Date: June 13th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 2257)
---------------------------------------

Vector Time (GMT): 2010/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3270918
05                 A    =         6728419
62  meter
 Y    =        3379782
85  meter          E    =           
0010054
 Z    =       -4818428
59                 I    =           51
30278
 XDOT =      -3237
245844                 Wp   =           24
31598
 YDOT =      -6553
706113  meter/sec      RA   =          258
91075  deg
 ZDOT =      -2392
142059                 TA   =          222
15982
                                          MA   =          222
23719
                                          Ha   =            193
465  n
mi
                                          Hp   =            189
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10731358
44                 X    =        -3285061
00
 Y    =       11088526
40  feet           Y    =         3343127
37  meter
 Z    =      -15808492
76                 Z    =        -4834352
57
 XDOT =     -10620
885314                 XDOT =       -3152
099803
 YDOT =     -21501
660476  feet/sec       YDOT =       -6589
430373  meter/sec
 ZDOT =      -7848
235102                 ZDOT =       -2407
663243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8842477
79                 X    =         2695187
23
 Y    =       12566556
36  feet           Y    =         3830286
38  meter
 Z    =      -15871930
03                 Z    =        -4837764
27
 XDOT =     -22214
178382                 XDOT =       -6770
881571
 YDOT =       5610
396627  feet/sec       YDOT =        1710
048892  meter/sec
 ZDOT =      -7910
101568                 ZDOT =       -2410
998958


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   10162
52005891  
00016717  00000-0  10270-3 0  9007
2 25544  51
6491 259
6137 0009202 307
4153  52
6171 15
71760772 22589


Satellite: ISS
Catalog Number: 25544
Epoch time:      10162
52005891   =   yrday
fracday
Element set:     900
Inclination:       51
6491  deg
RA of node:       259
6137  deg
Eccentricity:     
0009202     
Arg of perigee:   307
4153  deg
Mean anomaly:      52
6171  deg
Mean motion:   15
71760772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2258
Checksum:              290


Coasting Arc #2 (Orbit 2273)
---------------------------------------

Vector Time (GMT): 2010/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3703471
40                 A    =         6735232
70  meter
 Y    =        4925001
84  meter          E    =           
0007526
 Z    =        2718191
63                 I    =           51
33245
 XDOT =      -2832
508352                 Wp   =           61
72822
 YDOT =       4974
566329  meter/sec      RA   =          253
72811  deg
 ZDOT =      -5139
699259                 TA   =           87
14674
                                          MA   =           87
06060
                                          Ha   =            193
663  n
mi
                                          Hp   =            188
919

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12150496
73                 X    =         3634919
34
 Y    =       16158142
53  feet           Y    =         4966032
40  meter
 Z    =        8917951
53                 Z    =         2736017
70
 XDOT =      -9293
006403                 XDOT =       -2862
956480
 YDOT =      16320
755673  feet/sec       YDOT =        4942
722367  meter/sec
 ZDOT =     -16862
530376                 ZDOT =       -5153
532574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18024672
55                 X    =         5493920
19
 Y    =       -9086194
59  feet           Y    =        -2769472
11  meter
 Z    =        8989007
02                 Z    =         2739849
34
 XDOT =      13798
921179                 XDOT =        4205
911175
 YDOT =      10590
689927  feet/sec       YDOT =        3228
042290  meter/sec
 ZDOT =     -16917
635276                 ZDOT =       -5156
495232


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   10163
53732610  
00016717  00000-0  10270-3 0  9016
2 25544  51
6485 254
4083 0009100 312
4168  47
6223 15
71785852 22740


Satellite: ISS
Catalog Number: 25544
Epoch time:      10163
53732610   =   yrday
fracday
Element set:     901
Inclination:       51
6485  deg
RA of node:       254
4083  deg
Eccentricity:     
0009100     
Arg of perigee:   312
4168  deg
Mean anomaly:      47
6223  deg
Mean motion:   15
71785852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2274
Checksum:              290


Coasting Arc #3 (Orbit 2289)
---------------------------------------

Vector Time (GMT): 2010/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1514031
17                 A    =         6731042
87  meter
 Y    =       -5120257
26  meter          E    =           
0005571
 Z    =        4092389
52                 I    =           51
32827
 XDOT =       4994
156463                 Wp   =           43
08640
 YDOT =       4487
876687  meter/sec      RA   =          248
63537  deg
 ZDOT =       3768
418628                 TA   =            8
09761
                                          MA   =            8
08862
                                          Ha   =            193
719  n
mi
                                          Hp   =            188
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4967293
86                 X    =         1551294
22
 Y    =      -16798744
30  feet           Y    =        -5103118
97  meter
 Z    =       13426474
79                 Z    =         4099834
12
 XDOT =      16385
027765                 XDOT =        4925
294758
 YDOT =      14724
004877  feet/sec       YDOT =        4543
338505  meter/sec
 ZDOT =      12363
578176                 ZDOT =        3792
513897

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15815955
23                 X    =        -4820703
16
 Y    =       -7478666
83  feet           Y    =        -2279497
65  meter
 Z    =       13456119
28                 Z    =         4101425
16
 XDOT =      16569
621545                 XDOT =        5050
420647
 YDOT =     -12629
235756  feet/sec       YDOT =       -3849
391058  meter/sec
 ZDOT =      12459
630306                 ZDOT =        3797
695317


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   10164
55457834  
00016717  00000-0  10270-3 0  9022
2 25544  51
6485 249
2015 0009221 316
1011  43
9417 15
71834289 22900


Satellite: ISS
Catalog Number: 25544
Epoch time:      10164
55457834   =   yrday
fracday
Element set:     902
Inclination:       51
6485  deg
RA of node:       249
2015  deg
Eccentricity:     
0009221     
Arg of perigee:   316
1011  deg
Mean anomaly:      43
9417  deg
Mean motion:   15
71834289  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2290
Checksum:              296


Coasting Arc #4 (Orbit 2304)
---------------------------------------

Vector Time (GMT): 2010/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4798494
34                 A    =         6731887
98  meter
 Y    =       -2779952
46  meter          E    =           
0005419
 Z    =       -3812180
26                 I    =           51
34259
 XDOT =        466
300398                 Wp   =            2
98812
 YDOT =      -6473
234969  meter/sec      RA   =          243
44498  deg
 ZDOT =       4139
122729                 TA   =          310
50706
                                          MA   =          310
55427
                                          Ha   =            193
843  n
mi
                                          Hp   =            188
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15743091
66                 X    =        -4748533
00
 Y    =       -9120578
94  feet           Y    =        -2833331
99  meter
 Z    =      -12507153
09                 Z    =        -3835370
40
 XDOT =       1529
856949                 XDOT =         518
543641
 YDOT =     -21237
647535  feet/sec       YDOT =       -6467
729223  meter/sec
 ZDOT =      13579
798981                 ZDOT =        4141
513633

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11237269
60                 X    =        -3425119
77
 Y    =       14227877
99  feet           Y    =         4336657
21  meter
 Z    =      -12599604
50                 Z    =        -3840359
45
 XDOT =     -19783
722233                 XDOT =       -6030
078537
 YDOT =      -3607
356488  feet/sec       YDOT =       -1099
522258  meter/sec
 ZDOT =      13589
288021                 ZDOT =        4142
014989


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   10165
50824266  
00016717  00000-0  10270-3 0  9036
2 25544  51
6475 244
3218 0009240 320
3421  39
7056 15
71853357 23059


Satellite: ISS
Catalog Number: 25544
Epoch time:      10165
50824266   =   yrday
fracday
Element set:     903
Inclination:       51
6475  deg
RA of node:       244
3218  deg
Eccentricity:     
0009240     
Arg of perigee:   320
3421  deg
Mean anomaly:      39
7056  deg
Mean motion:   15
71853357  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2305
Checksum:              289


Coasting Arc #5 (Orbit 2320)
---------------------------------------

Vector Time (GMT): 2010/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         753473
10                 A    =         6734184
59  meter
 Y    =        5937059
29  meter          E    =           
0006475
 Z    =       -3094261
73                 I    =           51
36353
 XDOT =      -5678
935223                 Wp   =          351
14203
 YDOT =      -1814
754569  meter/sec      RA   =          238
35626  deg
 ZDOT =      -4857
233975                 TA   =          224
87088
                                          MA   =          224
92325
                                          Ha   =            194
173  n
mi
                                          Hp   =            188
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2472024
60                 X    =          702059
05
 Y    =       19478540
96  feet           Y    =         5945198
14  meter
 Z    =      -10151777
33                 Z    =        -3090725
24
 XDOT =     -18631
677242                 XDOT =       -5634
624892
 YDOT =      -5953
919188  feet/sec       YDOT =       -1878
011209  meter/sec
 ZDOT =     -15935
807004                 ZDOT =       -4884
714682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19641825
29                 X    =         5986828
35
 Y    =        -100743
75  feet           Y    =          -30706
70  meter
 Z    =      -10137632
70                 Z    =        -3089950
45
 XDOT =      -8211
169004                 XDOT =       -2502
764312
 YDOT =      16225
042849  feet/sec       YDOT =        4945
393060  meter/sec
 ZDOT =     -16045
369217                 ZDOT =       -4890
628537


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   10166
52547222  
00016717  00000-0  10270-3 0  9044
2 25544  51
6464 239
1153 0009289 324
6487  35
4058 15
71843423 23215


Satellite: ISS
Catalog Number: 25544
Epoch time:      10166
52547222   =   yrday
fracday
Element set:     904
Inclination:       51
6464  deg
RA of node:       239
1153  deg
Eccentricity:     
0009289     
Arg of perigee:   324
6487  deg
Mean anomaly:      35
4058  deg
Mean motion:   15
71843423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2321
Checksum:              303


Coasting Arc #6 (Orbit 2336)
---------------------------------------

Vector Time (GMT): 2010/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4888581
35                 A    =         6728807
69  meter
 Y    =         378176
02  meter          E    =           
0011912
 Z    =        4611673
48                 I    =           51
36355
 XDOT =       2204
623013                 Wp   =           11
42942
 YDOT =       6785
116258  meter/sec      RA   =          233
17079  deg
 ZDOT =      -2880
628249                 TA   =          107
27643
                                          MA   =          107
14605
                                          Ha   =            194
232  n
mi
                                          Hp   =            187
755

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16038652
72                 X    =         4861586
73
 Y    =        1240734
99  feet           Y    =          432691
44  meter
 Z    =       15130162
34                 Z    =         4635356
47
 XDOT =       7233
015135                 XDOT =        2142
580198
 YDOT =      22260
880113  feet/sec       YDOT =        6809
423194  meter/sec
 ZDOT =      -9450
880081                 ZDOT =       -2870
067986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2936349
08                 X    =          894999
20
 Y    =      -15725441
75  feet           Y    =        -4793114
65  meter
 Z    =       15224583
83                 Z    =         4640453
15
 XDOT =      21764
623752                 XDOT =        6633
857320
 YDOT =      -5085
361015  feet/sec       YDOT =       -1550
018037  meter/sec
 ZDOT =      -9408
714363                 ZDOT =       -2867
776138


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   10167
54268687  
00016717  00000-0  10270-3 0  9053
2 25544  51
6469 233
9082 0009509 328
4179  31
6411 15
71906718 23373


Satellite: ISS
Catalog Number: 25544
Epoch time:      10167
54268687   =   yrday
fracday
Element set:     905
Inclination:       51
6469  deg
RA of node:       233
9082  deg
Eccentricity:     
0009509     
Arg of perigee:   328
4179  deg
Mean anomaly:      31
6411  deg
Mean motion:   15
71906718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2337
Checksum:              330


Coasting Arc #7 (Orbit 2352)
---------------------------------------

Vector Time (GMT): 2010/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3062068
60                 A    =         6736710
89  meter
 Y    =       -5678852
64  meter          E    =           
0016551
 Z    =        1900089
87                 I    =           51
40799
 XDOT =       5195
711056                 Wp   =           32
29972
 YDOT =       -920
207227  meter/sec      RA   =          228
07261  deg
 ZDOT =       5614
156409                 TA   =          348
88930
                                          MA   =          348
92581
                                          Ha   =            194
543  n
mi
                                          Hp   =            187
568

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10046156
83                 X    =        -3007569
29
 Y    =      -18631406
30  feet           Y    =        -5712790
03  meter
 Z    =        6233890
66                 Z    =         1885346
11
 XDOT =      17046
296116                 XDOT =        5178
342470
 YDOT =      -3019
052583  feet/sec       YDOT =        -862
203508  meter/sec
 ZDOT =      18419
148323                 ZDOT =        5639
354686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19459769
29                 X    =        -5931337
68
 Y    =        8372703
71  feet           Y    =         2552000
09  meter
 Z    =        6175044
29                 Z    =         1882153
50
 XDOT =       -878
031888                 XDOT =        -267
624119
 YDOT =     -15720
524214  feet/sec       YDOT =       -4791
615781  meter/sec
 ZDOT =      18519
605019                 ZDOT =        5644
775610


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   10168
55989263  
00016717  00000-0  10270-3 0  9066
2 25544  51
6462 228
7013 0009461 333
9388  26
1296 15
71871070 23532


Satellite: ISS
Catalog Number: 25544
Epoch time:      10168
55989263   =   yrday
fracday
Element set:     906
Inclination:       51
6462  deg
RA of node:       228
7013  deg
Eccentricity:     
0009461     
Arg of perigee:   333
9388  deg
Mean anomaly:      26
1296  deg
Mean motion:   15
71871070  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2353
Checksum:              322


Coasting Arc #8 (Orbit 2367)
---------------------------------------

Vector Time (GMT): 2010/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3952374
56                 A    =         6726768
21  meter
 Y    =        1896059
60  meter          E    =           
0011827
 Z    =       -5109656
05                 I    =           51
39575
 XDOT =      -4689
123170                 Wp   =           58
65626
 YDOT =      -5924
885626  meter/sec      RA   =          222
90704  deg
 ZDOT =       1437
018694                 TA   =          225
12795
                                          MA   =          225
22405
                                          Ha   =            194
622  n
mi
                                          Hp   =            187
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12967108
14                 X    =        -3948461
20
 Y    =        6220667
99  feet           Y    =         1851884
25  meter
 Z    =      -16763963
41                 Z    =        -5128846
90
 XDOT =     -15384
262369                 XDOT =       -4629
502270
 YDOT =     -19438
601136  feet/sec       YDOT =       -5976
989001  meter/sec
 ZDOT =       4714
628262                 ZDOT =        1414
383160

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5271316
50                 X    =         1606697
27
 Y    =       13284772
27  feet           Y    =         4049198
59  meter
 Z    =      -16840460
83                 Z    =        -5132972
46
 XDOT =     -19535
414573                 XDOT =       -5954
394362
 YDOT =      13578
342162  feet/sec       YDOT =        4138
678691  meter/sec
 ZDOT =       4624
301961                 ZDOT =        1409
487238


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   10169
51350930  
00016717  00000-0  10270-3 0  9077
2 25544  51
6460 223
8198 0009557 337
2768  22
7970 15
71890542 23687


Satellite: ISS
Catalog Number: 25544
Epoch time:      10169
51350930   =   yrday
fracday
Element set:     907
Inclination:       51
6460  deg
RA of node:       223
8198  deg
Eccentricity:     
0009557     
Arg of perigee:   337
2768  deg
Mean anomaly:      22
7970  deg
Mean motion:   15
71890542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2368
Checksum:              328


Coasting Arc #9 (Orbit 2383)
---------------------------------------

Vector Time (GMT): 2010/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4989450
90                 A    =         6737873
02  meter
 Y    =        4487658
18  meter          E    =           
0004257
 Z    =        -613878
60                 I    =           51
45722
 XDOT =      -3621
886580                 Wp   =           79
18685
 YDOT =       3214
309604  meter/sec      RA   =          217
78995  deg
 ZDOT =      -5974
383229                 TA   =          107
50163
                                          MA   =          107
45510
                                          Ha   =            194
796  n
mi
                                          Hp   =            186
945

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16369589
56                 X    =         4941880
38
 Y    =       14723287
98  feet           Y    =         4543187
28  meter
 Z    =       -2014037
40                 Z    =         -589754
86
 XDOT =     -11882
829986                 XDOT =       -3628
537880
 YDOT =      10545
635183  feet/sec       YDOT =        3173
770997  meter/sec
 ZDOT =     -19600
994845                 ZDOT =       -5991
994167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15606535
29                 X    =         4756871
96
 Y    =      -15541980
98  feet           Y    =        -4737195
80  meter
 Z    =       -1917785
51                 Z    =         -584541
02
 XDOT =       8744
854489                 XDOT =        2665
431648
 YDOT =      11193
905914  feet/sec       YDOT =        3411
902523  meter/sec
 ZDOT =     -19671
179637                 ZDOT =       -5995
775553


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   10170
53068883  
00016717  00000-0  10270-3 0  9085
2 25544  51
6467 218
6126 0009586 342
1950  17
8875 15
71945891 23842


Satellite: ISS
Catalog Number: 25544
Epoch time:      10170
53068883   =   yrday
fracday
Element set:     908
Inclination:       51
6467  deg
RA of node:       218
6126  deg
Eccentricity:     
0009586     
Arg of perigee:   342
1950  deg
Mean anomaly:      17
8875  deg
Mean motion:   15
71945891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2384
Checksum:              341


Coasting Arc #10 (Orbit 2399)
---------------------------------------

Vector Time (GMT): 2010/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2218031
34                 A    =         6725917
59  meter
 Y    =       -3557744
46  meter          E    =           
0009099
 Z    =        5259202
72                 I    =           51
44108
 XDOT =       6503
924694                 Wp   =             
58062
 YDOT =       4118
454367  meter/sec      RA   =          212
65170  deg
 ZDOT =         52
023732                 TA   =           88
97635
                                          MA   =           88
87210
                                          Ha   =            194
830  n
mi
                                          Hp   =            186
719

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7277005
70                 X    =         2232101
45
 Y    =      -11672389
97  feet           Y    =        -3532863
11  meter
 Z    =       17254602
08                 Z    =         5270011
69
 XDOT =      21338
335609                 XDOT =        6457
135278
 YDOT =      13511
989393  feet/sec       YDOT =        4190
923510  meter/sec
 ZDOT =        170
681536                 ZDOT =          83
506834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11389883
36                 X    =        -3471636
45
 Y    =       -7614606
72  feet           Y    =        -2320932
13  meter
 Z    =       17297662
10                 Z    =         5272327
41
 XDOT =      13760
154532                 XDOT =        4194
095101
 YDOT =     -19975
890149  feet/sec       YDOT =       -6088
651317  meter/sec
 ZDOT =        296
284569                 ZDOT =          90
307537


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   10171
54785563  
00016717  00000-0  10270-3 0  9099
2 25544  51
6461 213
4056 0009568 346
0023  14
0873 15
71959401 24003


Satellite: ISS
Catalog Number: 25544
Epoch time:      10171
54785563   =   yrday
fracday
Element set:     909
Inclination:       51
6461  deg
RA of node:       213
4056  deg
Eccentricity:     
0009568     
Arg of perigee:   346
0023  deg
Mean anomaly:      14
0873  deg
Mean motion:   15
71959401  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2400
Checksum:              296


Coasting Arc #11 (Orbit 2414)
---------------------------------------

Vector Time (GMT): 2010/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6172309
47                 A    =         6737778
85  meter
 Y    =       -2577230
27  meter          E    =           
0018389
 Z    =        -711113
95                 I    =           51
50733
 XDOT =       1277
200622                 Wp   =           16
23013
 YDOT =      -4692
579693  meter/sec      RA   =          207
51266  deg
 ZDOT =       5975
507423                 TA   =          336
00711
                                          MA   =          336
09268
                                          Ha   =            195
054  n
mi
                                          Hp   =            186
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20250359
14                 X    =        -6139577
18
 Y    =       -8455479
88  feet           Y    =        -2646069
59  meter
 Z    =       -2333051
02                 Z    =         -741020
13
 XDOT =       4190
290753                 XDOT =        1300
550829
 YDOT =     -15395
602667  feet/sec       YDOT =       -4678
167602  meter/sec
 ZDOT =      19604
683147                 ZDOT =        5981
768133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8877044
02                 X    =        -2705723
02
 Y    =       20054908
43  feet           Y    =         6112736
09  meter
 Z    =       -2452355
97                 Z    =         -747478
10
 XDOT =     -13843
932971                 XDOT =       -4219
630770
 YDOT =      -3748
252463  feet/sec       YDOT =       -1142
467351  meter/sec
 ZDOT =      19629
594201                 ZDOT =        5983
100313


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   10172
50143908  
00016717  00000-0  10270-3 0  9109
2 25544  51
6464 208
5240 0009732 350
0258  10
0709 15
71949639 24156


Satellite: ISS
Catalog Number: 25544
Epoch time:      10172
50143908   =   yrday
fracday
Element set:     910
Inclination:       51
6464  deg
RA of node:       208
5240  deg
Eccentricity:     
0009732     
Arg of perigee:   350
0258  deg
Mean anomaly:      10
0709  deg
Mean motion:   15
71949639  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2415
Checksum:              289


Coasting Arc #12 (Orbit 2430)
---------------------------------------

Vector Time (GMT): 2010/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          47238
78                 A    =         6726710
93  meter
 Y    =        4405105
04  meter          E    =           
0017536
 Z    =       -5096972
07                 I    =           51
49786
 XDOT =      -7336
134117                 Wp   =           45
32501
 YDOT =      -1705
256862  meter/sec      RA   =          202
40320  deg
 ZDOT =      -1532
891583                 TA   =          209
86061
                                          MA   =          209
96078
                                          Ha   =            195
172  n
mi
                                          Hp   =            186
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         154982
88                 X    =           22736
93
 Y    =       14452444
34  feet           Y    =         4405497
16  meter
 Z    =      -16722349
32                 Z    =        -5096801
34
 XDOT =     -24068
681486                 XDOT =       -7309
073821
 YDOT =      -5594
674745  feet/sec       YDOT =       -1787
142321  meter/sec
 ZDOT =      -5029
171859                 ZDOT =       -1568
465349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14452739
99                 X    =         4405195
15
 Y    =        -200017
74  feet           Y    =          -60965
41  meter
 Z    =      -16721615
76                 Z    =        -5096748
48
 XDOT =      -5698
790262                 XDOT =       -1736
991272
 YDOT =      22963
668271  feet/sec       YDOT =        6999
326089  meter/sec
 ZDOT =      -5171
084297                 ZDOT =       -1576
146494


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   10173
51858195  
00016717  00000-0  10270-3 0  9113
2 25544  51
6467 203
3169 0009623 353
8259   6
2783 15
71975028 24311


Satellite: ISS
Catalog Number: 25544
Epoch time:      10173
51858195   =   yrday
fracday
Element set:     911
Inclination:       51
6467  deg
RA of node:       203
3169  deg
Eccentricity:     
0009623     
Arg of perigee:   353
8259  deg
Mean anomaly:       6
2783  deg
Mean motion:   15
71975028  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2431
Checksum:              318


Coasting Arc #13 (Orbit 2446)
---------------------------------------

Vector Time (GMT): 2010/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6438738
70                 A    =         6736126
50  meter
 Y    =         386259
24  meter          E    =           
0013554
 Z    =        1939811
02                 I    =           51
55701
 XDOT =       1392
907664                 Wp   =           71
13602
 YDOT =       5087
114939  meter/sec      RA   =          197
24431  deg
 ZDOT =      -5600
217730                 TA   =           87
29033
                                          MA   =           87
13519
                                          Ha   =            195
275  n
mi
                                          Hp   =            185
865

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21124470
81                 X    =         6424517
64
 Y    =        1267254
74  feet           Y    =          458181
17  meter
 Z    =        6364209
38                 Z    =         1971056
10
 XDOT =       4569
907035                 XDOT =        1363
124072
 YDOT =      16690
009641  feet/sec       YDOT =        5102
525804  meter/sec
 ZDOT =     -18373
417750                 ZDOT =       -5593
522322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         983049
30                 X    =          299633
43
 Y    =      -21101675
86  feet           Y    =        -6431790
80  meter
 Z    =        6488856
02                 Z    =         1977803
32
 XDOT =      15086
050836                 XDOT =        4598
228295
 YDOT =      -4974
653373  feet/sec       YDOT =       -1516
274348  meter/sec
 ZDOT =     -18346
650060                 ZDOT =       -5592
058938


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   10174
53571165  
00016717  00000-0  10270-3 0  9126
2 25544  51
6452 198
1093 0009738 358
4718   1
6412 15
72018587 24474


Satellite: ISS
Catalog Number: 25544
Epoch time:      10174
53571165   =   yrday
fracday
Element set:     912
Inclination:       51
6452  deg
RA of node:       198
1093  deg
Eccentricity:     
0009738     
Arg of perigee:   358
4718  deg
Mean anomaly:       1
6412  deg
Mean motion:   15
72018587  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2447
Checksum:              314


Coasting Arc #14 (Orbit 2462)
---------------------------------------

Vector Time (GMT): 2010/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2372468
24                 A    =         6728583
21  meter
 Y    =       -4264511
97  meter          E    =           
0010017
 Z    =        4622730
39                 I    =           51
55981
 XDOT =       7095
199190                 Wp   =           52
33339
 YDOT =       -817
297177  meter/sec      RA   =          192
15775  deg
 ZDOT =       2889
186703                 TA   =            9
07002
                                          MA   =            9
05194
                                          Ha   =            195
460  n
mi
                                          Hp   =            185
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7783688
47                 X    =        -2347061
78
 Y    =      -13991180
99  feet           Y    =        -4290901
21  meter
 Z    =       15166438
27                 Z    =         4611265
76
 XDOT =      23278
212565                 XDOT =        7089
775862
 YDOT =      -2681
421186  feet/sec       YDOT =        -737
985344  meter/sec
 ZDOT =       9478
959000                 ZDOT =        2923
641886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13742539
88                 X    =        -4188726
15
 Y    =        8298695
68  feet           Y    =         2529442
44  meter
 Z    =       15120649
76                 Z    =         4608774
05
 XDOT =      -2787
146817                 XDOT =        -849
522350
 YDOT =     -22126
490419  feet/sec       YDOT =       -6744
154280  meter/sec
 ZDOT =       9616
417116                 ZDOT =        2931
083937


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   10175
55282936  
00016717  00000-0  10270-3 0  9135
2 25544  51
6444 192
9014 0009774   2
6350 357
4862 15
72017652 24631


Satellite: ISS
Catalog Number: 25544
Epoch time:      10175
55282936   =   yrday
fracday
Element set:     913
Inclination:       51
6444  deg
RA of node:       192
9014  deg
Eccentricity:     
0009774     
Arg of perigee:     2
6350  deg
Mean anomaly:     357
4862  deg
Mean motion:   15
72017652  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2463
Checksum:              310


Coasting Arc #15 (Orbit 2477)
---------------------------------------

Vector Time (GMT): 2010/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 799347
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5725356
62                 A    =         6733529
15  meter
 Y    =        1751336
45  meter          E    =           
0012144
 Z    =       -3072890
56                 I    =           51
60754
 XDOT =      -3971
722303                 Wp   =           26
90812
 YDOT =      -4404
749098  meter/sec      RA   =          186
98803  deg
 ZDOT =       4907
797185                 TA   =          297
45957
                                          MA   =          297
58300
                                          Ha   =            195
406  n
mi
                                          Hp   =            185
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18783978
42                 X    =        -5729587
37
 Y    =        5745854
49  feet           Y    =         1687289
08  meter
 Z    =      -10081661
94                 Z    =        -3100714
17
 XDOT =     -13030
584984                 XDOT =       -3946
013517
 YDOT =     -14451
276567  feet/sec       YDOT =       -4449
020535  meter/sec
 ZDOT =      16101
696800                 ZDOT =        4888
564152

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6635235
96                 X    =         2022419
92
 Y    =       18427581
40  feet           Y    =         5616726
81  meter
 Z    =      -10192668
15                 Z    =        -3106725
25
 XDOT =     -12462
108710                 XDOT =       -3798
450735
 YDOT =      13318
349401  feet/sec       YDOT =        4059
432897  meter/sec
 ZDOT =      16024
901683                 ZDOT =        4884
390033


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   10176
50636449  
00016717  00000-0  10270-3 0  9144
2 25544  51
6451 188
0202 0009827   5
9584 354
1693 15
72052402 24782


Satellite: ISS
Catalog Number: 25544
Epoch time:      10176
50636449   =   yrday
fracday
Element set:     914
Inclination:       51
6451  deg
RA of node:       188
0202  deg
Eccentricity:     
0009827     
Arg of perigee:     5
9584  deg
Mean anomaly:     354
1693  deg
Mean motion:   15
72052402  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2478
Checksum:              310

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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