Date: October 11th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8880 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 667)
---------------------------------------

Vector Time (GMT): 2008/284/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -263331
84                 A    =         6726893
41  meter
 Y    =       -4576796
47  meter          E    =           
0003374
 Z    =        4920036
41                 I    =           51
81867
 XDOT =       6834
195047                 Wp   =           87
60123
 YDOT =      -2773
127115  meter/sec      RA   =          144
26936  deg
 ZDOT =      -2212
446171                 TA   =           23
84675
                                          MA   =           23
83112
                                          Ha   =            192
738  n
mi
                                          Hp   =            187
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -863949
61                 X    =         -236034
68
 Y    =      -15015736
46  feet           Y    =        -4579588
29  meter
 Z    =       16141851
75                 Z    =         4918823
71
 XDOT =      22421
899759                 XDOT =        6875
444438
 YDOT =      -9098
186072  feet/sec       YDOT =       -2696
472690  meter/sec
 ZDOT =      -7258
681663                 ZDOT =       -2179
144971

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3851451
44                 X    =         1173922
40
 Y    =       14544817
87  feet           Y    =         4433260
49  meter
 Z    =       16136688
74                 Z    =         4918462
73
 XDOT =     -19210
592350                 XDOT =       -5855
388548
 YDOT =      13002
517279  feet/sec       YDOT =        3963
167267  meter/sec
 ZDOT =      -7129
998873                 ZDOT =       -2173
223657


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   08284
52312925  
00020000  00000-0  20000-3 0  9000
2 25544  51
6426 145
0254 0003829 210
8874 149
2064 15
72165478  6681


Satellite: ISS
Catalog Number: 25544
Epoch time:      08284
52312925   =   yrday
fracday
Element set:     900
Inclination:       51
6426  deg
RA of node:       145
0254  deg
Eccentricity:     
0003829     
Arg of perigee:   210
8874  deg
Mean anomaly:     149
2064  deg
Mean motion:   15
72165478  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             668
Checksum:              293


Coasting Arc #2 (Orbit 683)
---------------------------------------

Vector Time (GMT): 2008/285/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5621626
66                 A    =         6736628
86  meter
 Y    =        3447112
02  meter          E    =           
0010569
 Z    =        1356621
59                 I    =           51
87358
 XDOT =      -1504
167895                 Wp   =           68
81070
 YDOT =      -4768
730345  meter/sec      RA   =          139
19210  deg
 ZDOT =       5851
457147                 TA   =          306
03140
                                          MA   =          306
12930
                                          Ha   =            192
600  n
mi
                                          Hp   =            187
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18443657
03                 X    =        -5666345
32
 Y    =       11309422
63  feet           Y    =         3383997
81  meter
 Z    =        4450858
24                 Z    =         1329202
50
 XDOT =      -4934
934040                 XDOT =       -1479
157071
 YDOT =     -15645
440763  feet/sec       YDOT =       -4785
410524  meter/sec
 ZDOT =      19197
694053                 ZDOT =        5844
210929

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15669009
73                 X    =         4775914
17
 Y    =      -14949402
05  feet           Y    =        -4556577
75  meter
 Z    =        4345017
41                 Z    =         1324361
31
 XDOT =       7140
236850                 XDOT =        2176
344192
 YDOT =      13087
290275  feet/sec       YDOT =        3989
006076  meter/sec
 ZDOT =      19169
144678                 ZDOT =        5842
755298


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   08285
54016624  
00020000  00000-0  20000-3 0  9011
2 25544  51
6418 139
8163 0003875 215
0119 145
0788 15
72172582  6841


Satellite: ISS
Catalog Number: 25544
Epoch time:      08285
54016624   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:       139
8163  deg
Eccentricity:     
0003875     
Arg of perigee:   215
0119  deg
Mean anomaly:     145
0788  deg
Mean motion:   15
72172582  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             684
Checksum:              294


Coasting Arc #3 (Orbit 698)
---------------------------------------

Vector Time (GMT): 2008/286/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2261438
66                 A    =         6725515
34  meter
 Y    =        3577783
12  meter          E    =           
0012998
 Z    =       -5237620
07                 I    =           51
85664
 XDOT =      -5793
285067                 Wp   =          111
28348
 YDOT =       4975
404133  meter/sec      RA   =          134
06548  deg
 ZDOT =        894
466337                 TA   =          167
23941
                                          MA   =          167
20648
                                          Ha   =            192
447  n
mi
                                          Hp   =            187
466

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7419418
17                 X    =         2246707
09
 Y    =       11738133
60  feet           Y    =         3602989
00  meter
 Z    =      -17183792
89                 Z    =        -5226669
92
 XDOT =     -19006
840770                 XDOT =       -5852
835500
 YDOT =      16323
504372  feet/sec       YDOT =        4910
287387  meter/sec
 ZDOT =       2934
600842                 ZDOT =         866
176982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9992450
18                 X    =        -3045698
81
 Y    =       -9718573
01  feet           Y    =        -2962221
05  meter
 Z    =      -17141019
89                 Z    =        -5224582
86
 XDOT =      14099
388536                 XDOT =        4297
493626
 YDOT =     -19496
714932  feet/sec       YDOT =       -5942
598711  meter/sec
 ZDOT =       2825
538269                 ZDOT =         861
224064


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   08286
49362434  
00020000  00000-0  20000-3 0  9020
2 25544  51
6406 134
9323 0003820 219
2826 140
8059 15
72189601  6993


Satellite: ISS
Catalog Number: 25544
Epoch time:      08286
49362434   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:       134
9323  deg
Eccentricity:     
0003820     
Arg of perigee:   219
2826  deg
Mean anomaly:     140
8059  deg
Mean motion:   15
72189601  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             699
Checksum:              295


Coasting Arc #4 (Orbit 714)
---------------------------------------

Vector Time (GMT): 2008/287/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4354232
23                 A    =         6737368
25  meter
 Y    =       -5127252
30  meter          E    =           
0012733
 Z    =        -204907
24                 I    =           51
91562
 XDOT =       3505
625518                 Wp   =          154
27156
 YDOT =       3213
117064  meter/sec      RA   =          128
97113  deg
 ZDOT =      -6056
600977                 TA   =           27
94539
                                          MA   =           27
87707
                                          Ha   =            192
419  n
mi
                                          Hp   =            187
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14285538
82                 X    =         4412237
80
 Y    =      -16821693
90  feet           Y    =        -5078236
45  meter
 Z    =        -672267
85                 Z    =         -183612
54
 XDOT =      11501
396057                 XDOT =        3498
857932
 YDOT =      10541
722652  feet/sec       YDOT =        3252
280621  meter/sec
 ZDOT =     -19870
738114                 ZDOT =       -6039
586979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9745569
06                 X    =        -2970449
45
 Y    =       19803367
75  feet           Y    =         6036066
49  meter
 Z    =        -590303
98                 Z    =         -179924
65
 XDOT =     -12394
820029                 XDOT =       -3777
941145
 YDOT =      -6673
248459  feet/sec       YDOT =       -2034
006130  meter/sec
 ZDOT =     -19804
517398                 ZDOT =       -6036
416903


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   08287
51063100  
00020000  00000-0  20000-3 0  9033
2 25544  51
6404 129
7242 0003891 222
7207 137
3653 15
72174219  7152


Satellite: ISS
Catalog Number: 25544
Epoch time:      08287
51063100   =   yrday
fracday
Element set:     903
Inclination:       51
6404  deg
RA of node:       129
7242  deg
Eccentricity:     
0003891     
Arg of perigee:   222
7207  deg
Mean anomaly:     137
3653  deg
Mean motion:   15
72174219  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             715
Checksum:              267


Coasting Arc #5 (Orbit 730)
---------------------------------------

Vector Time (GMT): 2008/288/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3708563
33                 A    =         6725305
97  meter
 Y    =       -1903111
47  meter          E    =           
0003517
 Z    =        5278210
88                 I    =           51
89176
 XDOT =       3994
980799                 Wp   =          184
99542
 YDOT =      -6565
980686  meter/sec      RA   =          123
86860  deg
 ZDOT =        436
107533                 TA   =          260
85599
                                          MA   =          260
89578
                                          Ha   =            192
337  n
mi
                                          Hp   =            187
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12167202
51                 X    =        -3712648
13
 Y    =       -6243804
03  feet           Y    =        -1944605
22  meter
 Z    =       17316964
84                 Z    =         5260184
38
 XDOT =      13106
892384                 XDOT =        4065
987146
 YDOT =     -21541
931386  feet/sec       YDOT =       -6520
909454  meter/sec
 ZDOT =       1430
798993                 ZDOT =         455
688669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13470715
87                 X    =         4105874
20
 Y    =        2825870
87  feet           Y    =          861325
44  meter
 Z    =       17246954
65                 Z    =         5256871
78
 XDOT =      -6816
038900                 XDOT =       -2077
528657
 YDOT =      23231
634947  feet/sec       YDOT =        7081
002332  meter/sec
 ZDOT =       1505
993575                 ZDOT =         459
026842


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   08288
52762062  
00020000  00000-0  20000-3 0  9049
2 25544  51
6395 124
5141 0003808 227
6859 132
3981 15
72199688  7311


Satellite: ISS
Catalog Number: 25544
Epoch time:      08288
52762062   =   yrday
fracday
Element set:     904
Inclination:       51
6395  deg
RA of node:       124
5141  deg
Eccentricity:     
0003808     
Arg of perigee:   227
6859  deg
Mean anomaly:     132
3981  deg
Mean motion:   15
72199688  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             731
Checksum:              312


Coasting Arc #6 (Orbit 745)
---------------------------------------

Vector Time (GMT): 2008/289/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2533204
96                 A    =         6736793
94  meter
 Y    =        6165878
79  meter          E    =           
0006257
 Z    =        -951647
64                 I    =           51
94488
 XDOT =      -4754
665336                 Wp   =           29
56442
 YDOT =      -1036
639942  meter/sec      RA   =          118
75168  deg
 ZDOT =       5961
802147                 TA   =          320
09587
                                          MA   =          320
14185
                                          Ha   =            192
010  n
mi
                                          Hp   =            187
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8311039
91                 X    =        -2597341
46
 Y    =       20229261
11  feet           Y    =         6137192
38  meter
 Z    =       -3122203
55                 Z    =         -964110
43
 XDOT =     -15599
295723                 XDOT =       -4771
682389
 YDOT =      -3401
049680  feet/sec       YDOT =       -1089
904227  meter/sec
 ZDOT =      19559
718331                 ZDOT =        5938
661939

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2352254
36                 X    =          716967
13
 Y    =      -21736221
04  feet           Y    =        -6625200
17  meter
 Z    =       -3169879
96                 Z    =         -966179
41
 XDOT =      14452
789799                 XDOT =        4405
210331
 YDOT =      -1265
036034  feet/sec       YDOT =        -385
582983  meter/sec
 ZDOT =      19469
985036                 ZDOT =        5934
451439


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   08289
48103253  
00020000  00000-0  20000-3 0  9057
2 25544  51
6382 119
6292 0003877 233
2047 126
8760 15
72235121  7469


Satellite: ISS
Catalog Number: 25544
Epoch time:      08289
48103253   =   yrday
fracday
Element set:     905
Inclination:       51
6382  deg
RA of node:       119
6292  deg
Eccentricity:     
0003877     
Arg of perigee:   233
2047  deg
Mean anomaly:     126
8760  deg
Mean motion:   15
72235121  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             746
Checksum:              288


Coasting Arc #7 (Orbit 761)
---------------------------------------

Vector Time (GMT): 2008/290/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4409685
02                 A    =         6726002
72  meter
 Y    =        -134244
39  meter          E    =           
0010038
 Z    =       -5085744
65                 I    =           51
92093
 XDOT =      -1740
492752                 Wp   =           85
19451
 YDOT =       7294
805372  meter/sec      RA   =          113
67251  deg
 ZDOT =      -1703
724814                 TA   =          168
47133
                                          MA   =          168
44832
                                          Ha   =            191
931  n
mi
                                          Hp   =            187
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14467470
55                 X    =         4435564
89
 Y    =        -440434
35  feet           Y    =          -84788
11  meter
 Z    =      -16685513
93                 Z    =        -5064258
81
 XDOT =      -5710
278057                 XDOT =       -1813
658421
 YDOT =      23933
088491  feet/sec       YDOT =        7274
933063  meter/sec
 ZDOT =      -5589
648339                 ZDOT =       -1712
358240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13789544
59                 X    =        -4203053
19
 Y    =        4703217
50  feet           Y    =         1433540
70  meter
 Z    =      -16602297
03                 Z    =        -5060380
13
 XDOT =      -1267
384001                 XDOT =        -386
298643
 YDOT =     -23539
094860  feet/sec       YDOT =       -7174
716113  meter/sec
 ZDOT =      -5622
400081                 ZDOT =       -1713
707545


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   08290
49799047  
00020000  00000-0  20000-3 0  9063
2 25544  51
6374 114
4192 0003822 235
8590 124
2210 15
72272324  7629


Satellite: ISS
Catalog Number: 25544
Epoch time:      08290
49799047   =   yrday
fracday
Element set:     906
Inclination:       51
6374  deg
RA of node:       114
4192  deg
Eccentricity:     
0003822     
Arg of perigee:   235
8590  deg
Mean anomaly:     124
2210  deg
Mean motion:   15
72272324  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             762
Checksum:              284


Coasting Arc #8 (Orbit 777)
---------------------------------------

Vector Time (GMT): 2008/291/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         487377
37                 A    =         6735139
02  meter
 Y    =       -6402202
17  meter          E    =           
0011810
 Z    =        2011373
12                 I    =           51
96404
 XDOT =       5091
635256                 Wp   =          125
58743
 YDOT =      -1379
946213  meter/sec      RA   =          108
53896  deg
 ZDOT =      -5609
974529                 TA   =           32
10715
                                          MA   =           32
03527
                                          Ha   =            191
609  n
mi
                                          Hp   =            187
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1599007
12                 X    =          549160
42
 Y    =      -21004600
29  feet           Y    =        -6396406
62  meter
 Z    =        6598993
19                 Z    =         2013890
85
 XDOT =      16704
840078                 XDOT =        5133
940706
 YDOT =      -4527
382588  feet/sec       YDOT =       -1322
771975  meter/sec
 ZDOT =     -18405
428244                 ZDOT =       -5585
135850

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5036750
76                 X    =         1535201
63
 Y    =       20451411
10  feet           Y    =         6233590
10  meter
 Z    =        6608153
61                 Z    =         2014165
22
 XDOT =     -13082
653400                 XDOT =       -3987
592756
 YDOT =       9155
097290  feet/sec       YDOT =        2790
473654  meter/sec
 ZDOT =     -18309
330686                 ZDOT =       -5580
683993


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   08291
51492977  
00020000  00000-0  20000-3 0  9070
2 25544  51
6384 109
2095 0003889 244
0677 116
0085 15
72343563  7785


Satellite: ISS
Catalog Number: 25544
Epoch time:      08291
51492977   =   yrday
fracday
Element set:     907
Inclination:       51
6384  deg
RA of node:       109
2095  deg
Eccentricity:     
0003889     
Arg of perigee:   244
0677  deg
Mean anomaly:     116
0085  deg
Mean motion:   15
72343563  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             778
Checksum:              317


Coasting Arc #9 (Orbit 793)
---------------------------------------

Vector Time (GMT): 2008/292/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4293536
41                 A    =         6727651
07  meter
 Y    =        2252622
55  meter          E    =           
0006471
 Z    =        4663095
33                 I    =           51
94587
 XDOT =       -606
516360                 Wp   =          143
79997
 YDOT =      -7116
295081  meter/sec      RA   =          103
47723  deg
 ZDOT =       2872
134865                 TA   =          277
88046
                                          MA   =          277
95390
                                          Ha   =            191
716  n
mi
                                          Hp   =            187
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14086405
54                 X    =        -4341059
56
 Y    =        7390493
93  feet           Y    =         2204343
86  meter
 Z    =       15298869
19                 Z    =         4642121
42
 XDOT =      -1989
883070                 XDOT =        -540
848397
 YDOT =     -23347
424806  feet/sec       YDOT =       -7122
710432  meter/sec
 ZDOT =       9423
014648                 ZDOT =        2869
347585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10981024
04                 X    =         3347016
13
 Y    =      -11616234
71  feet           Y    =        -3540628
34  meter
 Z    =       15217812
66                 Z    =         4638389
30
 XDOT =       8713
390376                 XDOT =        2655
841387
 YDOT =      20597
266412  feet/sec       YDOT =        6278
046802  meter/sec
 ZDOT =       9411
569328                 ZDOT =        2868
646331


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   08292
53185600  
00020000  00000-0  20000-3 0  9086
2 25544  51
6377 103
9991 0003829 245
3247 114
7517 15
72311072  7947


Satellite: ISS
Catalog Number: 25544
Epoch time:      08292
53185600   =   yrday
fracday
Element set:     908
Inclination:       51
6377  deg
RA of node:       103
9991  deg
Eccentricity:     
0003829     
Arg of perigee:   245
3247  deg
Mean anomaly:     114
7517  deg
Mean motion:   15
72311072  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             794
Checksum:              295


Coasting Arc #10 (Orbit 808)
---------------------------------------

Vector Time (GMT): 2008/293/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1493495
35                 A    =         6733063
55  meter
 Y    =        5853479
49  meter          E    =           
0000778
 Z    =       -2973752
26                 I    =           51
97051
 XDOT =      -4508
564971                 Wp   =           79
36101
 YDOT =       3699
259527  meter/sec      RA   =           98
33060  deg
 ZDOT =       5018
479920                 TA   =          246
53560
                                          MA   =          246
54378
                                          Ha   =            191
545  n
mi
                                          Hp   =            187
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4899919
14                 X    =         1442376
04
 Y    =       19204329
02  feet           Y    =         5869894
91  meter
 Z    =       -9756405
06                 Z    =        -2966620
64
 XDOT =     -14791
879827                 XDOT =       -4573
974968
 YDOT =      12136
678239  feet/sec       YDOT =        3648
476215  meter/sec
 ZDOT =      16464
829135                 ZDOT =        4996
418134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11241503
33                 X    =        -3426410
21
 Y    =      -16339910
94  feet           Y    =        -4980404
86  meter
 Z    =       -9728248
23                 Z    =        -2965170
06
 XDOT =       8629
272456                 XDOT =        2630
202245
 YDOT =     -15686
238775  feet/sec       YDOT =       -4781
165579  meter/sec
 ZDOT =      16379
675040                 ZDOT =        4992
524952


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   08293
48520661  
00020000  00000-0  20000-3 0  9092
2 25544  51
6380  99
1145 0003780 246
3386 113
7380 15
72348586  8093


Satellite: ISS
Catalog Number: 25544
Epoch time:      08293
48520661   =   yrday
fracday
Element set:     909
Inclination:       51
6380  deg
RA of node:        99
1145  deg
Eccentricity:     
0003780     
Arg of perigee:   246
3386  deg
Mean anomaly:     113
7380  deg
Mean motion:   15
72348586  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             809
Checksum:              307


Coasting Arc #11 (Orbit 824)
---------------------------------------

Vector Time (GMT): 2008/294/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3430294
27                 A    =         6729615
79  meter
 Y    =       -4115202
99  meter          E    =           
0003781
 Z    =       -4076520
68                 I    =           51
96277
 XDOT =       2688
366994                 Wp   =           70
62928
 YDOT =       6078
132453  meter/sec      RA   =           93
28035  deg
 ZDOT =      -3875
285328                 TA   =          159
62025
                                          MA   =          159
60515
                                          Ha   =            191
456  n
mi
                                          Hp   =            187
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11254246
28                 X    =         3495859
48
 Y    =      -13501322
16  feet           Y    =        -4076476
73  meter
 Z    =      -13374411
68                 Z    =        -4059696
93
 XDOT =       8820
101686                 XDOT =        2639
026245
 YDOT =      19941
379439  feet/sec       YDOT =        6107
919574  meter/sec
 ZDOT =     -12714
190708                 ZDOT =       -3862
344694

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5727232
67                 X    =        -1745660
52
 Y    =       16669508
29  feet           Y    =         5080866
13  meter
 Z    =      -13309581
00                 Z    =        -4056760
29
 XDOT =     -14244
521329                 XDOT =       -4341
730101
 YDOT =     -15000
695538  feet/sec       YDOT =       -4572
212000  meter/sec
 ZDOT =     -12663
506096                 ZDOT =       -3859
836658


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   08294
50209728  
00020000  00000-0  20000-3 0  9106
2 25544  51
6385  93
9053 0003618 251
6124 108
4645 15
72393241  8258


Satellite: ISS
Catalog Number: 25544
Epoch time:      08294
50209728   =   yrday
fracday
Element set:     910
Inclination:       51
6385  deg
RA of node:        93
9053  deg
Eccentricity:     
0003618     
Arg of perigee:   251
6124  deg
Mean anomaly:     108
4645  deg
Mean motion:   15
72393241  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             825
Checksum:              286


Coasting Arc #12 (Orbit 840)
---------------------------------------

Vector Time (GMT): 2008/295/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628516
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3101865
04                 A    =         6730663
95  meter
 Y    =       -4628044
31  meter          E    =           
0007942
 Z    =        3769993
77                 I    =           51
96608
 XDOT =       3150
652739                 Wp   =           87
13524
 YDOT =      -5587
514149  meter/sec      RA   =           88
12814  deg
 ZDOT =      -4258
906042                 TA   =           47
50635
                                          MA   =           47
43927
                                          Ha   =            191
431  n
mi
                                          Hp   =            187
595

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10176722
56                 X    =        -3068197
12
 Y    =      -15183872
41  feet           Y    =        -4662542
96  meter
 Z    =       12368745
96                 Z    =         3755006
45
 XDOT =      10336
787203                 XDOT =        3233
588297
 YDOT =     -18331
739333  feet/sec       YDOT =       -5551
817957  meter/sec
 ZDOT =     -13972
788851                 ZDOT =       -4243
398616

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15194354
78                 X    =         4631239
34
 Y    =       10231847
45  feet           Y    =         3118667
10  meter
 Z    =       12310256
73                 Z    =         3752166
25
 XDOT =      -2034
513119                 XDOT =        -620
119599
 YDOT =      19792
539818  feet/sec       YDOT =        6032
766137  meter/sec
 ZDOT =     -13913
181329                 ZDOT =       -4240
737669


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   08295
51897043  
00020000  00000-0  20000-3 0  9112
2 25544  51
6380  88
6948 0003753 254
7985 105
2762 15
72385762  8418


Satellite: ISS
Catalog Number: 25544
Epoch time:      08295
51897043   =   yrday
fracday
Element set:     911
Inclination:       51
6380  deg
RA of node:        88
6948  deg
Eccentricity:     
0003753     
Arg of perigee:   254
7985  deg
Mean anomaly:     105
2762  deg
Mean motion:   15
72385762  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             841
Checksum:              322

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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