Date: September 28th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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


276/12:01:12 220 -2 2 2 3 2 3
N/A -0 6 0 0 193 8
000/00:04:40 440 0 5 0 0 187 1

Coasting Arc #1 (Orbit 447)
---------------------------------------

Vector Time (GMT): 2008/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5646008
97                 A    =         6731449
69  meter
 Y    =         529808
57  meter          E    =           
0015384
 Z    =        3610105
86                 I    =           51
44691
 XDOT =       2249
448109                 Wp   =          107
23596
 YDOT =       5928
979089  meter/sec      RA   =          215
84813  deg
 ZDOT =      -4377
314697                 TA   =           29
39421
                                          MA   =           29
30778
                                          Ha   =            194
390  n
mi
                                          Hp   =            185
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18523651
47                 X    =         5622127
70
 Y    =        1738217
10  feet           Y    =          592812
26  meter
 Z    =       11844179
32                 Z    =         3637476
10
 XDOT =       7380
079098                 XDOT =        2204
246320
 YDOT =      19452
031132  feet/sec       YDOT =        5953
880636  meter/sec
 ZDOT =     -14361
268690                 ZDOT =       -4366
497146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18536534
32                 X    =        -5649935
66
 Y    =        -152662
72  feet           Y    =          -46531
60  meter
 Z    =       11950114
46                 Z    =         3642394
89
 XDOT =      -9110
487408                 XDOT =       -2776
876562
 YDOT =     -17390
407864  feet/sec       YDOT =       -5300
596317  meter/sec
 ZDOT =     -14318
800502                 ZDOT =       -4364
370393


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   08270
53953531  
00020000  00000-0  20000-3 0  9000
2 25544  51
6389 216
6349 0006160 152
7145 207
4342 15
72231492  4487


Satellite: ISS
Catalog Number: 25544
Epoch time:      08270
53953531   =   yrday
fracday
Element set:     900
Inclination:       51
6389  deg
RA of node:       216
6349  deg
Eccentricity:     
0006160     
Arg of perigee:   152
7145  deg
Mean anomaly:     207
4342  deg
Mean motion:   15
72231492  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             448
Checksum:              279


Coasting Arc #2 (Orbit 463)
---------------------------------------

Vector Time (GMT): 2008/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3023397
58                 A    =         6732164
14  meter
 Y    =       -4954170
41  meter          E    =           
0016038
 Z    =        3404401
65                 I    =           51
47446
 XDOT =       6154
389975                 Wp   =          111
37078
 YDOT =       -587
292645  meter/sec      RA   =          210
76498  deg
 ZDOT =       4587
904569                 TA   =          288
92470
                                          MA   =          289
09848
                                          Ha   =            194
434  n
mi
                                          Hp   =            185
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9919283
39                 X    =        -2984312
57
 Y    =      -16253839
94  feet           Y    =        -4987760
94  meter
 Z    =       11169296
75                 Z    =         3389809
33
 XDOT =      20191
568161                 XDOT =        6138
212461
 YDOT =      -1926
813139  feet/sec       YDOT =        -518
560726  meter/sec
 ZDOT =      15052
180344                 ZDOT =        4617
763475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11599509
63                 X    =         3535530
53
 Y    =       15142667
68  feet           Y    =         4615485
11  meter
 Z    =       11112320
98                 Z    =         3387035
44
 XDOT =     -18696
606783                 XDOT =       -5698
725747
 YDOT =       3135
404462  feet/sec       YDOT =         955
671280  meter/sec
 ZDOT =      15167
630382                 ZDOT =        4623
093740


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   08271
55650769  
00020000  00000-0  20000-3 0  9011
2 25544  51
6395 211
4260 0006232 157
2622 202
8817 15
72259784  4647


Satellite: ISS
Catalog Number: 25544
Epoch time:      08271
55650769   =   yrday
fracday
Element set:     901
Inclination:       51
6395  deg
RA of node:       211
4260  deg
Eccentricity:     
0006232     
Arg of perigee:   157
2622  deg
Mean anomaly:     202
8817  deg
Mean motion:   15
72259784  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             464
Checksum:              290


Coasting Arc #3 (Orbit 478)
---------------------------------------

Vector Time (GMT): 2008/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4928685
79                 A    =         6728819
77  meter
 Y    =        1478333
00  meter          E    =           
0013869
 Z    =       -4350228
10                 I    =           51
48972
 XDOT =      -4553
142221                 Wp   =          130
82808
 YDOT =      -5176
969652  meter/sec      RA   =          205
58161  deg
 ZDOT =       3397
448312                 TA   =          173
57598
                                          MA   =          173
55818
                                          Ha   =            194
277  n
mi
                                          Hp   =            185
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16170228
96                 X    =        -4923717
61
 Y    =        4850173
87  feet           Y    =         1423244
93  meter
 Z    =      -14272401
90                 Z    =        -4374159
96
 XDOT =     -14938
130645                 XDOT =       -4511
418460
 YDOT =     -16984
808570  feet/sec       YDOT =       -5227
651893  meter/sec
 ZDOT =      11146
483962                 ZDOT =        3375
430796

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15391345
32                 X    =         4691282
05
 Y    =       -6742407
52  feet           Y    =        -2055085
81  meter
 Z    =      -14364831
28                 Z    =        -4378400
57
 XDOT =      16436
662415                 XDOT =        5009
894704
 YDOT =      13943
071628  feet/sec       YDOT =        4249
848232  meter/sec
 ZDOT =      11060
753438                 ZDOT =        3371
317648


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   08272
50990646  
00020000  00000-0  20000-3 0  9029
2 25544  51
6399 206
5421 0006119 160
7358 199
4037 15
72266376  4790


Satellite: ISS
Catalog Number: 25544
Epoch time:      08272
50990646   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       206
5421  deg
Eccentricity:     
0006119     
Arg of perigee:   160
7358  deg
Mean anomaly:     199
4037  deg
Mean motion:   15
72266376  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             479
Checksum:              311


Coasting Arc #4 (Orbit 494)
---------------------------------------

Vector Time (GMT): 2008/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4835518
74                 A    =         6734326
13  meter
 Y    =        3945249
36  meter          E    =           
0010929
 Z    =       -2520608
06                 I    =           51
53629
 XDOT =      -4915
807283                 Wp   =          149
12116
 YDOT =       2653
877625  meter/sec      RA   =          200
49607  deg
 ZDOT =      -5295
947344                 TA   =           59
45251
                                          MA   =           59
34470
                                          Ha   =            194
189  n
mi
                                          Hp   =            185
528

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15864562
80                 X    =         4803287
78
 Y    =       12943731
51  feet           Y    =         3999142
48  meter
 Z    =       -8269711
48                 Z    =        -2497195
42
 XDOT =     -16127
976649                 XDOT =       -4919
390874
 YDOT =       8706
947588  feet/sec       YDOT =        2598
885693  meter/sec
 ZDOT =     -17375
155328                 ZDOT =       -5319
837642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17533323
13                 X    =        -5344156
89
 Y    =      -10644432
28  feet           Y    =        -3244422
96  meter
 Z    =       -8178710
63                 Z    =        -2492871
00
 XDOT =      13909
625515                 XDOT =        4239
653857
 YDOT =      -9539
875731  feet/sec       YDOT =       -2907
754123  meter/sec
 ZDOT =     -17467
302480                 ZDOT =       -5324
033796


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   08273
52684988  
00020000  00000-0  20000-3 0  9032
2 25544  51
6408 201
3329 0006096 164
4363 195
6988 15
72297694  4950


Satellite: ISS
Catalog Number: 25544
Epoch time:      08273
52684988   =   yrday
fracday
Element set:     903
Inclination:       51
6408  deg
RA of node:       201
3329  deg
Eccentricity:     
0006096     
Arg of perigee:   164
4363  deg
Mean anomaly:     195
6988  deg
Mean motion:   15
72297694  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             495
Checksum:              334


Coasting Arc #5 (Orbit 510)
---------------------------------------

Vector Time (GMT): 2008/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3507293
84                 A    =         6726597
68  meter
 Y    =       -3042140
16  meter          E    =           
0007232
 Z    =        4860661
44                 I    =           51
53841
 XDOT =       6375
404956                 Wp   =          110
03211
 YDOT =       3652
987534  meter/sec      RA   =          195
32730  deg
 ZDOT =      -2313
650195                 TA   =            2
52428
                                          MA   =            2
52063
                                          Ha   =            193
938  n
mi
                                          Hp   =            185
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11506869
54                 X    =         3517438
20
 Y    =       -9980774
79  feet           Y    =        -3002862
45  meter
 Z    =       15947051
95                 Z    =         4877725
08
 XDOT =      20916
682926                 XDOT =        6345
322331
 YDOT =      11984
867239  feet/sec       YDOT =        3724
112603  meter/sec
 ZDOT =      -7590
715862                 ZDOT =       -2282
751265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9743647
33                 X    =        -2969863
71
 Y    =       11618327
69  feet           Y    =         3541266
28  meter
 Z    =       16012750
43                 Z    =         4880686
33
 XDOT =     -21707
097029                 XDOT =       -6616
323174
 YDOT =      -7906
547399  feet/sec       YDOT =       -2409
915647  meter/sec
 ZDOT =      -7470
777705                 ZDOT =       -2277
093044


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   08274
54377794  
00020000  00000-0  20000-3 0  9040
2 25544  51
6406 196
1245 0006071 168
5805 191
5496 15
72321122  5117


Satellite: ISS
Catalog Number: 25544
Epoch time:      08274
54377794   =   yrday
fracday
Element set:     904
Inclination:       51
6406  deg
RA of node:       196
1245  deg
Eccentricity:     
0006071     
Arg of perigee:   168
5805  deg
Mean anomaly:     191
5496  deg
Mean motion:   15
72321122  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             511
Checksum:              289


Coasting Arc #6 (Orbit 526)
---------------------------------------

Vector Time (GMT): 2008/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6135682
97                 A    =         6735982
72  meter
 Y    =       -2324586
59  meter          E    =           
0013160
 Z    =        1511131
13                 I    =           51
59856
 XDOT =       2991
215007                 Wp   =           87
32442
 YDOT =      -4112
576247  meter/sec      RA   =          190
23146  deg
 ZDOT =       5776
323121                 TA   =          289
31736
                                          MA   =          289
45963
                                          Ha   =            193
909  n
mi
                                          Hp   =            185
772

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20130193
46                 X    =        -6116574
00
 Y    =       -7626596
41  feet           Y    =        -2393092
39  meter
 Z    =        4957779
30                 Z    =         1481369
91
 XDOT =       9813
697530                 XDOT =        3008
919240
 YDOT =     -13492
704223  feet/sec       YDOT =       -4079
027387  meter/sec
 ZDOT =      18951
191342                 ZDOT =        5790
898030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21164853
49                 X    =         6451047
34
 Y    =        4070575
74  feet           Y    =         1240711
48  meter
 Z    =        4842378
22                 Z    =         1475956
88
 XDOT =      -6960
326473                 XDOT =       -2121
507509
 YDOT =      13408
931032  feet/sec       YDOT =        4087
042179  meter/sec
 ZDOT =      19007
153204                 ZDOT =        5793
380297


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   08275
56069072  
00020000  00000-0  20000-3 0  9051
2 25544  51
6406 190
9147 0006040 172
5935 187
5318 15
72334605  5270


Satellite: ISS
Catalog Number: 25544
Epoch time:      08275
56069072   =   yrday
fracday
Element set:     905
Inclination:       51
6406  deg
RA of node:       190
9147  deg
Eccentricity:     
0006040     
Arg of perigee:   172
5935  deg
Mean anomaly:     187
5318  deg
Mean motion:   15
72334605  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             527
Checksum:              293


Coasting Arc #7 (Orbit 541)
---------------------------------------

Vector Time (GMT): 2008/276/11:59:58
000
Vector Time (MET): N/A
Weight (LBS)     : 628649
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1641814
68                 A    =         6725458
63  meter
 Y    =        3978276
39  meter          E    =           
0016337
 Z    =       -5181631
51                 I    =           51
59213
 XDOT =      -7436
712591                 Wp   =          120
06382
 YDOT =      -1571
971244  meter/sec      RA   =          185
08188  deg
 ZDOT =       1144
093248                 TA   =          160
91633
                                          MA   =          160
85505
                                          Ha   =            193
765  n
mi
                                          Hp   =            186
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5386531
11                 X    =        -1661006
39
 Y    =       13052087
89  feet           Y    =         3959809
13  meter
 Z    =      -17000103
38                 Z    =        -5189654
42
 XDOT =     -24398
663357                 XDOT =       -7424
139761
 YDOT =      -5157
385970  feet/sec       YDOT =       -1655
062506  meter/sec
 ZDOT =       3753
586773                 ZDOT =        1107
995500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2746255
79                 X    =          837058
76
 Y    =      -13812582
64  feet           Y    =        -4210075
19  meter
 Z    =      -17030733
12                 Z    =        -5190967
45
 XDOT =      23946
515184                 XDOT =        7298
897828
 YDOT =        283
836826  feet/sec       YDOT =          86
513465  meter/sec
 ZDOT =       3613
737283                 ZDOT =        1101
467124


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   08276
51403164  
00020000  00000-0  20000-3 0  9062
2 25544  51
6411 186
0308 0005958 180
4745 179
6413 15
72265513  5421


Satellite: ISS
Catalog Number: 25544
Epoch time:      08276
51403164   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:       186
0308  deg
Eccentricity:     
0005958     
Arg of perigee:   180
4745  deg
Mean anomaly:     179
6413  deg
Mean motion:   15
72265513  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             542
Checksum:              285


Coasting Arc #8 (Orbit 541)
---------------------------------------

Vector Time (GMT): 2008/276/12:03:32
440
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3171894
43                 A    =         6728088
32  meter
 Y    =        3526146
35  meter          E    =           
0013386
 Z    =       -4784099
21                 I    =           51
59793
 XDOT =      -6762
525374                 Wp   =          133
40850
 YDOT =      -2623
897606  meter/sec      RA   =          185
05899  deg
 ZDOT =       2545
070072                 TA   =          161
60627
                                          MA   =          161
55782
                                          Ha   =            193
838  n
mi
                                          Hp   =            187
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10406477
78                 X    =        -3187847
81
 Y    =       11568721
63  feet           Y    =         3490586
98  meter
 Z    =      -15695863
55                 Z    =        -4799547
53
 XDOT =     -22186
763037                 XDOT =       -6745
045686
 YDOT =      -8608
587946  feet/sec       YDOT =       -2699
422218  meter/sec
 ZDOT =       8349
967427                 ZDOT =        2512
259566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7753704
61                 X    =         2363329
16
 Y    =      -13421685
15  feet           Y    =        -4090929
63  meter
 Z    =      -15755274
21                 Z    =        -4802207
58
 XDOT =      22539
944577                 XDOT =        6870
175107
 YDOT =       3351
366282  feet/sec       YDOT =        1021
496443  meter/sec
 ZDOT =       8222
728326                 ZDOT =        2506
287594


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   08276
51403161  
00020000  00000-0  20000-3 0  9070
2 25544  51
6411 186
0308 0005686 194
0938 166
0067 15
71932794  5420


Satellite: ISS
Catalog Number: 25544
Epoch time:      08276
51403161   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       186
0308  deg
Eccentricity:     
0005686     
Arg of perigee:   194
0938  deg
Mean anomaly:     166
0067  deg
Mean motion:   15
71932794  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             542
Checksum:              292


Coasting Arc #9 (Orbit 557)
---------------------------------------

Vector Time (GMT): 2008/277/12:03:32
440
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6405413
97                 A    =         6736979
70  meter
 Y    =        1278968
96  meter          E    =           
0012315
 Z    =       -1620770
28                 I    =           51
65709
 XDOT =      -2357
455466                 Wp   =          165
99983
 YDOT =       4548
116746  meter/sec      RA   =          179
97307  deg
 ZDOT =      -5748
654588                 TA   =           31
88225
                                          MA   =           31
80778
                                          Ha   =            193
806  n
mi
                                          Hp   =            187
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21015137
70                 X    =         6398509
85
 Y    =        4196092
38  feet           Y    =         1350559
35  meter
 Z    =       -5317487
80                 Z    =        -1589668
91
 XDOT =      -7734
433944                 XDOT =       -2380
211494
 YDOT =      14921
642869  feet/sec       YDOT =        4521
626926  meter/sec
 ZDOT =     -18860
415315                 ZDOT =       -5760
162756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21452913
11                 X    =        -6538847
92
 Y    =         531660
22  feet           Y    =          162050
04  meter
 Z    =       -5196993
08                 Z    =        -1584043
49
 XDOT =       4199
215729                 XDOT =        1279
920954
 YDOT =     -14668
419338  feet/sec       YDOT =       -4470
934214  meter/sec
 ZDOT =     -18904
479873                 ZDOT =       -5762
085465


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   08277
53119369  
00020000  00000-0  20000-3 0  9088
2 25544  51
6412 180
8232 0005811 198
4890 161
6062 15
71932594  5585


Satellite: ISS
Catalog Number: 25544
Epoch time:      08277
53119369   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:       180
8232  deg
Eccentricity:     
0005811     
Arg of perigee:   198
4890  deg
Mean anomaly:     161
6062  deg
Mean motion:   15
71932594  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             558
Checksum:              305


Coasting Arc #10 (Orbit 573)
---------------------------------------

Vector Time (GMT): 2008/278/12:03:32
440
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         867627
72                 A    =         6726128
17  meter
 Y    =       -4196157
81  meter          E    =           
0003268
 Z    =        5183411
00                 I    =           51
65037
 XDOT =       7615
170579                 Wp   =          165
58390
 YDOT =        198
369457  meter/sec      RA   =          174
83014  deg
 ZDOT =      -1117
038643                 TA   =          295
06030
                                          MA   =          295
09423
                                          Ha   =            193
433  n
mi
                                          Hp   =            187
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2846547
63                 X    =          889304
77
 Y    =      -13766921
95  feet           Y    =        -4186334
23  meter
 Z    =       17005941
61                 Z    =         5187678
73
 XDOT =      24984
155442                 XDOT =        7617
812879
 YDOT =        650
818427  feet/sec       YDOT =         283
541449  meter/sec
 ZDOT =      -3664
824944                 ZDOT =       -1080
036992

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         585084
16                 X    =          178333
65
 Y    =       14026449
78  feet           Y    =         4275261
89  meter
 Z    =       17022027
10                 Z    =         5188313
86
 XDOT =     -23426
383254                 XDOT =       -7140
361616
 YDOT =       5239
108387  feet/sec       YDOT =        1596
880236  meter/sec
 ZDOT =      -3521
593614                 ZDOT =       -1073
381734


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   08278
54833863  
00020000  00000-0  20000-3 0  9093
2 25544  51
6408 175
6156 0005704 203
8085 156
2814 15
72019238  5740


Satellite: ISS
Catalog Number: 25544
Epoch time:      08278
54833863   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       175
6156  deg
Eccentricity:     
0005704     
Arg of perigee:   203
8085  deg
Mean anomaly:     156
2814  deg
Mean motion:   15
72019238  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             574
Checksum:              305


Coasting Arc #11 (Orbit 589)
---------------------------------------

Vector Time (GMT): 2008/279/12:03:32
440
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6660757
81                 A    =         6737825
90  meter
 Y    =         942412
27  meter          E    =           
0007766
 Z    =         330458
54                 I    =           51
71885
 XDOT =       -370
283788                 Wp   =           63
61111
 YDOT =      -4767
764757  meter/sec      RA   =          169
72497  deg
 ZDOT =       6027
928841                 TA   =          299
97244
                                          MA   =          300
04950
                                          Ha   =            193
328  n
mi
                                          Hp   =            187
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21852879
95                 X    =        -6672406
31
 Y    =        3091903
76  feet           Y    =          867862
70  meter
 Z    =        1084181
55                 Z    =          298071
72
 XDOT =      -1214
841823                 XDOT =        -346
225450
 YDOT =     -15642
272826  feet/sec       YDOT =       -4771
770945  meter/sec
 ZDOT =      19776
669427                 ZDOT =        6026
188428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20363592
35                 X    =         6206822
95
 Y    =       -8525741
62  feet           Y    =        -2598646
05  meter
 Z    =         958914
49                 Z    =          292277
14
 XDOT =       4623
745449                 XDOT =        1409
317613
 YDOT =      13311
262357  feet/sec       YDOT =        4057
272766  meter/sec
 ZDOT =      19769
444087                 ZDOT =        6025
726558


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   08279
56547107  
00020000  00000-0  20000-3 0  9101
2 25544  51
6410 170
4072 0005654 207
4631 152
6233 15
72005454  5902


Satellite: ISS
Catalog Number: 25544
Epoch time:      08279
56547107   =   yrday
fracday
Element set:     910
Inclination:       51
6410  deg
RA of node:       170
4072  deg
Eccentricity:     
0005654     
Arg of perigee:   207
4631  deg
Mean anomaly:     152
6233  deg
Mean motion:   15
72005454  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             590
Checksum:              265


Coasting Arc #12 (Orbit 604)
---------------------------------------

Vector Time (GMT): 2008/280/12:03:32
440
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1471594
02                 A    =         6725724
29  meter
 Y    =        3915908
72  meter          E    =           
0012639
 Z    =       -5276490
07                 I    =           51
70725
 XDOT =      -7329
765226                 Wp   =          108
97041
 YDOT =       2298
568347  meter/sec      RA   =          164
60967  deg
 ZDOT =       -343
071296                 TA   =          157
79816
                                          MA   =          157
74339
                                          Ha   =            193
116  n
mi
                                          Hp   =            187
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4828064
36                 X    =         1453328
93
 Y    =       12847469
54  feet           Y    =         3932262
79  meter
 Z    =      -17311319
12                 Z    =        -5269385
33
 XDOT =     -24047
786174                 XDOT =       -7353
256818
 YDOT =       7541
234735  feet/sec       YDOT =        2216
471333  meter/sec
 ZDOT =      -1125
561995                 ZDOT =        -378
736878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8210725
51                 X    =        -2502629
13
 Y    =      -11041602
98  feet           Y    =        -3365480
59  meter
 Z    =      -17283415
15                 Z    =        -5267984
94
 XDOT =      20309
607335                 XDOT =        6190
368316
 YDOT =     -13149
111043  feet/sec       YDOT =       -4007
849046  meter/sec
 ZDOT =      -1263
398124                 ZDOT =        -385
083748


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   08280
51901754  
00020000  00000-0  20000-3 0  9111
2 25544  51
6412 165
5246 0005643 211
7138 148
3685 15
72046604  6052


Satellite: ISS
Catalog Number: 25544
Epoch time:      08280
51901754   =   yrday
fracday
Element set:     911
Inclination:       51
6412  deg
RA of node:       165
5246  deg
Eccentricity:     
0005643     
Arg of perigee:   211
7138  deg
Mean anomaly:     148
3685  deg
Mean motion:   15
72046604  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             605
Checksum:              275


Coasting Arc #13 (Orbit 620)
---------------------------------------

Vector Time (GMT): 2008/281/12:03:32
440
Vector Time (MET): N/A
Weight (LBS)     : 628524
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5947758
78                 A    =         6737451
48  meter
 Y    =       -3005415
26  meter          E    =           
0014869
 Z    =         927248
15                 I    =           51
77441
 XDOT =       2913
665056                 Wp   =          147
90237
 YDOT =       3918
909620  meter/sec      RA   =          159
48446  deg
 ZDOT =      -5956
343492                 TA   =           21
99383
                                          MA   =           21
93009
                                          Ha   =            193
091  n
mi
                                          Hp   =            187
826

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19513644
29                 X    =         5976419
31
 Y    =       -9860286
30  feet           Y    =        -2938743
74  meter
 Z    =        3042152
74                 Z    =          956212
35
 XDOT =       9559
268557                 XDOT =        2898
561808
 YDOT =      12857
315025  feet/sec       YDOT =        3951
407414  meter/sec
 ZDOT =     -19541
809358                 ZDOT =       -5942
225455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15856405
14                 X    =        -4833032
29
 Y    =       15029605
32  feet           Y    =         4581023
70  meter
 Z    =        3153986
79                 Z    =          961335
17
 XDOT =     -11851
582896                 XDOT =       -3612
362467
 YDOT =      -8393
590962  feet/sec       YDOT =       -2558
366525  meter/sec
 ZDOT =     -19486
749348                 ZDOT =       -5939
561201


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   08281
53612098  
00020000  00000-0  20000-3 0  9125
2 25544  51
6412 160
3168 0005764 214
4811 145
5978 15
72010310  6217


Satellite: ISS
Catalog Number: 25544
Epoch time:      08281
53612098   =   yrday
fracday
Element set:     912
Inclination:       51
6412  deg
RA of node:       160
3168  deg
Eccentricity:     
0005764     
Arg of perigee:   214
4811  deg
Mean anomaly:     145
5978  deg
Mean motion:   15
72010310  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             621
Checksum:              264

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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