Date: July 20th 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 1009)
---------------------------------------

Vector Time (GMT): 2009/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1083731
96                 A    =         6719244
83  meter
 Y    =        4041775
52  meter          E    =           
0011213
 Z    =       -5265632
56                 I    =           51
66783
 XDOT =      -7531
196620                 Wp   =          114
84032
 YDOT =       1530
204177  meter/sec      RA   =          170
75967  deg
 ZDOT =       -380
715399                 TA   =          151
57389
                                          MA   =          151
51268
                                          Ha   =            189
619  n
mi
                                          Hp   =            184
728

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3555551
06                 X    =         1064034
91
 Y    =       13260418
39  feet           Y    =         4053784
82  meter
 Z    =      -17275697
37                 Z    =        -5260415
28
 XDOT =     -24708
650328                 XDOT =       -7545
898454
 YDOT =       5020
354911  feet/sec       YDOT =        1445
903761  meter/sec
 ZDOT =      -1249
066269                 ZDOT =        -417
337270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11106685
02                 X    =         3385317
60
 Y    =       -8114068
74  feet           Y    =        -2473168
15  meter
 Z    =      -17254964
35                 Z    =        -5259313
13
 XDOT =      12849
231736                 XDOT =        3916
445833
 YDOT =      20513
394124  feet/sec       YDOT =        6252
482529  meter/sec
 ZDOT =      -1392
778884                 ZDOT =        -424
519004


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   09194
51659774  
00010596  00000-0  82463-4 0  9007
2 25544  51
6362 171
6940 0007249 220
8002 139
2619 15
74320561 10106


Satellite: ISS
Catalog Number: 25544
Epoch time:      09194
51659774   =   yrday
fracday
Element set:     900
Inclination:       51
6362  deg
RA of node:       171
6940  deg
Eccentricity:     
0007249     
Arg of perigee:   220
8002  deg
Mean anomaly:     139
2619  deg
Mean motion:   15
74320561  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1010
Checksum:              293


Coasting Arc #2 (Orbit 1025)
---------------------------------------

Vector Time (GMT): 2009/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6467813
37                 A    =         6731138
41  meter
 Y    =       -1819749
74  meter          E    =           
0014239
 Z    =         198465
16                 I    =           51
73791
 XDOT =       1467
586747                 Wp   =          163
16229
 YDOT =       4546
476326  meter/sec      RA   =          165
62069  deg
 ZDOT =      -6046
199472                 TA   =           14
68271
                                          MA   =           14
64140
                                          Ha   =            189
349  n
mi
                                          Hp   =            184
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21219860
14                 X    =         6486717
31
 Y    =       -5970307
56  feet           Y    =        -1747317
19  meter
 Z    =         651132
42                 Z    =          229931
45
 XDOT =       4814
917148                 XDOT =        1446
009460
 YDOT =      14916
260913  feet/sec       YDOT =        4562
767700  meter/sec
 ZDOT =     -19836
612440                 ZDOT =       -6039
121911

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13398327
51                 X    =        -4083810
22
 Y    =      -17499595
33  feet           Y    =        -5333876
66  meter
 Z    =         774592
38                 Z    =          236095
76
 XDOT =      10756
002381                 XDOT =        3278
429526
 YDOT =      -9123
464176  feet/sec       YDOT =       -2780
831881  meter/sec
 ZDOT =     -19808
543285                 ZDOT =       -6037
643993


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   09195
53220718  
00010596  00000-0  82463-4 0  9013
2 25544  51
6366 166
4755 0007192 225
8436 134
2136 15
74357923 10267


Satellite: ISS
Catalog Number: 25544
Epoch time:      09195
53220718   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       166
4755  deg
Eccentricity:     
0007192     
Arg of perigee:   225
8436  deg
Mean anomaly:     134
2136  deg
Mean motion:   15
74357923  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1026
Checksum:              310


Coasting Arc #3 (Orbit 1041)
---------------------------------------

Vector Time (GMT): 2009/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1470467
56                 A    =         6719062
62  meter
 Y    =       -3895555
93  meter          E    =           
0005823
 Z    =        5276120
04                 I    =           51
72578
 XDOT =       7237
761165                 Wp   =          213
12735
 YDOT =      -2625
791445  meter/sec      RA   =          160
49255  deg
 ZDOT =         73
717654                 TA   =          236
14617
                                          MA   =          236
20160
                                          Ha   =            189
216  n
mi
                                          Hp   =            185
069

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4824368
64                 X    =        -1452427
95
 Y    =      -12780695
30  feet           Y    =        -3911899
28  meter
 Z    =       17310105
12                 Z    =         5269019
89
 XDOT =      23745
935580                 XDOT =        7266
227177
 YDOT =      -8614
801328  feet/sec       YDOT =       -2544
695408  meter/sec
 ZDOT =        241
855820                 ZDOT =         108
947566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9888597
40                 X    =        -3014044
49
 Y    =        9476760
95  feet           Y    =         2888516
74  meter
 Z    =       17281987
38                 Z    =         5267549
75
 XDOT =     -16421
859259                 XDOT =       -5005
382702
 YDOT =     -17857
028987  feet/sec       YDOT =       -5442
822435  meter/sec
 ZDOT =        380
060091                 ZDOT =         115
842316


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   09196
54780467  
00010596  00000-0  82463-4 0  9028
2 25544  51
6365 161
2573 0007232 230
0953 129
9575 15
74364502 10421


Satellite: ISS
Catalog Number: 25544
Epoch time:      09196
54780467   =   yrday
fracday
Element set:     902
Inclination:       51
6365  deg
RA of node:       161
2573  deg
Eccentricity:     
0007232     
Arg of perigee:   230
0953  deg
Mean anomaly:     129
9575  deg
Mean motion:   15
74364502  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1042
Checksum:              309


Coasting Arc #4 (Orbit 1057)
---------------------------------------

Vector Time (GMT): 2009/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6141689
45                 A    =         6731015
31  meter
 Y    =        2746039
26  meter          E    =           
0005232
 Z    =          81692
99                 I    =           51
79396
 XDOT =      -1874
515815                 Wp   =           35
93376
 YDOT =      -4378
085269  meter/sec      RA   =          155
36226  deg
 ZDOT =       6048
787009                 TA   =          324
95161
                                          MA   =          324
98603
                                          Ha   =            188
970  n
mi
                                          Hp   =            185
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20149899
77                 X    =        -6172336
51
 Y    =        9009315
14  feet           Y    =         2677187
92  meter
 Z    =         268021
61                 Z    =           51782
52
 XDOT =      -6149
986269                 XDOT =       -1854
803969
 YDOT =     -14363
796814  feet/sec       YDOT =       -4398
937782  meter/sec
 ZDOT =      19845
101735                 ZDOT =        6039
727897

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16347413
12                 X    =         4982691
52
 Y    =       14832310
30  feet           Y    =         4520888
18  meter
 Z    =         150702
04                 Z    =           45933
98
 XDOT =      -9553
552585                 XDOT =       -2911
922828
 YDOT =      10316
877302  feet/sec       YDOT =        3144
584202  meter/sec
 ZDOT =      19809
262856                 ZDOT =        6037
863318


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   09197
56338798  
00010596  00000-0  82463-4 0  9038
2 25544  51
6362 156
0383 0007265 233
2978 126
7518 15
74407449 10584


Satellite: ISS
Catalog Number: 25544
Epoch time:      09197
56338798   =   yrday
fracday
Element set:     903
Inclination:       51
6362  deg
RA of node:       156
0383  deg
Eccentricity:     
0007265     
Arg of perigee:   233
2978  deg
Mean anomaly:     126
7518  deg
Mean motion:   15
74407449  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1058
Checksum:              342


Coasting Arc #5 (Orbit 1072)
---------------------------------------

Vector Time (GMT): 2009/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1796655
89                 A    =         6718968
34  meter
 Y    =        3760450
73  meter          E    =           
0009836
 Z    =       -5277968
51                 I    =           51
78059
 XDOT =      -6780
092202                 Wp   =          116
26590
 YDOT =       3629
478964  meter/sec      RA   =          150
23107  deg
 ZDOT =        274
073194                 TA   =          156
35499
                                          MA   =          156
30975
                                          Ha   =            188
748  n
mi
                                          Hp   =            185
472

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5894540
34                 X    =         1780111
81
 Y    =       12337436
78  feet           Y    =         3780450
30  meter
 Z    =      -17316169
64                 Z    =        -5269279
94
 XDOT =     -22244
396989                 XDOT =       -6821
505141
 YDOT =      11907
739384  feet/sec       YDOT =        3553
428411  meter/sec
 ZDOT =        899
190270                 ZDOT =         241
035426

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8707148
63                 X    =         2653938
90
 Y    =      -10598671
02  feet           Y    =        -3230474
93  meter
 Z    =      -17281823
34                 Z    =        -5267499
76
 XDOT =      19336
996938                 XDOT =        5893
916667
 YDOT =      14610
294864  feet/sec       YDOT =        4453
217875  meter/sec
 ZDOT =        769
620315                 ZDOT =         234
580272


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   09198
51548710  
00010596  00000-0  82463-4 0  9042
2 25544  51
6369 151
1454 0007258 238
3409 121
7047 15
74403278 10738


Satellite: ISS
Catalog Number: 25544
Epoch time:      09198
51548710   =   yrday
fracday
Element set:     904
Inclination:       51
6369  deg
RA of node:       151
1454  deg
Eccentricity:     
0007258     
Arg of perigee:   238
3409  deg
Mean anomaly:     121
7047  deg
Mean motion:   15
74403278  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1073
Checksum:              310


Coasting Arc #6 (Orbit 1088)
---------------------------------------

Vector Time (GMT): 2009/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5678248
33                 A    =         6730911
57  meter
 Y    =       -3577256
22  meter          E    =           
0011951
 Z    =        -399203
82                 I    =           51
84704
 XDOT =       2238
794932                 Wp   =          174
20381
 YDOT =       4224
824955  meter/sec      RA   =          145
11095  deg
 ZDOT =      -6041
322154                 TA   =           10
12676
                                          MA   =           10
10270
                                          Ha   =            188
545  n
mi
                                          Hp   =            185
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18629423
65                 X    =         5719767
05
 Y    =      -11736404
92  feet           Y    =        -3513526
51  meter
 Z    =       -1309723
83                 Z    =         -371518
72
 XDOT =       7345
127729                 XDOT =        2220
733421
 YDOT =      13860
974263  feet/sec       YDOT =        4249
760552  meter/sec
 ZDOT =     -19820
610741                 ZDOT =       -6030
489229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18650124
05                 X    =        -5684557
81
 Y    =      -11715122
42  feet           Y    =        -3570769
31  meter
 Z    =       -1201158
57                 Z    =         -366113
13
 XDOT =       8407
913508                 XDOT =        2562
732037
 YDOT =     -11367
303789  feet/sec       YDOT =       -3464
754195  meter/sec
 ZDOT =     -19777
813754                 ZDOT =       -6028
277632


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   09199
53104656  
00010596  00000-0  82463-4 0  9053
2 25544  51
6376 145
9267 0007264 242
4182 117
6244 15
74425002 10899


Satellite: ISS
Catalog Number: 25544
Epoch time:      09199
53104656   =   yrday
fracday
Element set:     905
Inclination:       51
6376  deg
RA of node:       145
9267  deg
Eccentricity:     
0007264     
Arg of perigee:   242
4182  deg
Mean anomaly:     117
6244  deg
Mean motion:   15
74425002  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1089
Checksum:              312


Coasting Arc #7 (Orbit 1104)
---------------------------------------

Vector Time (GMT): 2009/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2111894
28                 A    =         6718906
63  meter
 Y    =       -3620218
32  meter          E    =           
0004408
 Z    =        5254784
76                 I    =           51
83122
 XDOT =       6187
107850                 Wp   =          248
03759
 YDOT =      -4537
333884  meter/sec      RA   =          139
97786  deg
 ZDOT =       -641
386411                 TA   =          208
03298
                                          MA   =          208
05672
                                          Ha   =            188
301  n
mi
                                          Hp   =            185
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6928787
01                 X    =        -2096782
03
 Y    =      -11877356
69  feet           Y    =        -3643751
26  meter
 Z    =       17240107
48                 Z    =         5244561
27
 XDOT =      20298
910269                 XDOT =        6240
500967
 YDOT =     -14886
266025  feet/sec       YDOT =       -4467
847365  meter/sec
 ZDOT =      -2104
286124                 ZDOT =        -611
200826

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7462520
43                 X    =        -2274576
23
 Y    =       11609515
65  feet           Y    =         3538580
37  meter
 Z    =       17199736
40                 Z    =         5242479
66
 XDOT =     -21568
434220                 XDOT =       -6574
058750
 YDOT =     -10931
797116  feet/sec       YDOT =       -3332
011761  meter/sec
 ZDOT =      -1985
929547                 ZDOT =        -605
311326


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   09200
54659252  
00010596  00000-0  82463-4 0  9065
2 25544  51
6381 140
7084 0007289 246
8660 113
1736 15
74459885 11053


Satellite: ISS
Catalog Number: 25544
Epoch time:      09200
54659252   =   yrday
fracday
Element set:     906
Inclination:       51
6381  deg
RA of node:       140
7084  deg
Eccentricity:     
0007289     
Arg of perigee:   246
8660  deg
Mean anomaly:     113
1736  deg
Mean motion:   15
74459885  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1105
Checksum:              318


Coasting Arc #8 (Orbit 1120)
---------------------------------------

Vector Time (GMT): 2009/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5105995
14                 A    =         6730625
51  meter
 Y    =        4317387
34  meter          E    =           
0006863
 Z    =         730814
69                 I    =           51
89300
 XDOT =      -2584
049940                 Wp   =           33
23660
 YDOT =      -4075
338190  meter/sec      RA   =          134
86631  deg
 ZDOT =       6000
815486                 TA   =          334
70003
                                          MA   =          334
73363
                                          Ha   =            188
002  n
mi
                                          Hp   =            185
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16751952
57                 X    =        -5157443
53
 Y    =       14164656
62  feet           Y    =         4260001
31  meter
 Z    =        2397686
01                 Z    =          705885
97
 XDOT =      -8477
854134                 XDOT =       -2567
437221
 YDOT =     -13370
532121  feet/sec       YDOT =       -4104
142796  meter/sec
 ZDOT =      19687
714849                 ZDOT =        5988
301928

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20325395
97                 X    =         6195180
69
 Y    =        8282680
27  feet           Y    =         2524560
95  meter
 Z    =        2299955
76                 Z    =          701026
52
 XDOT =      -7255
398904                 XDOT =       -2211
445586
 YDOT =      12331
536302  feet/sec       YDOT =        3758
652265  meter/sec
 ZDOT =      19638
314948                 ZDOT =        5985
758396


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   09201
56212604  
00010596  00000-0  82463-4 0  9075
2 25544  51
6383 135
4888 0007296 250
8504 109
1869 15
74470314 11218


Satellite: ISS
Catalog Number: 25544
Epoch time:      09201
56212604   =   yrday
fracday
Element set:     907
Inclination:       51
6383  deg
RA of node:       135
4888  deg
Eccentricity:     
0007296     
Arg of perigee:   250
8504  deg
Mean anomaly:     109
1869  deg
Mean motion:   15
74470314  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1121
Checksum:              303


Coasting Arc #9 (Orbit 1135)
---------------------------------------

Vector Time (GMT): 2009/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2404562
08                 A    =         6719041
55  meter
 Y    =        3504729
93  meter          E    =           
0008318
 Z    =       -5210742
88                 I    =           51
87538
 XDOT =      -5474
315739                 Wp   =          118
11483
 YDOT =       5308
241537  meter/sec      RA   =          129
72881  deg
 ZDOT =       1041
534667                 TA   =          161
80604
                                          MA   =          161
77626
                                          Ha   =            187
750  n
mi
                                          Hp   =            185
975

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7888983
20                 X    =         2390505
20
 Y    =       11498457
78  feet           Y    =         3531541
44  meter
 Z    =      -17095613
11                 Z    =        -5199095
30
 XDOT =     -17960
353475                 XDOT =       -5538
326022
 YDOT =      17415
490607  feet/sec       YDOT =        5246
666457  meter/sec
 ZDOT =       3417
108488                 ZDOT =        1014
786408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6266621
95                 X    =         1910066
37
 Y    =      -12519973
97  feet           Y    =        -3816088
07  meter
 Z    =      -17049641
52                 Z    =        -5196730
74
 XDOT =      22987
183053                 XDOT =        7006
493395
 YDOT =       6983
579838  feet/sec       YDOT =        2128
595135  meter/sec
 ZDOT =       3312
266487                 ZDOT =        1009
578825


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   09202
51417667  
00010596  00000-0  82463-4 0  9088
2 25544  51
6393 130
5961 0007295 254
8012 105
2345 15
74489356 11362


Satellite: ISS
Catalog Number: 25544
Epoch time:      09202
51417667   =   yrday
fracday
Element set:     908
Inclination:       51
6393  deg
RA of node:       130
5961  deg
Eccentricity:     
0007295     
Arg of perigee:   254
8012  deg
Mean anomaly:     105
2345  deg
Mean motion:   15
74489356  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1136
Checksum:              310


Coasting Arc #10 (Orbit 1151)
---------------------------------------

Vector Time (GMT): 2009/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4443104
52                 A    =         6730258
07  meter
 Y    =       -4927174
08  meter          E    =           
0009179
 Z    =       -1093267
90                 I    =           51
93222
 XDOT =       2920
315189                 Wp   =          187
96654
 YDOT =       3949
335637  meter/sec      RA   =          124
62767  deg
 ZDOT =      -5933
652723                 TA   =            3
95197
                                          MA   =            3
94472
                                          Ha   =            187
543  n
mi
                                          Hp   =            185
935

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14577114
57                 X    =         4503181
57
 Y    =      -16165269
28  feet           Y    =        -4877152
62  meter
 Z    =       -3586836
95                 Z    =        -1071538
58
 XDOT =       9581
086578                 XDOT =        2904
759909
 YDOT =      12957
137916  feet/sec       YDOT =        3981
906163  meter/sec
 ZDOT =     -19467
364578                 ZDOT =       -5919
503408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21266663
90                 X    =        -6482079
16
 Y    =       -4705397
19  feet           Y    =        -1434205
06  meter
 Z    =       -3501691
48                 Z    =        -1067315
56
 XDOT =       6132
627116                 XDOT =        1869
224745
 YDOT =     -13278
915701  feet/sec       YDOT =       -4047
413506  meter/sec
 ZDOT =     -19411
528208                 ZDOT =       -5916
633798


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   09203
52968505  
00010596  00000-0  82463-4 0  9093
2 25544  51
6401 125
3775 0007321 258
3795 101
6547 15
74500187 11522


Satellite: ISS
Catalog Number: 25544
Epoch time:      09203
52968505   =   yrday
fracday
Element set:     909
Inclination:       51
6401  deg
RA of node:       125
3775  deg
Eccentricity:     
0007321     
Arg of perigee:   258
3795  deg
Mean anomaly:     101
6547  deg
Mean motion:   15
74500187  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1152
Checksum:              305


Coasting Arc #11 (Orbit 1167)
---------------------------------------

Vector Time (GMT): 2009/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2703618
76                 A    =         6719196
76  meter
 Y    =       -3393680
61  meter          E    =           
0004024
 Z    =        5133861
84                 I    =           51
91117
 XDOT =       4675
606173                 Wp   =          295
94430
 YDOT =      -5939
234799  meter/sec      RA   =          119
48617  deg
 ZDOT =      -1462
931567                 TA   =          168
03105
                                          MA   =          168
02148
                                          Ha   =            187
098  n
mi
                                          Hp   =            185
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8870140
30                 X    =        -2690407
87
 Y    =      -11134122
74  feet           Y    =        -3423840
73  meter
 Z    =       16843378
74                 Z    =         5120759
71
 XDOT =      15339
915266                 XDOT =        4748
778694
 YDOT =     -19485
678474  feet/sec       YDOT =       -5886
540149  meter/sec
 ZDOT =      -4799
644249                 ZDOT =       -1440
040918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5020056
25                 X    =        -1530113
15
 Y    =       13386032
79  feet           Y    =         4080062
80  meter
 Z    =       16791683
85                 Z    =         5118105
24
 XDOT =     -23618
383366                 XDOT =       -7198
883250
 YDOT =      -2945
649881  feet/sec       YDOT =        -897
834084  meter/sec
 ZDOT =      -4709
982548                 ZDOT =       -1435
602681


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
54517920  
00010596  00000-0  82463-4 0  9109
2 25544  51
6398 120
1588 0007388 263
1506  96
8817 15
74555244 11685


Satellite: ISS
Catalog Number: 25544
Epoch time:      09204
54517920   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:       120
1588  deg
Eccentricity:     
0007388     
Arg of perigee:   263
1506  deg
Mean anomaly:      96
8817  deg
Mean motion:   15
74555244  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1168
Checksum:              324


Coasting Arc #12 (Orbit 1183)
---------------------------------------

Vector Time (GMT): 2009/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3714805
03                 A    =         6729727
88  meter
 Y    =        5409654
28  meter          E    =           
0008112
 Z    =        1468673
97                 I    =           51
96026
 XDOT =      -3269
470592                 Wp   =           38
11637
 YDOT =      -3830
159711  meter/sec      RA   =          114
39259  deg
 ZDOT =       5827
471940                 TA   =          337
98307
                                          MA   =          338
01789
                                          Ha   =            186
696  n
mi
                                          Hp   =            185
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12187680
55                 X    =        -3782155
02
 Y    =       17748209
58  feet           Y    =         5367736
46  meter
 Z    =        4818484
17                 Z    =         1450464
67
 XDOT =     -10726
609555                 XDOT =       -3254
706301
 YDOT =     -12566
140784  feet/sec       YDOT =       -3866
638753  meter/sec
 ZDOT =      19119
002428                 ZDOT =        5811
624749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21517025
99                 X    =         6558389
52
 Y    =        1112675
00  feet           Y    =          339143
34  meter
 Z    =        4747192
53                 Z    =         1446944
28
 XDOT =      -4948
789335                 XDOT =       -1508
390989
 YDOT =      14244
062163  feet/sec       YDOT =        4341
590147  meter/sec
 ZDOT =      19056
488044                 ZDOT =        5808
417556


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
56066227  
00010596  00000-0  82463-4 0  9112
2 25544  51
6400 114
9390 0007321 267
2590  92
7735 15
74541213 11849


Satellite: ISS
Catalog Number: 25544
Epoch time:      09205
56066227   =   yrday
fracday
Element set:     911
Inclination:       51
6400  deg
RA of node:       114
9390  deg
Eccentricity:     
0007321     
Arg of perigee:   267
2590  deg
Mean anomaly:      92
7735  deg
Mean motion:   15
74541213  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1184
Checksum:              291


Coasting Arc #13 (Orbit 1198)
---------------------------------------

Vector Time (GMT): 2009/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3017429
86                 A    =         6719627
66  meter
 Y    =        3294423
02  meter          E    =           
0006250
 Z    =       -5024996
82                 I    =           51
93822
 XDOT =      -3817
539532                 Wp   =          119
94889
 YDOT =       6406
157778  meter/sec      RA   =          109
24533  deg
 ZDOT =       1906
254585                 TA   =          168
39175
                                          MA   =          168
37733
                                          Ha   =            186
562  n
mi
                                          Hp   =            185
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9899704
26                 X    =         3004776
92
 Y    =       10808474
48  feet           Y    =         3328095
27  meter
 Z    =      -16486210
03                 Z    =        -5010368
90
 XDOT =     -12524
735996                 XDOT =       -3898
150642
 YDOT =      21017
578011  feet/sec       YDOT =        6363
016971  meter/sec
 ZDOT =       6254
116093                 ZDOT =        1887
513891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3729170
95                 X    =         1136651
30
 Y    =      -14241470
02  feet           Y    =        -4340800
06  meter
 Z    =      -16428517
94                 Z    =        -5007412
27
 XDOT =      23435
810379                 XDOT =        7143
235003
 YDOT =       -998
147564  feet/sec       YDOT =        -304
235378  meter/sec
 ZDOT =       6180
784557                 ZDOT =        1883
903133


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
51266391  
00010596  00000-0  82463-4 0  9123
2 25544  51
6404 110
0458 0007384 270
8654  89
1664 15
74577012 11998


Satellite: ISS
Catalog Number: 25544
Epoch time:      09206
51266391   =   yrday
fracday
Element set:     912
Inclination:       51
6404  deg
RA of node:       110
0458  deg
Eccentricity:     
0007384     
Arg of perigee:   270
8654  deg
Mean anomaly:      89
1664  deg
Mean motion:   15
74577012  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1199
Checksum:              311


Coasting Arc #14 (Orbit 1214)
---------------------------------------

Vector Time (GMT): 2009/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2954936
65                 A    =         6729073
18  meter
 Y    =       -5745490
17  meter          E    =           
0005957
 Z    =       -1866795
59                 I    =           51
97870
 XDOT =       3640
190786                 Wp   =          210
14817
 YDOT =       3717
726079  meter/sec      RA   =          104
16013  deg
 ZDOT =      -5677
390591                 TA   =          350
48377
                                          MA   =          350
49505
                                          Ha   =            186
670  n
mi
                                          Hp   =            185
727

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9694674
05                 X    =         3028032
54
 Y    =      -18850033
37  feet           Y    =        -5712037
52  meter
 Z    =       -6124657
43                 Z    =        -1852263
48
 XDOT =      11942
883156                 XDOT =        3625
927408
 YDOT =      12197
264040  feet/sec       YDOT =        3758
353429  meter/sec
 ZDOT =     -18626
609549                 ZDOT =       -5659
741161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21087311
19                 X    =        -6427412
45
 Y    =        2308385
27  feet           Y    =          703595
83  meter
 Z    =       -6067829
59                 Z    =        -1849474
46
 XDOT =       3673
345722                 XDOT =        1119
635776
 YDOT =     -15246
457602  feet/sec       YDOT =       -4647
120277  meter/sec
 ZDOT =     -18557
015948                 ZDOT =       -5656
178461


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
52812058  
00010596  00000-0  82463-4 0  9133
2 25544  51
6405 104
8262 0007497 273
9771  86
0535 15
74567188 12157


Satellite: ISS
Catalog Number: 25544
Epoch time:      09207
52812058   =   yrday
fracday
Element set:     913
Inclination:       51
6405  deg
RA of node:       104
8262  deg
Eccentricity:     
0007497     
Arg of perigee:   273
9771  deg
Mean anomaly:      86
0535  deg
Mean motion:   15
74567188  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1215
Checksum:              320


Coasting Arc #15 (Orbit 1230)
---------------------------------------

Vector Time (GMT): 2009/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3354633
04                 A    =         6720075
80  meter
 Y    =       -3192728
71  meter          E    =           
0005065
 Z    =        4872681
86                 I    =           51
95508
 XDOT =       2940
078098                 Wp   =          340
86412
 YDOT =      -6709
801566  meter/sec      RA   =           99
00712  deg
 ZDOT =      -2368
357586                 TA   =          132
15006
                                          MA   =          132
10702
                                          Ha   =            187
077  n
mi
                                          Hp   =            185
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11006013
93                 X    =        -3342352
51
 Y    =      -10474831
72  feet           Y    =        -3230173
86  meter
 Z    =       15986489
04                 Z    =         4856414
78
 XDOT =       9645
925519                 XDOT =        3026
394696
 YDOT =     -22013
784666  feet/sec       YDOT =       -6676
441103  meter/sec
 ZDOT =      -7770
202055                 ZDOT =       -2353
865604

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2336731
11                 X    =         -712235
64
 Y    =       15081126
57  feet           Y    =         4596727
38  meter
 Z    =       15922361
10                 Z    =         4853135
66
 XDOT =     -22528
806463                 XDOT =       -6866
780210
 YDOT =       4667
011202  feet/sec       YDOT =        1422
505014  meter/sec
 ZDOT =      -7713
573338                 ZDOT =       -2351
097154


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
54356252  
00010596  00000-0  82463-4 0  9146
2 25544  51
6403  99
6064 0007571 279
4223  80
6085 15
74650800 12314


Satellite: ISS
Catalog Number: 25544
Epoch time:      09208
54356252   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:        99
6064  deg
Eccentricity:     
0007571     
Arg of perigee:   279
4223  deg
Mean anomaly:      80
6085  deg
Mean motion:   15
74650800  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1231
Checksum:              300

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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