Date: October 23rd 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5543 41 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


303/01:34:10 987 2 6 3 0 3 1
N/A 1 7 -0 9 191 6
000/00:06:21 973 0 4 -0 1 189 3

Coasting Arc #1 (Orbit 856)
---------------------------------------

Vector Time (GMT): 2008/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2372993
11                 A    =         6734904
96  meter
 Y    =       -5943920
26  meter          E    =           
0011120
 Z    =        2077382
59                 I    =           51
97990
 XDOT =       3957
556662                 Wp   =          121
44038
 YDOT =      -3535
565185  meter/sec      RA   =           82
93779  deg
 ZDOT =      -5579
350266                 TA   =           35
48739
                                          MA   =           35
41347
                                          Ha   =            191
328  n
mi
                                          Hp   =            187
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7785410
48                 X    =        -2316442
52
 Y    =      -19501050
72  feet           Y    =        -5970140
22  meter
 Z    =        6815559
66                 Z    =         2065991
90
 XDOT =      12984
109782                 XDOT =        4023
901545
 YDOT =     -11599
623310  feet/sec       YDOT =       -3490
938612  meter/sec
 ZDOT =     -18304
954942                 ZDOT =       -5559
963063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16646977
66                 X    =         5073998
79
 Y    =       12821411
16  feet           Y    =         3907966
12  meter
 Z    =        6770893
57                 Z    =         2063768
36
 XDOT =      -4445
448774                 XDOT =       -1354
972786
 YDOT =      15427
103195  feet/sec       YDOT =        4702
181054  meter/sec
 ZDOT =     -18230
125732                 ZDOT =       -5556
542323


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   08296
53586466  
00020000  00000-0  20000-3 0  9007
2 25544  51
6396  83
4945 0003773 257
4344 102
6396 15
72394757  8571


Satellite: ISS
Catalog Number: 25544
Epoch time:      08296
53586466   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:        83
4945  deg
Eccentricity:     
0003773     
Arg of perigee:   257
4344  deg
Mean anomaly:     102
6396  deg
Mean motion:   15
72394757  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             857
Checksum:              330


Coasting Arc #2 (Orbit 872)
---------------------------------------

Vector Time (GMT): 2008/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2875854
50                 A    =         6727303
47  meter
 Y    =        3923819
16  meter          E    =           
0005505
 Z    =        4645349
06                 I    =           51
95098
 XDOT =      -3645
247089                 Wp   =          139
20489
 YDOT =      -6124
292139  meter/sec      RA   =           77
87729  deg
 ZDOT =       2910
339578                 TA   =          282
07438
                                          MA   =          282
13606
                                          Ha   =            191
228  n
mi
                                          Hp   =            187
546

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9435218
19                 X    =        -2942084
08
 Y    =       12873422
45  feet           Y    =         3891289
55  meter
 Z    =       15240646
53                 Z    =         4631216
99
 XDOT =     -11959
472078                 XDOT =       -3590
631410
 YDOT =     -20092
821977  feet/sec       YDOT =       -6164
749927  meter/sec
 ZDOT =       9548
358196                 ZDOT =        2892
763631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1387222
63                 X    =          422825
46
 Y    =      -15952433
50  feet           Y    =        -4862301
73  meter
 Z    =       15186215
24                 Z    =         4628758
41
 XDOT =      19582
667178                 XDOT =        5968
796956
 YDOT =      10746
095151  feet/sec       YDOT =        3275
409802  meter/sec
 ZDOT =       9479
705249                 ZDOT =        2889
414160


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   08297
55272438  
00020000  00000-0  20000-3 0  9012
2 25544  51
6406  78
2845 0003818 261
5558  98
5172 15
72445766  8737


Satellite: ISS
Catalog Number: 25544
Epoch time:      08297
55272438   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:        78
2845  deg
Eccentricity:     
0003818     
Arg of perigee:   261
5558  deg
Mean anomaly:      98
5172  deg
Mean motion:   15
72445766  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             873
Checksum:              321


Coasting Arc #3 (Orbit 887)
---------------------------------------

Vector Time (GMT): 2008/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3879351
17                 A    =         6732844
49  meter
 Y    =        4625229
72  meter          E    =           
0001549
 Z    =       -2980102
04                 I    =           51
96299
 XDOT =      -2461
617466                 Wp   =           20
73751
 YDOT =       5293
387687  meter/sec      RA   =           72
73073  deg
 ZDOT =       5013
326406                 TA   =          305
06629
                                          MA   =          305
08082
                                          Ha   =            191
207  n
mi
                                          Hp   =            187
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12727530
09                 X    =         3841819
80
 Y    =       15174638
19  feet           Y    =         4668400
87  meter
 Z    =       -9777237
68                 Z    =        -2961347
26
 XDOT =      -8076
172790                 XDOT =       -2544
980247
 YDOT =      17366
757502  feet/sec       YDOT =        5265
394600  meter/sec
 ZDOT =      16447
921281                 ZDOT =        5001
164930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18935319
91                 X    =        -5771485
51
 Y    =       -5927663
69  feet           Y    =        -1806751
89  meter
 Z    =       -9704148
91                 Z    =        -2957824
59
 XDOT =      -2874
568195                 XDOT =        -876
168386
 YDOT =     -17655
949353  feet/sec       YDOT =       -5381
533363  meter/sec
 ZDOT =      16401
243001                 ZDOT =        4999
098867


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   08298
50602182  
00020000  00000-0  20000-3 0  9022
2 25544  51
6416  73
4007 0003677 266
2473  93
8269 15
72431634  8886


Satellite: ISS
Catalog Number: 25544
Epoch time:      08298
50602182   =   yrday
fracday
Element set:     902
Inclination:       51
6416  deg
RA of node:        73
4007  deg
Eccentricity:     
0003677     
Arg of perigee:   266
2473  deg
Mean anomaly:      93
8269  deg
Mean motion:   15
72431634  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             888
Checksum:              300


Coasting Arc #4 (Orbit 903)
---------------------------------------

Vector Time (GMT): 2008/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1331604
89                 A    =         6729384
50  meter
 Y    =       -5181356
86  meter          E    =           
0004199
 Z    =       -4086929
09                 I    =           51
94187
 XDOT =       5046
665648                 Wp   =           52
85050
 YDOT =       4339
658588  meter/sec      RA   =           67
67821  deg
 ZDOT =      -3857
681054                 TA   =          177
59291
                                          MA   =          177
59089
                                          Ha   =            191
139  n
mi
                                          Hp   =            187
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4368782
44                 X    =         1409298
66
 Y    =      -16999202
31  feet           Y    =        -5166031
91  meter
 Z    =      -13408560
00                 Z    =        -4080271
01
 XDOT =      16557
301995                 XDOT =        5016
504102
 YDOT =      14237
725025  feet/sec       YDOT =        4395
924466  meter/sec
 ZDOT =     -12656
433903                 ZDOT =       -3833
237354

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5672913
68                 X    =         1729104
09
 Y    =       16629993
91  feet           Y    =         5068822
14  meter
 Z    =      -13383197
42                 Z    =        -4079198
57
 XDOT =     -20512
422212                 XDOT =       -6252
186290
 YDOT =      -3110
985410  feet/sec       YDOT =        -948
228353  meter/sec
 ZDOT =     -12561
325909                 ZDOT =       -3828
692137


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   08299
52286035  
00020000  00000-0  20000-3 0  9031
2 25544  51
6418  68
1908 0003740 270
9542  89
1192 15
72446935  9041


Satellite: ISS
Catalog Number: 25544
Epoch time:      08299
52286035   =   yrday
fracday
Element set:     903
Inclination:       51
6418  deg
RA of node:        68
1908  deg
Eccentricity:     
0003740     
Arg of perigee:   270
9542  deg
Mean anomaly:      89
1192  deg
Mean motion:   15
72446935  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             904
Checksum:              304


Coasting Arc #5 (Orbit 919)
---------------------------------------

Vector Time (GMT): 2008/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4796169
14                 A    =         6730621
40  meter
 Y    =       -2878732
30  meter          E    =           
0008198
 Z    =        3737560
70                 I    =           51
93411
 XDOT =        473
843402                 Wp   =           79
11845
 YDOT =      -6374
184431  meter/sec      RA   =           62
52436  deg
 ZDOT =      -4292
037893                 TA   =           55
99926
                                          MA   =           55
92141
                                          Ha   =            191
265  n
mi
                                          Hp   =            187
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15735463
05                 X    =        -4781779
08
 Y    =       -9444659
77  feet           Y    =        -2932285
19  meter
 Z    =       12262338
26                 Z    =         3714295
42
 XDOT =       1554
604336                 XDOT =         565
935826
 YDOT =     -20912
678581  feet/sec       YDOT =       -6368
370941  meter/sec
 ZDOT =     -14081
489150                 ZDOT =       -4289
511884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18375704
15                 X    =         5600914
62
 Y    =       -1161469
46  feet           Y    =         -354015
89  meter
 Z    =       12171927
58                 Z    =         3710003
53
 XDOT =      10405
421861                 XDOT =        3171
572583
 YDOT =      16825
233441  feet/sec       YDOT =        5128
331153  meter/sec
 ZDOT =     -14072
235138                 ZDOT =       -4289
217270


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   08300
53968829  
00020000  00000-0  20000-3 0  9044
2 25544  51
6423  62
9809 0003643 274
6234  85
4512 15
72449000  9209


Satellite: ISS
Catalog Number: 25544
Epoch time:      08300
53968829   =   yrday
fracday
Element set:     904
Inclination:       51
6423  deg
RA of node:        62
9809  deg
Eccentricity:     
0003643     
Arg of perigee:   274
6234  deg
Mean anomaly:      85
4512  deg
Mean motion:   15
72449000  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             920
Checksum:              285


Coasting Arc #6 (Orbit 935)
---------------------------------------

Vector Time (GMT): 2008/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         547097
75                 A    =         6731409
77  meter
 Y    =        5788313
94  meter          E    =           
0008886
 Z    =        3384123
65                 I    =           51
92420
 XDOT =      -5725
705058                 Wp   =           85
98476
 YDOT =      -2188
860672  meter/sec      RA   =           57
47184  deg
 ZDOT =       4659
728212                 TA   =          313
73514
                                          MA   =          313
80868
                                          Ha   =            191
086  n
mi
                                          Hp   =            187
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1794940
12                 X    =          465891
27
 Y    =       18990531
30  feet           Y    =         5793977
98  meter
 Z    =       11102767
88                 Z    =         3386584
06
 XDOT =     -18785
121580                 XDOT =       -5723
440101
 YDOT =      -7181
301416  feet/sec       YDOT =       -2252
875978  meter/sec
 ZDOT =      15287
822217                 ZDOT =        4631
917497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12427898
29                 X    =        -3788023
40
 Y    =      -14463297
86  feet           Y    =        -4408413
19  meter
 Z    =       11112781
05                 Z    =         3387175
66
 XDOT =      18483
197237                 XDOT =        5633
678518
 YDOT =      -4194
001942  feet/sec       YDOT =       -1278
331792  meter/sec
 ZDOT =      15179
858142                 ZDOT =        4626
820762


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   08301
55650206  
00020000  00000-0  20000-3 0  9055
2 25544  51
6436  57
7709 0003722 279
5430  80
5311 15
72522204  9362


Satellite: ISS
Catalog Number: 25544
Epoch time:      08301
55650206   =   yrday
fracday
Element set:     905
Inclination:       51
6436  deg
RA of node:        57
7709  deg
Eccentricity:     
0003722     
Arg of perigee:   279
5430  deg
Mean anomaly:      80
5311  deg
Mean motion:   15
72522204  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             936
Checksum:              269


Coasting Arc #7 (Orbit 950)
---------------------------------------

Vector Time (GMT): 2008/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5040348
65                 A    =         6728269
71  meter
 Y    =         926038
53  meter          E    =           
0005169
 Z    =       -4364975
53                 I    =           51
89678
 XDOT =       1745
855800                 Wp   =          114
23857
 YDOT =       6660
937126  meter/sec      RA   =           52
31846  deg
 ZDOT =       3430
209886                 TA   =          190
27215
                                          MA   =          190
28272
                                          Ha   =            191
194  n
mi
                                          Hp   =            187
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16536576
93                 X    =         5050823
87
 Y    =        3038184
15  feet           Y    =          982461
11  meter
 Z    =      -14320785
86                 Z    =        -4340463
30
 XDOT =       5727
873359                 XDOT =        1654
578482
 YDOT =      21853
468260  feet/sec       YDOT =        6679
950000  meter/sec
 ZDOT =      11253
969442                 ZDOT =        3438
469685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15172696
31                 X    =        -4624637
83
 Y    =        7429148
42  feet           Y    =         2264404
44  meter
 Z    =      -14225712
20                 Z    =        -4335997
08
 XDOT =     -16996
844902                 XDOT =       -5180
638326
 YDOT =     -13107
909821  feet/sec       YDOT =       -3995
290913  meter/sec
 ZDOT =      11286
518599                 ZDOT =        3440
130869


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   08302
50975781  
00020000  00000-0  20000-3 0  9060
2 25544  51
6439  52
8878 0003762 285
4497  74
6250 15
72508398  9512


Satellite: ISS
Catalog Number: 25544
Epoch time:      08302
50975781   =   yrday
fracday
Element set:     906
Inclination:       51
6439  deg
RA of node:        52
8878  deg
Eccentricity:     
0003762     
Arg of perigee:   285
4497  deg
Mean anomaly:      74
6250  deg
Mean motion:   15
72508398  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             951
Checksum:              324


Coasting Arc #8 (Orbit 959)
---------------------------------------

Vector Time (GMT): 2008/303/01:37:21
973
Vector Time (MET): N/A
Weight (LBS)     : 642049
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3866903
93                 A    =         6726311
07  meter
 Y    =       -1777557
69  meter          E    =           
0008472
 Z    =       -5216004
87                 I    =           51
87491
 XDOT =       4302
058745                 Wp   =           92
85629
 YDOT =       6289
385848  meter/sec      RA   =           49
43646  deg
 ZDOT =       1047
033207                 TA   =          187
10253
                                          MA   =          187
11454
                                          Ha   =            191
580  n
mi
                                          Hp   =            189
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12686692
69                 X    =         3911832
72
 Y    =       -5831882
19  feet           Y    =        -1734064
56  meter
 Z    =      -17112876
86                 Z    =        -5197109
68
 XDOT =      14114
365961                 XDOT =        4226
323602
 YDOT =      20634
468006  feet/sec       YDOT =        6337
070505  meter/sec
 ZDOT =       3435
148317                 ZDOT =        1067
749293

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1011924
04                 X    =          308434
45
 Y    =      -14015533
49  feet           Y    =        -4271934
61  meter
 Z    =      -17039788
92                 Z    =        -5193727
66
 XDOT =      23843
787835                 XDOT =        7267
586532
 YDOT =      -2548
905747  feet/sec       YDOT =        -776
906472  meter/sec
 ZDOT =       3515
936111                 ZDOT =        1071
657327


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   08303
08170698  
00020000  00000-0  20000-3 0  9079
2 25544  51
6444  49
9582 0006050 285
4361  74
6133 15
71955861  9600


Satellite: ISS
Catalog Number: 25544
Epoch time:      08303
08170698   =   yrday
fracday
Element set:     907
Inclination:       51
6444  deg
RA of node:        49
9582  deg
Eccentricity:     
0006050     
Arg of perigee:   285
4361  deg
Mean anomaly:      74
6133  deg
Mean motion:   15
71955861  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             960
Checksum:              301


Coasting Arc #9 (Orbit 975)
---------------------------------------

Vector Time (GMT): 2008/304/01:37:21
973
Vector Time (MET): N/A
Weight (LBS)     : 642049
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4665929
39                 A    =         6738017
84  meter
 Y    =       -4847928
20  meter          E    =           
0006962
 Z    =        -262051
75                 I    =           51
89451
 XDOT =       3586
634335                 Wp   =          161
58988
 YDOT =      -3127
720933  meter/sec      RA   =           44
34562  deg
 ZDOT =      -6048
735907                 TA   =           21
24497
                                          MA   =           21
21607
                                          Ha   =            191
708  n
mi
                                          Hp   =            189
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15308167
27                 X    =        -4610099
24
 Y    =      -15905276
25  feet           Y    =        -4899793
15  meter
 Z    =        -859749
83                 Z    =         -284584
04
 XDOT =      11767
173015                 XDOT =        3650
727094
 YDOT =     -10261
551619  feet/sec       YDOT =       -3087
254670  meter/sec
 ZDOT =     -19844
934077                 ZDOT =       -6031
155814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21192148
13                 X    =        -6459366
75
 Y    =        6168643
06  feet           Y    =         1880202
40  meter
 Z    =        -947453
54                 Z    =         -288783
84
 XDOT =      -3122
411606                 XDOT =        -951
711058
 YDOT =     -13741
725683  feet/sec       YDOT =       -4188
477988  meter/sec
 ZDOT =     -19777
044221                 ZDOT =       -6028
043079


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   08304
09886288  
00020000  00000-0  20000-3 0  9081
2 25544  51
6447  44
7510 0006060 288
5283  71
5221 15
71937315  9760


Satellite: ISS
Catalog Number: 25544
Epoch time:      08304
09886288   =   yrday
fracday
Element set:     908
Inclination:       51
6447  deg
RA of node:        44
7510  deg
Eccentricity:     
0006060     
Arg of perigee:   288
5283  deg
Mean anomaly:      71
5221  deg
Mean motion:   15
71937315  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             976
Checksum:              303


Coasting Arc #10 (Orbit 991)
---------------------------------------

Vector Time (GMT): 2008/305/01:37:21
973
Vector Time (MET): N/A
Weight (LBS)     : 642049
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2233497
83                 A    =         6725847
57  meter
 Y    =        3528902
58  meter          E    =           
0003556
 Z    =        5274744
96                 I    =           51
83253
 XDOT =      -6168
904516                 Wp   =          296
72313
 YDOT =      -4578
994896  meter/sec      RA   =           39
24248  deg
 ZDOT =        453
117533                 TA   =          148
99260
                                          MA   =          148
97161
                                          Ha   =            191
937  n
mi
                                          Hp   =            189
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7327748
80                 X    =        -2298417
17
 Y    =       11577764
36  feet           Y    =         3503563
16  meter
 Z    =       17305593
71                 Z    =         5263736
71
 XDOT =     -20239
188046                 XDOT =       -6119
444193
 YDOT =     -15022
949135  feet/sec       YDOT =       -4647
702619  meter/sec
 ZDOT =       1486
606080                 ZDOT =         423
268031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7010535
96                 X    =         2136811
36
 Y    =       11834630
25  feet           Y    =         3607195
30  meter
 Z    =       17263198
32                 Z    =         5261822
85
 XDOT =     -21651
536616                 XDOT =       -6599
388360
 YDOT =      10835
198976  feet/sec       YDOT =        3302
568648  meter/sec
 ZDOT =       1370
570128                 ZDOT =         417
749775


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
11600571  
00020000  00000-0  20000-3 0  9095
2 25544  51
6449  39
5435 0006168 293
7134  66
3380 15
72005493  9922


Satellite: ISS
Catalog Number: 25544
Epoch time:      08305
11600571   =   yrday
fracday
Element set:     909
Inclination:       51
6449  deg
RA of node:        39
5435  deg
Eccentricity:     
0006168     
Arg of perigee:   293
7134  deg
Mean anomaly:      66
3380  deg
Mean motion:   15
72005493  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             992
Checksum:              289


Coasting Arc #11 (Orbit 1006)
---------------------------------------

Vector Time (GMT): 2008/306/01:37:21
973
Vector Time (MET): N/A
Weight (LBS)     : 642049
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5922694
79                 A    =         6737395
63  meter
 Y    =        3021120
56  meter          E    =           
0010634
 Z    =       -1045691
99                 I    =           51
84823
 XDOT =      -1358
037403                 Wp   =            2
80977
 YDOT =       4712
401948  meter/sec      RA   =           34
12284  deg
 ZDOT =       5935
784264                 TA   =          345
79512
                                          MA   =          345
82500
                                          Ha   =            192
131  n
mi
                                          Hp   =            188
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19431413
36                 X    =         5893551
87
 Y    =        9911812
86  feet           Y    =         3087188
66  meter
 Z    =       -3430747
98                 Z    =        -1016989
34
 XDOT =      -4455
503290                 XDOT =       -1439
467123
 YDOT =      15460
636311  feet/sec       YDOT =        4696
760008  meter/sec
 ZDOT =      19474
357820                 ZDOT =        5928
989151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17364870
60                 X    =         5292812
56
 Y    =      -13230176
17  feet           Y    =        -4032557
70  meter
 Z    =       -3319276
81                 Z    =        -1011715
57
 XDOT =      10987
154086                 XDOT =        3348
884565
 YDOT =       9552
509094  feet/sec       YDOT =        2911
604772  meter/sec
 ZDOT =      19448
374025                 ZDOT =        5927
864403


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
06956906  
00020000  00000-0  20000-3 0  9108
2 25544  51
6453  34
6614 0006211 298
0904  61
9630 15
72011793 10071


Satellite: ISS
Catalog Number: 25544
Epoch time:      08306
06956906   =   yrday
fracday
Element set:     910
Inclination:       51
6453  deg
RA of node:        34
6614  deg
Eccentricity:     
0006211     
Arg of perigee:   298
0904  deg
Mean anomaly:      61
9630  deg
Mean motion:   15
72011793  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1007
Checksum:              271


Coasting Arc #12 (Orbit 1022)
---------------------------------------

Vector Time (GMT): 2008/307/01:37:21
973
Vector Time (MET): N/A
Weight (LBS)     : 642049
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          63102
72                 A    =         6726853
36  meter
 Y    =       -4485899
37  meter          E    =           
0010005
 Z    =       -5020603
23                 I    =           51
78783
 XDOT =       7108
898180                 Wp   =           48
31207
 YDOT =       2233
892589  meter/sec      RA   =           29
04043  deg
 ZDOT =      -1902
541217                 TA   =          203
31367
                                          MA   =          203
35907
                                          Ha   =            192
250  n
mi
                                          Hp   =            188
774

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         207029
92                 X    =          137649
90
 Y    =      -14717517
62  feet           Y    =        -4484776
62  meter
 Z    =      -16471795
37                 Z    =        -5020115
84
 XDOT =      23323
156758                 XDOT =        7092
632517
 YDOT =       7329
043928  feet/sec       YDOT =        2313
297558  meter/sec
 ZDOT =      -6241
933128                 ZDOT =       -1868
044672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13244162
48                 X    =        -4036820
72
 Y    =       -6425859
99  feet           Y    =        -1958602
12  meter
 Z    =      -16470237
17                 Z    =        -5020128
29
 XDOT =      15953
269251                 XDOT =        4862
556468
 YDOT =     -17190
779851  feet/sec       YDOT =       -5239
749699  meter/sec
 ZDOT =      -6108
063168                 ZDOT =       -1861
737654


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
08669160  
00020000  00000-0  20000-3 0  9115
2 25544  51
6450  29
4539 0006321 302
7989  57
2564 15
72036759 10235


Satellite: ISS
Catalog Number: 25544
Epoch time:      08307
08669160   =   yrday
fracday
Element set:     911
Inclination:       51
6450  deg
RA of node:        29
4539  deg
Eccentricity:     
0006321     
Arg of perigee:   302
7989  deg
Mean anomaly:      57
2564  deg
Mean motion:   15
72036759  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1023
Checksum:              292


Coasting Arc #13 (Orbit 1038)
---------------------------------------

Vector Time (GMT): 2008/308/01:37:21
973
Vector Time (MET): N/A
Weight (LBS)     : 642049
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6288126
97                 A    =         6735682
15  meter
 Y    =        -846439
41  meter          E    =           
0008348
 Z    =        2252699
55                 I    =           51
79094
 XDOT =      -1256
595610                 Wp   =           94
66413
 YDOT =      -5265
988910  meter/sec      RA   =           23
89582  deg
 ZDOT =      -5469
650873                 TA   =           60
13409
                                          MA   =           60
05117
                                          Ha   =            192
451  n
mi
                                          Hp   =            188
663

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20630337
83                 X    =        -6289138
05
 Y    =       -2777032
20  feet           Y    =         -916762
67  meter
 Z    =        7390746
57                 Z    =         2222148
63
 XDOT =      -4122
689009                 XDOT =       -1171
045895
 YDOT =     -17276
866501  feet/sec       YDOT =       -5279
562230  meter/sec
 ZDOT =     -17945
048796                 ZDOT =       -5475
548061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10859036
61                 X    =        -3309834
36
 Y    =       17808461
83  feet           Y    =         5428019
17  meter
 Z    =        7272268
74                 Z    =         2216587
51
 XDOT =     -16135
680601                 XDOT =       -4918
155447
 YDOT =      -2478
829010  feet/sec       YDOT =        -755
547082  meter/sec
 ZDOT =     -17968
290987                 ZDOT =       -5476
735093


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
10380486  
00020000  00000-0  20000-3 0  9121
2 25544  51
6450  24
2464 0006213 307
0359  53
0235 15
72022779 10397


Satellite: ISS
Catalog Number: 25544
Epoch time:      08308
10380486   =   yrday
fracday
Element set:     912
Inclination:       51
6450  deg
RA of node:        24
2464  deg
Eccentricity:     
0006213     
Arg of perigee:   307
0359  deg
Mean anomaly:      53
0235  deg
Mean motion:   15
72022779  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1039
Checksum:              260

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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