Date: November 5th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 18535 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 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 2626)
---------------------------------------

Vector Time (GMT): 2009/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         150205
87                 A    =         6716960
71  meter
 Y    =       -4560681
41  meter          E    =           
0006862
 Z    =       -4935191
49                 I    =           51
46915
 XDOT =       7133
881231                 Wp   =          120
53489
 YDOT =      -2013
996978  meter/sec      RA   =          331
34239  deg
 ZDOT =       2076
994299                 TA   =          169
64760
                                          MA   =          169
63346
                                          Ha   =            185
301  n
mi
                                          Hp   =            183
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         492801
43                 X    =          225167
94
 Y    =      -14962865
53  feet           Y    =        -4558582
84  meter
 Z    =      -16191573
12                 Z    =        -4934279
45
 XDOT =      23405
122150                 XDOT =        7145
781958
 YDOT =      -6607
601635  feet/sec       YDOT =       -1934
155066  meter/sec
 ZDOT =       6814
285757                 ZDOT =        2111
680602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8785009
74                 X    =         2677670
97
 Y    =       12127040
10  feet           Y    =         3696321
82  meter
 Z    =      -16188135
80                 Z    =        -4934143
79
 XDOT =     -13402
013626                 XDOT =       -4084
933753
 YDOT =      18993
011194  feet/sec       YDOT =        5789
069812  meter/sec
 ZDOT =       6950
983314                 ZDOT =        2118
659714


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   09303
51224173  
00016717  00000-0  10270-3 0  9007
2 25544  51
6446 331
8295 0006365 269
1559  90
8876 15
75622694 26278


Satellite: ISS
Catalog Number: 25544
Epoch time:      09303
51224173   =   yrday
fracday
Element set:     900
Inclination:       51
6446  deg
RA of node:       331
8295  deg
Eccentricity:     
0006365     
Arg of perigee:   269
1559  deg
Mean anomaly:      90
8876  deg
Mean motion:   15
75622694  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2627
Checksum:              329


Coasting Arc #2 (Orbit 2642)
---------------------------------------

Vector Time (GMT): 2009/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6039513
98                 A    =         6724928
00  meter
 Y    =        1797127
50  meter          E    =           
0004221
 Z    =       -2341201
22                 I    =           51
47038
 XDOT =        461
799751                 Wp   =          211
15843
 YDOT =      -5477
428388  meter/sec      RA   =          326
22016  deg
 ZDOT =      -5395
044758                 TA   =          355
27856
                                          MA   =          355
28254
                                          Ha   =            185
252  n
mi
                                          Hp   =            183
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19814678
41                 X    =        -6047787
41
 Y    =        5896087
59  feet           Y    =         1729543
73  meter
 Z    =       -7681106
36                 Z    =        -2370562
24
 XDOT =       1515
091045                 XDOT =         549
223943
 YDOT =     -17970
565578  feet/sec       YDOT =       -5471
775682  meter/sec
 ZDOT =     -17700
278078                 ZDOT =       -5392
588678

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11607647
34                 X    =         3538010
91
 Y    =      -17054530
48  feet           Y    =        -5198220
89  meter
 Z    =       -7796809
42                 Z    =        -2376467
51
 XDOT =       8848
203139                 XDOT =        2696
932317
 YDOT =      14111
080251  feet/sec       YDOT =        4301
057261  meter/sec
 ZDOT =     -17690
784402                 ZDOT =       -5392
151086


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   09304
52700113  
00016717  00000-0  10270-3 0  9013
2 25544  51
6440 326
6057 0006264 272
8450  87
1997 15
75683339 26433


Satellite: ISS
Catalog Number: 25544
Epoch time:      09304
52700113   =   yrday
fracday
Element set:     901
Inclination:       51
6440  deg
RA of node:       326
6057  deg
Eccentricity:     
0006264     
Arg of perigee:   272
8450  deg
Mean anomaly:      87
1997  deg
Mean motion:   15
75683339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2643
Checksum:              310


Coasting Arc #3 (Orbit 2658)
---------------------------------------

Vector Time (GMT): 2009/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -619984
14                 A    =         6718718
03  meter
 Y    =        5029124
52  meter          E    =           
0004842
 Z    =        4412051
21                 I    =           51
42439
 XDOT =      -6668
756329                 Wp   =           30
87286
 YDOT =       2047
348574  meter/sec      RA   =          321
01296  deg
 ZDOT =      -3265
114664                 TA   =           91
99116
                                          MA   =           91
93571
                                          Ha   =            185
335  n
mi
                                          Hp   =            183
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2034068
71                 X    =         -697608
30
 Y    =       16499752
35  feet           Y    =         5021757
57  meter
 Z    =       14475233
64                 Z    =         4408850
56
 XDOT =     -21879
121814                 XDOT =       -6675
292608
 YDOT =       6717
022881  feet/sec       YDOT =        1972
737989  meter/sec
 ZDOT =     -10712
318452                 ZDOT =       -3297
528521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9017098
41                 X    =        -2748411
60
 Y    =      -13979676
96  feet           Y    =        -4261005
54  meter
 Z    =       14462787
43                 Z    =         4408257
61
 XDOT =      11328
644929                 XDOT =        3452
970974
 YDOT =     -18541
081646  feet/sec       YDOT =       -5651
321686  meter/sec
 ZDOT =     -10840
046402                 ZDOT =       -3304
046143


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   09305
54173028  
00016717  00000-0  10270-3 0  9026
2 25544  51
6427 321
3813 0006213 277
7881  82
2578 15
75754603 26597


Satellite: ISS
Catalog Number: 25544
Epoch time:      09305
54173028   =   yrday
fracday
Element set:     902
Inclination:       51
6427  deg
RA of node:       321
3813  deg
Eccentricity:     
0006213     
Arg of perigee:   277
7881  deg
Mean anomaly:      82
2578  deg
Mean motion:   15
75754603  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2659
Checksum:              317


Coasting Arc #4 (Orbit 2674)
---------------------------------------

Vector Time (GMT): 2009/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5579566
14                 A    =         6722206
16  meter
 Y    =       -1705209
61  meter          E    =           
0006694
 Z    =        3331910
03                 I    =           51
41349
 XDOT =       -927
753988                 Wp   =           78
20107
 YDOT =       6069
785829  meter/sec      RA   =          315
89769  deg
 ZDOT =       4653
490515                 TA   =          321
17691
                                          MA   =          321
22498
                                          Ha   =            185
366  n
mi
                                          Hp   =            183
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18305663
19                 X    =         5582032
99
 Y    =       -5594519
73  feet           Y    =        -1642801
84  meter
 Z    =       10931463
37                 Z    =         3359022
54
 XDOT =      -3043
812297                 XDOT =       -1018
165079
 YDOT =      19913
995503  feet/sec       YDOT =        6058
905600  meter/sec
 ZDOT =      15267
357333                 ZDOT =        4648
763734

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10061540
57                 X    =        -3066757
57
 Y    =       16211543
99  feet           Y    =         4941278
61  meter
 Z    =       11038301
04                 Z    =         3364474
16
 XDOT =      -9555
546016                 XDOT =       -2912
530426
 YDOT =     -16327
836898  feet/sec       YDOT =       -4976
724686  meter/sec
 ZDOT =      15248
926932                 ZDOT =        4647
872929


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   09306
55643084  
00016717  00000-0  10270-3 0  9033
2 25544  51
6422 316
1567 0006175 282
1509  77
8963 15
75771691 26756


Satellite: ISS
Catalog Number: 25544
Epoch time:      09306
55643084   =   yrday
fracday
Element set:     903
Inclination:       51
6422  deg
RA of node:       316
1567  deg
Eccentricity:     
0006175     
Arg of perigee:   282
1509  deg
Mean anomaly:      77
8963  deg
Mean motion:   15
75771691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2675
Checksum:              333


Coasting Arc #5 (Orbit 2689)
---------------------------------------

Vector Time (GMT): 2009/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         953516
77                 A    =         6721267
32  meter
 Y    =       -5568643
33  meter          E    =           
0000873
 Z    =       -3639890
16                 I    =           51
39022
 XDOT =       6106
613377                 Wp   =          330
05854
 YDOT =      -1789
815787  meter/sec      RA   =          310
67982  deg
 ZDOT =       4338
232955                 TA   =          346
06586
                                          MA   =          346
06827
                                          Ha   =            185
635  n
mi
                                          Hp   =            183
272

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3128335
86                 X    =         1033398
01
 Y    =      -18269827
21  feet           Y    =        -5557533
78  meter
 Z    =      -11941896
87                 Z    =        -3635063
97
 XDOT =      20034
820792                 XDOT =        6105
098430
 YDOT =      -5872
099039  feet/sec       YDOT =       -1721
536656  meter/sec
 ZDOT =      14233
047754                 ZDOT =        4367
896218

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9878747
48                 X    =         3011042
23
 Y    =       15698187
62  feet           Y    =         4784807
59  meter
 Z    =      -11923054
39                 Z    =        -3634146
98
 XDOT =      -9718
826101                 XDOT =       -2962
298196
 YDOT =      17014
273496  feet/sec       YDOT =        5185
950562  meter/sec
 ZDOT =      14349
941571                 ZDOT =        4373
862191


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   09307
50768388  
00016717  00000-0  10270-3 0  9045
2 25544  51
6427 311
2589 0006199 286
2672  73
7810 15
75811439 26901


Satellite: ISS
Catalog Number: 25544
Epoch time:      09307
50768388   =   yrday
fracday
Element set:     904
Inclination:       51
6427  deg
RA of node:       311
2589  deg
Eccentricity:     
0006199     
Arg of perigee:   286
2672  deg
Mean anomaly:      73
7810  deg
Mean motion:   15
75811439  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2690
Checksum:              340


Coasting Arc #6 (Orbit 2705)
---------------------------------------

Vector Time (GMT): 2009/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5078641
05                 A    =         6719105
40  meter
 Y    =        1336240
98  meter          E    =           
0005386
 Z    =       -4196390
13                 I    =           51
36383
 XDOT =       1229
430429                 Wp   =           21
50704
 YDOT =      -6685
877838  meter/sec      RA   =          305
56196  deg
 ZDOT =      -3613
389207                 TA   =          211
54469
                                          MA   =          211
57699
                                          Ha   =            185
752  n
mi
                                          Hp   =            183
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16662208
16                 X    =        -5072819
68
 Y    =        4383992
70  feet           Y    =         1279481
42  meter
 Z    =      -13767684
14                 Z    =        -4221048
77
 XDOT =       4033
564399                 XDOT =        1321
655480
 YDOT =     -21935
294745  feet/sec       YDOT =       -6671
613748  meter/sec
 ZDOT =     -11854
951468                 ZDOT =       -3607
192814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9112906
71                 X    =         2777613
97
 Y    =      -14529904
98  feet           Y    =        -4428715
04  meter
 Z    =      -13864865
38                 Z    =        -4226010
97
 XDOT =      10931
487647                 XDOT =        3331
917435
 YDOT =      18156
091779  feet/sec       YDOT =        5533
976774  meter/sec
 ZDOT =     -11830
740669                 ZDOT =       -3606
009756


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   09308
52232505  
00016717  00000-0  10270-3 0  9056
2 25544  51
6416 306
0332 0006182 289
9277  70
1221 15
75861696 27065


Satellite: ISS
Catalog Number: 25544
Epoch time:      09308
52232505   =   yrday
fracday
Element set:     905
Inclination:       51
6416  deg
RA of node:       306
0332  deg
Eccentricity:     
0006182     
Arg of perigee:   289
9277  deg
Mean anomaly:      70
1221  deg
Mean motion:   15
75861696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2706
Checksum:              305


Coasting Arc #7 (Orbit 2721)
---------------------------------------

Vector Time (GMT): 2009/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1146842
09                 A    =         6723705
01  meter
 Y    =        6086823
98  meter          E    =           
0007727
 Z    =        2608801
40                 I    =           51
36336
 XDOT =      -5536
429170                 Wp   =           92
82172
 YDOT =       1199
401550  meter/sec      RA   =          300
34439  deg
 ZDOT =      -5219
361179                 TA   =           57
38120
                                          MA   =           57
30664
                                          Ha   =            185
894  n
mi
                                          Hp   =            182
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3762605
29                 X    =        -1227494
23
 Y    =       19969894
94  feet           Y    =         6073548
16  meter
 Z    =        8559059
71                 Z    =         2603034
44
 XDOT =     -18164
137697                 XDOT =       -5524
074168
 YDOT =       3935
044457  feet/sec       YDOT =        1137
559418  meter/sec
 ZDOT =     -17123
888383                 ZDOT =       -5246
227817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11154115
53                 X    =        -3399774
41
 Y    =      -16997791
63  feet           Y    =        -5180926
89  meter
 Z    =        8536521
08                 Z    =         2601931
62
 XDOT =       8999
304769                 XDOT =        2742
988094
 YDOT =     -14579
790274  feet/sec       YDOT =       -4443
920075  meter/sec
 ZDOT =     -17229
785865                 ZDOT =       -5251
638732


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   09309
53693468  
00016717  00000-0  10270-3 0  9068
2 25544  51
6414 300
8079 0006292 295
0611  64
9900 15
75942438 27222


Satellite: ISS
Catalog Number: 25544
Epoch time:      09309
53693468   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       300
8079  deg
Eccentricity:     
0006292     
Arg of perigee:   295
0611  deg
Mean anomaly:      64
9900  deg
Mean motion:   15
75942438  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2722
Checksum:              324


Coasting Arc #8 (Orbit 2737)
---------------------------------------

Vector Time (GMT): 2009/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4604888
83                 A    =         6716262
32  meter
 Y    =        -682833
84  meter          E    =           
0000582
 Z    =        4841275
62                 I    =           51
32402
 XDOT =      -1357
645728                 Wp   =          168
77424
 YDOT =       7222
898172  meter/sec      RA   =          295
21400  deg
 ZDOT =       2309
493851                 TA   =          258
64052
                                          MA   =          258
64706
                                          Ha   =            185
887  n
mi
                                          Hp   =            182
865

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15107902
99                 X    =         4588663
57
 Y    =       -2240268
49  feet           Y    =         -631430
37  meter
 Z    =       15883450
21                 Z    =         4863607
22
 XDOT =      -4454
218268                 XDOT =       -1449
531887
 YDOT =      23697
172480  feet/sec       YDOT =        7207
202228  meter/sec
 ZDOT =       7577
079563                 ZDOT =        2302
675646

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9018888
47                 X    =        -2748957
20
 Y    =       12211581
88  feet           Y    =         3722090
16  meter
 Z    =       15971488
50                 Z    =         4868109
70
 XDOT =     -12708
619189                 XDOT =       -3873
587129
 YDOT =     -19263
766527  feet/sec       YDOT =       -5871
596037  meter/sec
 ZDOT =       7550
434815                 ZDOT =        2301
372532


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   09310
55151473  
00016717  00000-0  10270-3 0  9078
2 25544  51
6410 295
5827 0006300 298
3725  61
6804 15
75961486 27389


Satellite: ISS
Catalog Number: 25544
Epoch time:      09310
55151473   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       295
5827  deg
Eccentricity:     
0006300     
Arg of perigee:   298
3725  deg
Mean anomaly:      61
6804  deg
Mean motion:   15
75961486  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2738
Checksum:              321


Coasting Arc #9 (Orbit 2752)
---------------------------------------

Vector Time (GMT): 2009/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1184525
33                 A    =         6725600
00  meter
 Y    =       -6469036
22  meter          E    =           
0010221
 Z    =       -1375959
66                 I    =           51
34426
 XDOT =       5055
739932                 Wp   =             
68553
 YDOT =       -307
288369  meter/sec      RA   =          290
01022  deg
 ZDOT =       5807
572809                 TA   =          344
11145
                                          MA   =          344
14349
                                          Ha   =            186
042  n
mi
                                          Hp   =            182
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3886237
96                 X    =         1263459
46
 Y    =      -21223872
11  feet           Y    =        -6455348
71  meter
 Z    =       -4514303
33                 Z    =        -1370013
86
 XDOT =      16587
073269                 XDOT =        5030
587695
 YDOT =      -1008
163940  feet/sec       YDOT =        -250
893158  meter/sec
 ZDOT =      19053
716565                 ZDOT =        5832
072908

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12565573
59                 X    =         3829986
83
 Y    =       17546256
16  feet           Y    =         5348098
88  meter
 Z    =       -4491078
09                 Z    =        -1368880
60
 XDOT =      -9428
802383                 XDOT =       -2873
898966
 YDOT =      11645
111828  feet/sec       YDOT =        3549
430085  meter/sec
 ZDOT =      19150
324951                 ZDOT =        5837
019045


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   09311
50265426  
00016717  00000-0  10270-3 0  9089
2 25544  51
6408 290
6843 0006084 302
2682  57
7892 15
76025384 27535


Satellite: ISS
Catalog Number: 25544
Epoch time:      09311
50265426   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:       290
6843  deg
Eccentricity:     
0006084     
Arg of perigee:   302
2682  deg
Mean anomaly:      57
7892  deg
Mean motion:   15
76025384  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2753
Checksum:              318


Coasting Arc #10 (Orbit 2768)
---------------------------------------

Vector Time (GMT): 2009/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4254248
59                 A    =         6714466
26  meter
 Y    =        -209796
82  meter          E    =           
0011001
 Z    =       -5199425
86                 I    =           51
29793
 XDOT =       1343
488911                 Wp   =           61
37882
 YDOT =      -7537
355742  meter/sec      RA   =          284
85592  deg
 ZDOT =       -791
198727                 TA   =          201
02964
                                          MA   =          201
07491
                                          Ha   =            186
181  n
mi
                                          Hp   =            182
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13957508
49                 X    =        -4226328
19
 Y    =        -688309
77  feet           Y    =         -257213
95  meter
 Z    =      -17058483
78                 Z    =        -5220025
48
 XDOT =       4407
772018                 XDOT =        1431
516638
 YDOT =     -24728
857420  feet/sec       YDOT =       -7521
839826  meter/sec
 ZDOT =      -2595
796349                 ZDOT =        -784
458540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9948012
46                 X    =         3032154
20
 Y    =       -9671828
87  feet           Y    =        -2947973
44  meter
 Z    =      -17139733
28                 Z    =        -5224190
70
 XDOT =      14377
430132                 XDOT =        4382
240704
 YDOT =      19364
193349  feet/sec       YDOT =        5902
206133  meter/sec
 ZDOT =      -2569
483334                 ZDOT =        -783
178520


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   09312
51717276  
00016717  00000-0  10270-3 0  9097
2 25544  51
6409 285
4581 0006217 306
4747  53
5844 15
76049882 27690


Satellite: ISS
Catalog Number: 25544
Epoch time:      09312
51717276   =   yrday
fracday
Element set:     909
Inclination:       51
6409  deg
RA of node:       285
4581  deg
Eccentricity:     
0006217     
Arg of perigee:   306
4747  deg
Mean anomaly:      53
5844  deg
Mean motion:   15
76049882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2769
Checksum:              341


Coasting Arc #11 (Orbit 2784)
---------------------------------------

Vector Time (GMT): 2009/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1150019
59                 A    =         6726151
45  meter
 Y    =        6623994
45  meter          E    =           
0005927
 Z    =         -25565
59                 I    =           51
33171
 XDOT =      -4737
747970                 Wp   =          139
50073
 YDOT =       -842
723964  meter/sec      RA   =          279
67483  deg
 ZDOT =      -6013
162076                 TA   =           40
77832
                                          MA   =           40
73398
                                          Ha   =            186
324  n
mi
                                          Hp   =            182
168

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3773030
14                 X    =        -1223880
58
 Y    =       21732265
26  feet           Y    =         6610721
28  meter
 Z    =         -83876
60                 Z    =          -31331
68
 XDOT =     -15543
792551                 XDOT =       -4698
761123
 YDOT =      -2764
842402  feet/sec       YDOT =        -895
486100  meter/sec
 ZDOT =     -19728
222033                 ZDOT =       -6036
083681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13633250
45                 X    =        -4155414
74
 Y    =      -17339472
67  feet           Y    =        -5285071
27  meter
 Z    =        -106371
83                 Z    =          -32422
13
 XDOT =      11110
026325                 XDOT =        3386
336024
 YDOT =      -8626
171801  feet/sec       YDOT =       -2629
257165  meter/sec
 ZDOT =     -19818
657060                 ZDOT =       -6040
726672


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   09313
53165875  
00016717  00000-0  10270-3 0  9104
2 25544  51
6411 280
2323 0006323 310
8391  49
2225 15
76118517 27857


Satellite: ISS
Catalog Number: 25544
Epoch time:      09313
53165875   =   yrday
fracday
Element set:     910
Inclination:       51
6411  deg
RA of node:       280
2323  deg
Eccentricity:     
0006323     
Arg of perigee:   310
8391  deg
Mean anomaly:      49
2225  deg
Mean motion:   15
76118517  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2785
Checksum:              295


Coasting Arc #12 (Orbit 2800)
---------------------------------------

Vector Time (GMT): 2009/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4068287
23                 A    =         6714222
26  meter
 Y    =        1287414
25  meter          E    =           
0006322
 Z    =        5186050
99                 I    =           51
28782
 XDOT =      -1284
316092                 Wp   =          344
71675
 YDOT =       7546
356876  meter/sec      RA   =          274
49200  deg
 ZDOT =       -860
062868                 TA   =          113
54314
                                          MA   =          113
47671
                                          Ha   =            186
318  n
mi
                                          Hp   =            181
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13347399
04                 X    =         4028395
50
 Y    =        4223800
02  feet           Y    =         1332685
16  meter
 Z    =       17014602
98                 Z    =         5205718
13
 XDOT =      -4213
635471                 XDOT =       -1364
427224
 YDOT =      24758
388700  feet/sec       YDOT =        7531
546976  meter/sec
 ZDOT =      -2821
728569                 ZDOT =        -866
496715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11878077
97                 X    =        -3620438
16
 Y    =        7228930
48  feet           Y    =         2203378
01  meter
 Z    =       17092223
09                 Z    =         5209709
60
 XDOT =     -15407
986310                 XDOT =       -4696
354227
 YDOT =     -18541
619579  feet/sec       YDOT =       -5651
485648  meter/sec
 ZDOT =      -2846
813214                 ZDOT =        -867
708668


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   09314
54611323  
00016717  00000-0  10270-3 0  9111
2 25544  51
6410 275
0065 0006305 314
2377  45
8269 15
76150984 28016


Satellite: ISS
Catalog Number: 25544
Epoch time:      09314
54611323   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:       275
0065  deg
Eccentricity:     
0006305     
Arg of perigee:   314
2377  deg
Mean anomaly:      45
8269  deg
Mean motion:   15
76150984  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2801
Checksum:              291


Coasting Arc #13 (Orbit 2816)
---------------------------------------

Vector Time (GMT): 2009/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1103720
84                 A    =         6724893
34  meter
 Y    =       -6459154
68  meter          E    =           
0013889
 Z    =        1472056
60                 I    =           51
32345
 XDOT =       4647
867809                 Wp   =           35
80952
 YDOT =       2114
158238  meter/sec      RA   =          269
33733  deg
 ZDOT =       5775
422374                 TA   =          340
49591
                                          MA   =          340
54900
                                          Ha   =            186
334  n
mi
                                          Hp   =            181
736

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3621131
36                 X    =         1168715
08
 Y    =      -21191452
37  feet           Y    =        -6446448
81  meter
 Z    =        4829582
03                 Z    =         1477576
50
 XDOT =      15248
910135                 XDOT =        4595
824997
 YDOT =       6936
214692  feet/sec       YDOT =        2165
842491  meter/sec
 ZDOT =      18948
236134                 ZDOT =        5797
875708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13922759
51                 X    =         4243657
10
 Y    =       16374942
30  feet           Y    =         4991082
41  meter
 Z    =        4851096
88                 Z    =         1478614
33
 XDOT =     -13850
712496                 XDOT =       -4221
697169
 YDOT =       6121
077272  feet/sec       YDOT =        1865
704353  meter/sec
 ZDOT =      19036
881433                 ZDOT =        5802
441461


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   09315
56053354  
00016717  00000-0  10270-3 0  9129
2 25544  51
6410 269
7800 0006232 317
2767  42
7912 15
76229184 28175


Satellite: ISS
Catalog Number: 25544
Epoch time:      09315
56053354   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:       269
7800  deg
Eccentricity:     
0006232     
Arg of perigee:   317
2767  deg
Mean anomaly:      42
7912  deg
Mean motion:   15
76229184  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2817
Checksum:              308


Coasting Arc #14 (Orbit 2831)
---------------------------------------

Vector Time (GMT): 2009/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4086645
75                 A    =         6715770
54  meter
 Y    =       -2392442
25  meter          E    =           
0007357
 Z    =       -4767756
00                 I    =           51
29492
 XDOT =       1279
873036                 Wp   =           79
62922
 YDOT =      -7167
466144  meter/sec      RA   =          264
12690  deg
 ZDOT =       2504
153964                 TA   =          214
97755
                                          MA   =          215
02590
                                          Ha   =            186
451  n
mi
                                          Hp   =            181
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13407630
40                 X    =        -4036427
86
 Y    =       -7849219
99  feet           Y    =        -2437860
79  meter
 Z    =      -15642244
09                 Z    =        -4787487
39
 XDOT =       4199
058516                 XDOT =        1347
760753
 YDOT =     -23515
308872  feet/sec       YDOT =       -7152
774251  meter/sec
 ZDOT =       8215
728227                 ZDOT =        2510
536686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14482059
79                 X    =         4414131
82
 Y    =       -5403784
05  feet           Y    =        -1647073
38  meter
 Z    =      -15720167
61                 Z    =        -4791507
09
 XDOT =      15262
370267                 XDOT =        4651
970457
 YDOT =      16973
616836  feet/sec       YDOT =        5173
558411  meter/sec
 ZDOT =       8240
612988                 ZDOT =        2511
738839


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   09316
51152467  
00016717  00000-0  10270-3 0  9131
2 25544  51
6414 264
8800 0006353 321
3356  38
7353 15
76250847 28320


Satellite: ISS
Catalog Number: 25544
Epoch time:      09316
51152467   =   yrday
fracday
Element set:     913
Inclination:       51
6414  deg
RA of node:       264
8800  deg
Eccentricity:     
0006353     
Arg of perigee:   321
3356  deg
Mean anomaly:      38
7353  deg
Mean motion:   15
76250847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2832
Checksum:              305


Coasting Arc #15 (Orbit 2847)
---------------------------------------

Vector Time (GMT): 2009/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1183214
67                 A    =         6721969
46  meter
 Y    =        5963082
53  meter          E    =           
0003295
 Z    =       -2872937
70                 I    =           51
32154
 XDOT =      -4756
598558                 Wp   =            9
36776
 YDOT =      -3368
019397  meter/sec      RA   =          258
99391  deg
 ZDOT =      -5029
280845                 TA   =          203
81494
                                          MA   =          203
83019
                                          Ha   =            186
589  n
mi
                                          Hp   =            181
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3881937
88                 X    =        -1235850
35
 Y    =       19563919
05  feet           Y    =         5949556
83  meter
 Z    =       -9425648
62                 Z    =        -2878813
75
 XDOT =     -15605
638314                 XDOT =       -4694
151226
 YDOT =     -11049
932404  feet/sec       YDOT =       -3420
861303  meter/sec
 ZDOT =     -16500
265240                 ZDOT =       -5052
237379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13051636
25                 X    =        -3978138
73
 Y    =      -15067790
44  feet           Y    =        -4592662
53  meter
 Z    =       -9448582
15                 Z    =        -2879927
84
 XDOT =      17160
392365                 XDOT =        5230
487593
 YDOT =      -4455
600904  feet/sec       YDOT =       -1358
067156  meter/sec
 ZDOT =     -16590
952320                 ZDOT =       -5056
922267


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   09317
52588282  
00016717  00000-0  10270-3 0  9142
2 25544  51
6422 259
6530 0006367 325
4580  34
6170 15
76319021 28489


Satellite: ISS
Catalog Number: 25544
Epoch time:      09317
52588282   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       259
6530  deg
Eccentricity:     
0006367     
Arg of perigee:   325
4580  deg
Mean anomaly:      34
6170  deg
Mean motion:   15
76319021  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2848
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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