Date: September 12th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 ET - UTC (sec) : 66 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 1950)
---------------------------------------

Vector Time (GMT): 2009/254/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2655463
38                 A    =         6728942
19  meter
 Y    =        5571274
40  meter          E    =           
0012874
 Z    =       -2690854
91                 I    =           51
41497
 XDOT =      -5690
183972                 Wp   =           93
85984
 YDOT =        225
302640  meter/sec      RA   =          224
15920  deg
 ZDOT =      -5170
977490                 TA   =          116
88941
                                          MA   =          116
75778
                                          Ha   =            193
298  n
mi
                                          Hp   =            180
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8712150
19                 X    =         2606038
86
 Y    =       18278459
31  feet           Y    =         5600693
01  meter
 Z    =       -8828264
14                 Z    =        -2678074
61
 XDOT =     -18668
582585                 XDOT =       -5667
160560
 YDOT =        739
181891  feet/sec       YDOT =         161
800397  meter/sec
 ZDOT =     -16965
149244                 ZDOT =       -5198
564699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19867588
86                 X    =         6055641
08
 Y    =       -4021708
37  feet           Y    =        -1225816
71  meter
 Z    =       -8777622
59                 Z    =        -2675419
37
 XDOT =      -4123
160184                 XDOT =       -1256
739224
 YDOT =      16736
373424  feet/sec       YDOT =        5101
246620  meter/sec
 ZDOT =     -17073
699906                 ZDOT =       -5204
063731


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   09254
26591782  
00020000  00000-0  20000-3 0  9009
2 25544  51
6389 224
9551 0009030  77
3566 282
8606 15
74042333 19518


Satellite: ISS
Catalog Number: 25544
Epoch time:      09254
26591782   =   yrday
fracday
Element set:     900
Inclination:       51
6389  deg
RA of node:       224
9551  deg
Eccentricity:     
0009030     
Arg of perigee:    77
3566  deg
Mean anomaly:     282
8606  deg
Mean motion:   15
74042333  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1951
Checksum:              299


Coasting Arc #2 (Orbit 1966)
---------------------------------------

Vector Time (GMT): 2009/255/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4955989
68                 A    =         6722983
04  meter
 Y    =        -599992
14  meter          E    =           
0017476
 Z    =        4491113
50                 I    =           51
41831
 XDOT =       3570
856514                 Wp   =           73
55875
 YDOT =       6081
669200  meter/sec      RA   =          218
96164  deg
 ZDOT =      -3113
131143                 TA   =           47
61892
                                          MA   =           47
47112
                                          Ha   =            193
041  n
mi
                                          Hp   =            180
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16259808
67                 X    =         4940513
46
 Y    =       -1968478
15  feet           Y    =         -544657
94  meter
 Z    =       14734624
34                 Z    =         4515152
18
 XDOT =      11715
408511                 XDOT =        3517
707929
 YDOT =      19952
982939  feet/sec       YDOT =        6121
303486  meter/sec
 ZDOT =     -10213
684851                 ZDOT =       -3095
912882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1773096
23                 X    =          540439
73
 Y    =      -16196186
56  feet           Y    =        -4936597
66  meter
 Z    =       14829197
87                 Z    =         4519939
51
 XDOT =      20931
695555                 XDOT =        6379
980805
 YDOT =      -7042
073760  feet/sec       YDOT =       -2146
424082  meter/sec
 ZDOT =     -10145
536638                 ZDOT =       -3092
359567


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   09255
28171299  
00020000  00000-0  20000-3 0  9010
2 25544  51
6392 219
7380 0008877  80
1011 280
1154 15
74100803 19672


Satellite: ISS
Catalog Number: 25544
Epoch time:      09255
28171299   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       219
7380  deg
Eccentricity:     
0008877     
Arg of perigee:    80
1011  deg
Mean anomaly:     280
1154  deg
Mean motion:   15
74100803  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1967
Checksum:              284


Coasting Arc #3 (Orbit 1982)
---------------------------------------

Vector Time (GMT): 2009/256/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3549031
59                 A    =         6728772
73  meter
 Y    =       -5005935
29  meter          E    =           
0022773
 Z    =        2736497
47                 I    =           51
46057
 XDOT =       5624
298363                 Wp   =           81
29867
 YDOT =      -1158
707767  meter/sec      RA   =          213
85754  deg
 ZDOT =       5141
715173                 TA   =          310
08084
                                          MA   =          310
28029
                                          Ha   =            193
340  n
mi
                                          Hp   =            180
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11643804
43                 X    =        -3506083
98
 Y    =      -16423672
20  feet           Y    =        -5045382
54  meter
 Z    =        8978010
08                 Z    =         2719360
57
 XDOT =      18452
422450                 XDOT =        5611
859735
 YDOT =      -3801
534668  feet/sec       YDOT =       -1095
883154  meter/sec
 ZDOT =      16869
144270                 ZDOT =        5169
007750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18524327
38                 X    =        -5646214
99
 Y    =        7960955
73  feet           Y    =         2426499
31  meter
 Z    =        8910237
58                 Z    =         2715840
42
 XDOT =        743
870724                 XDOT =         226
731797
 YDOT =     -17391
737550  feet/sec       YDOT =       -5301
001605  meter/sec
 ZDOT =      16976
501967                 ZDOT =        5174
437799


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   09256
29750030  
00020000  00000-0  20000-3 0  9029
2 25544  51
6385 214
5209 0009158  84
1630 276
0577 15
74072198 19837


Satellite: ISS
Catalog Number: 25544
Epoch time:      09256
29750030   =   yrday
fracday
Element set:     902
Inclination:       51
6385  deg
RA of node:       214
5209  deg
Eccentricity:     
0009158     
Arg of perigee:    84
1630  deg
Mean anomaly:     276
0577  deg
Mean motion:   15
74072198  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1983
Checksum:              298


Coasting Arc #4 (Orbit 1997)
---------------------------------------

Vector Time (GMT): 2009/257/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4839826
41                 A    =         6723136
68  meter
 Y    =        1408044
93  meter          E    =           
0018593
 Z    =       -4466491
10                 I    =           51
46785
 XDOT =      -4496
378879                 Wp   =           99
62526
 YDOT =      -5355
032833  meter/sec      RA   =          208
66215  deg
 ZDOT =       3192
284036                 TA   =          202
40050
                                          MA   =          202
48179
                                          Ha   =            193
257  n
mi
                                          Hp   =            180
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15878695
56                 X    =        -4833514
42
 Y    =        4619569
97  feet           Y    =         1353958
40  meter
 Z    =      -14653842
20                 Z    =        -4489987
52
 XDOT =     -14751
899210                 XDOT =       -4451
671245
 YDOT =     -17569
005357  feet/sec       YDOT =       -5405
063990  meter/sec
 ZDOT =      10473
372823                 ZDOT =        3170
549390

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1459566
19                 X    =          444875
77
 Y    =       16389820
87  feet           Y    =         4995617
40  meter
 Z    =      -14746251
36                 Z    =        -4494657
41
 XDOT =     -18919
099337                 XDOT =       -5766
541478
 YDOT =      11006
486878  feet/sec       YDOT =        3354
777200  meter/sec
 ZDOT =      10387
464079                 ZDOT =        3166
099051


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   09257
24978855  
00020000  00000-0  20000-3 0  9033
2 25544  51
6386 209
6294 0009158  87
1965 273
0246 15
74099143 19986


Satellite: ISS
Catalog Number: 25544
Epoch time:      09257
24978855   =   yrday
fracday
Element set:     903
Inclination:       51
6386  deg
RA of node:       209
6294  deg
Eccentricity:     
0009158     
Arg of perigee:    87
1965  deg
Mean anomaly:     273
0246  deg
Mean motion:   15
74099143  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1998
Checksum:              341


Coasting Arc #5 (Orbit 2013)
---------------------------------------

Vector Time (GMT): 2009/258/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4269640
74                 A    =         6728305
18  meter
 Y    =        4345878
97  meter          E    =           
0013536
 Z    =       -2863704
58                 I    =           51
51294
 XDOT =      -5432
659055                 Wp   =          100
19780
 YDOT =       2018
760672  meter/sec      RA   =          203
56165  deg
 ZDOT =      -5058
798613                 TA   =          112
72222
                                          MA   =          112
57909
                                          Ha   =            193
272  n
mi
                                          Hp   =            180
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14008007
67                 X    =         4234638
28
 Y    =       14258133
12  feet           Y    =         4393428
80  meter
 Z    =       -9395356
22                 Z    =        -2843048
01
 XDOT =     -17823
684564                 XDOT =       -5430
254896
 YDOT =       6623
230552  feet/sec       YDOT =        1958
022753  meter/sec
 ZDOT =     -16597
108312                 ZDOT =       -5085
184474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16528684
67                 X    =         5037943
09
 Y    =      -11306995
58  feet           Y    =        -3446372
25  meter
 Z    =       -9313742
08                 Z    =        -2838828
59
 XDOT =       2545
156718                 XDOT =         775
763768
 YDOT =      17415
703041  feet/sec       YDOT =        5308
306287  meter/sec
 ZDOT =     -16700
862096                 ZDOT =       -5090
422767


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   09258
26555158  
00020000  00000-0  20000-3 0  9044
2 25544  51
6394 204
4114 0009219  91
0312 269
1907 15
74128462 20144


Satellite: ISS
Catalog Number: 25544
Epoch time:      09258
26555158   =   yrday
fracday
Element set:     904
Inclination:       51
6394  deg
RA of node:       204
4114  deg
Eccentricity:     
0009219     
Arg of perigee:    91
0312  deg
Mean anomaly:     269
1907  deg
Mean motion:   15
74128462  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2014
Checksum:              280


Coasting Arc #6 (Orbit 2029)
---------------------------------------

Vector Time (GMT): 2009/259/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4620037
91                 A    =         6723238
81  meter
 Y    =       -2133707
25  meter          E    =           
0017959
 Z    =        4379840
31                 I    =           51
52361
 XDOT =       5267
632839                 Wp   =           81
97784
 YDOT =       4538
873809  meter/sec      RA   =          198
36916  deg
 ZDOT =      -3331
264626                 TA   =           41
58769
                                          MA   =           41
45122
                                          Ha   =            193
066  n
mi
                                          Hp   =            180
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15157604
69                 X    =         4622277
72
 Y    =       -7000351
87  feet           Y    =        -2082030
46  meter
 Z    =       14369554
84                 Z    =         4402289
85
 XDOT =      17282
259972                 XDOT =        5232
669416
 YDOT =      14891
318272  feet/sec       YDOT =        4597
583875  meter/sec
 ZDOT =     -10929
345887                 ZDOT =       -3305
759896

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4487913
02                 X    =        -1367915
89
 Y    =      -16002263
16  feet           Y    =        -4877489
81  meter
 Z    =       14457808
37                 Z    =         4406739
99
 XDOT =      16317
163031                 XDOT =        4973
471292
 YDOT =     -14401
176993  feet/sec       YDOT =       -4389
478747  meter/sec
 ZDOT =     -10828
615909                 ZDOT =       -3300
562129


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   09259
28130176  
00020000  00000-0  20000-3 0  9057
2 25544  51
6386 199
1940 0009144  94
4188 265
8020 15
74164878 20305


Satellite: ISS
Catalog Number: 25544
Epoch time:      09259
28130176   =   yrday
fracday
Element set:     905
Inclination:       51
6386  deg
RA of node:       199
1940  deg
Eccentricity:     
0009144     
Arg of perigee:    94
4188  deg
Mean anomaly:     265
8020  deg
Mean motion:   15
74164878  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2030
Checksum:              304


Coasting Arc #7 (Orbit 2045)
---------------------------------------

Vector Time (GMT): 2009/260/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4884507
82                 A    =         6728104
88  meter
 Y    =       -3552743
10  meter          E    =           
0022519
 Z    =        2944380
03                 I    =           51
56842
 XDOT =       5118
038972                 Wp   =           88
85669
 YDOT =      -2867
471149  meter/sec      RA   =          193
27372  deg
 ZDOT =       4998
163961                 TA   =          305
15648
                                          MA   =          305
36725
                                          Ha   =            193
330  n
mi
                                          Hp   =            180
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16025288
13                 X    =        -4858720
60
 Y    =      -11655981
30  feet           Y    =        -3607220
10  meter
 Z    =        9660039
46                 Z    =         2920714
16
 XDOT =      16791
466442                 XDOT =        5125
443086
 YDOT =      -9407
713744  feet/sec       YDOT =       -2810
196383  meter/sec
 ZDOT =      16398
175724                 ZDOT =        5023
045505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13844761
31                 X    =        -4219883
25
 Y    =       14240462
01  feet           Y    =         4340492
82  meter
 Z    =        9566605
90                 Z    =         2915901
48
 XDOT =      -5873
480251                 XDOT =       -1790
236781
 YDOT =     -16864
074319  feet/sec       YDOT =       -5140
169852  meter/sec
 ZDOT =      16495
960149                 ZDOT =        5027
968653


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   09260
29704282  
00020000  00000-0  20000-3 0  9066
2 25544  51
6388 193
9762 0009336  97
7521 262
4703 15
74134348 20468


Satellite: ISS
Catalog Number: 25544
Epoch time:      09260
29704282   =   yrday
fracday
Element set:     906
Inclination:       51
6388  deg
RA of node:       193
9762  deg
Eccentricity:     
0009336     
Arg of perigee:    97
7521  deg
Mean anomaly:     262
4703  deg
Mean motion:   15
74134348  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2046
Checksum:              306


Coasting Arc #8 (Orbit 2060)
---------------------------------------

Vector Time (GMT): 2009/261/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4300702
48                 A    =         6723517
73  meter
 Y    =        2854450
18  meter          E    =           
0018075
 Z    =       -4326293
45                 I    =           51
58441
 XDOT =      -5851
537306                 Wp   =          106
40440
 YDOT =      -3595
708973  meter/sec      RA   =          188
08435  deg
 ZDOT =       3451
391877                 TA   =          198
52791
                                          MA   =          198
59381
                                          Ha   =            193
151  n
mi
                                          Hp   =            180
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14109916
28                 X    =        -4311285
44
 Y    =        9364994
04  feet           Y    =         2806297
58  meter
 Z    =      -14193876
16                 Z    =        -4347212
27
 XDOT =     -19197
957041                 XDOT =       -5827
660814
 YDOT =     -11796
945448  feet/sec       YDOT =       -3661
010456  meter/sec
 ZDOT =      11323
464163                 ZDOT =        3423
023462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7513815
12                 X    =         2290210
85
 Y    =       15099525
52  feet           Y    =         4602335
38  meter
 Z    =      -14276059
78                 Z    =        -4351343
02
 XDOT =     -13039
329119                 XDOT =       -3974
387516
 YDOT =      17067
461496  feet/sec       YDOT =        5202
162264  meter/sec
 ZDOT =      11211
501609                 ZDOT =        3417
265690


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   09261
24928635  
00020000  00000-0  20000-3 0  9073
2 25544  51
6403 189
0849 0009153 101
3790 258
8402 15
74158214 20615


Satellite: ISS
Catalog Number: 25544
Epoch time:      09261
24928635   =   yrday
fracday
Element set:     907
Inclination:       51
6403  deg
RA of node:       189
0849  deg
Eccentricity:     
0009153     
Arg of perigee:   101
3790  deg
Mean anomaly:     258
8402  deg
Mean motion:   15
74158214  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2061
Checksum:              290


Coasting Arc #9 (Orbit 2076)
---------------------------------------

Vector Time (GMT): 2009/262/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5304691
42                 A    =         6727533
73  meter
 Y    =        2740665
88  meter          E    =           
0013683
 Z    =       -3106606
65                 I    =           51
62700
 XDOT =      -4717
216789                 Wp   =          106
03121
 YDOT =       3622
857881  meter/sec      RA   =          182
99369  deg
 ZDOT =      -4880
223821                 TA   =          110
03602
                                          MA   =          109
88866
                                          Ha   =            193
139  n
mi
                                          Hp   =            180
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17403843
25                 X    =         5288742
00
 Y    =        8991685
95  feet           Y    =         2799896
56  meter
 Z    =      -10192279
03                 Z    =        -3080875
31
 XDOT =     -15476
433034                 XDOT =       -4733
670212
 YDOT =      11886
016671  feet/sec       YDOT =        3570
014692  meter/sec
 ZDOT =     -16011
233008                 ZDOT =       -4903
180542

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10849747
38                 X    =         3307003
00
 Y    =      -16373343
33  feet           Y    =        -4990595
05  meter
 Z    =      -10090755
07                 Z    =        -3075662
14
 XDOT =       8935
827864                 XDOT =        2723
640333
 YDOT =      15800
671821  feet/sec       YDOT =        4816
044771  meter/sec
 ZDOT =     -16101
393535                 ZDOT =       -4907
704749


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   09262
26500200  
00020000  00000-0  20000-3 0  9081
2 25544  51
6396 183
8668 0009164 105
6789 254
5385 15
74185605 20778


Satellite: ISS
Catalog Number: 25544
Epoch time:      09262
26500200   =   yrday
fracday
Element set:     908
Inclination:       51
6396  deg
RA of node:       183
8668  deg
Eccentricity:     
0009164     
Arg of perigee:   105
6789  deg
Mean anomaly:     254
5385  deg
Mean motion:   15
74185605  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2077
Checksum:              311


Coasting Arc #10 (Orbit 2092)
---------------------------------------

Vector Time (GMT): 2009/263/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3904826
34                 A    =         6723707
32  meter
 Y    =       -3481793
39  meter          E    =           
0018203
 Z    =        4207782
69                 I    =           51
64377
 XDOT =       6273
100111                 Wp   =           90
40731
 YDOT =       2633
605047  meter/sec      RA   =          177
80692  deg
 ZDOT =      -3628
913248                 TA   =           36
53607
                                          MA   =           36
41202
                                          Ha   =            192
921  n
mi
                                          Hp   =            180
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12811110
04                 X    =         3923029
25
 Y    =      -11423206
67  feet           Y    =        -3438025
16  meter
 Z    =       13805061
32                 Z    =         4226797
09
 XDOT =      20581
037110                 XDOT =        6260
813264
 YDOT =       8640
436507  feet/sec       YDOT =        2703
685515  meter/sec
 ZDOT =     -11905
883361                 ZDOT =       -3598
468260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10197955
42                 X    =        -3108336
81
 Y    =      -13731322
68  feet           Y    =        -4185307
15  meter
 Z    =       13879711
51                 Z    =         4230536
07
 XDOT =       9509
883415                 XDOT =        2898
612465
 YDOT =     -19019
859978  feet/sec       YDOT =       -5797
253321  meter/sec
 ZDOT =     -11785
798143                 ZDOT =       -3592
311274


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   09263
28070480  
00020000  00000-0  20000-3 0  9097
2 25544  51
6386 178
6490 0009107 108
8110 251
4042 15
74233322 20936


Satellite: ISS
Catalog Number: 25544
Epoch time:      09263
28070480   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:       178
6490  deg
Eccentricity:     
0009107     
Arg of perigee:   108
8110  deg
Mean anomaly:     251
4042  deg
Mean motion:   15
74233322  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2093
Checksum:              275


Coasting Arc #11 (Orbit 2108)
---------------------------------------

Vector Time (GMT): 2009/264/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5599617
09                 A    =         6727092
67  meter
 Y    =       -1850852
05  meter          E    =           
0021440
 Z    =        3221076
49                 I    =           51
68410
 XDOT =       4202
549511                 Wp   =           97
72759
 YDOT =      -4344
331321  meter/sec      RA   =          172
72217  deg
 ZDOT =       4779
718440                 TA   =          299
92896
                                          MA   =          300
14172
                                          Ha   =            193
014  n
mi
                                          Hp   =            180
333

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18371447
13                 X    =        -5594152
00
 Y    =       -6072349
26  feet           Y    =        -1913439
48  meter
 Z    =       10567836
24                 Z    =         3193886
55
 XDOT =      13787
892095                 XDOT =        4227
596872
 YDOT =     -14253
055515  feet/sec       YDOT =       -4297
195540  meter/sec
 ZDOT =      15681
490946                 ZDOT =        4800
195888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7442030
13                 X    =        -2268330
78
 Y    =       17923568
29  feet           Y    =         5463103
62  meter
 Z    =       10460618
79                 Z    =         3188396
61
 XDOT =     -11874
751097                 XDOT =       -3619
424134
 YDOT =     -14187
217924  feet/sec       YDOT =       -4324
264023  meter/sec
 ZDOT =      15761
853671                 ZDOT =        4804
212999


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   09264
29639612  
00020000  00000-0  20000-3 0  9109
2 25544  51
6380 173
4317 0009045 112
8601 247
3518 15
74235270 21096


Satellite: ISS
Catalog Number: 25544
Epoch time:      09264
29639612   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:       173
4317  deg
Eccentricity:     
0009045     
Arg of perigee:   112
8601  deg
Mean anomaly:     247
3518  deg
Mean motion:   15
74235270  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2109
Checksum:              277


Coasting Arc #12 (Orbit 2123)
---------------------------------------

Vector Time (GMT): 2009/265/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3423605
43                 A    =         6724121
72  meter
 Y    =        4085680
10  meter          E    =           
0016768
 Z    =       -4116578
94                 I    =           51
70357
 XDOT =      -6488
624509                 Wp   =          113
41651
 YDOT =      -1627
985368  meter/sec      RA   =          167
53841  deg
 ZDOT =       3786
202015                 TA   =          195
43162
                                          MA   =          195
48281
                                          Ha   =            192
910  n
mi
                                          Hp   =            180
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11232301
28                 X    =        -3449039
85
 Y    =       13404462
26  feet           Y    =         4047252
90  meter
 Z    =      -13505836
42                 Z    =        -4133273
08
 XDOT =     -21288
138152                 XDOT =       -6488
330819
 YDOT =      -5341
159344  feet/sec       YDOT =       -1700
543143  meter/sec
 ZDOT =      12421
922623                 ZDOT =        3754
680583

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12733757
53                 X    =         3881249
30
 Y    =       11913117
70  feet           Y    =         3631118
27  meter
 Z    =      -13571325
06                 Z    =        -4136539
88
 XDOT =      -5703
958713                 XDOT =       -1738
566616
 YDOT =      20085
355696  feet/sec       YDOT =        6122
016416  meter/sec
 ZDOT =      12297
651171                 ZDOT =        3748
324077


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   09265
24859515  
00020000  00000-0  20000-3 0  9112
2 25544  51
6377 168
5399 0008989 115
8766 244
3325 15
74222925 21241


Satellite: ISS
Catalog Number: 25544
Epoch time:      09265
24859515   =   yrday
fracday
Element set:     911
Inclination:       51
6377  deg
RA of node:       168
5399  deg
Eccentricity:     
0008989     
Arg of perigee:   115
8766  deg
Mean anomaly:     244
3325  deg
Mean motion:   15
74222925  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2124
Checksum:              325


Coasting Arc #13 (Orbit 2139)
---------------------------------------

Vector Time (GMT): 2009/266/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5710395
87                 A    =         6726492
92  meter
 Y    =        1017201
24  meter          E    =           
0013463
 Z    =       -3412410
04                 I    =           51
73939
 XDOT =      -3632
998089                 Wp   =          109
91270
 YDOT =       4967
919720  meter/sec      RA   =          162
45674  deg
 ZDOT =      -4617
817955                 TA   =          110
31194
                                          MA   =          110
16722
                                          Ha   =            192
891  n
mi
                                          Hp   =            180
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18734894
59                 X    =         5715174
05
 Y    =        3337274
39  feet           Y    =         1081084
84  meter
 Z    =      -11195571
01                 Z    =        -3384656
96
 XDOT =     -11919
285070                 XDOT =       -3665
847356
 YDOT =      16298
949213  feet/sec       YDOT =        4927
109569  meter/sec
 ZDOT =     -15150
321376                 ZDOT =       -4635
547280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4103314
45                 X    =         1250690
24
 Y    =      -18647628
23  feet           Y    =        -5683797
08  meter
 Z    =      -11086174
17                 Z    =        -3379065
89
 XDOT =      14441
314462                 XDOT =        4401
712648
 YDOT =      12188
308912  feet/sec       YDOT =        3714
996557  meter/sec
 ZDOT =     -15219
841547                 ZDOT =       -4639
007704


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   09266
26426217  
00020000  00000-0  20000-3 0  9125
2 25544  51
6366 163
3207 0009016 119
8689 240
3372 15
74252297 21401


Satellite: ISS
Catalog Number: 25544
Epoch time:      09266
26426217   =   yrday
fracday
Element set:     912
Inclination:       51
6366  deg
RA of node:       163
3207  deg
Eccentricity:     
0009016     
Arg of perigee:   119
8689  deg
Mean anomaly:     240
3372  deg
Mean motion:   15
74252297  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2140
Checksum:              288


Coasting Arc #14 (Orbit 2155)
---------------------------------------

Vector Time (GMT): 2009/267/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2886441
02                 A    =         6724447
25  meter
 Y    =       -4590921
86  meter          E    =           
0018262
 Z    =        3958660
96                 I    =           51
76086
 XDOT =       6560
405668                 Wp   =           98
73300
 YDOT =        667
199388  meter/sec      RA   =          157
27590  deg
 ZDOT =      -3996
876032                 TA   =           32
61829
                                          MA   =           32
50561
                                          Ha   =            192
625  n
mi
                                          Hp   =            180
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9469950
85                 X    =         2918332
28
 Y    =      -15062079
59  feet           Y    =        -4558465
58  meter
 Z    =       12987732
82                 Z    =         3972761
02
 XDOT =      21523
640642                 XDOT =        6571
873680
 YDOT =       2188
974371  feet/sec       YDOT =         740
625744  meter/sec
 ZDOT =     -13113
110341                 ZDOT =       -3964
977352

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14834875
76                 X    =        -4521670
13
 Y    =       -9748551
87  feet           Y    =        -2971358
61  meter
 Z    =       13042990
92                 Z    =         3975503
63
 XDOT =       1989
448890                 XDOT =         606
384022
 YDOT =     -20460
003416  feet/sec       YDOT =       -6236
209041  meter/sec
 ZDOT =     -12987
392179                 ZDOT =       -3958
557136


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   09267
27991552  
00020000  00000-0  20000-3 0  9137
2 25544  51
6361 158
1025 0008793 123
4473 236
7532 15
74294614 21562


Satellite: ISS
Catalog Number: 25544
Epoch time:      09267
27991552   =   yrday
fracday
Element set:     913
Inclination:       51
6361  deg
RA of node:       158
1025  deg
Eccentricity:     
0008793     
Arg of perigee:   123
4473  deg
Mean anomaly:     236
7532  deg
Mean motion:   15
74294614  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2156
Checksum:              301


Coasting Arc #15 (Orbit 2171)
---------------------------------------

Vector Time (GMT): 2009/268/05:44:50
891
Vector Time (MET): N/A
Weight (LBS)     : 711041
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5699501
63                 A    =         6725820
60  meter
 Y    =        -159963
93  meter          E    =           
0020035
 Z    =        3556813
58                 I    =           51
79278
 XDOT =       2959
837511                 Wp   =          107
70485
 YDOT =      -5535
795697  meter/sec      RA   =          152
20012  deg
 ZDOT =       4467
442202                 TA   =          294
63799
                                          MA   =          294
84654
                                          Ha   =            192
617  n
mi
                                          Hp   =            180
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18699152
33                 X    =        -5714567
80
 Y    =        -524816
04  feet           Y    =         -223783
30  meter
 Z    =       11669335
90                 Z    =         3529088
56
 XDOT =       9710
752989                 XDOT =        2999
817529
 YDOT =     -18162
059372  feet/sec       YDOT =       -5502
473448  meter/sec
 ZDOT =      14656
962606                 ZDOT =        4481
918413

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -646828
56                 X    =         -197153
35
 Y    =       18763082
23  feet           Y    =         5718987
46  meter
 Z    =       11560081
68                 Z    =         3523512
89
 XDOT =     -16730
523627                 XDOT =       -5099
463602
 YDOT =      -9696
002939  feet/sec       YDOT =       -2955
341696  meter/sec
 ZDOT =      14713
653014                 ZDOT =        4484
721439


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   09268
29555605  
00020000  00000-0  20000-3 0  9146
2 25544  51
6362 152
8847 0008770 128
3127 231
8826 15
74337775 21727


Satellite: ISS
Catalog Number: 25544
Epoch time:      09268
29555605   =   yrday
fracday
Element set:     914
Inclination:       51
6362  deg
RA of node:       152
8847  deg
Eccentricity:     
0008770     
Arg of perigee:   128
3127  deg
Mean anomaly:     231
8826  deg
Mean motion:   15
74337775  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2172
Checksum:              315

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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