Date: September 7th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 117)
---------------------------------------

Vector Time (GMT): 2008/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5684041
13                 A    =         6737942
86  meter
 Y    =       -3551807
36  meter          E    =           
0019113
 Z    =         612604
61                 I    =           51
46816
 XDOT =       2078
646331                 Wp   =           61
18588
 YDOT =       4380
835296  meter/sec      RA   =          323
82585  deg
 ZDOT =       5981
376402                 TA   =          305
49589
                                          MA   =          305
67405
                                          Ha   =            195
625  n
mi
                                          Hp   =            184
647

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18648428
92                 X    =         5720359
62
 Y    =      -11652911
29  feet           Y    =        -3488042
06  meter
 Z    =        2009857
66                 Z    =          640306
10
 XDOT =       6819
705812                 XDOT =        2000
448035
 YDOT =      14372
819214  feet/sec       YDOT =        4403
642765  meter/sec
 ZDOT =      19623
938326                 ZDOT =        5991
284519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21104180
29                 X    =        -6432554
15
 Y    =        6142255
62  feet           Y    =         1872159
51  meter
 Z    =        2116610
65                 Z    =          645142
93
 XDOT =      -2095
463419                 XDOT =        -638
697250
 YDOT =     -14116
670912  feet/sec       YDOT =       -4302
761294  meter/sec
 ZDOT =      19662
613950                 ZDOT =        5993
164732


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   08249
56233711  
00020000  00000-0  20000-3 0  9000
2 25544  51
6425 324
0421 0006399  82
3294 277
8595 15
71916473  1183


Satellite: ISS
Catalog Number: 25544
Epoch time:      08249
56233711   =   yrday
fracday
Element set:     900
Inclination:       51
6425  deg
RA of node:       324
0421  deg
Eccentricity:     
0006399     
Arg of perigee:    82
3294  deg
Mean anomaly:     277
8595  deg
Mean motion:   15
71916473  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             118
Checksum:              295


Coasting Arc #2 (Orbit 132)
---------------------------------------

Vector Time (GMT): 2008/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2803261
08                 A    =         6726008
94  meter
 Y    =       -3134100
84  meter          E    =           
0021312
 Z    =       -5267951
97                 I    =           51
40430
 XDOT =       5752
784979                 Wp   =           88
38438
 YDOT =      -5090
679087  meter/sec      RA   =          318
68553  deg
 ZDOT =        -32
144567                 TA   =          181
30606
                                          MA   =          181
31164
                                          Ha   =            195
568  n
mi
                                          Hp   =            184
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9197050
79                 X    =        -2742415
85
 Y    =      -10282483
08  feet           Y    =        -3165108
31  meter
 Z    =      -17283306
97                 Z    =        -5281422
48
 XDOT =      18873
966465                 XDOT =        5809
438362
 YDOT =     -16701
703041  feet/sec       YDOT =       -5026
031365  meter/sec
 ZDOT =       -105
461179                 ZDOT =          -4
059819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6168735
07                 X    =         1880230
45
 Y    =       12265810
18  feet           Y    =         3738618
94  meter
 Z    =      -17335642
75                 Z    =        -5283903
91
 XDOT =     -21620
714613                 XDOT =       -6589
993814
 YDOT =      10875
033301  feet/sec       YDOT =        3314
710150  meter/sec
 ZDOT =          2
639939                 ZDOT =            
804653


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   08250
51592465  
00020000  00000-0  20000-3 0  9012
2 25544  51
6415 319
1600 0006291  85
6567 274
5314 15
71932703  1330


Satellite: ISS
Catalog Number: 25544
Epoch time:      08250
51592465   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:       319
1600  deg
Eccentricity:     
0006291     
Arg of perigee:    85
6567  deg
Mean anomaly:     274
5314  deg
Mean motion:   15
71932703  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             133
Checksum:              274


Coasting Arc #3 (Orbit 148)
---------------------------------------

Vector Time (GMT): 2008/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4218453
14                 A    =         6737735
70  meter
 Y    =        5203295
99  meter          E    =           
0018738
 Z    =         660403
71                 I    =           51
42334
 XDOT =      -4125
788717                 Wp   =          115
17981
 YDOT =      -2571
394577  meter/sec      RA   =          313
54288  deg
 ZDOT =      -5970
293784                 TA   =           57
61043
                                          MA   =           57
42925
                                          Ha   =            195
545  n
mi
                                          Hp   =            184
523

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13840069
37                 X    =        -4279531
84
 Y    =       17071181
07  feet           Y    =         5155781
30  meter
 Z    =        2166678
82                 Z    =          639762
12
 XDOT =     -13536
052221                 XDOT =       -4067
725659
 YDOT =      -8436
333915  feet/sec       YDOT =       -2617
206801  meter/sec
 ZDOT =     -19587
578031                 ZDOT =       -5990
195907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17528588
88                 X    =         5342713
89
 Y    =      -13268713
75  feet           Y    =        -4044303
95  meter
 Z    =        2087354
25                 Z    =          636225
58
 XDOT =      10052
711804                 XDOT =        3064
066558
 YDOT =      10120
112673  feet/sec       YDOT =        3084
610343  meter/sec
 ZDOT =     -19664
724792                 ZDOT =       -5993
808116


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   08251
53307237  
00020000  00000-0  20000-3 0  9027
2 25544  51
6417 313
9521 0006484  88
4779 271
7126 15
71989013  1499


Satellite: ISS
Catalog Number: 25544
Epoch time:      08251
53307237   =   yrday
fracday
Element set:     902
Inclination:       51
6417  deg
RA of node:       313
9521  deg
Eccentricity:     
0006484     
Arg of perigee:    88
4779  deg
Mean anomaly:     271
7126  deg
Mean motion:   15
71989013  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             149
Checksum:              298


Coasting Arc #4 (Orbit 164)
---------------------------------------

Vector Time (GMT): 2008/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4224606
79                 A    =         6726481
45  meter
 Y    =        1212523
58  meter          E    =           
0010586
 Z    =        5083839
79                 I    =           51
36649
 XDOT =      -3700
201227                 Wp   =          105
96019
 YDOT =       6590
345555  meter/sec      RA   =          308
42416  deg
 ZDOT =       1497
536595                 TA   =          329
60202
                                          MA   =          329
66336
                                          Ha   =            195
360  n
mi
                                          Hp   =            184
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13860258
51                 X    =         4186037
81
 Y    =        3978095
74  feet           Y    =         1259549
83  meter
 Z    =       16679264
41                 Z    =         5104269
26
 XDOT =     -12139
767804                 XDOT =       -3780
895281
 YDOT =      21621
868618  feet/sec       YDOT =        6548
516565  meter/sec
 ZDOT =       4913
177804                 ZDOT =        1479
365128

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12537217
96                 X    =        -3821344
03
 Y    =       -6935869
49  feet           Y    =        -2114053
02  meter
 Z    =       16758333
84                 Z    =         5107940
15
 XDOT =      16160
209901                 XDOT =        4925
631978
 YDOT =     -17465
211917  feet/sec       YDOT =       -5323
396592  meter/sec
 ZDOT =       4843
523173                 ZDOT =        1476
305863


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   08252
55020541  
00020000  00000-0  20000-3 0  9031
2 25544  51
6416 308
7444 0006389  92
4338 267
7556 15
72014438  1655


Satellite: ISS
Catalog Number: 25544
Epoch time:      08252
55020541   =   yrday
fracday
Element set:     903
Inclination:       51
6416  deg
RA of node:       308
7444  deg
Eccentricity:     
0006389     
Arg of perigee:    92
4338  deg
Mean anomaly:     267
7556  deg
Mean motion:   15
72014438  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             165
Checksum:              288


Coasting Arc #5 (Orbit 179)
---------------------------------------

Vector Time (GMT): 2008/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2150884
09                 A    =         6736256
74  meter
 Y    =       -6085655
99  meter          E    =           
0011948
 Z    =       -1925993
05                 I    =           51
38161
 XDOT =       5277
442863                 Wp   =           65
32642
 YDOT =        104
278385  meter/sec      RA   =          303
25496  deg
 ZDOT =       5596
268872                 TA   =          273
20675
                                          MA   =          273
34344
                                          Ha   =            195
524  n
mi
                                          Hp   =            184
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7056706
33                 X    =         2228131
11
 Y    =      -19966062
97  feet           Y    =        -6061171
63  meter
 Z    =       -6318874
83                 Z    =        -1915356
53
 XDOT =      17314
445089                 XDOT =        5248
699006
 YDOT =        342
120686  feet/sec       YDOT =         163
133006  meter/sec
 ZDOT =      18360
462179                 ZDOT =        5621
836783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11040605
53                 X    =        -3365176
57
 Y    =       18084714
24  feet           Y    =         5512220
90  meter
 Z    =       -6278303
47                 Z    =        -1913626
90
 XDOT =     -15453
483718                 XDOT =       -4710
221837
 YDOT =      -3062
699822  feet/sec       YDOT =        -933
510906  meter/sec
 ZDOT =      18459
298518                 ZDOT =        5626
394188


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   08253
50375691  
00020000  00000-0  20000-3 0  9047
2 25544  51
6411 303
8621 0006471  94
6125 265
5776 15
72007569  1807


Satellite: ISS
Catalog Number: 25544
Epoch time:      08253
50375691   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:       303
8621  deg
Eccentricity:     
0006471     
Arg of perigee:    94
6125  deg
Mean anomaly:     265
5776  deg
Mean motion:   15
72007569  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             180
Checksum:              286


Coasting Arc #6 (Orbit 195)
---------------------------------------

Vector Time (GMT): 2008/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4771674
30                 A    =         6728367
33  meter
 Y    =        1044717
50  meter          E    =           
0016967
 Z    =       -4642844
87                 I    =           51
34076
 XDOT =       1203
408129                 Wp   =           80
86283
 YDOT =      -7043
247899  meter/sec      RA   =          298
15326  deg
 ZDOT =      -2827
803294                 TA   =          161
05339
                                          MA   =          160
99018
                                          Ha   =            195
503  n
mi
                                          Hp   =            184
305

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15655099
42                 X    =        -4760447
90
 Y    =        3427550
87  feet           Y    =          991420
67  meter
 Z    =      -15232430
66                 Z    =        -4665998
25
 XDOT =       3948
189399                 XDOT =        1295
814292
 YDOT =     -23107
768699  feet/sec       YDOT =       -7029
274024  meter/sec
 ZDOT =      -9277
569863                 ZDOT =       -2821
732728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15934595
57                 X    =         4856864
73
 Y    =        -432729
10  feet           Y    =         -131895
83  meter
 Z    =      -15321833
97                 Z    =        -4670094
99
 XDOT =      -8315
289932                 XDOT =       -2534
500371
 YDOT =      20777
948793  feet/sec       YDOT =        6333
118792  meter/sec
 ZDOT =      -9254
740319                 ZDOT =       -2820
844849


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   08254
52086464  
00020000  00000-0  20000-3 0  9058
2 25544  51
6416 298
6537 0006575  98
6952 261
4955 15
72026799  1963


Satellite: ISS
Catalog Number: 25544
Epoch time:      08254
52086464   =   yrday
fracday
Element set:     905
Inclination:       51
6416  deg
RA of node:       298
6537  deg
Eccentricity:     
0006575     
Arg of perigee:    98
6952  deg
Mean anomaly:     261
4955  deg
Mean motion:   15
72026799  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             196
Checksum:              333


Coasting Arc #7 (Orbit 211)
---------------------------------------

Vector Time (GMT): 2008/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          51757
79                 A    =         6733738
86  meter
 Y    =        6020036
85  meter          E    =           
0019799
 Z    =        2996341
97                 I    =           51
34598
 XDOT =      -5353
768893                 Wp   =           97
81333
 YDOT =       2515
332932  meter/sec      RA   =          292
96595  deg
 ZDOT =      -4935
984385                 TA   =           47
39702
                                          MA   =           47
23019
                                          Ha   =            195
404  n
mi
                                          Hp   =            184
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         169809
02                 X    =          -30118
65
 Y    =       19750777
08  feet           Y    =         6020157
90  meter
 Z    =        9830518
28                 Z    =         2996394
42
 XDOT =     -17564
858572                 XDOT =       -5357
519917
 YDOT =       8252
404631  feet/sec       YDOT =        2455
442940  meter/sec
 ZDOT =     -16194
174491                 ZDOT =       -4962
001942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3275572
59                 X    =          998394
53
 Y    =      -19477623
16  feet           Y    =        -5936779
54  meter
 Z    =        9831273
57                 Z    =         2996572
18
 XDOT =      17207
961538                 XDOT =        5244
986677
 YDOT =      -5372
396689  feet/sec       YDOT =       -1637
506511  meter/sec
 ZDOT =     -16294
515648                 ZDOT =       -4966
568369


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   08255
53795697  
00020000  00000-0  20000-3 0  9066
2 25544  51
6409 293
4458 0006565 100
8707 259
3194 15
72085068  2127


Satellite: ISS
Catalog Number: 25544
Epoch time:      08255
53795697   =   yrday
fracday
Element set:     906
Inclination:       51
6409  deg
RA of node:       293
4458  deg
Eccentricity:     
0006565     
Arg of perigee:   100
8707  deg
Mean anomaly:     259
3194  deg
Mean motion:   15
72085068  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             212
Checksum:              315


Coasting Arc #8 (Orbit 227)
---------------------------------------

Vector Time (GMT): 2008/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4357109
26                 A    =         6730917
71  meter
 Y    =       -3301157
54  meter          E    =           
0017825
 Z    =        3914999
14                 I    =           51
32554
 XDOT =       1281
543388                 Wp   =          101
82442
 YDOT =       6457
757886  meter/sec      RA   =          287
87348  deg
 ZDOT =       4000
005446                 TA   =          306
40438
                                          MA   =          306
56865
                                          Ha   =            195
414  n
mi
                                          Hp   =            184
308

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14294977
87                 X    =         4374681
30
 Y    =      -10830569
35  feet           Y    =        -3252335
41  meter
 Z    =       12844485
36                 Z    =         3936208
62
 XDOT =       4204
538674                 XDOT =        1189
805308
 YDOT =      21186
869705  feet/sec       YDOT =        6471
576077  meter/sec
 ZDOT =      13123
377446                 ZDOT =        4006
008030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15724052
56                 X    =        -4792691
22
 Y    =        8502756
01  feet           Y    =         2591640
03  meter
 Z    =       12926164
94                 Z    =         3939895
07
 XDOT =       -185
557926                 XDOT =         -56
558056
 YDOT =     -20423
900715  feet/sec       YDOT =       -6225
204938  meter/sec
 ZDOT =      13147
184628                 ZDOT =        4007
261875


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   08256
55503733  
00020000  00000-0  20000-3 0  9078
2 25544  51
6402 288
2375 0006767 104
3094 255
8820 15
72076600  2288


Satellite: ISS
Catalog Number: 25544
Epoch time:      08256
55503733   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:       288
2375  deg
Eccentricity:     
0006767     
Arg of perigee:   104
3094  deg
Mean anomaly:     255
8820  deg
Mean motion:   15
72076600  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             228
Checksum:              288


Coasting Arc #9 (Orbit 242)
---------------------------------------

Vector Time (GMT): 2008/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2086231
07                 A    =         6730839
38  meter
 Y    =       -5061592
61  meter          E    =           
0013504
 Z    =       -3929820
71                 I    =           51
31874
 XDOT =       4377
162732                 Wp   =          107
16316
 YDOT =      -4897
325553  meter/sec      RA   =          282
67836  deg
 ZDOT =       3991
413873                 TA   =          204
50540
                                          MA   =          204
56964
                                          Ha   =            195
393  n
mi
                                          Hp   =            184
276

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6844590
14                 X    =        -2010386
24
 Y    =      -16606274
96  feet           Y    =        -5084498
24  meter
 Z    =      -12893112
56                 Z    =        -3939770
99
 XDOT =      14360
770117                 XDOT =        4412
210648
 YDOT =     -16067
341052  feet/sec       YDOT =       -4848
181366  meter/sec
 ZDOT =      13095
189872                 ZDOT =        4012
763449

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4422655
02                 X    =         1348025
25
 Y    =       17379617
92  feet           Y    =         5297307
54  meter
 Z    =      -12932058
50                 Z    =        -3941691
43
 XDOT =     -15092
017020                 XDOT =       -4600
046788
 YDOT =      13627
638591  feet/sec       YDOT =        4153
704243  meter/sec
 ZDOT =      13177
254506                 ZDOT =        4016
427173


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   08257
50853589  
00020000  00000-0  20000-3 0  9082
2 25544  51
6412 283
3548 0006682 107
3049 252
8844 15
72108074  2437


Satellite: ISS
Catalog Number: 25544
Epoch time:      08257
50853589   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:       283
3548  deg
Eccentricity:     
0006682     
Arg of perigee:   107
3049  deg
Mean anomaly:     252
8844  deg
Mean motion:   15
72108074  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             243
Checksum:              301


Coasting Arc #10 (Orbit 258)
---------------------------------------

Vector Time (GMT): 2008/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3139815
00                 A    =         6733448
70  meter
 Y    =        5123233
92  meter          E    =           
0011159
 Z    =       -3043226
90                 I    =           51
32179
 XDOT =      -3302
005557                 Wp   =          109
32133
 YDOT =      -4923
712944  meter/sec      RA   =          277
58403  deg
 ZDOT =      -4900
464145                 TA   =          106
04189
                                          MA   =          105
91897
                                          Ha   =            195
307  n
mi
                                          Hp   =            184
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10301230
32                 X    =        -3182087
06
 Y    =       16808510
22  feet           Y    =         5087886
08  meter
 Z    =       -9984340
23                 Z    =        -3058583
20
 XDOT =     -10833
351565                 XDOT =       -3222
896879
 YDOT =     -16153
913858  feet/sec       YDOT =       -4960
195977  meter/sec
 ZDOT =     -16077
638272                 ZDOT =       -4916
312670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12194030
78                 X    =         3716740
58
 Y    =      -15452119
74  feet           Y    =        -4709806
10  meter
 Z    =      -10043207
68                 Z    =        -3061169
70
 XDOT =       7590
203439                 XDOT =        2313
494008
 YDOT =      16440
985465  feet/sec       YDOT =        5011
212370  meter/sec
 ZDOT =     -16139
379050                 ZDOT =       -4919
282734


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   08258
52558729  
00020000  00000-0  20000-3 0  9094
2 25544  51
6404 278
1457 0006652 111
4202 248
7671 15
72126145  2591


Satellite: ISS
Catalog Number: 25544
Epoch time:      08258
52558729   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:       278
1457  deg
Eccentricity:     
0006652     
Arg of perigee:   111
4202  deg
Mean anomaly:     248
7671  deg
Mean motion:   15
72126145  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             259
Checksum:              297


Coasting Arc #11 (Orbit 274)
---------------------------------------

Vector Time (GMT): 2008/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3542713
55                 A    =         6728125
63  meter
 Y    =        3391215
50  meter          E    =           
0013501
 Z    =        4594934
90                 I    =           51
30040
 XDOT =      -2599
878769                 Wp   =           86
33371
 YDOT =       6650
841741  meter/sec      RA   =          272
39237  deg
 ZDOT =      -2895
861537                 TA   =           32
49325
                                          MA   =           32
41021
                                          Ha   =            195
147  n
mi
                                          Hp   =            184
331

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11623075
96                 X    =         3482207
70
 Y    =       11126035
11  feet           Y    =         3430494
30  meter
 Z    =       15075245
74                 Z    =         4611998
16
 XDOT =      -8529
785989                 XDOT =       -2659
988705
 YDOT =      21820
346918  feet/sec       YDOT =        6621
432027  meter/sec
 ZDOT =      -9500
858062                 ZDOT =       -2908
638431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10324703
12                 X    =        -3146969
51
 Y    =      -12258952
84  feet           Y    =        -3736528
83  meter
 Z    =       15141537
80                 Z    =         4615140
72
 XDOT =       9791
371432                 XDOT =        2984
410012
 YDOT =     -20074
507219  feet/sec       YDOT =       -6118
709800  meter/sec
 ZDOT =      -9549
598627                 ZDOT =       -2910
717662


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   08259
54262382  
00020000  00000-0  20000-3 0  9106
2 25544  51
6391 272
9366 0006640 114
4080 245
7776 15
72169181  2759


Satellite: ISS
Catalog Number: 25544
Epoch time:      08259
54262382   =   yrday
fracday
Element set:     910
Inclination:       51
6391  deg
RA of node:       272
9366  deg
Eccentricity:     
0006640     
Arg of perigee:   114
4080  deg
Mean anomaly:     245
7776  deg
Mean motion:   15
72169181  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             275
Checksum:              297


Coasting Arc #12 (Orbit 290)
---------------------------------------

Vector Time (GMT): 2008/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 643009
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1293052
23                 A    =         6735646
92  meter
 Y    =       -6298412
82  meter          E    =           
0019036
 Z    =        1986025
07                 I    =           51
32583
 XDOT =       4584
727242                 Wp   =           83
70336
 YDOT =       2708
620515  meter/sec      RA   =          267
28782  deg
 ZDOT =       5561
420072                 TA   =          298
50749
                                          MA   =          298
69905
                                          Ha   =            195
179  n
mi
                                          Hp   =            184
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4242297
36                 X    =         1353738
16
 Y    =      -20664084
07  feet           Y    =        -6283613
67  meter
 Z    =        6515830
28                 Z    =         1992454
77
 XDOT =      15041
756042                 XDOT =        4527
081637
 YDOT =       8886
550247  feet/sec       YDOT =        2759
567786  meter/sec
 ZDOT =      18246
128844                 ZDOT =        5583
552603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5971338
09                 X    =        -1820063
85
 Y    =       20224445
08  feet           Y    =         6164410
86  meter
 Z    =        6540064
55                 Z    =         1993411
67
 XDOT =     -12640
186620                 XDOT =       -3852
728882
 YDOT =      -9706
229998  feet/sec       YDOT =       -2958
458903  meter/sec
 ZDOT =      18331
951655                 ZDOT =        5587
578865


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   08260
55964621  
00020000  00000-0  20000-3 0  9115
2 25544  51
6391 267
7280 0006601 118
3539 241
8289 15
72180452  2913


Satellite: ISS
Catalog Number: 25544
Epoch time:      08260
55964621   =   yrday
fracday
Element set:     911
Inclination:       51
6391  deg
RA of node:       267
7280  deg
Eccentricity:     
0006601     
Arg of perigee:   118
3539  deg
Mean anomaly:     241
8289  deg
Mean motion:   15
72180452  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             291
Checksum:              290

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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