Date: August 4th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8794 11 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 1340)
---------------------------------------

Vector Time (GMT): 2009/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2680490
88                 A    =         6733616
90  meter
 Y    =       -6154581
16  meter          E    =           
0005859
 Z    =        -474023
38                 I    =           51
95883
 XDOT =       4530
320616                 Wp   =          181
27947
 YDOT =      -1508
312143  meter/sec      RA   =           63
29829  deg
 ZDOT =      -6038
713715                 TA   =            3
85175
                                          MA   =            3
84724
                                          Ha   =            189
683  n
mi
                                          Hp   =            187
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8794261
41                 X    =        -2609167
40
 Y    =      -20192195
41  feet           Y    =        -6184157
14  meter
 Z    =       -1555194
82                 Z    =         -486872
43
 XDOT =      14863
256613                 XDOT =        4576
184537
 YDOT =      -4948
530652  feet/sec       YDOT =       -1457
394311  meter/sec
 ZDOT =     -19812
052871                 ZDOT =       -6016
594605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9324858
03                 X    =        -2842216
73
 Y    =       19948688
91  feet           Y    =         6080360
38  meter
 Z    =       -1606005
54                 Z    =         -489510
49
 XDOT =     -12167
611368                 XDOT =       -3708
687945
 YDOT =      -7274
561224  feet/sec       YDOT =       -2217
286261  meter/sec
 ZDOT =     -19725
116378                 ZDOT =       -6012
215472


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   09215
53082382  
00010596  00000-0  82463-4 0  9008
2 25544  51
6405  63
7812 0007945 288
7931  71
2370 15
73456696 13414


Satellite: ISS
Catalog Number: 25544
Epoch time:      09215
53082382   =   yrday
fracday
Element set:     900
Inclination:       51
6405  deg
RA of node:        63
7812  deg
Eccentricity:     
0007945     
Arg of perigee:   288
7931  deg
Mean anomaly:      71
2370  deg
Mean motion:   15
73456696  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1341
Checksum:              312


Coasting Arc #2 (Orbit 1356)
---------------------------------------

Vector Time (GMT): 2009/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3734953
48                 A    =         6721652
83  meter
 Y    =        1835915
70  meter          E    =           
0006217
 Z    =        5282636
00                 I    =           51
90346
 XDOT =      -3806
711498                 Wp   =          308
36628
 YDOT =      -6679
453263  meter/sec      RA   =           58
17816  deg
 ZDOT =       -366
590871                 TA   =          145
12387
                                          MA   =          145
08312
                                          Ha   =            189
945  n
mi
                                          Hp   =            187
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12253784
40                 X    =        -3780866
96
 Y    =        6023345
48  feet           Y    =         1793892
02  meter
 Z    =       17331482
93                 Z    =         5264380
64
 XDOT =     -12489
210952                 XDOT =       -3729
956993
 YDOT =     -21914
216743  feet/sec       YDOT =       -6721
592949  meter/sec
 ZDOT =      -1202
725955                 ZDOT =        -384
897715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12780581
18                 X    =         3895521
14
 Y    =        5057056
22  feet           Y    =         1541390
74  meter
 Z    =       17259755
23                 Z    =         5260773
39
 XDOT =      -7389
003291                 XDOT =       -2252
168203
 YDOT =      23064
923998  feet/sec       YDOT =        7030
188834  meter/sec
 ZDOT =      -1275
028822                 ZDOT =        -388
628785


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   09216
54699042  
00010596  00000-0  82463-4 0  9018
2 25544  51
6399  58
5655 0007960 293
0066  67
0257 15
73472226 13579


Satellite: ISS
Catalog Number: 25544
Epoch time:      09216
54699042   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:        58
5655  deg
Eccentricity:     
0007960     
Arg of perigee:   293
0066  deg
Mean anomaly:      67
0257  deg
Mean motion:   15
73472226  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1357
Checksum:              327


Coasting Arc #3 (Orbit 1372)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3933441
81                 A    =         6733597
40  meter
 Y    =        5452503
52  meter          E    =           
0012382
 Z    =         168322
96                 I    =           51
92596
 XDOT =      -3943
339337                 Wp   =            9
38331
 YDOT =       2656
072862  meter/sec      RA   =           53
06950  deg
 ZDOT =       6061
076331                 TA   =          352
43862
                                          MA   =          352
45728
                                          Ha   =            190
085  n
mi
                                          Hp   =            187
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12904992
80                 X    =         3871360
97
 Y    =       17888791
08  feet           Y    =         5496142
45  meter
 Z    =         552240
69                 Z    =          187280
85
 XDOT =     -12937
465017                 XDOT =       -4002
189880
 YDOT =       8714
149809  feet/sec       YDOT =        2611
646592  meter/sec
 ZDOT =      19885
421033                 ZDOT =        6041
777280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4131018
29                 X    =         1259134
37
 Y    =      -21665505
96  feet           Y    =        -6603646
22  meter
 Z    =         627052
47                 Z    =          191125
59
 XDOT =      13720
737196                 XDOT =        4182
080697
 YDOT =       3193
695904  feet/sec       YDOT =         973
438511  meter/sec
 ZDOT =      19809
621863                 ZDOT =        6037
972744


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
56314661  
00010596  00000-0  82463-4 0  9023
2 25544  51
6387  53
3494 0008034 297
0243  63
0100 15
73497107 13730


Satellite: ISS
Catalog Number: 25544
Epoch time:      09217
56314661   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:        53
3494  deg
Eccentricity:     
0008034     
Arg of perigee:   297
0243  deg
Mean anomaly:      63
0100  deg
Mean motion:   15
73497107  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1373
Checksum:              293


Coasting Arc #4 (Orbit 1387)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3103391
74                 A    =         6721450
32  meter
 Y    =       -2761304
41  meter          E    =           
0009115
 Z    =       -5291136
58                 I    =           51
86555
 XDOT =       5137
228269                 Wp   =           64
29692
 YDOT =       5728
331756  meter/sec      RA   =           47
95280  deg
 ZDOT =         27
559083                 TA   =          205
94112
                                          MA   =          205
98683
                                          Ha   =            190
219  n
mi
                                          Hp   =            187
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10181731
44                 X    =         3159741
30
 Y    =       -9059397
68  feet           Y    =        -2726285
09  meter
 Z    =      -17359371
97                 Z    =        -5275923
92
 XDOT =      16854
423455                 XDOT =        5072
657400
 YDOT =      18793
739357  feet/sec       YDOT =        5785
418219  meter/sec
 ZDOT =         90
416940                 ZDOT =          52
358702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13667111
96                 X    =        -4165735
72
 Y    =       -1010069
53  feet           Y    =         -307869
19  meter
 Z    =      -17299651
64                 Z    =        -5272933
82
 XDOT =       1566
069481                 XDOT =         477
337978
 YDOT =     -24193
858392  feet/sec       YDOT =       -7374
288038  meter/sec
 ZDOT =        188
221082                 ZDOT =          57
369786


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
51578366  
00010596  00000-0  82463-4 0  9034
2 25544  51
6379  48
4598 0007918 300
6166  59
4215 15
73526136 13883


Satellite: ISS
Catalog Number: 25544
Epoch time:      09218
51578366   =   yrday
fracday
Element set:     903
Inclination:       51
6379  deg
RA of node:        48
4598  deg
Eccentricity:     
0007918     
Arg of perigee:   300
6166  deg
Mean anomaly:      59
4215  deg
Mean motion:   15
73526136  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1388
Checksum:              337


Coasting Arc #5 (Orbit 1403)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4992885
76                 A    =         6733363
74  meter
 Y    =       -4512399
96  meter          E    =           
0004525
 Z    =         109413
60                 I    =           51
88598
 XDOT =       3111
564396                 Wp   =          148
87428
 YDOT =      -3592
286976  meter/sec      RA   =           42
83699  deg
 ZDOT =      -6054
580022                 TA   =           29
94184
                                          MA   =           29
91597
                                          Ha   =            190
368  n
mi
                                          Hp   =            186
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16380858
79                 X    =        -4942587
75
 Y    =      -14804461
81  feet           Y    =        -4567952
11  meter
 Z    =         358968
49                 Z    =           85280
63
 XDOT =      10208
544605                 XDOT =        3180
914195
 YDOT =     -11785
718424  feet/sec       YDOT =       -3557
103654  meter/sec
 ZDOT =     -19864
107683                 ZDOT =       -6039
296021

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1260889
36                 X    =          384319
08
 Y    =       22044818
64  feet           Y    =         6719260
72  meter
 Z    =         263840
71                 Z    =           80418
65
 XDOT =     -14019
508881                 XDOT =       -4273
146307
 YDOT =       1044
603324  feet/sec       YDOT =         318
395093  meter/sec
 ZDOT =     -19804
143938                 ZDOT =       -6036
303072


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
53191882  
00010596  00000-0  82463-4 0  9042
2 25544  51
6385  43
2449 0008134 305
6489  54
3916 15
73580661 14046


Satellite: ISS
Catalog Number: 25544
Epoch time:      09219
53191882   =   yrday
fracday
Element set:     904
Inclination:       51
6385  deg
RA of node:        43
2449  deg
Eccentricity:     
0008134     
Arg of perigee:   305
6489  deg
Mean anomaly:      54
3916  deg
Mean motion:   15
73580661  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1404
Checksum:              318


Coasting Arc #6 (Orbit 1419)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2300004
05                 A    =         6721524
77  meter
 Y    =        3469876
23  meter          E    =           
0005789
 Z    =        5280227
23                 I    =           51
82201
 XDOT =      -6215
565516                 Wp   =          319
72403
 YDOT =      -4533
287860  meter/sec      RA   =           37
72199  deg
 ZDOT =        276
094582                 TA   =          127
68720
                                          MA   =          127
63469
                                          Ha   =            190
634  n
mi
                                          Hp   =            186
534

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7545945
05                 X    =        -2364283
85
 Y    =       11384108
37  feet           Y    =         3443796
72  meter
 Z    =       17323580
16                 Z    =         5268897
93
 XDOT =     -20392
275316                 XDOT =       -6165
752758
 YDOT =     -14872
991667  feet/sec       YDOT =       -4602
515448  meter/sec
 ZDOT =        905
822118                 ZDOT =         246
020742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13390361
30                 X    =         4081382
12
 Y    =       -2962128
72  feet           Y    =         -902856
83  meter
 Z    =       17279168
31                 Z    =         5266690
50
 XDOT =       4281
999533                 XDOT =        1305
153458
 YDOT =      23863
434362  feet/sec       YDOT =        7273
574794  meter/sec
 ZDOT =        787
327564                 ZDOT =         239
977442


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
54804733  
00010596  00000-0  82463-4 0  9052
2 25544  51
6379  38
0286 0007863 308
9577  51
0885 15
73505619 14209


Satellite: ISS
Catalog Number: 25544
Epoch time:      09220
54804733   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:        38
0286  deg
Eccentricity:     
0007863     
Arg of perigee:   308
9577  deg
Mean anomaly:      51
0885  deg
Mean motion:   15
73505619  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1420
Checksum:              321


Coasting Arc #7 (Orbit 1434)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5809014
78                 A    =         6733356
26  meter
 Y    =        3366076
92  meter          E    =           
0013901
 Z    =        -373619
11                 I    =           51
83850
 XDOT =      -2101
340751                 Wp   =            7
60389
 YDOT =       4292
801160  meter/sec      RA   =           32
59688  deg
 ZDOT =       6042
809812                 TA   =          348
34381
                                          MA   =          348
37596
                                          Ha   =            190
640  n
mi
                                          Hp   =            186
262

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19058447
46                 X    =         5772757
95
 Y    =       11043559
46  feet           Y    =         3430834
02  meter
 Z    =       -1225784
49                 Z    =         -345487
28
 XDOT =      -6894
162570                 XDOT =       -2178
541957
 YDOT =      14083
993308  feet/sec       YDOT =        4268
871024  meter/sec
 ZDOT =      19825
491509                 ZDOT =        6032
414135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6539617
50                 X    =        -1993275
41
 Y    =      -21039899
83  feet           Y    =        -6412961
47  meter
 Z    =       -1114984
75                 Z    =         -339847
35
 XDOT =      13163
845787                 XDOT =        4012
340196
 YDOT =      -5132
622168  feet/sec       YDOT =       -1564
423237  meter/sec
 ZDOT =      19784
788471                 ZDOT =        6030
403526


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
50065425  
00010596  00000-0  82463-4 0  9067
2 25544  51
6384  33
1389 0007866 311
8757  48
1734 15
73568559 14359


Satellite: ISS
Catalog Number: 25544
Epoch time:      09221
50065425   =   yrday
fracday
Element set:     906
Inclination:       51
6384  deg
RA of node:        33
1389  deg
Eccentricity:     
0007866     
Arg of perigee:   311
8757  deg
Mean anomaly:      48
1734  deg
Mean motion:   15
73568559  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1435
Checksum:              326


Coasting Arc #8 (Orbit 1450)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1351976
80                 A    =         6721340
81  meter
 Y    =       -3968779
58  meter          E    =           
0011651
 Z    =       -5261991
33                 I    =           51
77305
 XDOT =       7000
166672                 Wp   =           54
60689
 YDOT =       3140
589219  meter/sec      RA   =           27
48517  deg
 ZDOT =       -564
436276                 TA   =          210
00067
                                          MA   =          210
06748
                                          Ha   =            190
745  n
mi
                                          Hp   =            186
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4435619
42                 X    =         1421817
52
 Y    =      -13020930
38  feet           Y    =        -3953270
44  meter
 Z    =      -17263751
08                 Z    =        -5255253
86
 XDOT =      22966
426088                 XDOT =        6967
269707
 YDOT =      10303
770405  feet/sec       YDOT =        3218
685260  meter/sec
 ZDOT =      -1851
825053                 ZDOT =        -530
509580

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12044982
29                 X    =        -3671310
60
 Y    =        6711641
19  feet           Y    =         2045708
23  meter
 Z    =      -17237422
18                 Z    =        -5253966
28
 XDOT =      -9824
993858                 XDOT =       -2994
658128
 YDOT =     -22093
695624  feet/sec       YDOT =       -6734
158426  meter/sec
 ZDOT =      -1718
248563                 ZDOT =        -523
722162


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
51675987  
00010596  00000-0  82463-4 0  9070
2 25544  51
6389  27
9244 0007747 316
6159  43
4394 15
73597051 14519


Satellite: ISS
Catalog Number: 25544
Epoch time:      09222
51675987   =   yrday
fracday
Element set:     907
Inclination:       51
6389  deg
RA of node:        27
9244  deg
Eccentricity:     
0007747     
Arg of perigee:   316
6159  deg
Mean anomaly:      43
4394  deg
Mean motion:   15
73597051  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1451
Checksum:              339


Coasting Arc #9 (Orbit 1466)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6365144
94                 A    =         6733057
94  meter
 Y    =       -2105656
23  meter          E    =           
0005536
 Z    =         600928
56                 I    =           51
78567
 XDOT =        986
487993                 Wp   =          112
13952
 YDOT =      -4708
436275  meter/sec      RA   =           22
35147  deg
 ZDOT =      -6007
452381                 TA   =           61
33624
                                          MA   =           61
28059
                                          Ha   =            190
910  n
mi
                                          Hp   =            185
754

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20883021
44                 X    =        -6344045
25
 Y    =       -6908320
96  feet           Y    =        -2176717
05  meter
 Z    =        1971550
41                 Z    =          570058
00
 XDOT =       3236
509163                 XDOT =        1068
248249
 YDOT =     -15447
625574  feet/sec       YDOT =       -4696
947539  meter/sec
 ZDOT =     -19709
489438                 ZDOT =       -6002
461522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11341954
09                 X    =         3457027
61
 Y    =       18858682
50  feet           Y    =         5748126
43  meter
 Z    =        1850044
82                 Z    =          563893
66
 XDOT =     -11235
882391                 XDOT =       -3424
696953
 YDOT =       8703
427070  feet/sec       YDOT =        2652
804571  meter/sec
 ZDOT =     -19690
059394                 ZDOT =       -6001
530103


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
53285274  
00010596  00000-0  82463-4 0  9080
2 25544  51
6387  22
7083 0008061 320
5236  39
5339 15
73640413 14674


Satellite: ISS
Catalog Number: 25544
Epoch time:      09223
53285274   =   yrday
fracday
Element set:     908
Inclination:       51
6387  deg
RA of node:        22
7083  deg
Eccentricity:     
0008061     
Arg of perigee:   320
5236  deg
Mean anomaly:      39
5339  deg
Mean motion:   15
73640413  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1467
Checksum:              304


Coasting Arc #10 (Orbit 1482)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -362951
52                 A    =         6721431
82  meter
 Y    =        4208535
87  meter          E    =           
0005218
 Z    =        5229211
23                 I    =           51
71853
 XDOT =      -7477
349642                 Wp   =          339
38992
 YDOT =      -1648
548080  meter/sec      RA   =           17
23910  deg
 ZDOT =        812
816490                 TA   =          102
91084
                                          MA   =          102
85255
                                          Ha   =            191
132  n
mi
                                          Hp   =            185
541

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1190785
83                 X    =         -435387
67
 Y    =       13807532
40  feet           Y    =         4204071
95  meter
 Z    =       17156204
82                 Z    =         5227272
21
 XDOT =     -24531
987016                 XDOT =       -7462
308074
 YDOT =      -5408
622311  feet/sec       YDOT =       -1732
080117  meter/sec
 ZDOT =       2666
720769                 ZDOT =         776
528021

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9812220
67                 X    =         2990764
86
 Y    =       -9800095
60  feet           Y    =        -2987069
14  meter
 Z    =       17148753
23                 Z    =         5226939
98
 XDOT =      14718
677896                 XDOT =        4486
253023
 YDOT =      19124
482387  feet/sec       YDOT =        5829
142232  meter/sec
 ZDOT =       2523
930569                 ZDOT =         769
294037


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
54893849  
00010596  00000-0  82463-4 0  9096
2 25544  51
6392  17
4929 0007877 324
7899  35
2743 15
73598905 14833


Satellite: ISS
Catalog Number: 25544
Epoch time:      09224
54893849   =   yrday
fracday
Element set:     909
Inclination:       51
6392  deg
RA of node:        17
4929  deg
Eccentricity:     
0007877     
Arg of perigee:   324
7899  deg
Mean anomaly:      35
2743  deg
Mean motion:   15
73598905  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1483
Checksum:              369


Coasting Arc #11 (Orbit 1497)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6629832
73                 A    =         6732950
09  meter
 Y    =         759053
23  meter          E    =           
0014915
 Z    =        -820581
97                 I    =           51
73008
 XDOT =        179
603985                 Wp   =            9
22474
 YDOT =       4860
243280  meter/sec      RA   =           12
09837  deg
 ZDOT =       5976
230024                 TA   =          341
83203
                                          MA   =          341
88527
                                          Ha   =            191
201  n
mi
                                          Hp   =            185
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21751419
72                 X    =         6624838
36
 Y    =        2490332
13  feet           Y    =          833164
03  meter
 Z    =       -2692198
05                 Z    =         -788386
33
 XDOT =        589
251920                 XDOT =          96
211119
 YDOT =      15945
680052  feet/sec       YDOT =        4861
785117  meter/sec
 ZDOT =      19607
053883                 ZDOT =        5976
900244

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15427739
08                 X    =        -4702374
87
 Y    =      -15555603
39  feet           Y    =        -4741347
91  meter
 Z    =       -2565543
63                 Z    =         -781977
70
 XDOT =       8467
189627                 XDOT =        2580
799398
 YDOT =     -11615
148633  feet/sec       YDOT =       -3540
297303  meter/sec
 ZDOT =      19609
886818                 ZDOT =        5977
093502


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
50150589  
00010596  00000-0  82463-4 0  9102
2 25544  51
6405  12
6041 0007812 328
1411  31
9278 15
73635393 14982


Satellite: ISS
Catalog Number: 25544
Epoch time:      09225
50150589   =   yrday
fracday
Element set:     910
Inclination:       51
6405  deg
RA of node:        12
6041  deg
Eccentricity:     
0007812     
Arg of perigee:   328
1411  deg
Mean anomaly:      31
9278  deg
Mean motion:   15
73635393  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1498
Checksum:              294


Coasting Arc #12 (Orbit 1513)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -661330
46                 A    =         6721371
30  meter
 Y    =       -4222511
02  meter          E    =           
0013996
 Z    =       -5198003
34                 I    =           51
66224
 XDOT =       7619
597982                 Wp   =           49
83020
 YDOT =        101
419239  meter/sec      RA   =            6
98730  deg
 ZDOT =      -1044
800973                 TA   =          210
15667
                                          MA   =          210
23732
                                          Ha   =            191
277  n
mi
                                          Hp   =            185
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2169719
36                 X    =         -588813
56
 Y    =      -13853382
62  feet           Y    =        -4229500
55  meter
 Z    =      -17053816
73                 Z    =        -5201040
25
 XDOT =      24998
681042                 XDOT =        7622
973032
 YDOT =        332
740284  feet/sec       YDOT =         186
645002  meter/sec
 ZDOT =      -3427
824714                 ZDOT =       -1007
776829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6838907
53                 X    =        -2084499
02
 Y    =       12224564
50  feet           Y    =         3726047
26  meter
 Z    =      -17065928
74                 Z    =        -5201695
08
 XDOT =     -18693
574911                 XDOT =       -5697
801633
 YDOT =     -15072
088611  feet/sec       YDOT =       -4593
972609  meter/sec
 ZDOT =      -3282
205364                 ZDOT =       -1000
416195


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
51756777  
00010596  00000-0  82463-4 0  9116
2 25544  51
6407   7
3900 0007881 332
6276  27
4471 15
73671879 15147


Satellite: ISS
Catalog Number: 25544
Epoch time:      09226
51756777   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:         7
3900  deg
Eccentricity:     
0007881     
Arg of perigee:   332
6276  deg
Mean anomaly:      27
4471  deg
Mean motion:   15
73671879  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1514
Checksum:              323


Coasting Arc #13 (Orbit 1529)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6632834
54                 A    =         6732698
99  meter
 Y    =         573463
86  meter          E    =           
0007979
 Z    =         993906
09                 I    =           51
67016
 XDOT =      -1303
415570                 Wp   =           93
54215
 YDOT =      -4731
122603  meter/sec      RA   =            1
83690  deg
 ZDOT =      -5928
308095                 TA   =           75
60868
                                          MA   =           75
52013
                                          Ha   =            191
425  n
mi
                                          Hp   =            184
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21761268
17                 X    =        -6643582
33
 Y    =        1881443
10  feet           Y    =          499231
43  meter
 Z    =        3260846
76                 Z    =          961657
92
 XDOT =      -4276
297803                 XDOT =       -1221
615997
 YDOT =     -15522
055783  feet/sec       YDOT =       -4745
240264  meter/sec
 ZDOT =     -19449
829708                 ZDOT =       -5934
441785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18579275
90                 X    =         5662963
29
 Y    =       11520159
63  feet           Y    =         3511344
65  meter
 Z    =        3134034
35                 Z    =          955253
67
 XDOT =      -5108
778447                 XDOT =       -1557
155671
 YDOT =      13574
543848  feet/sec       YDOT =        4137
520965  meter/sec
 ZDOT =     -19474
139924                 ZDOT =       -5935
717849


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
53361823  
00010596  00000-0  82463-4 0  9124
2 25544  51
6403   2
1733 0007956 335
8013  24
2776 15
73675993 15309


Satellite: ISS
Catalog Number: 25544
Epoch time:      09227
53361823   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:         2
1733  deg
Eccentricity:     
0007956     
Arg of perigee:   335
8013  deg
Mean anomaly:      24
2776  deg
Mean motion:   15
73675993  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1530
Checksum:              303


Coasting Arc #14 (Orbit 1545)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1604356
43                 A    =         6721366
48  meter
 Y    =        4000790
50  meter          E    =           
0005275
 Z    =        5155898
98                 I    =           51
60384
 XDOT =      -7470
410634                 Wp   =            4
24801
 YDOT =       1409
038040  meter/sec      RA   =          356
72325  deg
 ZDOT =       1236
287145                 TA   =           73
96278
                                          MA   =           73
90470
                                          Ha   =            191
497  n
mi
                                          Hp   =            184
583

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5263636
59                 X    =         1534453
53
 Y    =       13125953
10  feet           Y    =         4018340
04  meter
 Z    =       16915679
05                 Z    =         5163523
43
 XDOT =     -24509
221241                 XDOT =       -7491
617113
 YDOT =       4622
828215  feet/sec       YDOT =        1325
380840  meter/sec
 ZDOT =       4056
060187                 ZDOT =        1199
944918

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3477886
11                 X    =         1060059
68
 Y    =      -13670407
02  feet           Y    =        -4166740
06  meter
 Z    =       16945825
23                 Z    =         5165087
53
 XDOT =      21613
408741                 XDOT =        6587
766984
 YDOT =      10328
771714  feet/sec       YDOT =        3148
209618  meter/sec
 ZDOT =       3913
172915                 ZDOT =        1192
735105


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
54965688  
00010596  00000-0  82463-4 0  9136
2 25544  51
6415 356
9578 0008055 339
3607  20
7229 15
73716871 15460


Satellite: ISS
Catalog Number: 25544
Epoch time:      09228
54965688   =   yrday
fracday
Element set:     913
Inclination:       51
6415  deg
RA of node:       356
9578  deg
Eccentricity:     
0008055     
Arg of perigee:   339
3607  deg
Mean anomaly:      20
7229  deg
Mean motion:   15
73716871  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1546
Checksum:              346


Coasting Arc #15 (Orbit 1560)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6349359
62                 A    =         6732483
82  meter
 Y    =       -1876361
70  meter          E    =           
0015680
 Z    =       -1167459
58                 I    =           51
61194
 XDOT =       2368
035594                 Wp   =           12
67604
 YDOT =       4366
685772  meter/sec      RA   =          351
56698  deg
 ZDOT =       5890
497291                 TA   =          334
52410
                                          MA   =          334
60131
                                          Ha   =            191
760  n
mi
                                          Hp   =            184
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20831232
36                 X    =         6375540
74
 Y    =       -6156042
32  feet           Y    =        -1805212
95  meter
 Z    =       -3830247
98                 Z    =        -1136551
47
 XDOT =       7769
145650                 XDOT =        2290
416084
 YDOT =      14326
396890  feet/sec       YDOT =        4392
732071  meter/sec
 ZDOT =      19325
778515                 ZDOT =        5901
812828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20640857
63                 X    =        -6291333
40
 Y    =       -6834330
57  feet           Y    =        -2083103
96  meter
 Z    =       -3708749
18                 Z    =        -1130426
75
 XDOT =       1381
783937                 XDOT =         421
167744
 YDOT =     -14629
938585  feet/sec       YDOT =       -4459
205281  meter/sec
 ZDOT =      19370
461282                 ZDOT =        5904
116599


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
50218427  
00010596  00000-0  82463-4 0  9146
2 25544  51
6422 352
0689 0008109 343
9520  16
1385 15
73697015 15610


Satellite: ISS
Catalog Number: 25544
Epoch time:      09229
50218427   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       352
0689  deg
Eccentricity:     
0008109     
Arg of perigee:   343
9520  deg
Mean anomaly:      16
1385  deg
Mean motion:   15
73697015  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1561
Checksum:              306

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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