Date: November 2nd 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 997)
---------------------------------------

Vector Time (GMT): 2008/305/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1471418
52                 A    =         6725420
71  meter
 Y    =       -4014950
73  meter          E    =           
0010773
 Z    =       -5200356
86                 I    =           51
82356
 XDOT =       6556
496294                 Wp   =           75
81671
 YDOT =       3858
841358  meter/sec      RA   =           37
14653  deg
 ZDOT =      -1123
447601                 TA   =          183
46975
                                          MA   =          183
47723
                                          Ha   =            191
393  n
mi
                                          Hp   =            187
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4827488
57                 X    =         1541468
16
 Y    =      -13172410
54  feet           Y    =        -3998104
61  meter
 Z    =      -17061538
27                 Z    =        -5193038
49
 XDOT =      21510
814612                 XDOT =        6518
316478
 YDOT =      12660
240677  feet/sec       YDOT =        3931
946458  meter/sec
 ZDOT =      -3685
851710                 ZDOT =       -1091
687745

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2775733
97                 X    =          846043
71
 Y    =       13786553
68  feet           Y    =         4202141
56  meter
 Z    =      -17033477
97                 Z    =        -5191804
08
 XDOT =     -23964
704958                 XDOT =       -7304
442071
 YDOT =        420
848635  feet/sec       YDOT =         128
274664  meter/sec
 ZDOT =      -3562
467818                 ZDOT =       -1085
840191


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   08305
49690195  
00020000  00000-0  20000-3 0  9008
2 25544  51
6441  37
5933 0003842 277
2623  82
8102 15
72272330  9988


Satellite: ISS
Catalog Number: 25544
Epoch time:      08305
49690195   =   yrday
fracday
Element set:     900
Inclination:       51
6441  deg
RA of node:        37
5933  deg
Eccentricity:     
0003842     
Arg of perigee:   277
2623  deg
Mean anomaly:      82
8102  deg
Mean motion:   15
72272330  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             998
Checksum:              288


Coasting Arc #2 (Orbit 1013)
---------------------------------------

Vector Time (GMT): 2008/306/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6099117
39                 A    =         6736111
91  meter
 Y    =       -2410832
38  meter          E    =           
0010578
 Z    =        1513119
27                 I    =           51
83497
 XDOT =        545
512619                 Wp   =          124
11484
 YDOT =      -5034
196398  meter/sec      RA   =           32
01488  deg
 ZDOT =      -5799
140376                 TA   =           39
27039
                                          MA   =           39
19371
                                          Ha   =            191
481  n
mi
                                          Hp   =            187
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20010227
66                 X    =        -6079056
43
 Y    =       -7909555
05  feet           Y    =        -2478924
15  meter
 Z    =        4964302
06                 Z    =         1483537
53
 XDOT =       1789
739563                 XDOT =         629
937239
 YDOT =     -16516
392381  feet/sec       YDOT =       -5027
623814  meter/sec
 ZDOT =     -19026
051103                 ZDOT =       -5796
285392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21123073
93                 X    =         6438312
94
 Y    =       -4232370
97  feet           Y    =        -1290026
67  meter
 Z    =        4849469
10                 Z    =         1478118
18
 XDOT =       7060
654041                 XDOT =        2152
087352
 YDOT =      13362
525030  feet/sec       YDOT =        4072
897629  meter/sec
 ZDOT =     -19015
359876                 ZDOT =       -5795
881690


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   08306
51384137  
00020000  00000-0  20000-3 0  9019
2 25544  51
6437  32
3849 0003682 281
1343  78
9405 15
72287129 10141


Satellite: ISS
Catalog Number: 25544
Epoch time:      08306
51384137   =   yrday
fracday
Element set:     901
Inclination:       51
6437  deg
RA of node:        32
3849  deg
Eccentricity:     
0003682     
Arg of perigee:   281
1343  deg
Mean anomaly:      78
9405  deg
Mean motion:   15
72287129  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1014
Checksum:              282


Coasting Arc #3 (Orbit 1029)
---------------------------------------

Vector Time (GMT): 2008/307/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         562492
58                 A    =         6726537
03  meter
 Y    =        4595557
65  meter          E    =           
0003166
 Z    =        4878780
14                 I    =           51
77841
 XDOT =      -7165
926644                 Wp   =          140
67953
 YDOT =      -1590
615030  meter/sec      RA   =           26
93586  deg
 ZDOT =       2321
245605                 TA   =          286
73446
                                          MA   =          286
76920
                                          Ha   =            191
422  n
mi
                                          Hp   =            187
642

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1845448
11                 X    =          487361
69
 Y    =       15077288
89  feet           Y    =         4601427
41  meter
 Z    =       16006496
53                 Z    =         4881330
57
 XDOT =     -23510
258017                 XDOT =       -7158
884004
 YDOT =      -5218
553248  feet/sec       YDOT =       -1670
709320  meter/sec
 ZDOT =       7615
635186                 ZDOT =        2286
449687

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9855943
00                 X    =        -3004091
43
 Y    =      -11543974
26  feet           Y    =        -3518603
35  meter
 Z    =       16016719
26                 Z    =         4881896
03
 XDOT =      21625
323121                 XDOT =        6591
398487
 YDOT =      -8069
448482  feet/sec       YDOT =       -2459
567897  meter/sec
 ZDOT =       7480
651104                 ZDOT =        2280
102457


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   08307
53076532  
00020000  00000-0  20000-3 0  9020
2 25544  51
6442  27
1754 0003773 286
5678  73
5070 15
72347033 10303


Satellite: ISS
Catalog Number: 25544
Epoch time:      08307
53076532   =   yrday
fracday
Element set:     902
Inclination:       51
6442  deg
RA of node:        27
1754  deg
Eccentricity:     
0003773     
Arg of perigee:   286
5678  deg
Mean anomaly:      73
5070  deg
Mean motion:   15
72347033  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1030
Checksum:              275


Coasting Arc #4 (Orbit 1044)
---------------------------------------

Vector Time (GMT): 2008/308/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6232723
63                 A    =         6734297
71  meter
 Y    =         355468
57  meter          E    =           
0005051
 Z    =       -2517778
31                 I    =           51
77695
 XDOT =       1846
680935                 Wp   =            4
71487
 YDOT =       5248
534594  meter/sec      RA   =           21
78404  deg
 ZDOT =       5318
118469                 TA   =          326
85380
                                          MA   =          326
88543
                                          Ha   =            191
627  n
mi
                                          Hp   =            187
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20448568
35                 X    =         6240516
67
 Y    =        1166235
48  feet           Y    =          425210
21  meter
 Z    =       -8260427
53                 Z    =        -2487480
14
 XDOT =       6058
664485                 XDOT =        1762
018707
 YDOT =      17219
601686  feet/sec       YDOT =        5268
711567  meter/sec
 ZDOT =      17447
895239                 ZDOT =        5326
884494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17487749
64                 X    =        -5330266
09
 Y    =       10752184
27  feet           Y    =         3277265
77  meter
 Z    =       -8142963
95                 Z    =        -2481975
41
 XDOT =     -13944
008622                 XDOT =       -4250
133828
 YDOT =      -9453
512336  feet/sec       YDOT =       -2881
430560  meter/sec
 ZDOT =      17482
255215                 ZDOT =        5328
591389


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   08308
48412188  
00020000  00000-0  20000-3 0  9037
2 25544  51
6439  22
2928 0003889 292
9603  67
1149 15
72315516 10458


Satellite: ISS
Catalog Number: 25544
Epoch time:      08308
48412188   =   yrday
fracday
Element set:     903
Inclination:       51
6439  deg
RA of node:        22
2928  deg
Eccentricity:     
0003889     
Arg of perigee:   292
9603  deg
Mean anomaly:      67
1149  deg
Mean motion:   15
72315516  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1045
Checksum:              297


Coasting Arc #5 (Orbit 1060)
---------------------------------------

Vector Time (GMT): 2008/309/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2623641
16                 A    =         6728532
73  meter
 Y    =       -4393026
22  meter          E    =           
0007197
 Z    =       -4376668
89                 I    =           51
72950
 XDOT =       6867
577264                 Wp   =           46
17978
 YDOT =       -726
750857  meter/sec      RA   =           16
71489  deg
 ZDOT =      -3385
939155                 TA   =          189
70678
                                          MA   =          189
72069
                                          Ha   =            191
608  n
mi
                                          Hp   =            187
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8607746
60                 X    =        -2553061
17
 Y    =      -14412815
69  feet           Y    =        -4421970
44  meter
 Z    =      -14359149
90                 Z    =        -4389243
56
 XDOT =      22531
421469                 XDOT =        6891
642081
 YDOT =      -2384
353204  feet/sec       YDOT =        -649
818915  meter/sec
 ZDOT =     -11108
724261                 ZDOT =       -3352
517418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15348595
86                 X    =         4678252
02
 Y    =        6695657
32  feet           Y    =         2040836
35  meter
 Z    =      -14408210
21                 Z    =        -4391622
47
 XDOT =     -16435
617310                 XDOT =       -5009
576156
 YDOT =      14039
684762  feet/sec       YDOT =        4279
295916  meter/sec
 ZDOT =     -10979
229270                 ZDOT =       -3346
469081


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   08309
50102234  
00020000  00000-0  20000-3 0  9040
2 25544  51
6430  17
0837 0003788 296
5074  63
5699 15
72345109 10619


Satellite: ISS
Catalog Number: 25544
Epoch time:      08309
50102234   =   yrday
fracday
Element set:     904
Inclination:       51
6430  deg
RA of node:        17
0837  deg
Eccentricity:     
0003788     
Arg of perigee:   296
5074  deg
Mean anomaly:      63
5699  deg
Mean motion:   15
72345109  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1061
Checksum:              281


Coasting Arc #6 (Orbit 1076)
---------------------------------------

Vector Time (GMT): 2008/310/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5604957
39                 A    =         6731876
30  meter
 Y    =        1573459
17  meter          E    =           
0009621
 Z    =        3374392
78                 I    =           51
71306
 XDOT =      -4089
691928                 Wp   =           77
78267
 YDOT =      -4578
241305  meter/sec      RA   =           11
54831  deg
 ZDOT =      -4645
186503                 TA   =           62
50795
                                          MA   =           62
41018
                                          Ha   =            191
732  n
mi
                                          Hp   =            187
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18388967
83                 X    =        -5638527
97
 Y    =        5162267
63  feet           Y    =         1510593
47  meter
 Z    =       11070842
45                 Z    =         3347081
94
 XDOT =     -13417
624436                 XDOT =       -4015
627468
 YDOT =     -15020
476721  feet/sec       YDOT =       -4623
560314  meter/sec
 ZDOT =     -15240
113200                 ZDOT =       -4664
874834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11679526
87                 X    =         3559919
79
 Y    =      -15189537
53  feet           Y    =        -4629771
04  meter
 Z    =       10965094
58                 Z    =         3342160
83
 XDOT =      18564
642077                 XDOT =        5658
502905
 YDOT =       3186
459488  feet/sec       YDOT =         971
232852  meter/sec
 ZDOT =     -15316
761531                 ZDOT =       -4668
548915


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   08310
51790886  
00020000  00000-0  20000-3 0  9050
2 25544  51
6435  11
8742 0003858 303
7377  56
3418 15
72404804 10770


Satellite: ISS
Catalog Number: 25544
Epoch time:      08310
51790886   =   yrday
fracday
Element set:     905
Inclination:       51
6435  deg
RA of node:        11
8742  deg
Eccentricity:     
0003858     
Arg of perigee:   303
7377  deg
Mean anomaly:      56
3418  deg
Mean motion:   15
72404804  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1077
Checksum:              292


Coasting Arc #7 (Orbit 1092)
---------------------------------------

Vector Time (GMT): 2008/311/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4429213
20                 A    =         6730656
53  meter
 Y    =        3449613
06  meter          E    =           
0008635
 Z    =        3704430
46                 I    =           51
68001
 XDOT =      -5757
847390                 Wp   =           83
16129
 YDOT =       2766
632257  meter/sec      RA   =            6
48033  deg
 ZDOT =       4300
540394                 TA   =          321
42563
                                          MA   =          321
48730
                                          Ha   =            191
679  n
mi
                                          Hp   =            187
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14531539
37                 X    =         4372314
11
 Y    =       11317628
14  feet           Y    =         3498824
86  meter
 Z    =       12153643
23                 Z    =         3725809
80
 XDOT =     -18890
575428                 XDOT =       -5809
247988
 YDOT =       9076
877483  feet/sec       YDOT =        2701
957193  meter/sec
 ZDOT =      14109
384496                 ZDOT =        4272
443498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18363567
76                 X    =        -5597215
45
 Y    =         -79705
40  feet           Y    =          -24294
21  meter
 Z    =       12236764
81                 Z    =         3729765
91
 XDOT =       9421
626448                 XDOT =        2871
711741
 YDOT =     -17460
447852  feet/sec       YDOT =       -5321
944505  meter/sec
 ZDOT =      14000
677069                 ZDOT =        4267
406371


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   08311
53478300  
00020000  00000-0  20000-3 0  9068
2 25544  51
6433   6
6647 0003803 307
0381  53
0433 15
72414074 10935


Satellite: ISS
Catalog Number: 25544
Epoch time:      08311
53478300   =   yrday
fracday
Element set:     906
Inclination:       51
6433  deg
RA of node:         6
6647  deg
Eccentricity:     
0003803     
Arg of perigee:   307
0381  deg
Mean anomaly:      53
0433  deg
Mean motion:   15
72414074  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1093
Checksum:              255


Coasting Arc #8 (Orbit 1107)
---------------------------------------

Vector Time (GMT): 2008/312/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4314089
85                 A    =         6729411
38  meter
 Y    =       -3146162
20  meter          E    =           
0004393
 Z    =       -4099414
17                 I    =           51
64593
 XDOT =       5903
066968                 Wp   =           87
84364
 YDOT =       3144
474994  meter/sec      RA   =            1
30785  deg
 ZDOT =       3802
573936                 TA   =          221
20898
                                          MA   =          221
24215
                                          Ha   =            191
929  n
mi
                                          Hp   =            187
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14153838
08                 X    =         4368864
70
 Y    =      -10322054
48  feet           Y    =        -3097613
28  meter
 Z    =      -13449521
56                 Z    =        -4078322
89
 XDOT =      19367
017612                 XDOT =        5848
993643
 YDOT =      10316
519009  feet/sec       YDOT =        3210
184145  meter/sec
 ZDOT =      12475
636273                 ZDOT =        3831
120238

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4627468
07                 X    =        -1410452
27
 Y    =       16960209
72  feet           Y    =         5169471
92  meter
 Z    =      -13367998
98                 Z    =        -4074566
09
 XDOT =     -20266
203088                 XDOT =       -6177
138701
 YDOT =       4381
663519  feet/sec       YDOT =        1335
531040  meter/sec
 ZDOT =      12586
514931                 ZDOT =        3836
369751


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   08312
48809197  
00020000  00000-0  20000-3 0  9076
2 25544  51
6427   1
7811 0003731 313
9376  46
1478 15
72441625 11088


Satellite: ISS
Catalog Number: 25544
Epoch time:      08312
48809197   =   yrday
fracday
Element set:     907
Inclination:       51
6427  deg
RA of node:         1
7811  deg
Eccentricity:     
0003731     
Arg of perigee:   313
9376  deg
Mean anomaly:      46
1478  deg
Mean motion:   15
72441625  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1108
Checksum:              286


Coasting Arc #9 (Orbit 1123)
---------------------------------------

Vector Time (GMT): 2008/313/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5743247
92                 A    =         6732809
35  meter
 Y    =       -1945817
85  meter          E    =           
0002129
 Z    =       -2928739
36                 I    =           51
62874
 XDOT =       3996
666048                 Wp   =           55
67950
 YDOT =      -4245
171519  meter/sec      RA   =          356
23342  deg
 ZDOT =      -5018
419598                 TA   =          158
01247
                                          MA   =          158
00333
                                          Ha   =            192
022  n
mi
                                          Hp   =            186
965

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18842676
91                 X    =        -5706835
02
 Y    =       -6383916
82  feet           Y    =        -2009838
60  meter
 Z    =       -9608724
94                 Z    =        -2956552
21
 XDOT =      13112
421417                 XDOT =        4068
218314
 YDOT =     -13927
728080  feet/sec       YDOT =       -4200
078461  meter/sec
 ZDOT =     -16464
631228                 ZDOT =       -4998
829528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18524143
86                 X    =         5646159
05
 Y    =       -7111320
30  feet           Y    =        -2167530
43  meter
 Z    =       -9716670
21                 Z    =        -2961641
08
 XDOT =      -1759
903320                 XDOT =        -536
418532
 YDOT =      17802
806207  feet/sec       YDOT =        5426
295332  meter/sec
 ZDOT =     -16389
010454                 ZDOT =       -4995
370386


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   08313
50494213  
00020000  00000-0  20000-3 0  9080
2 25544  51
6432 356
5713 0003769 319
5052  40
5829 15
72442108 11243


Satellite: ISS
Catalog Number: 25544
Epoch time:      08313
50494213   =   yrday
fracday
Element set:     908
Inclination:       51
6432  deg
RA of node:       356
5713  deg
Eccentricity:     
0003769     
Arg of perigee:   319
5052  deg
Mean anomaly:      40
5829  deg
Mean motion:   15
72442108  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1124
Checksum:              275


Coasting Arc #10 (Orbit 1139)
---------------------------------------

Vector Time (GMT): 2008/314/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2585874
58                 A    =         6727207
63  meter
 Y    =        4129790
58  meter          E    =           
0008393
 Z    =        4637114
94                 I    =           51
58059
 XDOT =      -7047
226999                 Wp   =           36
32056
 YDOT =      -1189
152714  meter/sec      RA   =          351
06207  deg
 ZDOT =      -2861
532583                 TA   =           82
04892
                                          MA   =           81
95368
                                          Ha   =            192
098  n
mi
                                          Hp   =            186
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8483840
50                 X    =        -2654389
25
 Y    =       13549181
70  feet           Y    =         4100490
81  meter
 Z    =       15213631
69                 Z    =         4624385
95
 XDOT =     -23120
823488                 XDOT =       -7019
504751
 YDOT =      -3901
419666  feet/sec       YDOT =       -1267
803916  meter/sec
 ZDOT =      -9388
230259                 ZDOT =       -2895
701565

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2352743
58                 X    =         -717116
24
 Y    =      -15859068
22  feet           Y    =        -4833843
99  meter
 Z    =       15164597
47                 Z    =         4622169
31
 XDOT =      18863
602674                 XDOT =        5749
626095
 YDOT =     -11931
523325  feet/sec       YDOT =       -3636
728309  meter/sec
 ZDOT =      -9520
751544                 ZDOT =       -2901
925071


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   08314
52177767  
00020000  00000-0  20000-3 0  9096
2 25544  51
6429 351
3619 0003940 322
9060  37
1829 15
72488301 11400


Satellite: ISS
Catalog Number: 25544
Epoch time:      08314
52177767   =   yrday
fracday
Element set:     909
Inclination:       51
6429  deg
RA of node:       351
3619  deg
Eccentricity:     
0003940     
Arg of perigee:   322
9060  deg
Mean anomaly:      37
1829  deg
Mean motion:   15
72488301  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1140
Checksum:              288


Coasting Arc #11 (Orbit 1155)
---------------------------------------

Vector Time (GMT): 2008/315/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6405039
11                 A    =         6734716
46  meter
 Y    =          78743
12  meter          E    =           
0014079
 Z    =        2053189
15                 I    =           51
57645
 XDOT =      -1848
300938                 Wp   =           53
36722
 YDOT =       5004
481403  meter/sec      RA   =          345
97421  deg
 ZDOT =       5555
972532                 TA   =          329
56316
                                          MA   =          329
64481
                                          Ha   =            192
278  n
mi
                                          Hp   =            186
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21013907
85                 X    =         6393708
21
 Y    =         258343
57  feet           Y    =          150304
63  meter
 Z    =        6736184
89                 Z    =         2084278
30
 XDOT =      -6063
979455                 XDOT =       -1931
115259
 YDOT =      16418
902241  feet/sec       YDOT =        4983
349620  meter/sec
 ZDOT =      18228
256339                 ZDOT =        5546
792016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15822759
89                 X    =        -4822777
22
 Y    =       13771470
91  feet           Y    =         4197544
33  meter
 Z    =        6856683
59                 Z    =         2089917
16
 XDOT =      -5324
199137                 XDOT =       -1622
815897
 YDOT =     -15204
237550  feet/sec       YDOT =       -4634
251605  meter/sec
 ZDOT =      18193
038393                 ZDOT =        5545
238102


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   08315
53860457  
00020000  00000-0  20000-3 0  9105
2 25544  51
6425 346
1518 0003891 332
0802  28
0151 15
72445838 11569


Satellite: ISS
Catalog Number: 25544
Epoch time:      08315
53860457   =   yrday
fracday
Element set:     910
Inclination:       51
6425  deg
RA of node:       346
1518  deg
Eccentricity:     
0003891     
Arg of perigee:   332
0802  deg
Mean anomaly:      28
0151  deg
Mean motion:   15
72445838  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1156
Checksum:              276


Coasting Arc #12 (Orbit 1170)
---------------------------------------

Vector Time (GMT): 2008/316/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         622803
49                 A    =         6725607
61  meter
 Y    =       -4442380
33  meter          E    =           
0011044
 Z    =       -5020481
42                 I    =           51
51859
 XDOT =       7397
104954                 Wp   =           87
95025
 YDOT =      -1031
045460  meter/sec      RA   =          340
80987  deg
 ZDOT =       1833
807000                 TA   =          199
76308
                                          MA   =          199
80591
                                          Ha   =            192
325  n
mi
                                          Hp   =            186
683

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2043318
54                 X    =          696822
09
 Y    =      -14574738
61  feet           Y    =        -4435001
83  meter
 Z    =      -16471395
75                 Z    =        -5017276
02
 XDOT =      24268
717041                 XDOT =        7399
175871
 YDOT =      -3382
695079  feet/sec       YDOT =        -948
315210  meter/sec
 ZDOT =       6016
427165                 ZDOT =        1869
748445

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8318553
81                 X    =         2535495
20
 Y    =       12157237
07  feet           Y    =         3705525
86  meter
 Z    =      -16459291
71                 Z    =        -5016792
11
 XDOT =     -14620
558902                 XDOT =       -4456
346353
 YDOT =      18320
872250  feet/sec       YDOT =        5584
201862  meter/sec
 ZDOT =       6155
648724                 ZDOT =        1876
241731


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   08316
49186457  
00020000  00000-0  20000-3 0  9113
2 25544  51
6434 341
2675 0003938 333
3027  26
7932 15
72476873 11716


Satellite: ISS
Catalog Number: 25544
Epoch time:      08316
49186457   =   yrday
fracday
Element set:     911
Inclination:       51
6434  deg
RA of node:       341
2675  deg
Eccentricity:     
0003938     
Arg of perigee:   333
3027  deg
Mean anomaly:      26
7932  deg
Mean motion:   15
72476873  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1171
Checksum:              301

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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