Date: November 17th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6727 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 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 1218)
---------------------------------------

Vector Time (GMT): 2008/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -850197
50                 A    =         6727383
51  meter
 Y    =        4938178
11  meter          E    =           
0010376
 Z    =        4486450
85                 I    =           51
44457
 XDOT =      -6826
054614                 Wp   =           44
33038
 YDOT =       1685
566550  meter/sec      RA   =          325
29807  deg
 ZDOT =      -3137
168865                 TA   =           77
13043
                                          MA   =           77
01453
                                          Ha   =            192
464  n
mi
                                          Hp   =            186
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2789361
87                 X    =         -927148
86
 Y    =       16201371
76  feet           Y    =         4928239
93  meter
 Z    =       14719326
92                 Z    =         4482134
11
 XDOT =     -22395
192303                 XDOT =       -6829
155287
 YDOT =       5530
073984  feet/sec       YDOT =        1609
216694  meter/sec
 ZDOT =     -10292
548770                 ZDOT =       -3170
338211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11252340
88                 X    =        -3429713
50
 Y    =      -12005501
08  feet           Y    =        -3659276
73  meter
 Z    =       14702936
44                 Z    =         4481455
03
 XDOT =       8074
763078                 XDOT =        2461
187786
 YDOT =     -20377
565433  feet/sec       YDOT =       -6211
081944  meter/sec
 ZDOT =     -10420
993662                 ZDOT =       -3176
318868


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   08319
54208022  
00020000  00000-0  20000-3 0  9003
2 25544  51
6411 325
6449 0004071 346
4237  13
6815 15
72621174 12197


Satellite: ISS
Catalog Number: 25544
Epoch time:      08319
54208022   =   yrday
fracday
Element set:     900
Inclination:       51
6411  deg
RA of node:       325
6449  deg
Eccentricity:     
0004071     
Arg of perigee:   346
4237  deg
Mean anomaly:      13
6815  deg
Mean motion:   15
72621174  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1219
Checksum:              262


Coasting Arc #2 (Orbit 1234)
---------------------------------------

Vector Time (GMT): 2008/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5821316
99                 A    =         6733594
31  meter
 Y    =       -2411987
91  meter          E    =           
0014870
 Z    =        2349592
36                 I    =           51
44230
 XDOT =         99
944481                 Wp   =           57
76404
 YDOT =       5505
735358  meter/sec      RA   =          320
20356  deg
 ZDOT =       5387
347840                 TA   =          328
77381
                                          MA   =          328
86206
                                          Ha   =            192
408  n
mi
                                          Hp   =            185
994

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19098809
02                 X    =         5836441
40
 Y    =       -7913346
16  feet           Y    =        -2346806
32  meter
 Z    =        7708636
36                 Z    =         2377909
43
 XDOT =        327
901840                 XDOT =          12
199636
 YDOT =      18063
436214  feet/sec       YDOT =        5506
361693  meter/sec
 ZDOT =      17675
025723                 ZDOT =        5387
620955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4731482
29                 X    =        -1442155
80
 Y    =       20082254
52  feet           Y    =         6121071
18  meter
 Z    =        7818232
30                 Z    =         2382997
21
 XDOT =     -13316
812333                 XDOT =       -4058
964399
 YDOT =     -10040
521084  feet/sec       YDOT =       -3060
350826  meter/sec
 ZDOT =      17676
463135                 ZDOT =        5387
785964


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   08320
55881000  
00020000  00000-0  20000-3 0  9010
2 25544  51
6410 320
4346 0004062 349
5218  10
5859 15
72639347 12351


Satellite: ISS
Catalog Number: 25544
Epoch time:      08320
55881000   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:       320
4346  deg
Eccentricity:     
0004062     
Arg of perigee:   349
5218  deg
Mean anomaly:      10
5859  deg
Mean motion:   15
72639347  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1235
Checksum:              263


Coasting Arc #3 (Orbit 1249)
---------------------------------------

Vector Time (GMT): 2008/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -982718
38                 A    =         6725754
21  meter
 Y    =       -4529792
17  meter          E    =           
0011369
 Z    =       -4883034
13                 I    =           51
39362
 XDOT =       6312
408079                 Wp   =           86
54520
 YDOT =      -3778
694890  meter/sec      RA   =          315
02356  deg
 ZDOT =       2240
118706                 TA   =          205
31220
                                          MA   =          205
36794
                                          Ha   =            192
615  n
mi
                                          Hp   =            185
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3224141
67                 X    =         -908271
17
 Y    =      -14861522
86  feet           Y    =        -4540364
63  meter
 Z    =      -16020453
19                 Z    =        -4887627
98
 XDOT =      20710
000259                 XDOT =        6343
310628
 YDOT =     -12397
292946  feet/sec       YDOT =       -3707
933387  meter/sec
 ZDOT =       7349
470821                 ZDOT =        2270
859511

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13988586
90                 X    =         4263721
29
 Y    =        5915947
39  feet           Y    =         1803180
76  meter
 Z    =      -16038574
58                 Z    =        -4888557
53
 XDOT =      -1194
337626                 XDOT =        -364
034109
 YDOT =      23025
560827  feet/sec       YDOT =        7018
190940  meter/sec
 ZDOT =       7468
374812                 ZDOT =        2276
360643


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   08321
51198266  
00020000  00000-0  20000-3 0  9023
2 25544  51
6408 315
5494 0004174 353
5498   6
5610 15
72617945 12503


Satellite: ISS
Catalog Number: 25544
Epoch time:      08321
51198266   =   yrday
fracday
Element set:     902
Inclination:       51
6408  deg
RA of node:       315
5494  deg
Eccentricity:     
0004174     
Arg of perigee:   353
5498  deg
Mean anomaly:       6
5610  deg
Mean motion:   15
72617945  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1250
Checksum:              288


Coasting Arc #4 (Orbit 1265)
---------------------------------------

Vector Time (GMT): 2008/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5086815
90                 A    =         6734868
48  meter
 Y    =        4123189
86  meter          E    =           
0005239
 Z    =       -1573714
25                 I    =           51
40447
 XDOT =      -2039
895563                 Wp   =          113
99615
 YDOT =      -4700
513556  meter/sec      RA   =          309
91365  deg
 ZDOT =      -5738
970191                 TA   =           83
40075
                                          MA   =           83
34112
                                          Ha   =            192
687  n
mi
                                          Hp   =            185
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16689028
53                 X    =        -5124899
10
 Y    =       13527525
80  feet           Y    =         4066093
38  meter
 Z    =       -5163104
49                 Z    =        -1598518
38
 XDOT =      -6692
570746                 XDOT =       -1959
302829
 YDOT =     -15421
632403  feet/sec       YDOT =       -4722
873633  meter/sec
 ZDOT =     -18828
642360                 ZDOT =       -5748
684853

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1959032
63                 X    =         -597113
15
 Y    =      -21370087
99  feet           Y    =        -6513602
82  meter
 Z    =       -5258973
85                 Z    =        -1602935
23
 XDOT =      14917
633475                 XDOT =        4546
894683
 YDOT =       3261
791731  feet/sec       YDOT =         994
194119  meter/sec
 ZDOT =     -18866
632876                 ZDOT =       -5750
549701


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   08322
52868666  
00020000  00000-0  20000-3 0  9034
2 25544  51
6403 310
3380 0004214 358
8639   1
2513 15
72662202 12662


Satellite: ISS
Catalog Number: 25544
Epoch time:      08322
52868666   =   yrday
fracday
Element set:     903
Inclination:       51
6403  deg
RA of node:       310
3380  deg
Eccentricity:     
0004214     
Arg of perigee:   358
8639  deg
Mean anomaly:       1
2513  deg
Mean motion:   15
72662202  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1266
Checksum:              268


Coasting Arc #5 (Orbit 1281)
---------------------------------------

Vector Time (GMT): 2008/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2509830
87                 A    =         6724475
73  meter
 Y    =        3563747
37  meter          E    =           
0007716
 Z    =        5118693
93                 I    =           51
35119
 XDOT =      -5156
680764                 Wp   =           27
78140
 YDOT =       5560
964547  meter/sec      RA   =          304
74332  deg
 ZDOT =      -1335
668865                 TA   =           75
09310
                                          MA   =           75
00767
                                          Ha   =            192
653  n
mi
                                          Hp   =            185
634

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8234353
25                 X    =         2444927
99
 Y    =       11692084
55  feet           Y    =         3591450
45  meter
 Z    =       16793615
27                 Z    =         5130729
45
 XDOT =     -16918
243977                 XDOT =       -5211
992615
 YDOT =      18244
634340  feet/sec       YDOT =        5502
990403  meter/sec
 ZDOT =      -4382
115698                 ZDOT =       -1360
854184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14236862
06                 X    =        -4339395
56
 Y    =         493189
77  feet           Y    =          150324
24  meter
 Z    =       16840530
00                 Z    =         5132993
54
 XDOT =      -6126
241832                 XDOT =       -1867
278510
 YDOT =     -23050
400593  feet/sec       YDOT =       -7025
762101  meter/sec
 ZDOT =      -4479
359802                 ZDOT =       -1365
308868


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   08323
54537631  
00020000  00000-0  20000-3 0  9043
2 25544  51
6398 305
1270 0004268    
6826 359
4342 15
72682749 12828


Satellite: ISS
Catalog Number: 25544
Epoch time:      08323
54537631   =   yrday
fracday
Element set:     904
Inclination:       51
6398  deg
RA of node:       305
1270  deg
Eccentricity:     
0004268     
Arg of perigee:      
6826  deg
Mean anomaly:     359
4342  deg
Mean motion:   15
72682749  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1282
Checksum:              293


Coasting Arc #6 (Orbit 1297)
---------------------------------------

Vector Time (GMT): 2008/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3813657
34                 A    =         6735483
68  meter
 Y    =       -5489090
01  meter          E    =           
0016512
 Z    =         754175
84                 I    =           51
37308
 XDOT =       3586
748328                 Wp   =           42
47728
 YDOT =       3318
902195  meter/sec      RA   =          299
61750  deg
 ZDOT =       5954
935156                 TA   =          325
77446
                                          MA   =          325
88077
                                          Ha   =            192
637  n
mi
                                          Hp   =            185
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12511999
14                 X    =         3871090
11
 Y    =      -18008825
48  feet           Y    =        -5446122
40  meter
 Z    =        2474330
20                 Z    =          772841
98
 XDOT =      11767
547008                 XDOT =        3520
440947
 YDOT =      10888
786728  feet/sec       YDOT =        3358
640209  meter/sec
 ZDOT =      19537
188831                 ZDOT =        5972
198886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8695929
62                 X    =         2650519
35
 Y    =       20121813
80  feet           Y    =         6133128
85  meter
 Z    =        2546300
23                 Z    =          776112
31
 XDOT =     -13933
829015                 XDOT =       -4247
031084
 YDOT =       3515
177192  feet/sec       YDOT =        1071
426008  meter/sec
 ZDOT =      19604
361450                 ZDOT =        5975
409370


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   08324
56205070  
00020000  00000-0  20000-3 0  9056
2 25544  51
6397 299
9166 0004084   5
7993 354
3216 15
72751227 12987


Satellite: ISS
Catalog Number: 25544
Epoch time:      08324
56205070   =   yrday
fracday
Element set:     905
Inclination:       51
6397  deg
RA of node:       299
9166  deg
Eccentricity:     
0004084     
Arg of perigee:     5
7993  deg
Mean anomaly:     354
3216  deg
Mean motion:   15
72751227  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1298
Checksum:              305


Coasting Arc #7 (Orbit 1312)
---------------------------------------

Vector Time (GMT): 2008/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3630997
87                 A    =         6723842
11  meter
 Y    =       -2158230
11  meter          E    =           
0015955
 Z    =       -5244652
60                 I    =           51
32007
 XDOT =       3476
940104                 Wp   =           77
45331
 YDOT =      -6843
999559  meter/sec      RA   =          294
45918  deg
 ZDOT =        413
682731                 TA   =          196
47333
                                          MA   =          196
52523
                                          Ha   =            192
835  n
mi
                                          Hp   =            185
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11912722
68                 X    =        -3581116
42
 Y    =       -7080807
45  feet           Y    =        -2198554
92  meter
 Z    =      -17206865
47                 Z    =        -5262171
14
 XDOT =      11407
283806                 XDOT =        3551
202785
 YDOT =     -22454
066795  feet/sec       YDOT =       -6804
703196  meter/sec
 ZDOT =       1357
226809                 ZDOT =         430
754040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12140760
29                 X    =         3700503
74
 Y    =       -6504246
86  feet           Y    =        -1982494
44  meter
 Z    =      -17274945
08                 Z    =        -5265403
26
 XDOT =      12945
201298                 XDOT =        3945
697356
 YDOT =      20423
029839  feet/sec       YDOT =        6224
939495  meter/sec
 ZDOT =       1422
908272                 ZDOT =         433
702441


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   08325
51517370  
00020000  00000-0  20000-3 0  9062
2 25544  51
6397 295
0307 0004342   8
8633 351
2605 15
72711374 13138


Satellite: ISS
Catalog Number: 25544
Epoch time:      08325
51517370   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:       295
0307  deg
Eccentricity:     
0004342     
Arg of perigee:     8
8633  deg
Mean anomaly:     351
2605  deg
Mean motion:   15
72711374  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1313
Checksum:              272


Coasting Arc #8 (Orbit 1328)
---------------------------------------

Vector Time (GMT): 2008/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2213167
57                 A    =         6735719
95  meter
 Y    =        6358675
35  meter          E    =           
0010532
 Z    =          18234
03                 I    =           51
34979
 XDOT =      -4547
312174                 Wp   =          113
65763
 YDOT =      -1557
633140  meter/sec      RA   =          289
31479  deg
 ZDOT =      -6010
275925                 TA   =           66
14368
                                          MA   =           66
03334
                                          Ha   =            192
874  n
mi
                                          Hp   =            185
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7261048
47                 X    =        -2284195
41
 Y    =       20861795
76  feet           Y    =         6333529
29  meter
 Z    =          59822
93                 Z    =            7309
95
 XDOT =     -14919
003196                 XDOT =       -4500
359170
 YDOT =      -5110
344947  feet/sec       YDOT =       -1608
221094  meter/sec
 ZDOT =     -19718
753035                 ZDOT =       -6032
253141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14466246
34                 X    =        -4409311
88
 Y    =      -16693361
58  feet           Y    =        -5088136
61  meter
 Z    =          17944
15                 Z    =            5469
38
 XDOT =      10592
801664                 XDOT =        3228
685947
 YDOT =      -9233
038174  feet/sec       YDOT =       -2814
230035  meter/sec
 ZDOT =     -19804
076497                 ZDOT =       -6036
282516


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   08326
53182225  
00020000  00000-0  20000-3 0  9073
2 25544  51
6399 289
8191 0004457  11
8699 348
2568 15
72755533 13291


Satellite: ISS
Catalog Number: 25544
Epoch time:      08326
53182225   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       289
8191  deg
Eccentricity:     
0004457     
Arg of perigee:    11
8699  deg
Mean anomaly:     348
2568  deg
Mean motion:   15
72755533  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1329
Checksum:              326


Coasting Arc #9 (Orbit 1344)
---------------------------------------

Vector Time (GMT): 2008/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4190469
61                 A    =         6723660
59  meter
 Y    =         516273
02  meter          E    =           
0004944
 Z    =        5229337
65                 I    =           51
30097
 XDOT =      -1513
497826                 Wp   =           47
17811
 YDOT =       7537
646626  meter/sec      RA   =          284
17089  deg
 ZDOT =        471
695481                 TA   =           38
33900
                                          MA   =           38
30386
                                          Ha   =            192
769  n
mi
                                          Hp   =            185
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13748259
89                 X    =         4158981
40
 Y    =        1693809
11  feet           Y    =          562957
03  meter
 Z    =       17156619
57                 Z    =         5249618
91
 XDOT =      -4965
544049                 XDOT =       -1599
963992
 YDOT =      24729
811765  feet/sec       YDOT =        7520
238344  meter/sec
 ZDOT =       1547
557351                 ZDOT =         464
132977

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8081762
11                 X    =        -2463321
09
 Y    =       11129380
59  feet           Y    =         3392235
20  meter
 Z    =       17235290
64                 Z    =         5253316
59
 XDOT =     -18431
263576                 XDOT =       -5617
849138
 YDOT =     -15720
844842  feet/sec       YDOT =       -4791
713508  meter/sec
 ZDOT =       1518
803562                 ZDOT =         462
931326


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   08327
54845694  
00020000  00000-0  20000-3 0  9082
2 25544  51
6401 284
6083 0004432  14
8148 345
3143 15
72774473 13452


Satellite: ISS
Catalog Number: 25544
Epoch time:      08327
54845694   =   yrday
fracday
Element set:     908
Inclination:       51
6401  deg
RA of node:       284
6083  deg
Eccentricity:     
0004432     
Arg of perigee:    14
8148  deg
Mean anomaly:     345
3143  deg
Mean motion:   15
72774473  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1345
Checksum:              296


Coasting Arc #10 (Orbit 1359)
---------------------------------------

Vector Time (GMT): 2008/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         408168
22                 A    =         6735336
34  meter
 Y    =       -6667673
05  meter          E    =           
0014620
 Z    =        -801105
99                 I    =           51
33435
 XDOT =       4880
052636                 Wp   =           33
28465
 YDOT =       -407
787782  meter/sec      RA   =          279
00955  deg
 ZDOT =       5943
739450                 TA   =          317
94371
                                          MA   =          318
05584
                                          Ha   =            192
922  n
mi
                                          Hp   =            184
946

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1339134
59                 X    =          486588
62
 Y    =      -21875567
76  feet           Y    =        -6662670
17  meter
 Z    =       -2628300
50                 Z    =         -798932
87
 XDOT =      16010
671377                 XDOT =        4855
375550
 YDOT =      -1337
886425  feet/sec       YDOT =        -353
354453  meter/sec
 ZDOT =      19500
457513                 ZDOT =        5967
387381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18694077
55                 X    =         5697954
84
 Y    =       11441450
70  feet           Y    =         3487354
17  meter
 Z    =       -2620377
86                 Z    =         -798691
17
 XDOT =      -5429
377943                 XDOT =       -1654
874397
 YDOT =      13310
406330  feet/sec       YDOT =        4057
011849  meter/sec
 ZDOT =      19592
112840                 ZDOT =        5971
675994


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   08328
50153892  
00020000  00000-0  20000-3 0  9092
2 25544  51
6399 279
7223 0004417  19
2446 340
8883 15
72792660 13608


Satellite: ISS
Catalog Number: 25544
Epoch time:      08328
50153892   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       279
7223  deg
Eccentricity:     
0004417     
Arg of perigee:    19
2446  deg
Mean anomaly:     340
8883  deg
Mean motion:   15
72792660  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1360
Checksum:              312


Coasting Arc #11 (Orbit 1375)
---------------------------------------

Vector Time (GMT): 2008/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4199139
72                 A    =         6724087
08  meter
 Y    =        1203265
84  meter          E    =           
0016905
 Z    =       -5126717
17                 I    =           51
29416
 XDOT =       -548
411342                 Wp   =           66
92949
 YDOT =      -7552
394222  meter/sec      RA   =          273
87848  deg
 ZDOT =      -1320
328576                 TA   =          190
33721
                                          MA   =          190
37201
                                          Ha   =            192
970  n
mi
                                          Hp   =            184
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13776705
12                 X    =        -4187377
39
 Y    =        3947722
56  feet           Y    =         1156374
71  meter
 Z    =      -16819938
23                 Z    =        -5147088
51
 XDOT =      -1799
249810                 XDOT =        -457
504384
 YDOT =     -24778
196266  feet/sec       YDOT =       -7558
018505  meter/sec
 ZDOT =      -4331
786666                 ZDOT =       -1322
772482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2678606
83                 X    =          816439
36
 Y    =      -13983811
61  feet           Y    =        -4262265
78  meter
 Z    =      -16898831
85                 Z    =        -5150763
95
 XDOT =      21873
472364                 XDOT =        6667
034376
 YDOT =       9448
900469  feet/sec       YDOT =        2880
024863  meter/sec
 ZDOT =      -4341
831794                 ZDOT =       -1323
390331


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   08329
51814609  
00020000  00000-0  20000-3 0  9106
2 25544  51
6408 274
5104 0004449  21
9066 338
2286 15
72808577 13763


Satellite: ISS
Catalog Number: 25544
Epoch time:      08329
51814609   =   yrday
fracday
Element set:     910
Inclination:       51
6408  deg
RA of node:       274
5104  deg
Eccentricity:     
0004449     
Arg of perigee:    21
9066  deg
Mean anomaly:     338
2286  deg
Mean motion:   15
72808577  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1376
Checksum:              301


Coasting Arc #12 (Orbit 1391)
---------------------------------------

Vector Time (GMT): 2008/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1343473
59                 A    =         6734530
53  meter
 Y    =        6422551
82  meter          E    =           
0014591
 Z    =        1496656
69                 I    =           51
32949
 XDOT =      -4558
228487                 Wp   =          100
25945
 YDOT =       2306
103367  meter/sec      RA   =          268
70326  deg
 ZDOT =      -5759
356228                 TA   =           63
19176
                                          MA   =           63
04260
                                          Ha   =            193
017  n
mi
                                          Hp   =            184
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4407721
75                 X    =         1264285
02
 Y    =       21071364
23  feet           Y    =         6437132
43  meter
 Z    =        4910290
96                 Z    =         1502991
64
 XDOT =     -14954
817870                 XDOT =       -4555
698224
 YDOT =       7565
955928  feet/sec       YDOT =        2255
145245  meter/sec
 ZDOT =     -18895
525684                 ZDOT =       -5781
494397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20862877
92                 X    =        -6359005
19
 Y    =       -5284328
36  feet           Y    =        -1610663
28  meter
 Z    =        4935337
67                 Z    =         1504290
92
 XDOT =       -690
569918                 XDOT =        -210
485711
 YDOT =     -15138
558936  feet/sec       YDOT =       -4614
232764  meter/sec
 ZDOT =     -18981
190425                 ZDOT =       -5785
466842


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   08330
53473940  
00020000  00000-0  20000-3 0  9110
2 25544  51
6415 269
2990 0004485  26
1659 333
9729 15
72830111 13921


Satellite: ISS
Catalog Number: 25544
Epoch time:      08330
53473940   =   yrday
fracday
Element set:     911
Inclination:       51
6415  deg
RA of node:       269
2990  deg
Eccentricity:     
0004485     
Arg of perigee:    26
1659  deg
Mean anomaly:     333
9729  deg
Mean motion:   15
72830111  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1392
Checksum:              293

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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