Date: August 6th 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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 1372)
---------------------------------------

Vector Time (GMT): 2009/217/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4894622
13                 A    =         6724594
20  meter
 Y    =        -514130
95  meter          E    =           
0007079
 Z    =        4585371
47                 I    =           51
89472
 XDOT =      -2128
616010                 Wp   =            4
87195
 YDOT =      -6751
050173  meter/sec      RA   =           52
93971  deg
 ZDOT =      -3021
891584                 TA   =          115
09601
                                          MA   =          115
02253
                                          Ha   =            190
051  n
mi
                                          Hp   =            187
282

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16058471
54                 X    =        -4910783
66
 Y    =       -1686781
34  feet           Y    =         -568956
22  meter
 Z    =       15043869
64                 Z    =         4561554
62
 XDOT =      -6983
648328                 XDOT =       -2038
286932
 YDOT =     -22149
114740  feet/sec       YDOT =       -6774
348307  meter/sec
 ZDOT =      -9914
342468                 ZDOT =       -3032
013307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11471414
15                 X    =         3496487
03
 Y    =       11486388
08  feet           Y    =         3501051
09  meter
 Z    =       14950160
52                 Z    =         4556808
93
 XDOT =      -7746
915401                 XDOT =       -2361
259814
 YDOT =      20724
190860  feet/sec       YDOT =        6316
733374  meter/sec
 ZDOT =      -9954
452864                 ZDOT =       -3034
117233


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   09217
56314942  
00010596  00000-0  82463-4 0  9003
2 25544  51
6382  53
3504 0008003 296
2578  63
7762 15
73494970 13731


Satellite: ISS
Catalog Number: 25544
Epoch time:      09217
56314942   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:        53
3504  deg
Eccentricity:     
0008003     
Arg of perigee:   296
2578  deg
Mean anomaly:      63
7762  deg
Mean motion:   15
73494970  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1373
Checksum:              314


Coasting Arc #2 (Orbit 1388)
---------------------------------------

Vector Time (GMT): 2009/218/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2510971
86                 A    =         6730763
88  meter
 Y    =        5710538
23  meter          E    =           
0009772
 Z    =        2510351
27                 I    =           51
89610
 XDOT =      -5555
287256                 Wp   =           41
72084
 YDOT =         95
353686  meter/sec      RA   =           47
86878  deg
 ZDOT =       5335
082585                 TA   =          346
60107
                                          MA   =          346
62700
                                          Ha   =            190
129  n
mi
                                          Hp   =            186
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8238096
64                 X    =         2434734
45
 Y    =       18735361
64  feet           Y    =         5738190
97  meter
 Z    =        8236060
58                 Z    =         2522364
46
 XDOT =     -18226
008057                 XDOT =       -5581
856947
 YDOT =        312
840178  feet/sec       YDOT =          33
082335  meter/sec
 ZDOT =      17503
551789                 ZDOT =        5308
031047

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5111490
32                 X    =         1557982
25
 Y    =      -19798179
13  feet           Y    =        -6034485
00  meter
 Z    =        8283566
60                 Z    =         2524831
10
 XDOT =      13174
360349                 XDOT =        4015
545034
 YDOT =      10686
697412  feet/sec       YDOT =        3257
305371  meter/sec
 ZDOT =      17397
144521                 ZDOT =        5302
649650


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   09218
57930103  
00010596  00000-0  82463-4 0  9019
2 25544  51
6374  48
1343 0007904 299
8817  60
1560 15
73523142 13897


Satellite: ISS
Catalog Number: 25544
Epoch time:      09218
57930103   =   yrday
fracday
Element set:     901
Inclination:       51
6374  deg
RA of node:        48
1343  deg
Eccentricity:     
0007904     
Arg of perigee:   299
8817  deg
Mean anomaly:      60
1560  deg
Mean motion:   15
73523142  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1389
Checksum:              306


Coasting Arc #3 (Orbit 1403)
---------------------------------------

Vector Time (GMT): 2009/219/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4740570
79                 A    =         6723940
38  meter
 Y    =        -673482
79  meter          E    =           
0004131
 Z    =       -4723843
31                 I    =           51
85210
 XDOT =       3598
344967                 Wp   =           79
93821
 YDOT =       6234
433778  meter/sec      RA   =           42
71007  deg
 ZDOT =       2724
951263                 TA   =          216
80318
                                          MA   =          216
83155
                                          Ha   =            190
400  n
mi
                                          Hp   =            186
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15553053
76                 X    =         4770696
59
 Y    =       -2209589
20  feet           Y    =         -620302
32  meter
 Z    =      -15498173
59                 Z    =        -4700740
91
 XDOT =      11805
593724                 XDOT =        3515
125958
 YDOT =      20454
179061  feet/sec       YDOT =        6274
207178  meter/sec
 ZDOT =       8940
128815                 ZDOT =        2742
229785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13809230
79                 X    =        -4209053
54
 Y    =       -7674148
85  feet           Y    =        -2339080
57  meter
 Z    =      -15407327
31                 Z    =        -4696153
36
 XDOT =       2405
498338                 XDOT =         733
195893
 YDOT =     -22396
621857  feet/sec       YDOT =       -6826
490342  meter/sec
 ZDOT =       9008
369378                 ZDOT =        2745
750987


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   09219
53193726  
00010596  00000-0  82463-4 0  9029
2 25544  51
6375  43
2445 0007758 304
0070  56
0355 15
73525747 14041


Satellite: ISS
Catalog Number: 25544
Epoch time:      09219
53193726   =   yrday
fracday
Element set:     902
Inclination:       51
6375  deg
RA of node:        43
2445  deg
Eccentricity:     
0007758     
Arg of perigee:   304
0070  deg
Mean anomaly:      56
0355  deg
Mean motion:   15
73525747  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1404
Checksum:              300


Coasting Arc #4 (Orbit 1419)
---------------------------------------

Vector Time (GMT): 2009/220/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3735218
40                 A    =         6731158
45  meter
 Y    =       -5122644
76  meter          E    =           
0002130
 Z    =       -2261253
26                 I    =           51
85462
 XDOT =       5228
398380                 Wp   =          289
70538
 YDOT =      -1394
922373  meter/sec      RA   =           37
63436  deg
 ZDOT =      -5471
539444                 TA   =          275
58264
                                          MA   =          275
60693
                                          Ha   =            190
501  n
mi
                                          Hp   =            186
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12254653
54                 X    =        -3666673
91
 Y    =      -16806577
28  feet           Y    =        -5164030
86  meter
 Z    =       -7418809
90                 Z    =        -2279232
27
 XDOT =      17153
537991                 XDOT =        5270
187389
 YDOT =      -4576
516972  feet/sec       YDOT =       -1336
221593  meter/sec
 ZDOT =     -17951
244894                 ZDOT =       -5446
038805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -42133
54                 X    =          -12842
30
 Y    =       20774458
05  feet           Y    =         6332054
81  meter
 Z    =       -7489755
09                 Z    =        -2282877
35
 XDOT =     -15123
886437                 XDOT =       -4609
760586
 YDOT =      -6472
132195  feet/sec       YDOT =       -1972
705893  meter/sec
 ZDOT =     -17850
998961                 ZDOT =       -5440
984483


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   09220
54807365  
00010596  00000-0  82463-4 0  9034
2 25544  51
6379  38
0297 0007861 309
2827  50
7638 15
73561459 14207


Satellite: ISS
Catalog Number: 25544
Epoch time:      09220
54807365   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:        38
0297  deg
Eccentricity:     
0007861     
Arg of perigee:   309
2827  deg
Mean anomaly:      50
7638  deg
Mean motion:   15
73561459  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1420
Checksum:              321


Coasting Arc #5 (Orbit 1435)
---------------------------------------

Vector Time (GMT): 2009/221/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4342077
37                 A    =         6723514
21  meter
 Y    =        1742693
82  meter          E    =           
0008772
 Z    =        4831587
07                 I    =           51
80349
 XDOT =      -4903
339646                 Wp   =            2
27080
 YDOT =      -5404
482590  meter/sec      RA   =           32
47558  deg
 ZDOT =      -2448
491599                 TA   =          111
65238
                                          MA   =          111
55893
                                          Ha   =            190
712  n
mi
                                          Hp   =            186
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14245660
65                 X    =        -4384712
47
 Y    =        5717499
42  feet           Y    =         1693899
73  meter
 Z    =       15851663
60                 Z    =         4810389
95
 XDOT =     -16087
072330                 XDOT =       -4830
647174
 YDOT =     -17731
242093  feet/sec       YDOT =       -5458
908144  meter/sec
 ZDOT =      -8033
108922                 ZDOT =       -2472
135235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15016159
40                 X    =         4576925
38
 Y    =        3574570
89  feet           Y    =         1089529
21  meter
 Z    =       15768363
44                 Z    =         4806197
18
 XDOT =       3175
068669                 XDOT =         967
760930
 YDOT =      22636
638397  feet/sec       YDOT =        6899
647383  meter/sec
 ZDOT =      -8126
343596                 ZDOT =       -2476
909528


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   09221
56420394  
00010596  00000-0  82463-4 0  9041
2 25544  51
6376  32
8139 0007730 311
9932  48
0572 15
73517359 14367


Satellite: ISS
Catalog Number: 25544
Epoch time:      09221
56420394   =   yrday
fracday
Element set:     904
Inclination:       51
6376  deg
RA of node:        32
8139  deg
Eccentricity:     
0007730     
Arg of perigee:   311
9932  deg
Mean anomaly:      48
0572  deg
Mean motion:   15
73517359  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1436
Checksum:              308


Coasting Arc #6 (Orbit 1451)
---------------------------------------

Vector Time (GMT): 2009/222/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4788318
49                 A    =         6731593
33  meter
 Y    =        4267169
91  meter          E    =           
0013089
 Z    =        2015521
66                 I    =           51
80651
 XDOT =      -4637
290215                 Wp   =           35
91542
 YDOT =       2556
358574  meter/sec      RA   =           27
39251  deg
 ZDOT =       5596
867428                 TA   =          346
50826
                                          MA   =          346
54322
                                          Ha   =            190
699  n
mi
                                          Hp   =            186
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15709706
33                 X    =         4730455
41
 Y    =       13999901
28  feet           Y    =         4320392
15  meter
 Z    =        6612603
88                 Z    =         2038642
64
 XDOT =     -15214
206741                 XDOT =       -4692
719587
 YDOT =       8387
003194  feet/sec       YDOT =        2504
191704  meter/sec
 ZDOT =      18362
425945                 ZDOT =        5574
205010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5111158
83                 X    =        -1557881
21
 Y    =      -20382706
67  feet           Y    =        -6212648
99  meter
 Z    =        6703727
54                 Z    =         2043296
15
 XDOT =      15901
184228                 XDOT =        4846
680953
 YDOT =       2030
960368  feet/sec       YDOT =         619
036720  meter/sec
 ZDOT =      18273
399808                 ZDOT =        5569
732262


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   09222
58032438  
00010596  00000-0  82463-4 0  9053
2 25544  51
6385  27
5985 0007718 315
7296  44
3248 15
73568395 14521


Satellite: ISS
Catalog Number: 25544
Epoch time:      09222
58032438   =   yrday
fracday
Element set:     905
Inclination:       51
6385  deg
RA of node:        27
5985  deg
Eccentricity:     
0007718     
Arg of perigee:   315
7296  deg
Mean anomaly:      44
3248  deg
Mean motion:   15
73568395  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1452
Checksum:              334


Coasting Arc #7 (Orbit 1466)
---------------------------------------

Vector Time (GMT): 2009/223/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3704011
83                 A    =         6722925
00  meter
 Y    =       -2685464
21  meter          E    =           
0007470
 Z    =       -4931320
27                 I    =           51
75103
 XDOT =       6000
939553                 Wp   =           70
88681
 YDOT =       4301
344775  meter/sec      RA   =           22
23507  deg
 ZDOT =       2170
084038                 TA   =          220
12891
                                          MA   =          220
18410
                                          Ha   =            190
961  n
mi
                                          Hp   =            185
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12152269
78                 X    =         3757721
25
 Y    =       -8810578
12  feet           Y    =        -2643743
39  meter
 Z    =      -16178872
28                 Z    =        -4913195
82
 XDOT =      19688
121893                 XDOT =        5941
853328
 YDOT =      14112
023541  feet/sec       YDOT =        4368
120397  meter/sec
 ZDOT =       7119
698287                 ZDOT =        2199
093074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15071262
02                 X    =        -4593720
66
 Y    =         677407
25  feet           Y    =          206473
73  meter
 Z    =      -16107701
15                 Z    =        -4909627
31
 XDOT =      -8678
252376                 XDOT =       -2645
131324
 YDOT =     -21461
110107  feet/sec       YDOT =       -6541
346361  meter/sec
 ZDOT =       7233
975173                 ZDOT =        2204
915633


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   09223
53293140  
00010596  00000-0  82463-4 0  9069
2 25544  51
6395  22
7102 0007683 319
9570  40
1026 15
73570563 14676


Satellite: ISS
Catalog Number: 25544
Epoch time:      09223
53293140   =   yrday
fracday
Element set:     906
Inclination:       51
6395  deg
RA of node:        22
7102  deg
Eccentricity:     
0007683     
Arg of perigee:   319
9570  deg
Mean anomaly:      40
1026  deg
Mean motion:   15
73570563  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1467
Checksum:              295


Coasting Arc #8 (Orbit 1482)
---------------------------------------

Vector Time (GMT): 2009/224/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5637134
46                 A    =         6731856
49  meter
 Y    =       -3215731
78  meter          E    =           
0000621
 Z    =       -1790220
15                 I    =           51
75340
 XDOT =       3810
851329                 Wp   =          357
65771
 YDOT =      -3514
634307  meter/sec      RA   =           17
14438  deg
 ZDOT =      -5685
864054                 TA   =          202
13362
                                          MA   =          202
13630
                                          Ha   =            191
071  n
mi
                                          Hp   =            185
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18494535
64                 X    =        -5592060
07
 Y    =      -10550301
12  feet           Y    =        -3278517
44  meter
 Z    =       -5873425
69                 Z    =        -1817495
96
 XDOT =      12502
793073                 XDOT =        3877
490229
 YDOT =     -11530
952450  feet/sec       YDOT =       -3471
646340  meter/sec
 ZDOT =     -18654
409626                 ZDOT =       -5667
189199

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10006938
90                 X    =         3050114
98
 Y    =       18760187
31  feet           Y    =         5718105
09  meter
 Z    =       -5980834
19                 Z    =        -1822958
26
 XDOT =     -15446
888780                 XDOT =       -4708
211700
 YDOT =       2315
142491  feet/sec       YDOT =         705
655431  meter/sec
 ZDOT =     -18581
107451                 ZDOT =       -5663
521551


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   09224
54903662  
00010596  00000-0  82463-4 0  9079
2 25544  51
6394  17
4946 0007826 324
5099  35
5542 15
73603742 14834


Satellite: ISS
Catalog Number: 25544
Epoch time:      09224
54903662   =   yrday
fracday
Element set:     907
Inclination:       51
6394  deg
RA of node:        17
4946  deg
Eccentricity:     
0007826     
Arg of perigee:   324
5099  deg
Mean anomaly:      35
5542  deg
Mean motion:   15
73603742  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1483
Checksum:              323


Coasting Arc #9 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2009/225/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2919849
26                 A    =         6722645
13  meter
 Y    =        3418319
64  meter          E    =           
0009873
 Z    =        5000558
80                 I    =           51
69330
 XDOT =      -6823
417159                 Wp   =            4
24918
 YDOT =      -3001
246109  meter/sec      RA   =           11
98560  deg
 ZDOT =      -1922
707008                 TA   =          104
36480
                                          MA   =          104
25518
                                          Ha   =            191
324  n
mi
                                          Hp   =            185
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9579557
96                 X    =        -2982148
30
 Y    =       11214959
46  feet           Y    =         3385319
57  meter
 Z    =       16406032
80                 Z    =         4986223
03
 XDOT =     -22386
539236                 XDOT =       -6780
009415
 YDOT =      -9846
607969  feet/sec       YDOT =       -3077
306752  meter/sec
 ZDOT =      -6308
093858                 ZDOT =       -1955
749897

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14084511
19                 X    =         4292959
01
 Y    =       -4583893
91  feet           Y    =        -1397170
86  meter
 Z    =       16349789
59                 Z    =         4983415
87
 XDOT =      13685
547811                 XDOT =        4171
354973
 YDOT =      18970
434459  feet/sec       YDOT =        5782
188423  meter/sec
 ZDOT =      -6438
171308                 ZDOT =       -1962
354615


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   09225
56513620  
00010596  00000-0  82463-4 0  9084
2 25544  51
6399  12
2796 0007688 328
6286  31
4417 15
73556144 14990


Satellite: ISS
Catalog Number: 25544
Epoch time:      09225
56513620   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:        12
2796  deg
Eccentricity:     
0007688     
Arg of perigee:   328
6286  deg
Mean anomaly:      31
4417  deg
Mean motion:   15
73556144  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1499
Checksum:              334


Coasting Arc #10 (Orbit 1514)
---------------------------------------

Vector Time (GMT): 2009/226/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6224140
53                 A    =         6732118
15  meter
 Y    =        1997731
08  meter          E    =           
0015892
 Z    =        1566008
45                 I    =           51
69783
 XDOT =      -2821
537986                 Wp   =           33
56105
 YDOT =       4252
875679  meter/sec      RA   =            6
88802  deg
 ZDOT =       5774
227572                 TA   =          343
70891
                                          MA   =          343
75993
                                          Ha   =            191
237  n
mi
                                          Hp   =            185
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20420408
55                 X    =         6193731
59
 Y    =        6554235
82  feet           Y    =         2067162
92  meter
 Z    =        5137823
01                 Z    =         1596171
56
 XDOT =      -9257
014390                 XDOT =       -2896
934764
 YDOT =      13953
004196  feet/sec       YDOT =        4220
901585  meter/sec
 ZDOT =      18944
316181                 ZDOT =        5760
337749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14324736
93                 X    =        -4366179
82
 Y    =      -15922282
70  feet           Y    =        -4853111
77  meter
 Z    =        5256533
42                 Z    =         1602191
39
 XDOT =      13953
996577                 XDOT =        4253
178157
 YDOT =      -6302
109853  feet/sec       YDOT =       -1920
883083  meter/sec
 ZDOT =      18889
856694                 ZDOT =        5757
628320


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   09226
58122334  
00010596  00000-0  82463-4 0  9096
2 25544  51
6410   7
0647 0007742 331
8019  28
2724 15
73630516 15152


Satellite: ISS
Catalog Number: 25544
Epoch time:      09226
58122334   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:         7
0647  deg
Eccentricity:     
0007742     
Arg of perigee:   331
8019  deg
Mean anomaly:      28
2724  deg
Mean motion:   15
73630516  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1515
Checksum:              288


Coasting Arc #11 (Orbit 1529)
---------------------------------------

Vector Time (GMT): 2009/227/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1980825
11                 A    =         6722092
67  meter
 Y    =       -3954925
27  meter          E    =           
0010804
 Z    =       -5069244
79                 I    =           51
63418
 XDOT =       7349
162363                 Wp   =           67
00618
 YDOT =       1546
322988  meter/sec      RA   =            1
72969  deg
 ZDOT =       1672
255567                 TA   =          219
04816
                                          MA   =          219
12620
                                          Ha   =            191
471  n
mi
                                          Hp   =            184
942

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6498770
03                 X    =         2049527
86
 Y    =      -12975476
62  feet           Y    =        -3932389
93  meter
 Z    =      -16631380
53                 Z    =        -5059455
47
 XDOT =      24111
425074                 XDOT =        7323
201441
 YDOT =       5073
238148  feet/sec       YDOT =        1628
360327  meter/sec
 ZDOT =       5486
402780                 ZDOT =        1707
894667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12090259
23                 X    =        -3685111
01
 Y    =        8105349
41  feet           Y    =         2470510
50  meter
 Z    =      -16593033
68                 Z    =        -5057556
67
 XDOT =     -17947
948229                 XDOT =       -5470
534620
 YDOT =     -15300
009733  feet/sec       YDOT =       -4663
442967  meter/sec
 ZDOT =       5626
635380                 ZDOT =        1714
998464


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   09227
53380046  
00010596  00000-0  82463-4 0  9100
2 25544  51
6410   2
1767 0007850 335
9555  24
1241 15
73639733 15307


Satellite: ISS
Catalog Number: 25544
Epoch time:      09227
53380046   =   yrday
fracday
Element set:     910
Inclination:       51
6410  deg
RA of node:         2
1767  deg
Eccentricity:     
0007850     
Arg of perigee:   335
9555  deg
Mean anomaly:      24
1241  deg
Mean motion:   15
73639733  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1530
Checksum:              287


Coasting Arc #12 (Orbit 1545)
---------------------------------------

Vector Time (GMT): 2009/228/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6554312
51                 A    =         6732309
74  meter
 Y    =        -701519
79  meter          E    =           
0002542
 Z    =       -1372609
88                 I    =           51
63919
 XDOT =       1723
507579                 Wp   =           75
96260
 YDOT =      -4720
584008  meter/sec      RA   =          356
62298  deg
 ZDOT =      -5825
640566                 TA   =          119
10656
                                          MA   =          119
08110
                                          Ha   =            191
615  n
mi
                                          Hp   =            184
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21503649
97                 X    =        -6539313
05
 Y    =       -2301574
11  feet           Y    =         -774729
96  meter
 Z    =       -4503313
26                 Z    =        -1404414
00
 XDOT =       5654
552426                 XDOT =        1804
465447
 YDOT =     -15487
480340  feet/sec       YDOT =       -4700
857539  meter/sec
 ZDOT =     -19112
993983                 ZDOT =       -5817
071652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17833277
76                 X    =         5435583
06
 Y    =       12187527
93  feet           Y    =         3714758
51  meter
 Z    =       -4628434
20                 Z    =        -1410746
74
 XDOT =     -11517
605281                 XDOT =       -3510
566090
 YDOT =       9617
407448  feet/sec       YDOT =        2931
385790  meter/sec
 ZDOT =     -19079
476011                 ZDOT =       -5815
424288


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   09228
54987366  
00010596  00000-0  82463-4 0  9111
2 25544  51
6412 356
9605 0007950 339
9268  20
1581 15
73647249 15467


Satellite: ISS
Catalog Number: 25544
Epoch time:      09228
54987366   =   yrday
fracday
Element set:     911
Inclination:       51
6412  deg
RA of node:       356
9605  deg
Eccentricity:     
0007950     
Arg of perigee:   339
9268  deg
Mean anomaly:      20
1581  deg
Mean motion:   15
73647249  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1546
Checksum:              338


Coasting Arc #13 (Orbit 1561)
---------------------------------------

Vector Time (GMT): 2009/229/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1015484
46                 A    =         6721856
40  meter
 Y    =        4250363
42  meter          E    =           
0010625
 Z    =        5108408
10                 I    =           51
57497
 XDOT =      -7559
813288                 Wp   =            8
47294
 YDOT =        -37
212208  meter/sec      RA   =          351
46250  deg
 ZDOT =      -1461
113996                 TA   =           95
60521
                                          MA   =           95
48402
                                          Ha   =            191
826  n
mi
                                          Hp   =            184
442

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3331641
93                 X    =        -1087752
58
 Y    =       13944761
86  feet           Y    =         4238603
19  meter
 Z    =       16759869
08                 Z    =         5103299
76
 XDOT =     -24802
537034                 XDOT =       -7551
737608
 YDOT =       -122
087296  feet/sec       YDOT =        -121
705206  meter/sec
 ZDOT =      -4793
681090                 ZDOT =       -1497
819332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9433076
32                 X    =         2875201
66
 Y    =      -10827775
34  feet           Y    =        -3300305
92  meter
 Z    =       16739945
79                 Z    =         5102335
48
 XDOT =      21179
822644                 XDOT =        6455
609942
 YDOT =      10762
950865  feet/sec       YDOT =        3280
547424  meter/sec
 ZDOT =      -4938
059171                 ZDOT =       -1505
120435


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   09229
56593912  
00010596  00000-0  82463-4 0  9125
2 25544  51
6421 351
7455 0008053 344
2983  15
7930 15
73647470 15623


Satellite: ISS
Catalog Number: 25544
Epoch time:      09229
56593912   =   yrday
fracday
Element set:     912
Inclination:       51
6421  deg
RA of node:       351
7455  deg
Eccentricity:     
0008053     
Arg of perigee:   344
2983  deg
Mean anomaly:      15
7930  deg
Mean motion:   15
73647470  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1562
Checksum:              318


Coasting Arc #14 (Orbit 1577)
---------------------------------------

Vector Time (GMT): 2009/230/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6586370
89                 A    =         6732519
16  meter
 Y    =        -640624
52  meter          E    =           
0018319
 Z    =        1174975
93                 I    =           51
58230
 XDOT =       -574
223835                 Wp   =           33
28244
 YDOT =       4943
219446  meter/sec      RA   =          346
34933  deg
 ZDOT =       5885
902062                 TA   =          339
61050
                                          MA   =          339
68354
                                          Ha   =            191
879  n
mi
                                          Hp   =            184
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21608828
38                 X    =         6587337
25
 Y    =       -2101786
47  feet           Y    =         -566966
51  meter
 Z    =        3854907
89                 Z    =         1206974
15
 XDOT =      -1883
936466                 XDOT =        -658
049122
 YDOT =      16217
911568  feet/sec       YDOT =        4936
329133  meter/sec
 ZDOT =      19310
702304                 ZDOT =        5882
909198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20287979
51                 X    =        -6183776
15
 Y    =       -7666213
43  feet           Y    =        -2336661
85  meter
 Z    =        3980746
69                 Z    =         1213331
59
 XDOT =       8407
271254                 XDOT =        2562
536278
 YDOT =     -12181
544446  feet/sec       YDOT =       -3712
934747  meter/sec
 ZDOT =      19299
132795                 ZDOT =        5882
375676


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   09230
58199560  
00010596  00000-0  82463-4 0  9131
2 25544  51
6427 346
5304 0008104 348
3926  11
7048 15
73657724 15789


Satellite: ISS
Catalog Number: 25544
Epoch time:      09230
58199560   =   yrday
fracday
Element set:     913
Inclination:       51
6427  deg
RA of node:       346
5304  deg
Eccentricity:     
0008104     
Arg of perigee:   348
3926  deg
Mean anomaly:      11
7048  deg
Mean motion:   15
73657724  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1578
Checksum:              320


Coasting Arc #15 (Orbit 1592)
---------------------------------------

Vector Time (GMT): 2009/231/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          -9342
58                 A    =         6721506
97  meter
 Y    =       -4325672
18  meter          E    =           
0014029
 Z    =       -5154566
83                 I    =           51
51694
 XDOT =       7443
011922                 Wp   =           65
79365
 YDOT =      -1489
795643  meter/sec      RA   =          341
18906  deg
 ZDOT =       1245
042841                 TA   =          216
09227
                                          MA   =          216
18705
                                          Ha   =            191
988  n
mi
                                          Hp   =            183
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -30651
52                 X    =           64067
91
 Y    =      -14191837
85  feet           Y    =        -4325366
09  meter
 Z    =      -16911308
51                 Z    =        -5154434
00
 XDOT =      24419
330452                 XDOT =        7453
069838
 YDOT =      -4887
780980  feet/sec       YDOT =       -1406
507302  meter/sec
 ZDOT =       4084
786224                 ZDOT =        1281
224572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6120993
29                 X    =        -1865678
75
 Y    =       12804456
26  feet           Y    =         3902798
27  meter
 Z    =      -16910969
74                 Z    =        -5154463
58
 XDOT =     -23212
854032                 XDOT =       -7075
277909
 YDOT =      -5549
885937  feet/sec       YDOT =       -1691
605233  meter/sec
 ZDOT =       4227
044790                 ZDOT =        1288
403252


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   09231
53454088  
00010596  00000-0  82463-4 0  9147
2 25544  51
6428 341
6424 0008167 351
9640   8
1391 15
73697079 15936


Satellite: ISS
Catalog Number: 25544
Epoch time:      09231
53454088   =   yrday
fracday
Element set:     914
Inclination:       51
6428  deg
RA of node:       341
6424  deg
Eccentricity:     
0008167     
Arg of perigee:   351
9640  deg
Mean anomaly:       8
1391  deg
Mean motion:   15
73697079  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1593
Checksum:              323

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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