              321


Coasting Arc #14 (Orbit 946)
---------------------------------------

Vector Time (GMT): 2009/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         155193
88                 A    =         6719600
89  meter
 Y    =        4250651
41  meter          E    =           
0012633
 Z    =       -5211316
63                 I    =           51
55064
 XDOT =      -7600
229657                 Wp   =          113
43361
 YDOT =       -801
445039  meter/sec      RA   =          191
30515  deg
 ZDOT =       -886
669794                 TA   =          148
14243
                                          MA   =          148
06596
                                          Ha   =            190
367  n
mi
                                          Hp   =            183
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         509166
26                 X    =          132966
03
 Y    =       13945706
73  feet           Y    =         4252263
41  meter
 Z    =      -17097495
51                 Z    =        -5210616
05
 XDOT =     -24935
136671                 XDOT =       -7586
395691
 YDOT =      -2629
412857  feet/sec       YDOT =        -886
357766  meter/sec
 ZDOT =      -2909
021633                 ZDOT =        -923
557607

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13174812
62                 X    =         4015682
89
 Y    =       -4611817
50  feet           Y    =        -1405681
97  meter
 Z    =      -17094495
93                 Z    =        -5210402
36
 XDOT =       4345
852900                 XDOT =        1324
615964
 YDOT =      23654
081965  feet/sec       YDOT =        7209
764183  meter/sec
 ZDOT =      -3053
868638                 ZDOT =        -930
819161


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   09190
51745774  
00010596  00000-0  82463-4 0  9133
2 25544  51
6371 192
2283 0007344 203
0439 157
0393 15
74274838  9478


Satellite: ISS
Catalog Number: 25544
Epoch time:      09190
51745774   =   yrday
fracday
Element set:     913
Inclination:       51
6371  deg
RA of node:       192
2283  deg
Eccentricity:     
0007344     
Arg of perigee:   203
0439  deg
Mean anomaly:     157
0393  deg
Mean motion:   15
74274838  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             947
Checksum:              321


Coasting Arc #15 (Orbit 962)
---------------------------------------

Vector Time (GMT): 2009/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6685746
00                 A    =         6731074
37  meter
 Y    =         198657
55  meter          E    =           
0016362
 Z    =         654767
27                 I    =           51
61896
 XDOT =        447
887876                 Wp   =          153
71605
 YDOT =       4823
631394  meter/sec      RA   =          186
14887  deg
 ZDOT =      -5994
442278                 TA   =           19
14456
                                          MA   =           19
08314
                                          Ha   =            190
120  n
mi
                                          Hp   =            184
001

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21934862
19                 X    =         6679846
99
 Y    =         651763
62  feet           Y    =          273388
40  meter
 Z    =        2148186
59                 Z    =          687231
79
 XDOT =       1469
448413                 XDOT =         423
035356
 YDOT =      15825
562317  feet/sec       YDOT =        4828
501786  meter/sec
 ZDOT =     -19666
805374                 ZDOT =       -5992
326192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6073295
29                 X    =        -1851140
41
 Y    =      -21074016
95  feet           Y    =        -6423360
37  meter
 Z    =        2275648
19                 Z    =          693617
57
 XDOT =      13049
041234                 XDOT =        3977
347768
 YDOT =      -5897
525778  feet/sec       YDOT =       -1797
565857  meter/sec
 ZDOT =     -19658
210360                 ZDOT =       -5991
822518


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   09191
53309538  
00010596  00000-0  82463-4 0  9141
2 25544  51
6368 187
0095 0007195 206
9041 153
1751 15
74315892  9631


Satellite: ISS
Catalog Number: 25544
Epoch time:      09191
53309538   =   yrday
fracday
Element set:     914
Inclination:       51
6368  deg
RA of node:       187
0095  deg
Eccentricity:     
0007195     
Arg of perigee:   206
9041  deg
Mean anomaly:     153
1751  deg
Mean motion:   15
74315892  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             963
Checksum:              322

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

The following information is a reminder of your current mailing list subscription:

You are subscribed to the following list: [list_name]

using the following email: example@example.com

You may automatically unsubscribe from this list at any time by visiting the following URL:

http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/

If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism

You may also change your subscription by visiting this list's main screen:

<[program_url]/list/[list]>

If you're still having trouble, please contact the list owner at:

<mailto:[list_owner_email]>

The following physical address is associated with this mailing list:

[physical_address]

Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list