Date: July 24th 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 1164)
---------------------------------------

Vector Time (GMT): 2009/204/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2455237
20                 A    =         6731451
56  meter
 Y    =        6138072
27  meter          E    =           
0007281
 Z    =       -1242324
30                 I    =           51
94394
 XDOT =      -4895
567808                 Wp   =          356
46765
 YDOT =       -766
264232  meter/sec      RA   =          120
26130  deg
 ZDOT =       5894
564144                 TA   =          349
96718
                                          MA   =          349
98170
                                          Ha   =            187
898  n
mi
                                          Hp   =            185
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8055240
15                 X    =        -2517656
85
 Y    =       20138032
40  feet           Y    =         6110267
50  meter
 Z    =       -4075867
14                 Z    =        -1254402
49
 XDOT =     -16061
574174                 XDOT =       -4915
269483
 YDOT =      -2513
990264  feet/sec       YDOT =        -821
120146  meter/sec
 ZDOT =      19339
121208                 ZDOT =        5870
734120

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15649545
77                 X    =         4769981
55
 Y    =       15004413
82  feet           Y    =         4573345
33  meter
 Z    =       -4123010
89                 Z    =        -1256693
72
 XDOT =      -7307
882789                 XDOT =       -2227
442674
 YDOT =      12905
759954  feet/sec       YDOT =        3933
675634  meter/sec
 ZDOT =      19245
398028                 ZDOT =        5865
997319


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   09204
35660096  
00010596  00000-0  82463-4 0  9000
2 25544  51
6386 121
1570 0005998 270
4448  89
6028 15
74012378 11652


Satellite: ISS
Catalog Number: 25544
Epoch time:      09204
35660096   =   yrday
fracday
Element set:     900
Inclination:       51
6386  deg
RA of node:       121
1570  deg
Eccentricity:     
0005998     
Arg of perigee:   270
4448  deg
Mean anomaly:      89
6028  deg
Mean motion:   15
74012378  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1165
Checksum:              312


Coasting Arc #2 (Orbit 1180)
---------------------------------------

Vector Time (GMT): 2009/205/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4311668
81                 A    =         6720710
98  meter
 Y    =         316888
24  meter          E    =           
0008295
 Z    =       -5152775
14                 I    =           51
92226
 XDOT =      -2197
741124                 Wp   =           67
72056
 YDOT =       7241
790707  meter/sec      RA   =          115
16960  deg
 ZDOT =      -1392
334086                 TA   =          188
98308
                                          MA   =          188
99793
                                          Ha   =            187
928  n
mi
                                          Hp   =            186
121

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14145895
06                 X    =         4332835
57
 Y    =        1039659
60  feet           Y    =          365222
62  meter
 Z    =      -16905430
26                 Z    =        -5131778
07
 XDOT =      -7210
436760                 XDOT =       -2271
793165
 YDOT =      23759
155862  feet/sec       YDOT =        7216
800345  meter/sec
 ZDOT =      -4568
025216                 ZDOT =       -1403
189756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6089752
24                 X    =         1856156
48
 Y    =      -12918474
88  feet           Y    =        -3937551
14  meter
 Z    =      -16822863
49                 Z    =        -5127608
79
 XDOT =      18647
088065                 XDOT =        5683
632442
 YDOT =      14799
493555  feet/sec       YDOT =        4510
885635  meter/sec
 ZDOT =      -4610
304525                 ZDOT =       -1405
220819


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   09205
37242327  
00010596  00000-0  82463-4 0  9017
2 25544  51
6392 115
9398 0006137 275
3155  84
7308 15
74014705 11814


Satellite: ISS
Catalog Number: 25544
Epoch time:      09205
37242327   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       115
9398  deg
Eccentricity:     
0006137     
Arg of perigee:   275
3155  deg
Mean anomaly:      84
7308  deg
Mean motion:   15
74014705  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1181
Checksum:              301


Coasting Arc #3 (Orbit 1196)
---------------------------------------

Vector Time (GMT): 2009/206/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1373458
60                 A    =         6731444
12  meter
 Y    =       -6476871
59  meter          E    =           
0008477
 Z    =        1186953
69                 I    =           51
97044
 XDOT =       4935
514784                 Wp   =          138
12023
 YDOT =        -39
953520  meter/sec      RA   =          110
03273  deg
 ZDOT =      -5911
157023                 TA   =           28
93439
                                          MA   =           28
88742
                                          Ha   =            188
041  n
mi
                                          Hp   =            186
001

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4506097
78                 X    =         1440016
10
 Y    =      -21249578
70  feet           Y    =        -6461140
70  meter
 Z    =        3894205
02                 Z    =         1193787
08
 XDOT =      16192
633805                 XDOT =        4964
309571
 YDOT =       -131
081104  feet/sec       YDOT =          15
399685  meter/sec
 ZDOT =     -19393
559786                 ZDOT =       -5887
110764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18418540
87                 X    =        -5613971
26
 Y    =      -11506505
95  feet           Y    =        -3507183
01  meter
 Z    =        3920716
49                 Z    =         1195034
39
 XDOT =       4635
629079                 XDOT =        1412
939743
 YDOT =     -14016
072738  feet/sec       YDOT =       -4272
098971  meter/sec
 ZDOT =     -19299
020810                 ZDOT =       -5882
341543


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   09206
38823425  
00010596  00000-0  82463-4 0  9024
2 25544  51
6394 110
7230 0006199 279
9173  80
1290 15
74039233 11972


Satellite: ISS
Catalog Number: 25544
Epoch time:      09206
38823425   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:       110
7230  deg
Eccentricity:     
0006199     
Arg of perigee:   279
9173  deg
Mean anomaly:      80
1290  deg
Mean motion:   15
74039233  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1197
Checksum:              306


Coasting Arc #4 (Orbit 1212)
---------------------------------------

Vector Time (GMT): 2009/207/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4285595
22                 A    =         6720443
18  meter
 Y    =         374840
97  meter          E    =           
0002850
 Z    =        5165558
31                 I    =           51
94316
 XDOT =        936
702771                 Wp   =          248
97599
 YDOT =      -7526
670828  meter/sec      RA   =          104
94213  deg
 ZDOT =       1322
891609                 TA   =          188
41750
                                          MA   =          188
42228
                                          Ha   =            188
260  n
mi
                                          Hp   =            186
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14060351
78                 X    =        -4314561
29
 Y    =        1229793
20  feet           Y    =          326754
65  meter
 Z    =       16947369
77                 Z    =         5144668
80
 XDOT =       3073
171822                 XDOT =        1014
371383
 YDOT =     -24693
801930  feet/sec       YDOT =       -7515
761883  meter/sec
 ZDOT =       4340
195567                 ZDOT =        1327
630245

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3469296
73                 X    =        -1057441
64
 Y    =       13782100
43  feet           Y    =         4200784
21  meter
 Z    =       16865257
60                 Z    =         5140530
52
 XDOT =     -21333
042706                 XDOT =       -6502
311417
 YDOT =     -10705
174339  feet/sec       YDOT =       -3262
937138  meter/sec
 ZDOT =       4358
420535                 ZDOT =        1328
446579


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   09207
40403295  
00010596  00000-0  82463-4 0  9038
2 25544  51
6397 105
5064 0006349 283
5153  76
5302 15
74083139 12134


Satellite: ISS
Catalog Number: 25544
Epoch time:      09207
40403295   =   yrday
fracday
Element set:     903
Inclination:       51
6397  deg
RA of node:       105
5064  deg
Eccentricity:     
0006349     
Arg of perigee:   283
5153  deg
Mean anomaly:      76
5302  deg
Mean motion:   15
74083139  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1213
Checksum:              292


Coasting Arc #5 (Orbit 1227)
---------------------------------------

Vector Time (GMT): 2009/208/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -256484
23                 A    =         6731426
19  meter
 Y    =        6626237
65  meter          E    =           
0009428
 Z    =       -1120498
74                 I    =           51
98615
 XDOT =      -4845
790923                 Wp   =          358
99987
 YDOT =        813
984579  meter/sec      RA   =           99
80662  deg
 ZDOT =       5931
294371                 TA   =          348
79141
                                          MA   =          348
81239
                                          Ha   =            188
432  n
mi
                                          Hp   =            185
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -841483
68                 X    =         -325117
75
 Y    =       21739624
83  feet           Y    =         6622985
82  meter
 Z    =       -3676176
98                 Z    =        -1121910
99
 XDOT =     -15898
264184                 XDOT =       -4883
345806
 YDOT =       2670
553082  feet/sec       YDOT =         759
585720  meter/sec
 ZDOT =      19459
627203                 ZDOT =        5907
662546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20407849
28                 X    =         6220312
46
 Y    =        7536629
56  feet           Y    =         2297164
69  meter
 Z    =       -3681380
49                 Z    =        -1122084
77
 XDOT =      -1888
497007                 XDOT =        -575
613888
 YDOT =      14560
151274  feet/sec       YDOT =        4437
934108  meter/sec
 ZDOT =      19366
752742                 ZDOT =        5902
986236


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   09208
35633574  
00010596  00000-0  82463-4 0  9049
2 25544  51
6393 100
6149 0006292 287
8401  72
2075 15
74070622 12289


Satellite: ISS
Catalog Number: 25544
Epoch time:      09208
35633574   =   yrday
fracday
Element set:     904
Inclination:       51
6393  deg
RA of node:       100
6149  deg
Eccentricity:     
0006292     
Arg of perigee:   287
8401  deg
Mean anomaly:      72
2075  deg
Mean motion:   15
74070622  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1228
Checksum:              298


Coasting Arc #6 (Orbit 1243)
---------------------------------------

Vector Time (GMT): 2009/209/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4157639
87                 A    =         6720328
92  meter
 Y    =       -1026995
80  meter          E    =           
0009442
 Z    =       -5186833
33                 I    =           51
95363
 XDOT =        338
597875                 Wp   =           60
21376
 YDOT =       7588
363449  meter/sec      RA   =           94
71451  deg
 ZDOT =      -1228
162181                 TA   =          198
07561
                                          MA   =          198
10921
                                          Ha   =            188
609  n
mi
                                          Hp   =            186
045

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13640550
75                 X    =         4194011
46
 Y    =       -3369408
79  feet           Y    =         -980298
85  meter
 Z    =      -17017169
71                 Z    =        -5166547
36
 XDOT =       1110
885416                 XDOT =         259
684489
 YDOT =      24896
205542  feet/sec       YDOT =        7591
708721  meter/sec
 ZDOT =      -4029
403482                 ZDOT =       -1226
708347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         824916
25                 X    =          251434
47
 Y    =      -14122451
88  feet           Y    =        -4304523
33  meter
 Z    =      -16937457
64                 Z    =        -5162537
09
 XDOT =      23096
727464                 XDOT =        7039
882531
 YDOT =       6185
942674  feet/sec       YDOT =        1885
475327  meter/sec
 ZDOT =      -4023
298630                 ZDOT =       -1226
301423


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   09209
37211393  
00010596  00000-0  82463-4 0  9054
2 25544  51
6401  95
3974 0006341 291
9496  68
0993 15
74094451 12446


Satellite: ISS
Catalog Number: 25544
Epoch time:      09209
37211393   =   yrday
fracday
Element set:     905
Inclination:       51
6401  deg
RA of node:        95
3974  deg
Eccentricity:     
0006341     
Arg of perigee:   291
9496  deg
Mean anomaly:      68
0993  deg
Mean motion:   15
74094451  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1244
Checksum:              320


Coasting Arc #7 (Orbit 1259)
---------------------------------------

Vector Time (GMT): 2009/210/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -844886
86                 A    =         6731440
46  meter
 Y    =       -6595843
03  meter          E    =           
0007529
 Z    =        1019518
82                 I    =           51
99307
 XDOT =       4641
241358                 Wp   =          131
08149
 YDOT =      -1518
301994  meter/sec      RA   =           89
58190  deg
 ZDOT =      -5953
057204                 TA   =           37
82952
                                          MA   =           37
77663
                                          Ha   =            188
746  n
mi
                                          Hp   =            185
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2771938
52                 X    =         -776020
84
 Y    =      -21639904
94  feet           Y    =        -6604906
09  meter
 Z    =        3344878
02                 Z    =         1015581
02
 XDOT =      15227
169809                 XDOT =        4686
793057
 YDOT =      -4981
305754  feet/sec       YDOT =       -1466
145645  meter/sec
 ZDOT =     -19531
027573                 ZDOT =       -5930
399662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21563012
00                 X    =        -6572406
06
 Y    =       -3333341
22  feet           Y    =        -1016002
40  meter
 Z    =        3329067
11                 Z    =         1014699
66
 XDOT =       -764
575570                 XDOT =        -233
042634
 YDOT =     -14548
315690  feet/sec       YDOT =       -4434
326622  meter/sec
 ZDOT =     -19442
009027                 ZDOT =       -5925
924352


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   09210
38788145  
00010596  00000-0  82463-4 0  9062
2 25544  51
6408  90
1804 0006335 295
8933  64
1576 15
74101038 12602


Satellite: ISS
Catalog Number: 25544
Epoch time:      09210
38788145   =   yrday
fracday
Element set:     906
Inclination:       51
6408  deg
RA of node:        90
1804  deg
Eccentricity:     
0006335     
Arg of perigee:   295
8933  deg
Mean anomaly:      64
1576  deg
Mean motion:   15
74101038  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1260
Checksum:              304


Coasting Arc #8 (Orbit 1275)
---------------------------------------

Vector Time (GMT): 2009/211/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3936776
25                 A    =         6720033
10  meter
 Y    =        1609788
65  meter          E    =           
0002734
 Z    =        5204809
35                 I    =           51
95389
 XDOT =      -1588
149573                 Wp   =          292
02055
 YDOT =      -7452
788115  meter/sec      RA   =           84
48836  deg
 ZDOT =       1105
291497                 TA   =          147
48539
                                          MA   =          147
46855
                                          Ha   =            188
939  n
mi
                                          Hp   =            185
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12915932
57                 X    =        -3979768
47
 Y    =        5281458
81  feet           Y    =         1565524
34  meter
 Z    =       17076146
17                 Z    =         5185580
35
 XDOT =      -5210
464478                 XDOT =       -1510
062462
 YDOT =     -24451
404578  feet/sec       YDOT =       -7470
111250  meter/sec
 ZDOT =       3626
284439                 ZDOT =        1097
765149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1696241
20                 X    =          517014
32
 Y    =       13943170
66  feet           Y    =         4249878
42  meter
 Z    =       17000607
26                 Z    =         5181785
09
 XDOT =     -23951
964629                 XDOT =       -7300
558819
 YDOT =      -1465
205373  feet/sec       YDOT =        -446
594598  meter/sec
 ZDOT =       3596
330511                 ZDOT =        1096
161540


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   09211
40363597  
00010596  00000-0  82463-4 0  9077
2 25544  51
6409  84
9635 0006499 299
0784  60
9728 15
74160865 12760


Satellite: ISS
Catalog Number: 25544
Epoch time:      09211
40363597   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:        84
9635  deg
Eccentricity:     
0006499     
Arg of perigee:   299
0784  deg
Mean anomaly:      60
9728  deg
Mean motion:   15
74160865  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1276
Checksum:              347


Coasting Arc #9 (Orbit 1290)
---------------------------------------

Vector Time (GMT): 2009/212/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1922085
61                 A    =         6731456
15  meter
 Y    =        6378808
17  meter          E    =           
0011588
 Z    =        -909541
04                 I    =           51
98810
 XDOT =      -4349
671128                 Wp   =            4
59850
 YDOT =       2160
958189  meter/sec      RA   =           79
35692  deg
 ZDOT =       5979
822637                 TA   =          345
51554
                                          MA   =          345
54872
                                          Ha   =            189
168  n
mi
                                          Hp   =            185
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6306055
15                 X    =         1855032
18
 Y    =       20927848
34  feet           Y    =         6399927
26  meter
 Z    =       -2984058
54                 Z    =         -900365
71
 XDOT =     -14270
574568                 XDOT =       -4402
560711
 YDOT =       7089
757837  feet/sec       YDOT =        2112
021159  meter/sec
 ZDOT =      19618
840674                 ZDOT =        5958
563905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21838922
97                 X    =         6656503
72
 Y    =       -1009162
15  feet           Y    =         -307592
62  meter
 Z    =       -2947678
49                 Z    =         -898452
40
 XDOT =       3280
442305                 XDOT =         999
878814
 YDOT =      14089
760615  feet/sec       YDOT =        4294
559035  meter/sec
 ZDOT =      19535
338224                 ZDOT =        5954
371091


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   09212
35589881  
00010596  00000-0  82463-4 0  9089
2 25544  51
6411  80
0721 0006510 304
1190  55
9356 15
74129604 12913


Satellite: ISS
Catalog Number: 25544
Epoch time:      09212
35589881   =   yrday
fracday
Element set:     908
Inclination:       51
6411  deg
RA of node:        80
0721  deg
Eccentricity:     
0006510     
Arg of perigee:   304
1190  deg
Mean anomaly:      55
9356  deg
Mean motion:   15
74129604  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1291
Checksum:              292


Coasting Arc #10 (Orbit 1306)
---------------------------------------

Vector Time (GMT): 2009/213/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3650066
80                 A    =         6719898
89  meter
 Y    =       -2140341
30  meter          E    =           
0011066
 Z    =       -5229254
52                 I    =           51
94377
 XDOT =       2784
833729                 Wp   =           57
97075
 YDOT =       7107
517566  meter/sec      RA   =           74
26009  deg
 ZDOT =       -961
015908                 TA   =          202
87715
                                          MA   =          202
92649
                                          Ha   =            189
255  n
mi
                                          Hp   =            185
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11975284
77                 X    =         3699131
65
 Y    =       -7022117
12  feet           Y    =        -2099249
11  meter
 Z    =      -17156346
84                 Z    =        -5211403
80
 XDOT =       9136
593599                 XDOT =        2709
817664
 YDOT =      23318
627184  feet/sec       YDOT =        7138
239895  meter/sec
 ZDOT =      -3152
939330                 ZDOT =        -947
668640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4084031
51                 X    =        -1244812
80
 Y    =      -13358103
66  feet           Y    =        -4071550
00  meter
 Z    =      -17086239
04                 Z    =        -5207885
66
 XDOT =      23817
682851                 XDOT =        7259
629733
 YDOT =      -3298
583198  feet/sec       YDOT =       -1005
408159  meter/sec
 ZDOT =      -3100
123466                 ZDOT =        -944
917633


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   09213
37163384  
00010596  00000-0  82463-4 0  9099
2 25544  51
6420  74
8547 0006462 308
2619  51
7963 15
74174514 13073


Satellite: ISS
Catalog Number: 25544
Epoch time:      09213
37163384   =   yrday
fracday
Element set:     909
Inclination:       51
6420  deg
RA of node:        74
8547  deg
Eccentricity:     
0006462     
Arg of perigee:   308
2619  deg
Mean anomaly:      51
7963  deg
Mean motion:   15
74174514  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1307
Checksum:              312


Coasting Arc #11 (Orbit 1322)
---------------------------------------

Vector Time (GMT): 2009/214/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2928402
86                 A    =         6731476
94  meter
 Y    =       -6009627
38  meter          E    =           
0007005
 Z    =         761359
37                 I    =           51
97341
 XDOT =       3989
746123                 Wp   =          123
08527
 YDOT =      -2708
950062  meter/sec      RA   =           69
13049  deg
 ZDOT =      -6001
067640                 TA   =           48
65561
                                          MA   =           48
59537
                                          Ha   =            189
377  n
mi
                                          Hp   =            185
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9607620
94                 X    =        -2864683
03
 Y    =      -19716625
25  feet           Y    =        -6042018
31  meter
 Z    =        2497898
19                 Z    =          747287
42
 XDOT =      13089
718252                 XDOT =        4048
893193
 YDOT =      -8887
631437  feet/sec       YDOT =       -2664
002918  meter/sec
 ZDOT =     -19688
542125                 ZDOT =       -5981
542422

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21304228
46                 X    =        -6493528
83
 Y    =        5239874
72  feet           Y    =         1597113
82  meter
 Z    =        2442283
68                 Z    =          744408
07
 XDOT =      -5516
038712                 XDOT =       -1681
288599
 YDOT =     -13230
112434  feet/sec       YDOT =       -4032
538270  meter/sec
 ZDOT =     -19611
867432                 ZDOT =       -5977
697193


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   09214
38735837  
00010596  00000-0  82463-4 0  9101
2 25544  51
6421  69
6374 0006481 311
5068  48
5538 15
74160439 13231


Satellite: ISS
Catalog Number: 25544
Epoch time:      09214
38735837   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        69
6374  deg
Eccentricity:     
0006481     
Arg of perigee:   311
5068  deg
Mean anomaly:      48
5538  deg
Mean motion:   15
74160439  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1323
Checksum:              312


Coasting Arc #12 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2009/215/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3315629
11                 A    =         6719658
23  meter
 Y    =        2579083
67  meter          E    =           
0003713
 Z    =        5246181
55                 I    =           51
92237
 XDOT =      -3895
980545                 Wp   =          328
49060
 YDOT =      -6596
036846  meter/sec      RA   =           64
02901  deg
 ZDOT =        783
741274                 TA   =          114
10015
                                          MA   =          114
06131
                                          Ha   =            189
564  n
mi
                                          Hp   =            184
978

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10878048
25                 X    =        -3369706
96
 Y    =        8461560
60  feet           Y    =         2541703
39  meter
 Z    =       17211881
73                 Z    =         5229943
47
 XDOT =     -12782
088403                 XDOT =       -3825
740178
 YDOT =     -21640
540833  feet/sec       YDOT =       -6639
211340  meter/sec
 ZDOT =       2571
329639                 ZDOT =         764
984792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6166313
86                 X    =         1879492
46
 Y    =       12413588
82  feet           Y    =         3783661
87  meter
 Z    =       17148125
26                 Z    =         5226748
58
 XDOT =     -22810
126606                 XDOT =       -6952
526589
 YDOT =       7896
174237  feet/sec       YDOT =        2406
753908  meter/sec
 ZDOT =       2497
263536                 ZDOT =         761
165926


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   09215
40307000  
00010596  00000-0  82463-4 0  9113
2 25544  51
6421  64
4197 0006622 315
1928  44
8700 15
74219548 13392


Satellite: ISS
Catalog Number: 25544
Epoch time:      09215
40307000   =   yrday
fracday
Element set:     911
Inclination:       51
6421  deg
RA of node:        64
4197  deg
Eccentricity:     
0006622     
Arg of perigee:   315
1928  deg
Mean anomaly:      44
8700  deg
Mean motion:   15
74219548  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1339
Checksum:              285


Coasting Arc #13 (Orbit 1353)
---------------------------------------

Vector Time (GMT): 2009/216/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3856470
74                 A    =         6731420
90  meter
 Y    =        5472945
44  meter          E    =           
0013692
 Z    =        -607126
96                 I    =           51
94806
 XDOT =      -3585
235232                 Wp   =           11
44516
 YDOT =       3190
970746  meter/sec      RA   =           58
90014  deg
 ZDOT =       6027
697518                 TA   =          341
96926
                                          MA   =          342
01778
                                          Ha   =            189
712  n
mi
                                          Hp   =            184
803

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12652463
07                 X    =         3797933
96
 Y    =       17955857
73  feet           Y    =         5515743
52  meter
 Z    =       -1991886
36                 Z    =         -588534
24
 XDOT =     -11762
582782                 XDOT =       -3649
931598
 YDOT =      10469
064127  feet/sec       YDOT =        3150
516194  meter/sec
 ZDOT =      19775
910492                 ZDOT =        6010
123990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19918500
18                 X    =         6071158
85
 Y    =       -9275662
87  feet           Y    =        -2827222
04  meter
 Z    =       -1918512
09                 Z    =         -584762
48
 XDOT =       7518
557785                 XDOT =        2291
656413
 YDOT =      12094
705036  feet/sec       YDOT =        3686
466095  meter/sec
 ZDOT =      19706
924402                 ZDOT =        6006
670558


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   09216
35529167  
00010596  00000-0  82463-4 0  9129
2 25544  51
6424  59
5281 0006706 319
4313  40
6350 15
74213642 13543


Satellite: ISS
Catalog Number: 25544
Epoch time:      09216
35529167   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:        59
5281  deg
Eccentricity:     
0006706     
Arg of perigee:   319
4313  deg
Mean anomaly:      40
6350  deg
Mean motion:   15
74213642  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1354
Checksum:              292


Coasting Arc #14 (Orbit 1369)
---------------------------------------

Vector Time (GMT): 2009/217/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2945744
96                 A    =         6719491
59  meter
 Y    =       -2970859
79  meter          E    =           
0012656
 Z    =       -5267915
84                 I    =           51
89186
 XDOT =       4894
983821                 Wp   =           58
44358
 YDOT =       5905
818025  meter/sec      RA   =           53
79328  deg
 ZDOT =       -587
953471                 TA   =          205
95082
                                          MA   =          206
01434
                                          Ha   =            189
806  n
mi
                                          Hp   =            184
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9664517
59                 X    =         3004336
71
 Y    =       -9746915
31  feet           Y    =        -2937590
70  meter
 Z    =      -17283188
45                 Z    =        -5253463
66
 XDOT =      16059
658204                 XDOT =        4831
436256
 YDOT =      19376
043390  feet/sec       YDOT =        5960
201340  meter/sec
 ZDOT =      -1928
981204                 ZDOT =        -564
328026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8053089
62                 X    =        -2454581
72
 Y    =      -11203141
26  feet           Y    =        -3414717
46  meter
 Z    =      -17226469
02                 Z    =        -5250627
76
 XDOT =      20887
749965                 XDOT =        6366
586189
 YDOT =     -12164
257362  feet/sec       YDOT =       -3707
665644  meter/sec
 ZDOT =      -1835
789442                 ZDOT =        -559
548622


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   09217
37098276  
00010596  00000-0  82463-4 0  9135
2 25544  51
6425  54
3102 0006778 323
4914  36
5787 15
74250107 13703


Satellite: ISS
Catalog Number: 25544
Epoch time:      09217
37098276   =   yrday
fracday
Element set:     913
Inclination:       51
6425  deg
RA of node:        54
3102  deg
Eccentricity:     
0006778     
Arg of perigee:   323
4914  deg
Mean anomaly:      36
5787  deg
Mean motion:   15
74250107  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1370
Checksum:              308


Coasting Arc #15 (Orbit 1385)
---------------------------------------

Vector Time (GMT): 2009/218/08:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4672033
64                 A    =         6731509
77  meter
 Y    =       -4825677
55  meter          E    =           
0006740
 Z    =         409504
90                 I    =           51
91326
 XDOT =       3158
493588                 Wp   =          115
45683
 YDOT =      -3576
774096  meter/sec      RA   =           48
66553  deg
 ZDOT =      -6040
247586                 TA   =           60
10881
                                          MA   =           60
04186
                                          Ha   =            189
929  n
mi
                                          Hp   =            184
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15328194
36                 X    =        -4619714
11
 Y    =      -15832275
44  feet           Y    =        -4877630
47  meter
 Z    =        1343520
00                 Z    =          386935
43
 XDOT =      10362
511773                 XDOT =        3227
596736
 YDOT =     -11734
823151  feet/sec       YDOT =       -3541
067217  meter/sec
 ZDOT =     -19817
085255                 ZDOT =       -6024
736331

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17869599
74                 X    =        -5446654
00
 Y    =       12904382
91  feet           Y    =         3933255
91  meter
 Z    =        1254528
15                 Z    =          382380
18
 XDOT =      -9168
658028                 XDOT =       -2794
606967
 YDOT =     -10750
595444  feet/sec       YDOT =       -3276
781491  meter/sec
 ZDOT =     -19756
225947                 ZDOT =       -6021
697669


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   09218
38666410  
00010596  00000-0  82463-4 0  9149
2 25544  51
6424  49
0923 0006681 326
5028  33
5712 15
74210718 13863


Satellite: ISS
Catalog Number: 25544
Epoch time:      09218
38666410   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:        49
0923  deg
Eccentricity:     
0006681     
Arg of perigee:   326
5028  deg
Mean anomaly:      33
5712  deg
Mean motion:   15
74210718  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1386
Checksum:              302

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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