Date: August 29th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 1702)
---------------------------------------

Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4623547
47                 A    =         6722386
89  meter
 Y    =        -238127
63  meter          E    =           
0018721
 Z    =       -4890663
79                 I    =           51
35374
 XDOT =       2692
507802                 Wp   =           51
49947
 YDOT =      -6853
212484  meter/sec      RA   =          305
30972  deg
 ZDOT =      -2205
991063                 TA   =          196
91001
                                          MA   =          196
97249
                                          Ha   =            192
741  n
mi
                                          Hp   =            182
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15169119
01                 X    =        -4596783
11
 Y    =        -781258
62  feet           Y    =         -289681
14  meter
 Z    =      -16045484
86                 Z    =        -4913059
96
 XDOT =       8833
687015                 XDOT =        2779
657789
 YDOT =     -22484
292927  feet/sec       YDOT =       -6822
615970  meter/sec
 ZDOT =      -7237
503488                 ZDOT =       -2192
699271

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13220215
03                 X    =         4029521
54
 Y    =        7287229
25  feet           Y    =         2221147
48  meter
 Z    =      -16133577
58                 Z    =        -4917514
45
 XDOT =     -17273
123685                 XDOT =       -5264
848099
 YDOT =      15386
072821  feet/sec       YDOT =        4689
674996  meter/sec
 ZDOT =      -7185
549495                 ZDOT =       -2190
155486


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   09238
51965709  
00020000  00000-0  20000-3 0  9003
2 25544  51
6410 305
8016 0008541  18
2704 341
8765 15
73760201 17039


Satellite: ISS
Catalog Number: 25544
Epoch time:      09238
51965709   =   yrday
fracday
Element set:     900
Inclination:       51
6410  deg
RA of node:       305
8016  deg
Eccentricity:     
0008541     
Arg of perigee:    18
2704  deg
Mean anomaly:     341
8765  deg
Mean motion:   15
73760201  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1703
Checksum:              274


Coasting Arc #2 (Orbit 1718)
---------------------------------------

Vector Time (GMT): 2009/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1778607
04                 A    =         6731042
03  meter
 Y    =        6186498
77  meter          E    =           
0016587
 Z    =        1959433
51                 I    =           51
36761
 XDOT =      -5300
784085                 Wp   =           80
05616
 YDOT =        255
794445  meter/sec      RA   =          300
11999  deg
 ZDOT =      -5576
334283                 TA   =           78
05659
                                          MA   =           77
87068
                                          Ha   =            192
835  n
mi
                                          Hp   =            182
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5835324
92                 X    =        -1857171
89
 Y    =       20296911
97  feet           Y    =         6166170
01  meter
 Z    =        6428587
64                 Z    =         1950602
39
 XDOT =     -17391
023901                 XDOT =       -5276
161697
 YDOT =        839
220619  feet/sec       YDOT =         196
655780  meter/sec
 ZDOT =     -18295
059982                 ZDOT =       -5602
025615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13875654
96                 X    =         4229299
63
 Y    =      -15934976
37  feet           Y    =        -4856980
80  meter
 Z    =        6394147
27                 Z    =         1948936
09
 XDOT =      14867
418692                 XDOT =        4531
589217
 YDOT =       5507
594486  feet/sec       YDOT =        1678
714799  meter/sec
 ZDOT =     -18396
091496                 ZDOT =       -5607
128688


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   09239
53562831  
00020000  00000-0  20000-3 0  9016
2 25544  51
6414 300
5855 0008796  22
0986 338
0555 15
73820617 17193


Satellite: ISS
Catalog Number: 25544
Epoch time:      09239
53562831   =   yrday
fracday
Element set:     901
Inclination:       51
6414  deg
RA of node:       300
5855  deg
Eccentricity:     
0008796     
Arg of perigee:    22
0986  deg
Mean anomaly:     338
0555  deg
Mean motion:   15
73820617  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1719
Checksum:              301


Coasting Arc #3 (Orbit 1734)
---------------------------------------

Vector Time (GMT): 2009/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4600018
28                 A    =         6722348
01  meter
 Y    =        -691005
20  meter          E    =           
0010389
 Z    =        4843399
99                 I    =           51
32419
 XDOT =      -1338
516289                 Wp   =           65
33972
 YDOT =       7233
238591  meter/sec      RA   =          295
00139  deg
 ZDOT =       2303
634894                 TA   =            2
15521
                                          MA   =            2
15074
                                          Ha   =            192
758  n
mi
                                          Hp   =            182
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15091923
49                 X    =         4583875
10
 Y    =       -2267077
43  feet           Y    =         -639655
51  meter
 Z    =       15890419
93                 Z    =         4865707
53
 XDOT =      -4391
457641                 XDOT =       -1430
490707
 YDOT =      23731
097738  feet/sec       YDOT =        7217
756184  meter/sec
 ZDOT =       7557
857263                 ZDOT =        2296
909248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14629559
41                 X    =        -4459089
71
 Y    =       -4010827
76  feet           Y    =        -1222500
30  meter
 Z    =       15978125
44                 Z    =         4870132
63
 XDOT =      13386
002592                 XDOT =        4080
053590
 YDOT =     -18826
488650  feet/sec       YDOT =       -5738
313741  meter/sec
 ZDOT =       7531
751099                 ZDOT =        2295
677735


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   09240
55159205  
00020000  00000-0  20000-3 0  9028
2 25544  51
6411 295
3697 0008721  26
1498 334
0104 15
73819355 17357


Satellite: ISS
Catalog Number: 25544
Epoch time:      09240
55159205   =   yrday
fracday
Element set:     902
Inclination:       51
6411  deg
RA of node:       295
3697  deg
Eccentricity:     
0008721     
Arg of perigee:    26
1498  deg
Mean anomaly:     334
0104  deg
Mean motion:   15
73819355  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1735
Checksum:              287


Coasting Arc #4 (Orbit 1749)
---------------------------------------

Vector Time (GMT): 2009/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         544383
18                 A    =         6730866
06  meter
 Y    =       -6378283
64  meter          E    =           
0015378
 Z    =       -2061640
11                 I    =           51
34095
 XDOT =       5186
954670                 Wp   =           34
21214
 YDOT =      -1335
674961  meter/sec      RA   =          289
80834  deg
 ZDOT =       5534
428193                 TA   =          302
67316
                                          MA   =          302
82140
                                          Ha   =            193
012  n
mi
                                          Hp   =            181
970

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1786034
07                 X    =          625680
78
 Y    =      -20926127
43  feet           Y    =        -6371741
40  meter
 Z    =       -6763911
12                 Z    =        -2058798
25
 XDOT =      17017
567814                 XDOT =        5174
619892
 YDOT =      -4382
135700  feet/sec       YDOT =       -1277
740531  meter/sec
 ZDOT =      18157
572813                 ZDOT =        5559
596198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9837386
87                 X    =        -2998435
52
 Y    =       18559779
57  feet           Y    =         5657020
81  meter
 Z    =       -6753045
42                 Z    =        -2058328
25
 XDOT =     -15928
499905                 XDOT =       -4855
006771
 YDOT =      -1838
866494  feet/sec       YDOT =        -560
486507  meter/sec
 ZDOT =      18256
501185                 ZDOT =        5564
581561


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   09241
50405178  
00020000  00000-0  20000-3 0  9038
2 25544  51
6408 290
4800 0008871  29
8334 330
3333 15
73811141 17505


Satellite: ISS
Catalog Number: 25544
Epoch time:      09241
50405178   =   yrday
fracday
Element set:     903
Inclination:       51
6408  deg
RA of node:       290
4800  deg
Eccentricity:     
0008871     
Arg of perigee:    29
8334  deg
Mean anomaly:     330
3333  deg
Mean motion:   15
73811141  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1750
Checksum:              265


Coasting Arc #5 (Orbit 1765)
---------------------------------------

Vector Time (GMT): 2009/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4416705
65                 A    =         6722510
73  meter
 Y    =        1602393
32  meter          E    =           
0019823
 Z    =       -4826351
97                 I    =           51
30436
 XDOT =        -51
416423                 Wp   =           56
40002
 YDOT =      -7308
625735  meter/sec      RA   =          284
68891  deg
 ZDOT =      -2375
689092                 TA   =          190
24696
                                          MA   =          190
28743
                                          Ha   =            193
113  n
mi
                                          Hp   =            181
665

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14490504
10                 X    =        -4410850
36
 Y    =        5257195
93  feet           Y    =         1553035
98  meter
 Z    =      -15834488
09                 Z    =        -4847793
82
 XDOT =       -168
689053                 XDOT =          41
854243
 YDOT =     -23978
430890  feet/sec       YDOT =       -7308
679144  meter/sec
 ZDOT =      -7794
255550                 ZDOT =       -2375
712492

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15319268
32                 X    =         4669312
98
 Y    =         507219
06  feet           Y    =          154600
37  meter
 Z    =      -15918749
27                 Z    =        -4852034
78
 XDOT =      -8813
485006                 XDOT =       -2686
350230
 YDOT =      21168
672251  feet/sec       YDOT =        6452
211302  meter/sec
 ZDOT =      -7794
715044                 ZDOT =       -2375
829145


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   09242
52000039  
00020000  00000-0  20000-3 0  9049
2 25544  51
6412 285
2637 0008892  34
2183 325
9551 15
73815237 17664


Satellite: ISS
Catalog Number: 25544
Epoch time:      09242
52000039   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:       285
2637  deg
Eccentricity:     
0008892     
Arg of perigee:    34
2183  deg
Mean anomaly:     325
9551  deg
Mean motion:   15
73815237  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1766
Checksum:              285


Coasting Arc #6 (Orbit 1781)
---------------------------------------

Vector Time (GMT): 2009/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         633354
34                 A    =         6730660
13  meter
 Y    =        6362246
65  meter          E    =           
0018880
 Z    =        2091419
58                 I    =           51
32525
 XDOT =      -4857
499936                 Wp   =           82
87956
 YDOT =       2309
447872  meter/sec      RA   =          279
49339  deg
 ZDOT =      -5509
639998                 TA   =           73
65319
                                          MA   =           73
44567
                                          Ha   =            193
159  n
mi
                                          Hp   =            181
556

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2077934
20                 X    =          552003
94
 Y    =       20873512
63  feet           Y    =         6368874
31  meter
 Z    =        6861612
79                 Z    =         2094298
84
 XDOT =     -15936
679580                 XDOT =       -4856
199089
 YDOT =       7576
928713  feet/sec       YDOT =        2255
135781  meter/sec
 ZDOT =     -18076
246713                 ZDOT =       -5533
234228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5566841
89                 X    =         1696773
41
 Y    =      -20220571
60  feet           Y    =        -6163230
22  meter
 Z    =        6873268
93                 Z    =         2094972
37
 XDOT =      16019
518798                 XDOT =        4882
749330
 YDOT =      -1815
547960  feet/sec       YDOT =        -553
379018  meter/sec
 ZDOT =     -18168
939305                 ZDOT =       -5537
892700


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   09243
53593941  
00020000  00000-0  20000-3 0  9051
2 25544  51
6406 280
0476 0009075  37
6731 322
5066 15
73865041 17821


Satellite: ISS
Catalog Number: 25544
Epoch time:      09243
53593941   =   yrday
fracday
Element set:     905
Inclination:       51
6406  deg
RA of node:       280
0476  deg
Eccentricity:     
0009075     
Arg of perigee:    37
6731  deg
Mean anomaly:     322
5066  deg
Mean motion:   15
73865041  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1782
Checksum:              294


Coasting Arc #7 (Orbit 1797)
---------------------------------------

Vector Time (GMT): 2009/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4033758
84                 A    =         6722473
07  meter
 Y    =       -2424953
67  meter          E    =           
0012595
 Z    =        4788294
52                 I    =           51
29321
 XDOT =       1413
128647                 Wp   =           75
36665
 YDOT =       7175
311158  meter/sec      RA   =          274
37376  deg
 ZDOT =       2441
168844                 TA   =          350
68343
                                          MA   =          350
70677
                                          Ha   =            193
143  n
mi
                                          Hp   =            181
413

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13234116
94                 X    =         4037314
96
 Y    =       -7955884
76  feet           Y    =        -2379825
89  meter
 Z    =       15709627
69                 Z    =         4807898
89
 XDOT =       4636
248842                 XDOT =        1320
929471
 YDOT =      23541
047107  feet/sec       YDOT =        7190
598101  meter/sec
 ZDOT =       8009
084134                 ZDOT =        2447
809716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15069860
86                 X    =        -4593293
59
 Y    =        2985352
84  feet           Y    =          909935
55  meter
 Z    =       15786618
31                 Z    =         4811761
26
 XDOT =       3949
549785                 XDOT =        1203
822774
 YDOT =     -22593
357930  feet/sec       YDOT =       -6886
455497  meter/sec
 ZDOT =       8035
593178                 ZDOT =        2449
248801


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   09244
55187145  
00020000  00000-0  20000-3 0  9060
2 25544  51
6398 274
8314 0009138  42
3207 317
8660 15
73860590 17982


Satellite: ISS
Catalog Number: 25544
Epoch time:      09244
55187145   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       274
8314  deg
Eccentricity:     
0009138     
Arg of perigee:    42
3207  deg
Mean anomaly:     317
8660  deg
Mean motion:   15
73860590  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1798
Checksum:              314


Coasting Arc #8 (Orbit 1812)
---------------------------------------

Vector Time (GMT): 2009/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1822058
40                 A    =         6730389
00  meter
 Y    =       -6102083
97  meter          E    =           
0015336
 Z    =       -2166210
96                 I    =           51
32011
 XDOT =       4340
609602                 Wp   =           44
46902
 YDOT =      -3229
063551  meter/sec      RA   =          269
17692  deg
 ZDOT =       5479
246349                 TA   =          291
16770
                                          MA   =          291
33151
                                          Ha   =            193
222  n
mi
                                          Hp   =            181
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5977881
88                 X    =        -1743165
51
 Y    =      -20019960
54  feet           Y    =        -6122018
25  meter
 Z    =       -7106991
34                 Z    =        -2174870
59
 XDOT =      14240
845151                 XDOT =        4349
778122
 YDOT =     -10594
040522  feet/sec       YDOT =       -3180
472883  meter/sec
 ZDOT =      17976
530016                 ZDOT =        5500
355100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -904044
73                 X    =         -275552
83
 Y    =       20862079
83  feet           Y    =         6358761
93  meter
 Z    =       -7141396
65                 Z    =        -2176697
70
 XDOT =     -15293
154473                 XDOT =       -4661
353483
 YDOT =       5481
079917  feet/sec       YDOT =        1670
633159  meter/sec
 ZDOT =      18059
392147                 ZDOT =        5504
502726


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   09245
50429977  
00020000  00000-0  20000-3 0  9079
2 25544  51
6406 269
9417 0009134  46
0461 314
1454 15
73901714 18133


Satellite: ISS
Catalog Number: 25544
Epoch time:      09245
50429977   =   yrday
fracday
Element set:     907
Inclination:       51
6406  deg
RA of node:       269
9417  deg
Eccentricity:     
0009134     
Arg of perigee:    46
0461  deg
Mean anomaly:     314
1454  deg
Mean motion:   15
73901714  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1813
Checksum:              294


Coasting Arc #9 (Orbit 1828)
---------------------------------------

Vector Time (GMT): 2009/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3528555
93                 A    =         6722515
43  meter
 Y    =        3162033
06  meter          E    =           
0020526
 Z    =       -4788363
21                 I    =           51
29438
 XDOT =      -2696
425473                 Wp   =           62
16387
 YDOT =      -6757
238577  meter/sec      RA   =          264
05725  deg
 ZDOT =      -2473
849323                 TA   =          183
46489
                                          MA   =          183
47913
                                          Ha   =            193
342  n
mi
                                          Hp   =            181
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11576627
07                 X    =        -3540391
34
 Y    =       10374124
22  feet           Y    =         3122508
26  meter
 Z    =      -15709853
04                 Z    =        -4805533
63
 XDOT =      -8846
540267                 XDOT =       -2608
647089
 YDOT =     -22169
417903  feet/sec       YDOT =       -6786
900918  meter/sec
 ZDOT =      -8116
303554                 ZDOT =       -2486
734863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14129769
89                 X    =         4306753
86
 Y    =       -6314199
16  feet           Y    =        -1924567
90  meter
 Z    =      -15777221
62                 Z    =        -4808897
15
 XDOT =       1052
289887                 XDOT =         320
737958
 YDOT =      22773
511509  feet/sec       YDOT =        6941
366308  meter/sec
 ZDOT =      -8167
382998                 ZDOT =       -2489
418338


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   09246
52021463  
00020000  00000-0  20000-3 0  9081
2 25544  51
6400 264
7249 0009142  49
2288 310
9667 15
73877429 18296


Satellite: ISS
Catalog Number: 25544
Epoch time:      09246
52021463   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:       264
7249  deg
Eccentricity:     
0009142     
Arg of perigee:    49
2288  deg
Mean anomaly:     310
9667  deg
Mean motion:   15
73877429  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1829
Checksum:              309


Coasting Arc #10 (Orbit 1844)
---------------------------------------

Vector Time (GMT): 2009/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2882039
12                 A    =         6730380
07  meter
 Y    =        5678868
68  meter          E    =           
0020700
 Z    =        2161798
45                 I    =           51
32418
 XDOT =      -3684
181695                 Wp   =           87
15404
 YDOT =       3971
284093  meter/sec      RA   =          258
85898  deg
 ZDOT =      -5474
490088                 TA   =           68
53164
                                          MA   =           68
31102
                                          Ha   =            193
380  n
mi
                                          Hp   =            180
967

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9455508
92                 X    =         2807821
29
 Y    =       18631458
93  feet           Y    =         5710682
51  meter
 Z    =        7092514
59                 Z    =         2175618
63
 XDOT =     -12087
210285                 XDOT =       -3701
721584
 YDOT =      13029
147286  feet/sec       YDOT =        3929
986971  meter/sec
 ZDOT =     -17960
925484                 ZDOT =       -5492
430568

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3545890
76                 X    =        -1080787
50
 Y    =      -20571475
15  feet           Y    =        -6270185
62  meter
 Z    =        7147219
25                 Z    =         2178472
43
 XDOT =      13772
028715                 XDOT =        4197
714352
 YDOT =      -8690
710465  feet/sec       YDOT =       -2648
928550  meter/sec
 ZDOT =     -18031
271843                 ZDOT =       -5495
931658


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   09247
53612068  
00020000  00000-0  20000-3 0  9091
2 25544  51
6386 259
5078 0009309  52
7438 307
4573 15
73909185 18452


Satellite: ISS
Catalog Number: 25544
Epoch time:      09247
53612068   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:       259
5078  deg
Eccentricity:     
0009309     
Arg of perigee:    52
7438  deg
Mean anomaly:     307
4573  deg
Mean motion:   15
73909185  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1845
Checksum:              325


Coasting Arc #11 (Orbit 1860)
---------------------------------------

Vector Time (GMT): 2009/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2878259
02                 A    =         6722494
26  meter
 Y    =       -3755966
72  meter          E    =           
0014075
 Z    =        4762315
64                 I    =           51
30392
 XDOT =       3890
716828                 Wp   =           83
80130
 YDOT =       6166
692422  meter/sec      RA   =          253
73979  deg
 ZDOT =       2507
262113                 TA   =          341
55076
                                          MA   =          341
60175
                                          Ha   =            193
346  n
mi
                                          Hp   =            180
936

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9443107
02                 X    =         2896910
57
 Y    =      -12322725
47  feet           Y    =        -3723675
68  meter
 Z    =       15624395
15                 Z    =         4776343
78
 XDOT =      12764
818991                 XDOT =        3809
290855
 YDOT =      20231
930520  feet/sec       YDOT =        6209
745625  meter/sec
 ZDOT =       8225
925566                 ZDOT =        2525
964889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12392711
31                 X    =        -3777298
41
 Y    =        9258616
91  feet           Y    =         2822026
43  meter
 Z    =       15679358
30                 Z    =         4779068
41
 XDOT =      -5955
890054                 XDOT =       -1815
355288
 YDOT =     -22054
506779  feet/sec       YDOT =       -6722
213666  meter/sec
 ZDOT =       8299
876732                 ZDOT =        2529
802428


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   09248
55201837  
00020000  00000-0  20000-3 0  9104
2 25544  51
6380 254
2907 0009277  56
3077 303
8969 15
73900683 18613


Satellite: ISS
Catalog Number: 25544
Epoch time:      09248
55201837   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:       254
2907  deg
Eccentricity:     
0009277     
Arg of perigee:    56
3077  deg
Mean anomaly:     303
8969  deg
Mean motion:   15
73900683  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1861
Checksum:              309


Coasting Arc #12 (Orbit 1875)
---------------------------------------

Vector Time (GMT): 2009/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3877108
20                 A    =         6730182
37  meter
 Y    =       -5035986
23  meter          E    =           
0015207
 Z    =       -2207803
53                 I    =           51
34039
 XDOT =       2884
565585                 Wp   =           53
57834
 YDOT =      -4598
495029  meter/sec      RA   =          248
54312  deg
 ZDOT =       5458
513080                 TA   =          281
57251
                                          MA   =          281
74319
                                          Ha   =            193
392  n
mi
                                          Hp   =            180
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12720171
26                 X    =        -3809781
65
 Y    =      -16522264
55  feet           Y    =        -5078966
07  meter
 Z    =       -7243449
92                 Z    =        -2226474
62
 XDOT =       9463
797850                 XDOT =        2909
255840
 YDOT =     -15086
925947  feet/sec       YDOT =       -4566
099631  meter/sec
 ZDOT =      17908
507480                 ZDOT =        5472
586665

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7950962
24                 X    =         2423453
29
 Y    =       19248275
85  feet           Y    =         5866874
48  meter
 Z    =       -7317214
33                 Z    =        -2230286
93
 XDOT =     -11553
117603                 XDOT =       -3521
390245
 YDOT =      11557
998942  feet/sec       YDOT =        3522
878077  meter/sec
 ZDOT =      17963
595005                 ZDOT =        5475
303758


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   09249
50441354  
00020000  00000-0  20000-3 0  9111
2 25544  51
6386 249
4009 0009320  60
1442 300
0647 15
73938035 18766


Satellite: ISS
Catalog Number: 25544
Epoch time:      09249
50441354   =   yrday
fracday
Element set:     911
Inclination:       51
6386  deg
RA of node:       249
4009  deg
Eccentricity:     
0009320     
Arg of perigee:    60
1442  deg
Mean anomaly:     300
0647  deg
Mean motion:   15
73938035  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1876
Checksum:              279


Coasting Arc #13 (Orbit 1891)
---------------------------------------

Vector Time (GMT): 2009/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2166101
05                 A    =         6722447
20  meter
 Y    =        4223025
94  meter          E    =           
0020903
 Z    =       -4780610
69                 I    =           51
32535
 XDOT =      -4915
097178                 Wp   =           68
24101
 YDOT =      -5351
039734  meter/sec      RA   =          243
42463  deg
 ZDOT =      -2501
023355                 TA   =          177
12604
                                          MA   =          177
11401
                                          Ha   =            193
469  n
mi
                                          Hp   =            180
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7106630
73                 X    =        -2189939
17
 Y    =       13855071
98  feet           Y    =         4198669
69  meter
 Z    =      -15684418
27                 Z    =        -4791191
88
 XDOT =     -16125
646910                 XDOT =       -4842
746029
 YDOT =     -17555
904640  feet/sec       YDOT =       -5405
598888  meter/sec
 ZDOT =      -8205
457200                 ZDOT =       -2524
724914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10172724
54                 X    =         3100646
44
 Y    =      -11733860
55  feet           Y    =        -3576480
69  meter
 Z    =      -15725787
37                 Z    =        -4793219
99
 XDOT =      10471
778678                 XDOT =        3191
798141
 YDOT =      20195
987254  feet/sec       YDOT =        6155
736915  meter/sec
 ZDOT =      -8299
037332                 ZDOT =       -2529
546579


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   09250
52029345  
00020000  00000-0  20000-3 0  9128
2 25544  51
6378 244
1829 0009271  63
2407 296
9704 15
73924217 18921


Satellite: ISS
Catalog Number: 25544
Epoch time:      09250
52029345   =   yrday
fracday
Element set:     912
Inclination:       51
6378  deg
RA of node:       244
1829  deg
Eccentricity:     
0009271     
Arg of perigee:    63
2407  deg
Mean anomaly:     296
9704  deg
Mean motion:   15
73924217  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1892
Checksum:              301


Coasting Arc #14 (Orbit 1907)
---------------------------------------

Vector Time (GMT): 2009/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4698476
43                 A    =         6730162
27  meter
 Y    =        4292014
79  meter          E    =           
0021757
 Z    =        2170236
66                 I    =           51
36641
 XDOT =      -2036
959732                 Wp   =           92
04175
 YDOT =       5021
708133  meter/sec      RA   =          238
22866  deg
 ZDOT =      -5474
905926                 TA   =           63
55183
                                          MA   =           63
32876
                                          Ha   =            193
389  n
mi
                                          Hp   =            180
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15414948
90                 X    =         4639590
45
 Y    =       14081413
36  feet           Y    =         4344226
79  meter
 Z    =        7120199
01                 Z    =         2192918
80
 XDOT =      -6682
938753                 XDOT =       -2066
365583
 YDOT =      16475
420385  feet/sec       YDOT =        4998
764925  meter/sec
 ZDOT =     -17962
289785                 ZDOT =       -5484
873283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11786376
70                 X    =        -3592487
62
 Y    =      -17196090
39  feet           Y    =        -5241368
35  meter
 Z    =        7209707
72                 Z    =         2197518
91
 XDOT =       8882
978547                 XDOT =        2707
531861
 YDOT =     -13698
837615  feet/sec       YDOT =       -4175
405705  meter/sec
 ZDOT =     -18001
194532                 ZDOT =       -5486
764093


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   09251
53616306  
00020000  00000-0  20000-3 0  9130
2 25544  51
6377 238
9658 0009286  65
7147 294
4985 15
73973033 19087


Satellite: ISS
Catalog Number: 25544
Epoch time:      09251
53616306   =   yrday
fracday
Element set:     913
Inclination:       51
6377  deg
RA of node:       238
9658  deg
Eccentricity:     
0009286     
Arg of perigee:    65
7147  deg
Mean anomaly:     294
4985  deg
Mean motion:   15
73973033  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1908
Checksum:              329


Coasting Arc #15 (Orbit 1923)
---------------------------------------

Vector Time (GMT): 2009/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1373875
18                 A    =         6722301
21  meter
 Y    =       -4521265
32  meter          E    =           
0014891
 Z    =        4768591
09                 I    =           51
35636
 XDOT =       5809
450495                 Wp   =           91
83870
 YDOT =       4410
309849  meter/sec      RA   =          233
11354  deg
 ZDOT =       2500
629677                 TA   =          333
58989
                                          MA   =          333
66572
                                          Ha   =            193
357  n
mi
                                          Hp   =            180
627

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4507464
50                 X    =         1401165
43
 Y    =      -14833547
64  feet           Y    =        -4505749
09  meter
 Z    =       15644983
88                 Z    =         4775331
89
 XDOT =      19059
876952                 XDOT =        5747
554134
 YDOT =      14469
520503  feet/sec       YDOT =        4474
928548  meter/sec
 ZDOT =       8204
165607                 ZDOT =        2528
701796

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7426989
27                 X    =        -2263746
33
 Y    =       13578269
18  feet           Y    =         4138656
45  meter
 Z    =       15671226
15                 Z    =         4776589
73
 XDOT =     -14566
672790                 XDOT =       -4439
921866
 YDOT =     -17591
320958  feet/sec       YDOT =       -5361
834628  meter/sec
 ZDOT =       8314
895293                 ZDOT =        2534
380085


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   09252
55202415  
00020000  00000-0  20000-3 0  9146
2 25544  51
6375 233
7494 0009162  69
6674 290
5482 15
73972105 19243


Satellite: ISS
Catalog Number: 25544
Epoch time:      09252
55202415   =   yrday
fracday
Element set:     914
Inclination:       51
6375  deg
RA of node:       233
7494  deg
Eccentricity:     
0009162     
Arg of perigee:    69
6674  deg
Mean anomaly:     290
5482  deg
Mean motion:   15
73972105  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1924
Checksum:              301

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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