Date: August 2nd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8794 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


213/08:18:49 534 2 7 4 1 4 1
N/A 2 0 -0 1 189 1
000/00:07:39 068 -2 4 0 2 187 8

Coasting Arc #1 (Orbit 1277)
---------------------------------------

Vector Time (GMT): 2009/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -218914
23                 A    =         6731527
59  meter
 Y    =       -6692660
24  meter          E    =           
0005228
 Z    =        -654696
73                 I    =           51
99368
 XDOT =       4779
848410                 Wp   =          169
73798
 YDOT =        431
339402  meter/sec      RA   =           83
74463  deg
 ZDOT =      -6019
976333                 TA   =           17
35586
                                          MA   =           17
33800
                                          Ha   =            188
785  n
mi
                                          Hp   =            185
839

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -718222
54                 X    =         -140879
11
 Y    =      -21957546
73  feet           Y    =        -6694671
88  meter
 Z    =       -2147955
16                 Z    =         -655571
43
 XDOT =      15681
917355                 XDOT =        4803
913628
 YDOT =       1415
155520  feet/sec       YDOT =         484
925709  meter/sec
 ZDOT =     -19750
578520                 ZDOT =       -5996
697463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16992530
53                 X    =        -5179323
30
 Y    =       13924347
22  feet           Y    =         4244141
03  meter
 Z    =       -2151714
24                 Z    =         -655842
50
 XDOT =      -7476
583701                 XDOT =       -2278
862712
 YDOT =     -12155
668780  feet/sec       YDOT =       -3705
047844  meter/sec
 ZDOT =     -19659
015272                 ZDOT =       -5992
067855


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
53049514  
00010596  00000-0  82463-4 0  9004
2 25544  51
6423  84
3170 0006762 297
3050  62
7425 15
74161341 12780


Satellite: ISS
Catalog Number: 25544
Epoch time:      09211
53049514   =   yrday
fracday
Element set:     900
Inclination:       51
6423  deg
RA of node:        84
3170  deg
Eccentricity:     
0006762     
Arg of perigee:   297
3050  deg
Mean anomaly:      62
7425  deg
Mean motion:   15
74161341  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1278
Checksum:              284


Coasting Arc #2 (Orbit 1293)
---------------------------------------

Vector Time (GMT): 2009/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4207550
58                 A    =         6719673
12  meter
 Y    =        -113848
48  meter          E    =           
0006144
 Z    =        5241282
67                 I    =           51
94996
 XDOT =       -854
980445                 Wp   =          330
92197
 YDOT =      -7604
381394  meter/sec      RA   =           78
61689  deg
 ZDOT =       -846
693686                 TA   =          127
13399
                                          MA   =          127
07785
                                          Ha   =            189
027  n
mi
                                          Hp   =            185
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13804299
80                 X    =        -4231425
77
 Y    =        -373518
62  feet           Y    =         -161033
92  meter
 Z    =       17195809
30                 Z    =         5220784
56
 XDOT =      -2805
053953                 XDOT =        -765
770359
 YDOT =     -24948
757853  feet/sec       YDOT =       -7613
443381  meter/sec
 ZDOT =      -2777
866424                 ZDOT =        -850
631403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8359043
17                 X    =         2547836
36
 Y    =       11117134
53  feet           Y    =         3388502
60  meter
 Z    =       17115191
61                 Z    =         5216710
40
 XDOT =     -16985
384317                 XDOT =       -5177
145140
 YDOT =      17096
970405  feet/sec       YDOT =        5211
156579  meter/sec
 ZDOT =      -2793
704576                 ZDOT =        -851
521155


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
54619255  
00010596  00000-0  82463-4 0  9012
2 25544  51
6423  79
0989 0006901 302
5107  57
5389 15
74233039 12949


Satellite: ISS
Catalog Number: 25544
Epoch time:      09212
54619255   =   yrday
fracday
Element set:     901
Inclination:       51
6423  deg
RA of node:        79
0989  deg
Eccentricity:     
0006901     
Arg of perigee:   302
5107  deg
Mean anomaly:      57
5389  deg
Mean motion:   15
74233039  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1294
Checksum:              311


Coasting Arc #3 (Orbit 1306)
---------------------------------------

Vector Time (GMT): 2009/213/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2092863
08                 A    =         6725958
45  meter
 Y    =       -4793276
47  meter          E    =           
0004405
 Z    =       -4231890
56                 I    =           51
95719
 XDOT =       4409
371387                 Wp   =            3
65659
 YDOT =       5147
455099  meter/sec      RA   =           74
30615  deg
 ZDOT =      -3645
570836                 TA   =          229
34843
                                          MA   =          229
38673
                                          Ha   =            189
120  n
mi
                                          Hp   =            187
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6866348
67                 X    =         2166864
28
 Y    =      -15725972
66  feet           Y    =        -4769458
54  meter
 Z    =      -13884155
37                 Z    =        -4221544
41
 XDOT =      14466
441557                 XDOT =        4369
193266
 YDOT =      16887
976045  feet/sec       YDOT =        5196
539093  meter/sec
 ZDOT =     -11960
534238                 ZDOT =       -3624
247286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13387993
97                 X    =        -4080660
56
 Y    =      -10785953
74  feet           Y    =        -3287558
70  meter
 Z    =      -13843682
68                 Z    =        -4219554
48
 XDOT =      19291
838861                 XDOT =        5880
152485
 YDOT =      -8685
285636  feet/sec       YDOT =       -2647
275062  meter/sec
 ZDOT =     -11876
437437                 ZDOT =       -3619
938131


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
37145007  
00010596  00000-0  82463-4 0  9024
2 25544  51
6415  74
8592 0007620 281
6185  78
4123 15
73467383 13078


Satellite: ISS
Catalog Number: 25544
Epoch time:      09213
37145007   =   yrday
fracday
Element set:     902
Inclination:       51
6415  deg
RA of node:        74
8592  deg
Eccentricity:     
0007620     
Arg of perigee:   281
6185  deg
Mean anomaly:      78
4123  deg
Mean motion:   15
73467383  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1307
Checksum:              302


Coasting Arc #4 (Orbit 1322)
---------------------------------------

Vector Time (GMT): 2009/214/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4291465
14                 A    =         6729030
19  meter
 Y    =       -3983447
47  meter          E    =           
0005598
 Z    =        3313073
74                 I    =           51
95763
 XDOT =       1743
555175                 Wp   =           73
11303
 YDOT =      -5818
494264  meter/sec      RA   =           69
14742  deg
 ZDOT =      -4729
248971                 TA   =           68
18280
                                          MA   =           68
12326
                                          Ha   =            189
369  n
mi
                                          Hp   =            187
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14079610
03                 X    =        -4262696
66
 Y    =      -13069053
38  feet           Y    =        -4031276
71  meter
 Z    =       10869664
51                 Z    =         3292295
50
 XDOT =       5720
325378                 XDOT =        1831
462472
 YDOT =     -19089
548110  feet/sec       YDOT =       -5798
504697  meter/sec
 ZDOT =     -15515
908698                 ZDOT =       -4720
566118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16108974
59                 X    =        -4910015
46
 Y    =       10550368
60  feet           Y    =         3215752
35  meter
 Z    =       10787763
49                 Z    =         3288110
31
 XDOT =     -16341
023667                 XDOT =       -4980
744014
 YDOT =      -9092
681990  feet/sec       YDOT =       -2771
449471  meter/sec
 ZDOT =     -15482
017018                 ZDOT =       -4718
918787


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
38763304  
00010596  00000-0  82463-4 0  9033
2 25544  51
6411  69
6451 0007646 285
2142  74
8175 15
73455198 13237


Satellite: ISS
Catalog Number: 25544
Epoch time:      09214
38763304   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:        69
6451  deg
Eccentricity:     
0007646     
Arg of perigee:   285
2142  deg
Mean anomaly:      74
8175  deg
Mean motion:   15
73455198  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1323
Checksum:              310


Coasting Arc #5 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2009/215/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -931473
75                 A    =         6726632
23  meter
 Y    =        5302768
21  meter          E    =           
0003308
 Z    =        4029427
68                 I    =           51
93850
 XDOT =      -5330
443806                 Wp   =           85
28060
 YDOT =      -3926
087901  meter/sec      RA   =           64
08776  deg
 ZDOT =       3932
063983                 TA   =          324
27341
                                          MA   =          324
29554
                                          Ha   =            189
700  n
mi
                                          Hp   =            187
490

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3056016
23                 X    =        -1010274
84
 Y    =       17397533
48  feet           Y    =         5291910
85  meter
 Z    =       13219907
08                 Z    =         4024711
88
 XDOT =     -17488
332698                 XDOT =       -5305
246350
 YDOT =     -12880
865816  feet/sec       YDOT =       -3985
555619  meter/sec
 ZDOT =      12900
472384                 ZDOT =        3906
229910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16240799
40                 X    =         4950195
66
 Y    =        6980957
12  feet           Y    =         2127795
73  meter
 Z    =       13201591
65                 Z    =         4023845
13
 XDOT =     -16005
150154                 XDOT =       -4878
369767
 YDOT =      13016
237848  feet/sec       YDOT =        3967
349296  meter/sec
 ZDOT =      12798
685157                 ZDOT =        3901
039236


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
40380510  
00010596  00000-0  82463-4 0  9042
2 25544  51
6415  64
4302 0007695 289
7678  70
2655 15
73474699 13393


Satellite: ISS
Catalog Number: 25544
Epoch time:      09215
40380510   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:        64
4302  deg
Eccentricity:     
0007695     
Arg of perigee:   289
7678  deg
Mean anomaly:      70
2655  deg
Mean motion:   15
73474699  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1339
Checksum:              325


Coasting Arc #6 (Orbit 1353)
---------------------------------------

Vector Time (GMT): 2009/216/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4957498
93                 A    =         6728187
09  meter
 Y    =        2837453
70  meter          E    =           
0003232
 Z    =       -3551254
23                 I    =           51
93013
 XDOT =       -351
122722                 Wp   =          322
58395
 YDOT =       6240
345014  meter/sec      RA   =           58
92550  deg
 ZDOT =       4496
262465                 TA   =          355
29763
                                          MA   =          355
30066
                                          Ha   =            189
959  n
mi
                                          Hp   =            187
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16264760
26                 X    =         4942652
57
 Y    =        9309231
29  feet           Y    =         2892808
71  meter
 Z    =      -11651096
55                 Z    =        -3527206
97
 XDOT =      -1151
977435                 XDOT =        -442
718801
 YDOT =      20473
572881  feet/sec       YDOT =        6235
905955  meter/sec
 ZDOT =      14751
517275                 ZDOT =        4494
334901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12517503
23                 X    =         3815334
99
 Y    =      -14025491
39  feet           Y    =        -4274969
78  meter
 Z    =      -11556382
15                 Z    =        -3522385
28
 XDOT =      18739
978981                 XDOT =        5711
945593
 YDOT =       4577
579734  feet/sec       YDOT =        1395
246303  meter/sec
 ZDOT =      14744
208310                 ZDOT =        4494
034693


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
35645664  
00010596  00000-0  82463-4 0  9052
2 25544  51
6419  59
5415 0007808 293
5367  66
4976 15
73505554 13546


Satellite: ISS
Catalog Number: 25544
Epoch time:      09216
35645664   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:        59
5415  deg
Eccentricity:     
0007808     
Arg of perigee:   293
5367  deg
Mean anomaly:      66
4976  deg
Mean motion:   15
73505554  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1354
Checksum:              338


Coasting Arc #7 (Orbit 1369)
---------------------------------------

Vector Time (GMT): 2009/217/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -318560
53                 A    =         6727186
51  meter
 Y    =       -5524852
23  meter          E    =           
0005398
 Z    =       -3828367
43                 I    =           51
91070
 XDOT =       5929
582681                 Wp   =          349
62486
 YDOT =       2560
970460  meter/sec      RA   =           53
86501  deg
 ZDOT =      -4183
129247                 TA   =          236
66553
                                          MA   =          236
71722
                                          Ha   =            190
036  n
mi
                                          Hp   =            187
164

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1045146
11                 X    =         -238159
91
 Y    =      -18126155
61  feet           Y    =        -5527964
70  meter
 Z    =      -12560260
58                 Z    =        -3829720
13
 XDOT =      19454
011419                 XDOT =        5920
825207
 YDOT =       8402
134054  feet/sec       YDOT =        2627
229913  meter/sec
 ZDOT =     -13724
177319                 ZDOT =       -4154
345027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17975264
13                 X    =        -5478860
51
 Y    =       -2529814
00  feet           Y    =         -771087
31  meter
 Z    =      -12565823
26                 Z    =        -3830062
93
 XDOT =      11814
949903                 XDOT =        3601
196731
 YDOT =     -16243
888330  feet/sec       YDOT =       -4951
137163  meter/sec
 ZDOT =     -13610
839131                 ZDOT =       -4148
583767


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
37260856  
00010596  00000-0  82463-4 0  9062
2 25544  51
6421  54
3269 0007962 297
3630  62
6722 15
73514951 13701


Satellite: ISS
Catalog Number: 25544
Epoch time:      09217
37260856   =   yrday
fracday
Element set:     906
Inclination:       51
6421  deg
RA of node:        54
3269  deg
Eccentricity:     
0007962     
Arg of perigee:   297
3630  deg
Mean anomaly:      62
6722  deg
Mean motion:   15
73514951  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1370
Checksum:              313


Coasting Arc #8 (Orbit 1385)
---------------------------------------

Vector Time (GMT): 2009/218/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5342927
78                 A    =         6727455
15  meter
 Y    =       -1621858
58  meter          E    =           
0007382
 Z    =        3753004
98                 I    =           51
89281
 XDOT =      -1089
262693                 Wp   =           41
63759
 YDOT =      -6311
938640  meter/sec      RA   =           48
69966  deg
 ZDOT =      -4268
247749                 TA   =           93
21301
                                          MA   =           93
12855
                                          Ha   =            190
233  n
mi
                                          Hp   =            186
906

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17529290
61                 X    =        -5342625
80
 Y    =       -5321058
32  feet           Y    =        -1681604
87  meter
 Z    =       12313008
45                 Z    =         3727050
23
 XDOT =      -3573
696498                 XDOT =        -997
866633
 YDOT =     -20708
460106  feet/sec       YDOT =       -6323
608126  meter/sec
 ZDOT =     -14003
437496                 ZDOT =       -4273
317670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8323538
09                 X    =        -2537014
41
 Y    =       16395546
92  feet           Y    =         4997362
70  meter
 Z    =       12210840
39                 Z    =         3721864
15
 XDOT =     -19804
611729                 XDOT =       -6036
445655
 YDOT =        415
176436  feet/sec       YDOT =         126
545778  meter/sec
 ZDOT =     -14023
657271                 ZDOT =       -4274
410736


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
38875062  
00010596  00000-0  82463-4 0  9076
2 25544  51
6418  49
1120 0007939 302
1922  57
8471 15
73544949 13862


Satellite: ISS
Catalog Number: 25544
Epoch time:      09218
38875062   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:        49
1120  deg
Eccentricity:     
0007939     
Arg of perigee:   302
1922  deg
Mean anomaly:      57
8471  deg
Mean motion:   15
73544949  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1386
Checksum:              328


Coasting Arc #9 (Orbit 1401)
---------------------------------------

Vector Time (GMT): 2009/219/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1574050
01                 A    =         6727760
10  meter
 Y    =        5436462
57  meter          E    =           
0006612
 Z    =        3629246
83                 I    =           51
87345
 XDOT =      -6212
410091                 Wp   =           55
18296
 YDOT =      -1144
461136  meter/sec      RA   =           43
63548  deg
 ZDOT =       4406
819375                 TA   =          348
14653
                                          MA   =          348
16209
                                          Ha   =            190
456  n
mi
                                          Hp   =            186
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5164206
08                 X    =         1495511
69
 Y    =       17836163
30  feet           Y    =         5453625
25  meter
 Z    =       11906977
80                 Z    =         3636702
87
 XDOT =     -20381
922871                 XDOT =       -6220
557922
 YDOT =      -3754
793754  feet/sec       YDOT =       -1213
977687  meter/sec
 ZDOT =      14458
068817                 ZDOT =        4376
620243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18418014
24                 X    =         5613810
74
 Y    =       -2206693
47  feet           Y    =         -672600
17  meter
 Z    =       11936545
62                 Z    =         3638259
10
 XDOT =      -7108
251204                 XDOT =       -2166
594967
 YDOT =      18270
149739  feet/sec       YDOT =        5568
741640  meter/sec
 ZDOT =      14339
226554                 ZDOT =        4370
596254


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   09219
40488258  
00010596  00000-0  82463-4 0  9088
2 25544  51
6420  43
8963 0008005 306
4344  53
6080 15
73528705 14022


Satellite: ISS
Catalog Number: 25544
Epoch time:      09219
40488258   =   yrday
fracday
Element set:     908
Inclination:       51
6420  deg
RA of node:        43
8963  deg
Eccentricity:     
0008005     
Arg of perigee:   306
4344  deg
Mean anomaly:      53
6080  deg
Mean motion:   15
73528705  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1402
Checksum:              300


Coasting Arc #10 (Orbit 1416)
---------------------------------------

Vector Time (GMT): 2009/220/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5438858
62                 A    =         6726773
38  meter
 Y    =         369446
45  meter          E    =           
0003242
 Z    =       -3938586
76                 I    =           51
84769
 XDOT =       2513
428740                 Wp   =             
64098
 YDOT =       6052
122939  meter/sec      RA   =           38
46705  deg
 ZDOT =       4041
740246                 TA   =          311
22312
                                          MA   =          311
25107
                                          Ha   =            190
688  n
mi
                                          Hp   =            186
509

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17844024
34                 X    =         5453455
81
 Y    =        1212094
65  feet           Y    =          430348
66  meter
 Z    =      -12921872
58                 Z    =        -3912129
75
 XDOT =       8246
157282                 XDOT =        2425
932338
 YDOT =      19856
046389  feet/sec       YDOT =        6079
740266  meter/sec
 ZDOT =      13260
302643                 ZDOT =        4053
737892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3731886
15                 X    =         1137478
90
 Y    =      -17567883
57  feet           Y    =        -5354690
91  meter
 Z    =      -12817786
93                 Z    =        -3906861
46
 XDOT =      19530
290432                 XDOT =        5952
832524
 YDOT =      -5553
049328  feet/sec       YDOT =       -1692
569435  meter/sec
 ZDOT =      13307
761124                 ZDOT =        4056
205591


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   09220
35749503  
00010596  00000-0  82463-4 0  9098
2 25544  51
6419  39
0071 0008203 309
1579  50
8854 15
73565336 14172


Satellite: ISS
Catalog Number: 25544
Epoch time:      09220
35749503   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:        39
0071  deg
Eccentricity:     
0008203     
Arg of perigee:   309
1579  deg
Mean anomaly:      50
8854  deg
Mean motion:   15
73565336  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1417
Checksum:              310


Coasting Arc #11 (Orbit 1432)
---------------------------------------

Vector Time (GMT): 2009/221/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2782178
15                 A    =         6728238
17  meter
 Y    =       -5072927
04  meter          E    =           
0005939
 Z    =       -3439143
34                 I    =           51
82848
 XDOT =       6165
624774                 Wp   =          349
25931
 YDOT =       -261
462592  meter/sec      RA   =           33
40016  deg
 ZDOT =      -4595
179741                 TA   =          231
27791
                                          MA   =          231
33102
                                          Ha   =            190
729  n
mi
                                          Hp   =            186
247

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9127881
06                 X    =        -2708538
50
 Y    =      -16643461
43  feet           Y    =        -5103627
22  meter
 Z    =      -11283278
67                 Z    =        -3452480
18
 XDOT =      20228
427735                 XDOT =        6190
412534
 YDOT =       -857
816902  feet/sec       YDOT =        -192
376314  meter/sec
 ZDOT =     -15076
049018                 ZDOT =       -4565
167292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17640717
46                 X    =        -5376890
68
 Y    =        6923620
19  feet           Y    =         2110319
43  meter
 Z    =      -11335959
14                 Z    =        -3455200
35
 XDOT =       2177
964810                 XDOT =         663
843674
 YDOT =     -18978
640786  feet/sec       YDOT =       -5784
689712  meter/sec
 ZDOT =     -14958
009519                 ZDOT =       -4559
201301


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   09221
37360600  
00010596  00000-0  82463-4 0  9100
2 25544  51
6417  33
7923 0008261 312
4672  47
5792 15
73562470 14330


Satellite: ISS
Catalog Number: 25544
Epoch time:      09221
37360600   =   yrday
fracday
Element set:     910
Inclination:       51
6417  deg
RA of node:        33
7923  deg
Eccentricity:     
0008261     
Arg of perigee:   312
4672  deg
Mean anomaly:      47
5792  deg
Mean motion:   15
73562470  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1433
Checksum:              290


Coasting Arc #12 (Orbit 1448)
---------------------------------------

Vector Time (GMT): 2009/222/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5281071
70                 A    =         6726053
30  meter
 Y    =         815483
98  meter          E    =           
0009771
 Z    =        4086798
21                 I    =           51
79656
 XDOT =      -3820
108181                 Wp   =           28
32259
 YDOT =      -5473
780154  meter/sec      RA   =           28
22855  deg
 ZDOT =      -3832
050969                 TA   =          101
04699
                                          MA   =          100
93708
                                          Ha   =            190
893  n
mi
                                          Hp   =            185
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17326350
71                 X    =        -5309650
85
 Y    =        2675472
37  feet           Y    =          756268
11  meter
 Z    =       13408130
61                 Z    =         4061073
55
 XDOT =     -12533
163322                 XDOT =       -3740
000243
 YDOT =     -17958
596307  feet/sec       YDOT =       -5516
050909  meter/sec
 ZDOT =     -12572
345698                 ZDOT =       -3850
414376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         794973
62                 X    =          242307
96
 Y    =       17590643
22  feet           Y    =         5361628
05  meter
 Z    =       13306984
48                 Z    =         4055968
87
 XDOT =     -17908
016482                 XDOT =       -5458
363424
 YDOT =      10405
264176  feet/sec       YDOT =        3171
524521  meter/sec
 ZDOT =     -12644
809764                 ZDOT =       -3854
138016


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   09222
38970498  
00010596  00000-0  82463-4 0  9115
2 25544  51
6423  28
5769 0008415 317
2518  42
7989 15
73641052 14496


Satellite: ISS
Catalog Number: 25544
Epoch time:      09222
38970498   =   yrday
fracday
Element set:     911
Inclination:       51
6423  deg
RA of node:        28
5769  deg
Eccentricity:     
0008415     
Arg of perigee:   317
2518  deg
Mean anomaly:      42
7989  deg
Mean motion:   15
73641052  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1449
Checksum:              331


Coasting Arc #13 (Orbit 1464)
---------------------------------------

Vector Time (GMT): 2009/223/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3857597
61                 A    =         6728626
84  meter
 Y    =        4438704
27  meter          E    =           
0010179
 Z    =        3255789
39                 I    =           51
77736
 XDOT =      -5843
944755                 Wp   =           46
61916
 YDOT =       1582
041137  meter/sec      RA   =           23
15631  deg
 ZDOT =       4764
909004                 TA   =          351
44450
                                          MA   =          351
46184
                                          Ha   =            191
035  n
mi
                                          Hp   =            185
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12656160
14                 X    =         3791860
57
 Y    =       14562678
07  feet           Y    =         4481474
59  meter
 Z    =       10681723
71                 Z    =         3274369
93
 XDOT =     -19173
047098                 XDOT =       -5884
348062
 YDOT =       5190
423678  feet/sec       YDOT =        1516
464738  meter/sec
 ZDOT =      15632
903557                 ZDOT =        4736
421103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15637844
44                 X    =         4766414
99
 Y    =      -11231081
19  feet           Y    =        -3423233
55  meter
 Z    =       10754991
39                 Z    =         3278121
37
 XDOT =       2615
750544                 XDOT =         797
280766
 YDOT =      18512
593741  feet/sec       YDOT =        5642
638572  meter/sec
 ZDOT =      15520
924997                 ZDOT =        4730
777939


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   09223
40579598  
00010596  00000-0  82463-4 0  9126
2 25544  51
6414  23
3610 0008423 321
1223  38
9333 15
73604369 14658


Satellite: ISS
Catalog Number: 25544
Epoch time:      09223
40579598   =   yrday
fracday
Element set:     912
Inclination:       51
6414  deg
RA of node:        23
3610  deg
Eccentricity:     
0008423     
Arg of perigee:   321
1223  deg
Mean anomaly:      38
9333  deg
Mean motion:   15
73604369  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1465
Checksum:              294


Coasting Arc #14 (Orbit 1479)
---------------------------------------

Vector Time (GMT): 2009/224/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4863090
13                 A    =         6725542
25  meter
 Y    =       -1926695
52  meter          E    =           
0004857
 Z    =       -4227220
86                 I    =           51
73838
 XDOT =       4976
971547                 Wp   =           34
60501
 YDOT =       4621
269688  meter/sec      RA   =           17
98137  deg
 ZDOT =       3625
267950                 TA   =          272
21727
                                          MA   =          272
27289
                                          Ha   =            191
243  n
mi
                                          Hp   =            185
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15955020
12                 X    =         4904808
40
 Y    =       -6321179
51  feet           Y    =        -1872080
20  meter
 Z    =      -13868834
84                 Z    =        -4203494
71
 XDOT =      16328
646808                 XDOT =        4907
314932
 YDOT =      15161
645957  feet/sec       YDOT =        4676
535522  meter/sec
 ZDOT =      11893
923720                 ZDOT =        3649
277008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5135382
78                 X    =        -1565264
67
 Y    =      -16453730
21  feet           Y    =        -5015096
97  meter
 Z    =      -13775600
28                 Z    =        -4198802
97
 XDOT =      15107
164681                 XDOT =        4604
663795
 YDOT =     -14735
867847  feet/sec       YDOT =       -4491
492520  meter/sec
 ZDOT =      11988
543400                 ZDOT =        3654
108028


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   09224
35836958  
00010596  00000-0  82463-4 0  9138
2 25544  51
6406  18
4713 0008369 324
3655  35
6948 15
73636358 14807


Satellite: ISS
Catalog Number: 25544
Epoch time:      09224
35836958   =   yrday
fracday
Element set:     913
Inclination:       51
6406  deg
RA of node:        18
4713  deg
Eccentricity:     
0008369     
Arg of perigee:   324
3655  deg
Mean anomaly:      35
6948  deg
Mean motion:   15
73636358  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1480
Checksum:              335


Coasting Arc #15 (Orbit 1495)
---------------------------------------

Vector Time (GMT): 2009/225/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4778897
10                 A    =         6728968
72  meter
 Y    =       -3596783
11  meter          E    =           
0006120
 Z    =       -3090129
80                 I    =           51
72084
 XDOT =       5249
864320                 Wp   =          359
34542
 YDOT =      -2762
299222  meter/sec      RA   =           12
90527  deg
 ZDOT =      -4897
637213                 TA   =          216
43740
                                          MA   =          216
47907
                                          Ha   =            191
320  n
mi
                                          Hp   =            185
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15678796
26                 X    =        -4723310
78
 Y    =      -11800469
51  feet           Y    =        -3649912
58  meter
 Z    =      -10138221
11                 Z    =        -3113210
85
 XDOT =      17223
964303                 XDOT =        5304
154477
 YDOT =      -9062
661491  feet/sec       YDOT =       -2703
288356  meter/sec
 ZDOT =     -16068
363559                 ZDOT =       -4872
001640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12653025
43                 X    =        -3856642
15
 Y    =       14937363
29  feet           Y    =         4552908
33  meter
 Z    =      -10229143
94                 Z    =        -3117843
07
 XDOT =      -6994
204491                 XDOT =       -2131
833529
 YDOT =     -16872
857880  feet/sec       YDOT =       -5142
847082  meter/sec
 ZDOT =     -15967
652585                 ZDOT =       -4866
940508


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   09225
37443809  
00010596  00000-0  82463-4 0  9141
2 25544  51
6400  13
2567 0008434 328
4066  31
6590 15
73643925 14969


Satellite: ISS
Catalog Number: 25544
Epoch time:      09225
37443809   =   yrday
fracday
Element set:     914
Inclination:       51
6400  deg
RA of node:        13
2567  deg
Eccentricity:     
0008434     
Arg of perigee:   328
4066  deg
Mean anomaly:      31
6590  deg
Mean motion:   15
73643925  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1496
Checksum:              310


Coasting Arc #16 (Orbit 1511)
---------------------------------------

Vector Time (GMT): 2009/226/08:22:39
068
Vector Time (MET): N/A
Weight (LBS)     : 701318
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4271944
05                 A    =         6725053
53  meter
 Y    =        2873072
31  meter          E    =           
0011746
 Z    =        4328854
65                 I    =           51
67861
 XDOT =      -5895
557620                 Wp   =           25
78154
 YDOT =      -3550
046595  meter/sec      RA   =            7
72681  deg
 ZDOT =      -3447
999995                 TA   =           99
10238
                                          MA   =           98
96945
                                          Ha   =            191
459  n
mi
                                          Hp   =            185
069

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14015564
47                 X    =        -4324782
50
 Y    =        9426090
25  feet           Y    =         2825005
18  meter
 Z    =       14202279
04                 Z    =         4307973
44
 XDOT =     -19342
380643                 XDOT =       -5838
672483
 YDOT =     -11647
134497  feet/sec       YDOT =       -3615
655868  meter/sec
 ZDOT =     -11312
335942                 ZDOT =       -3476
502656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8875640
40                 X    =         2705295
19
 Y    =       14451054
77  feet           Y    =         4404681
49  meter
 Z    =       14120268
36                 Z    =         4303857
80
 XDOT =     -11328
240148                 XDOT =       -3452
847597
 YDOT =      18165
454465  feet/sec       YDOT =        5536
830521  meter/sec
 ZDOT =     -11424
577572                 ZDOT =       -3482
211244


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   09226
39049462  
00010596  00000-0  82463-4 0  9152
2 25544  51
6403   8
0404 0008494 331
5968  28
4731 15
73675548 15122


Satellite: ISS
Catalog Number: 25544
Epoch time:      09226
39049462   =   yrday
fracday
Element set:     915
Inclination:       51
6403  deg
RA of node:         8
0404  deg
Eccentricity:     
0008494     
Arg of perigee:   331
5968  deg
Mean anomaly:      28
4731  deg
Mean motion:   15
73675548  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1512
Checksum:              314

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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