Date: August 12th 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 1450)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1316147
76                 A    =         6721438
38  meter
 Y    =       -3984886
51  meter          E    =           
0011682
 Z    =       -5259004
65                 I    =           51
77276
 XDOT =       7008
874421                 Wp   =           53
77006
 YDOT =       3114
388572  meter/sec      RA   =           27
49043  deg
 ZDOT =       -599
933317                 TA   =          210
49876
                                          MA   =          210
56675
                                          Ha   =            190
821  n
mi
                                          Hp   =            186
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4318070
09                 X    =         1386156
75
 Y    =      -13073774
64  feet           Y    =        -3969777
09  meter
 Z    =      -17253952
25                 Z    =        -5252440
83
 XDOT =      22994
994821                 XDOT =        6976
442227
 YDOT =      10217
810277  feet/sec       YDOT =        3192
584587  meter/sec
 ZDOT =      -1968
285161                 ZDOT =        -565
963191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11992259
20                 X    =        -3655240
61
 Y    =        6829299
89  feet           Y    =         2081570
60  meter
 Z    =      -17228307
04                 Z    =        -5251187
99
 XDOT =      -9895
408878                 XDOT =       -3016
120626
 YDOT =     -22052
767143  feet/sec       YDOT =       -6721
683425  meter/sec
 ZDOT =      -1834
538970                 ZDOT =        -559
167478


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
51681966  
00010596  00000-0  82463-4 0  9007
2 25544  51
6385  27
9292 0007843 316
8001  43
2545 15
73567394 14516


Satellite: ISS
Catalog Number: 25544
Epoch time:      09222
51681966   =   yrday
fracday
Element set:     900
Inclination:       51
6385  deg
RA of node:        27
9292  deg
Eccentricity:     
0007843     
Arg of perigee:   316
8001  deg
Mean anomaly:      43
2545  deg
Mean motion:   15
73567394  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1451
Checksum:              313


Coasting Arc #2 (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    =       -6371744
75                 A    =         6733135
73  meter
 Y    =       -2073612
05  meter          E    =           
0005551
 Z    =         642453
80                 I    =           51
78524
 XDOT =        929
280194                 Wp   =          110
66922
 YDOT =      -4727
214823  meter/sec      RA   =           22
35623  deg
 ZDOT =      -6001
688253                 TA   =           62
35363
                                          MA   =           62
29730
                                          Ha   =            190
992  n
mi
                                          Hp   =            185
800

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20904674
37                 X    =        -6351204
61
 Y    =       -6803189
15  feet           Y    =        -2144749
81  meter
 Z    =        2107788
05                 Z    =          611549
81
 XDOT =       3048
819535                 XDOT =        1011
226686
 YDOT =     -15509
234982  feet/sec       YDOT =       -4716
364776  meter/sec
 ZDOT =     -19690
578259                 ZDOT =       -5996
974857

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11427507
09                 X    =         3483104
16
 Y    =       18793585
18  feet           Y    =         5728284
76  meter
 Z    =        1986152
36                 Z    =          605379
24
 XDOT =     -11138
373324                 XDOT =       -3394
976189
 YDOT =       8866
324281  feet/sec       YDOT =        2702
455641  meter/sec
 ZDOT =     -19672
240294                 ZDOT =       -5996
098842


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
53293331  
00010596  00000-0  82463-4 0  9016
2 25544  51
6383  22
7133 0008151 320
6668  39
3902 15
73605694 14672


Satellite: ISS
Catalog Number: 25544
Epoch time:      09223
53293331   =   yrday
fracday
Element set:     901
Inclination:       51
6383  deg
RA of node:        22
7133  deg
Eccentricity:     
0008151     
Arg of perigee:   320
6668  deg
Mean anomaly:      39
3902  deg
Mean motion:   15
73605694  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1467
Checksum:              298


Coasting Arc #3 (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    =        -296791
37                 A    =         6721570
11  meter
 Y    =        4223066
07  meter          E    =           
0005182
 Z    =        5221779
80                 I    =           51
71829
 XDOT =      -7480
975984                 Wp   =          339
54290
 YDOT =      -1600
052497  meter/sec      RA   =           17
24500  deg
 ZDOT =        873
851861                 TA   =          102
17340
                                          MA   =          102
11535
                                          Ha   =            191
216  n
mi
                                          Hp   =            185
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -973724
95                 X    =         -369358
81
 Y    =       13855203
65  feet           Y    =         4219341
26  meter
 Z    =       17131823
48                 Z    =         5220161
86
 XDOT =     -24543
884463                 XDOT =       -7466
772931
 YDOT =      -5249
516067  feet/sec       YDOT =       -1683
629777  meter/sec
 ZDOT =       2866
968048                 ZDOT =         837
543740

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9675544
10                 X    =         2949105
84
 Y    =       -9975502
26  feet           Y    =        -3040533
09  meter
 Z    =       17125635
33                 Z    =         5219893
65
 XDOT =      14817
562608                 XDOT =        4516
393083
 YDOT =      19020
365432  feet/sec       YDOT =        5797
407384  meter/sec
 ZDOT =       2724
102560                 ZDOT =         830
306460


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
54904269  
00010596  00000-0  82463-4 0  9028
2 25544  51
6387  17
4979 0007968 324
9175  35
1462 15
73561725 14839


Satellite: ISS
Catalog Number: 25544
Epoch time:      09224
54904269   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:        17
4979  deg
Eccentricity:     
0007968     
Arg of perigee:   324
9175  deg
Mean anomaly:      35
1462  deg
Mean motion:   15
73561725  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1483
Checksum:              337


Coasting Arc #4 (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    =        6627292
06                 A    =         6733026
79  meter
 Y    =         705345
28  meter          E    =           
0014870
 Z    =        -887196
90                 I    =           51
72956
 XDOT =        276
306645                 Wp   =            8
51036
 YDOT =       4871
026686  meter/sec      RA   =           12
10341  deg
 ZDOT =       5963
648046                 TA   =          341
81377
                                          MA   =          341
86690
                                          Ha   =            191
298  n
mi
                                          Hp   =            185
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21743084
19                 X    =         6623222
05
 Y    =        2314124
93  feet           Y    =          779432
84  meter
 Z    =       -2910750
99                 Z    =         -855011
36
 XDOT =        906
517864                 XDOT =         192
847131
 YDOT =      15981
058681  feet/sec       YDOT =        4873
649537  meter/sec
 ZDOT =      19565
774430                 ZDOT =        5964
787886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15532425
67                 X    =        -4734283
34
 Y    =      -15413684
88  feet           Y    =        -4698091
15  meter
 Z    =       -2784138
46                 Z    =         -848605
40
 XDOT =       8251
909332                 XDOT =        2515
181964
 YDOT =     -11833
678246  feet/sec       YDOT =       -3606
905129  meter/sec
 ZDOT =      19570
454795                 ZDOT =        5965
074621


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
50163502  
00010596  00000-0  82463-4 0  9033
2 25544  51
6401  12
6092 0007895 328
3045  31
7641 15
73591817 14984


Satellite: ISS
Catalog Number: 25544
Epoch time:      09225
50163502   =   yrday
fracday
Element set:     903
Inclination:       51
6401  deg
RA of node:        12
6092  deg
Eccentricity:     
0007895     
Arg of perigee:   328
3045  deg
Mean anomaly:      31
7641  deg
Mean motion:   15
73591817  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1498
Checksum:              297


Coasting Arc #5 (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    =        -765033
40                 A    =         6721573
79  meter
 Y    =       -4223569
13  meter          E    =           
0014040
 Z    =       -5183164
09                 I    =           51
66210
 XDOT =       7606
810496                 Wp   =           48
69514
 YDOT =         26
851315  meter/sec      RA   =            6
99402  deg
 ZDOT =      -1137
540240                 TA   =          210
39559
                                          MA   =          210
47707
                                          Ha   =            191
378  n
mi
                                          Hp   =            185
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2509952
09                 X    =         -692569
04
 Y    =      -13856854
08  feet           Y    =        -4231718
62  meter
 Z    =      -17005131
52                 Z    =        -5186704
91
 XDOT =      24956
727349                 XDOT =        7611
470838
 YDOT =         88
094867  feet/sec       YDOT =         111
941276  meter/sec
 ZDOT =      -3732
087403                 ZDOT =       -1100
575101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6571698
89                 X    =        -2003053
82
 Y    =       12435654
42  feet           Y    =         3790387
47  meter
 Z    =      -17019225
47                 Z    =        -5187459
92
 XDOT =     -18796
091857                 XDOT =       -5729
048798
 YDOT =     -14873
478187  feet/sec       YDOT =       -4533
436152  meter/sec
 ZDOT =      -3586
703074                 ZDOT =       -1093
227097


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
51772629  
00010596  00000-0  82463-4 0  9042
2 25544  51
6403   7
3953 0007961 332
7717  27
3027 15
73623638 15147


Satellite: ISS
Catalog Number: 25544
Epoch time:      09226
51772629   =   yrday
fracday
Element set:     904
Inclination:       51
6403  deg
RA of node:         7
3953  deg
Eccentricity:     
0007961     
Arg of perigee:   332
7717  deg
Mean anomaly:      27
3027  deg
Mean motion:   15
73623638  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1514
Checksum:              309


Coasting Arc #6 (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    =       -6610547
86                 A    =         6732767
04  meter
 Y    =         650363
03  meter          E    =           
0008184
 Z    =        1090981
36                 I    =           51
66950
 XDOT =      -1445
067723                 Wp   =           91
75133
 YDOT =      -4718
069530  meter/sec      RA   =            1
84231  deg
 ZDOT =      -5905
732955                 TA   =           76
32509
                                          MA   =           76
23398
                                          Ha   =            191
532  n
mi
                                          Hp   =            184
962

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21688149
15                 X    =        -6622628
78
 Y    =        2133736
98  feet           Y    =          576372
36  meter
 Z    =        3579335
18                 Z    =         1058838
22
 XDOT =      -4741
035838                 XDOT =       -1363
513249
 YDOT =     -15479
230743  feet/sec       YDOT =       -4733
772602  meter/sec
 ZDOT =     -19375
764289                 ZDOT =       -5912
555381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18673083
83                 X    =         5691555
95
 Y    =       11275346
59  feet           Y    =         3436725
64  meter
 Z    =        3452938
90                 Z    =         1052455
78
 XDOT =      -4728
245148                 XDOT =       -1441
169121
 YDOT =      13811
626195  feet/sec       YDOT =        4209
783664  meter/sec
 ZDOT =     -19402
782856                 ZDOT =       -5913
968215


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
53380917  
00010596  00000-0  82463-4 0  9051
2 25544  51
6399   2
1788 0008023 335
9482  24
1306 15
73622411 15305


Satellite: ISS
Catalog Number: 25544
Epoch time:      09227
53380917   =   yrday
fracday
Element set:     905
Inclination:       51
6399  deg
RA of node:         2
1788  deg
Eccentricity:     
0008023     
Arg of perigee:   335
9482  deg
Mean anomaly:      24
1306  deg
Mean motion:   15
73622411  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1530
Checksum:              296


Coasting Arc #7 (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    =        1748437
19                 A    =         6721634
20  meter
 Y    =        3972784
15  meter          E    =           
0005151
 Z    =        5130751
14                 I    =           51
60385
 XDOT =      -7427
891119                 Wp   =            6
63799
 YDOT =       1509
562269  meter/sec      RA   =          356
73099  deg
 ZDOT =       1367
272572                 TA   =           70
29838
                                          MA   =           70
24281
                                          Ha   =            191
601  n
mi
                                          Hp   =            184
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5736342
47                 X    =         1678958
91
 Y    =       13034068
75  feet           Y    =         3991947
26  meter
 Z    =       16833173
04                 Z    =         5139076
56
 XDOT =     -24369
721520                 XDOT =       -7450
861134
 YDOT =       4952
632116  feet/sec       YDOT =        1426
370675  meter/sec
 ZDOT =       4485
802401                 ZDOT =        1331
132628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3040192
85                 X    =          926650
78
 Y    =      -13872311
38  feet           Y    =        -4228280
51  meter
 Z    =       16866075
19                 Z    =         5140779
72
 XDOT =      21680
214045                 XDOT =        6608
129241
 YDOT =      10012
987721  feet/sec       YDOT =        3051
958657  meter/sec
 ZDOT =       4343
714700                 ZDOT =        1323
964241


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
54988312  
00010596  00000-0  82463-4 0  9067
2 25544  51
6411 356
9635 0008117 339
4770  20
6066 15
73661234 15461


Satellite: ISS
Catalog Number: 25544
Epoch time:      09228
54988312   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:       356
9635  deg
Eccentricity:     
0008117     
Arg of perigee:   339
4770  deg
Mean anomaly:      20
6066  deg
Mean motion:   15
73661234  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1546
Checksum:              318


Coasting Arc #8 (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    =        6293905
23                 A    =         6732519
96  meter
 Y    =       -1974049
54  meter          E    =           
0015410
 Z    =       -1300502
93                 I    =           51
61107
 XDOT =       2555
657363                 Wp   =           11
81606
 YDOT =       4309
669974  meter/sec      RA   =          351
57289  deg
 ZDOT =       5853
611409                 TA   =          333
89647
                                          MA   =          333
97408
                                          Ha   =            191
882  n
mi
                                          Hp   =            184
451

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20649295
37                 X    =         6321829
12
 Y    =       -6476540
48  feet           Y    =        -1903511
16  meter
 Z    =       -4266741
90                 Z    =        -1269859
99
 XDOT =       8384
702634                 XDOT =        2478
840651
 YDOT =      14139
337185  feet/sec       YDOT =        4337
818862  meter/sec
 ZDOT =      19204
761840                 ZDOT =        5865
840342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20676258
45                 X    =        -6302123
58
 Y    =       -6468746
25  feet           Y    =        -1971673
86  meter
 Z    =       -4146290
00                 Z    =        -1263789
19
 XDOT =        795
536752                 XDOT =         242
479602
 YDOT =     -14825
104618  feet/sec       YDOT =       -4518
691888  meter/sec
 ZDOT =      19253
035082                 ZDOT =        5868
325093


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
50244648  
00010596  00000-0  82463-4 0  9072
2 25544  51
6418 352
0748 0008173 344
0849  16
0056 15
73635381 15610


Satellite: ISS
Catalog Number: 25544
Epoch time:      09229
50244648   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:       352
0748  deg
Eccentricity:     
0008173     
Arg of perigee:   344
0849  deg
Mean anomaly:      16
0056  deg
Mean motion:   15
73635381  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1561
Checksum:              312


Coasting Arc #9 (Orbit 1576)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2671784
95                 A    =         6721879
10  meter
 Y    =       -3509857
80  meter          E    =           
0015967
 Z    =       -5084654
46                 I    =           51
54650
 XDOT =       6918
120930                 Wp   =           46
82886
 YDOT =      -2959
931282  meter/sec      RA   =          346
46170  deg
 ZDOT =      -1584
394378                 TA   =          207
87397
                                          MA   =          207
95960
                                          Ha   =            191
920  n
mi
                                          Hp   =            184
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8765698
65                 X    =        -2607638
74
 Y    =      -11515281
51  feet           Y    =        -3539376
34  meter
 Z    =      -16681937
21                 Z    =        -5097478
10
 XDOT =      22697
247145                 XDOT =        6958
401758
 YDOT =      -9711
060635  feet/sec       YDOT =       -2882
343486  meter/sec
 ZDOT =      -5198
144285                 ZDOT =       -1550
689180

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         801838
73                 X    =          244400
45
 Y    =       14391175
66  feet           Y    =         4386430
34  meter
 Z    =      -16732523
06                 Z    =        -5100073
03
 XDOT =     -23240
208986                 XDOT =       -7083
615699
 YDOT =      -4623
897973  feet/sec       YDOT =       -1409
364102  meter/sec
 ZDOT =      -5065
686281                 ZDOT =       -1544
021178


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
51850500  
00010596  00000-0  82463-4 0  9086
2 25544  51
6421 346
8602 0008227 347
5492  12
5467 15
73655785 15770


Satellite: ISS
Catalog Number: 25544
Epoch time:      09230
51850500   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:       346
8602  deg
Eccentricity:     
0008227     
Arg of perigee:   347
5492  deg
Mean anomaly:      12
5467  deg
Mean motion:   15
73655785  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1577
Checksum:              316


Coasting Arc #10 (Orbit 1592)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5754254
86                 A    =         6732249
27  meter
 Y    =        3172221
28  meter          E    =           
0011152
 Z    =        1460309
17                 I    =           51
55283
 XDOT =      -3501
071742                 Wp   =           83
10103
 YDOT =      -3667
564564  meter/sec      RA   =          341
29569  deg
 ZDOT =      -5789
674900                 TA   =           80
81697
                                          MA   =           80
69084
                                          Ha   =            192
059  n
mi
                                          Hp   =            184
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18878788
91                 X    =        -5796393
27
 Y    =       10407550
13  feet           Y    =         3107638
19  meter
 Z    =        4791040
58                 Z    =         1432253
35
 XDOT =     -11486
455848                 XDOT =       -3431
675645
 YDOT =     -12032
692138  feet/sec       YDOT =       -3706
327470  meter/sec
 ZDOT =     -18994
996390                 ZDOT =       -5806
514236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21530068
87                 X    =         6562364
99
 Y    =        1491954
60  feet           Y    =          454747
76  meter
 Z    =        4680816
85                 Z    =         1426712
98
 XDOT =       3153
498283                 XDOT =         961
186277
 YDOT =      14706
594021  feet/sec       YDOT =        4482
569858  meter/sec
 ZDOT =     -19061
390018                 ZDOT =       -5809
911677


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
53455562  
00010596  00000-0  82463-4 0  9099
2 25544  51
6423 341
6449 0008170 351
8712   8
2318 15
73663234 15937


Satellite: ISS
Catalog Number: 25544
Epoch time:      09231
53455562   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:       341
6449  deg
Eccentricity:     
0008170     
Arg of perigee:   351
8712  deg
Mean anomaly:       8
2318  deg
Mean motion:   15
73663234  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1593
Checksum:              306


Coasting Arc #11 (Orbit 1608)
---------------------------------------

Vector Time (GMT): 2009/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3418405
83                 A    =         6721885
25  meter
 Y    =        2862377
56  meter          E    =           
0006345
 Z    =        5025955
19                 I    =           51
49148
 XDOT =      -6168
059956                 Wp   =           34
33135
 YDOT =       4263
263225  meter/sec      RA   =          336
18244  deg
 ZDOT =       1771
274533                 TA   =           38
60563
                                          MA   =           38
56028
                                          Ha   =            192
042  n
mi
                                          Hp   =            183
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11215242
22                 X    =         3361729
49
 Y    =        9391002
49  feet           Y    =         2900287
34  meter
 Z    =       16489354
30                 Z    =         5042423
77
 XDOT =     -20236
417179                 XDOT =       -6223
878429
 YDOT =      13987
084070  feet/sec       YDOT =        4193
976276  meter/sec
 ZDOT =       5811
268152                 ZDOT =        1741
175094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4498646
73                 X    =        -1371187
52
 Y    =      -13841607
42  feet           Y    =        -4218921
94  meter
 Z    =       16554258
44                 Z    =         5045737
97
 XDOT =      23588
759249                 XDOT =        7189
853819
 YDOT =       -873
712474  feet/sec       YDOT =        -266
307562  meter/sec
 ZDOT =       5693
060207                 ZDOT =        1735
244751


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   09232
55059611  
00010596  00000-0  82463-4 0  9109
2 25544  51
6430 336
4297 0008287 355
5276   4
5812 15
73718025 16098


Satellite: ISS
Catalog Number: 25544
Epoch time:      09232
55059611   =   yrday
fracday
Element set:     910
Inclination:       51
6430  deg
RA of node:       336
4297  deg
Eccentricity:     
0008287     
Arg of perigee:   355
5276  deg
Mean anomaly:       4
5812  deg
Mean motion:   15
73718025  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1609
Checksum:              307


Coasting Arc #12 (Orbit 1623)
---------------------------------------

Vector Time (GMT): 2009/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4958939
30                 A    =         6732005
99  meter
 Y    =       -4235271
92  meter          E    =           
0015641
 Z    =       -1635799
44                 I    =           51
49810
 XDOT =       4299
423407                 Wp   =           17
36119
 YDOT =       2831
087559  meter/sec      RA   =          331
01032  deg
 ZDOT =       5732
435881                 TA   =          324
52594
                                          MA   =          324
62986
                                          Ha   =            192
423  n
mi
                                          Hp   =            183
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16269485
88                 X    =         5013876
57
 Y    =      -13895249
07  feet           Y    =        -4179511
02  meter
 Z    =       -5366796
05                 Z    =        -1611575
72
 XDOT =      14105
719839                 XDOT =        4239
599460
 YDOT =       9288
345010  feet/sec       YDOT =        2878
831922  meter/sec
 ZDOT =      18807
204333                 ZDOT =        5753
176749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21118012
83                 X    =        -6436770
31
 Y    =        3579839
81  feet           Y    =         1091135
17  meter
 Z    =       -5271707
36                 Z    =        -1606816
40
 XDOT =      -6998
139065                 XDOT =       -2133
032787
 YDOT =     -13608
279123  feet/sec       YDOT =       -4147
803477  meter/sec
 ZDOT =      18888
912403                 ZDOT =        5757
340500


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   09233
50312898  
00010596  00000-0  82463-4 0  9115
2 25544  51
6430 331
5414 0008542 359
3427    
7723 15
73664775 16247


Satellite: ISS
Catalog Number: 25544
Epoch time:      09233
50312898   =   yrday
fracday
Element set:     911
Inclination:       51
6430  deg
RA of node:       331
5414  deg
Eccentricity:     
0008542     
Arg of perigee:   359
3427  deg
Mean anomaly:        
7723  deg
Mean motion:   15
73664775  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1624
Checksum:              302


Coasting Arc #13 (Orbit 1639)
---------------------------------------

Vector Time (GMT): 2009/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4031280
59                 A    =         6722199
53  meter
 Y    =       -2066000
17  meter          E    =           
0017550
 Z    =       -4981407
73                 I    =           51
43944
 XDOT =       5156
414705                 Wp   =           48
07797
 YDOT =      -5361
376014  meter/sec      RA   =          325
89663  deg
 ZDOT =      -1942
171568                 TA   =          203
03394
                                          MA   =          203
11272
                                          Ha   =            192
397  n
mi
                                          Hp   =            183
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13225986
18                 X    =        -3983680
07
 Y    =       -6778215
79  feet           Y    =        -2110814
36  meter
 Z    =      -16343201
22                 Z    =        -5000875
80
 XDOT =      16917
371079                 XDOT =        5225
417921
 YDOT =     -17589
816318  feet/sec       YDOT =       -5303
328212  meter/sec
 ZDOT =      -6371
953962                 ZDOT =       -1916
954146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8017020
71                 X    =         2443587
91
 Y    =       12413158
23  feet           Y    =         3783530
63  meter
 Z    =      -16419866
85                 Z    =        -5004775
42
 XDOT =     -22553
495784                 XDOT =       -6874
305515
 YDOT =       6237
456210  feet/sec       YDOT =        1901
176653  meter/sec
 ZDOT =      -6273
016294                 ZDOT =       -1912
015366


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   09234
51915481  
00010596  00000-0  82463-4 0  9125
2 25544  51
6426 326
3266 0008411   2
8662 357
2548 15
73692081 16409


Satellite: ISS
Catalog Number: 25544
Epoch time:      09234
51915481   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:       326
3266  deg
Eccentricity:     
0008411     
Arg of perigee:     2
8662  deg
Mean anomaly:     357
2548  deg
Mean motion:   15
73692081  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1640
Checksum:              304


Coasting Arc #14 (Orbit 1655)
---------------------------------------

Vector Time (GMT): 2009/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4027359
89                 A    =         6731687
42  meter
 Y    =        5099210
02  meter          E    =           
0014133
 Z    =        1753015
07                 I    =           51
44673
 XDOT =      -4854
447945                 Wp   =           79
89430
 YDOT =      -1869
747415  meter/sec      RA   =          320
71764  deg
 ZDOT =      -5672
600487                 TA   =           80
65030
                                          MA   =           80
49053
                                          Ha   =            192
554  n
mi
                                          Hp   =            183
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13213122
99                 X    =        -4092596
60
 Y    =       16729691
68  feet           Y    =         5053809
02  meter
 Z    =        5751361
77                 Z    =         1733291
62
 XDOT =     -15926
666485                 XDOT =       -4805
622978
 YDOT =      -6134
341912  feet/sec       YDOT =       -1923
759897  meter/sec
 ZDOT =     -18610
893987                 ZDOT =       -5696
064622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19675283
01                 X    =         5997026
26
 Y    =       -8260510
32  feet           Y    =        -2517803
55  meter
 Z    =        5674026
15                 Z    =         1729443
17
 XDOT =      10291
484480                 XDOT =        3136
844469
 YDOT =      11571
644179  feet/sec       YDOT =        3527
037146  meter/sec
 ZDOT =     -18703
264777                 ZDOT =       -5700
755104


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   09235
53517270  
00010596  00000-0  82463-4 0  9133
2 25544  51
6418 321
1115 0008497   7
9672 352
1625 15
73715421 16568


Satellite: ISS
Catalog Number: 25544
Epoch time:      09235
53517270   =   yrday
fracday
Element set:     913
Inclination:       51
6418  deg
RA of node:       321
1115  deg
Eccentricity:     
0008497     
Arg of perigee:     7
9672  deg
Mean anomaly:     352
1625  deg
Mean motion:   15
73715421  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1656
Checksum:              301


Coasting Arc #15 (Orbit 1671)
---------------------------------------

Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 701645
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4414351
27                 A    =         6722188
03  meter
 Y    =        1179371
18  meter          E    =           
0008320
 Z    =        4923263
71                 I    =           51
39320
 XDOT =      -3996
933386                 Wp   =           52
68559
 YDOT =       6248
973479  meter/sec      RA   =          315
60103  deg
 ZDOT =       2089
388452                 TA   =           17
02778
                                          MA   =           16
99988
                                          Ha   =            192
454  n
mi
                                          Hp   =            182
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14482779
76                 X    =         4376918
96
 Y    =        3869328
01  feet           Y    =         1228525
85  meter
 Z    =       16152439
98                 Z    =         4944617
65
 XDOT =     -13113
298509                 XDOT =       -4076
663276
 YDOT =      20501
881492  feet/sec       YDOT =        6203
831670  meter/sec
 ZDOT =       6854
948989                 ZDOT =        2069
777591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10910978
74                 X    =        -3325666
32
 Y    =      -10146490
55  feet           Y    =        -3092650
32  meter
 Z    =       16236477
41                 Z    =         4948878
31
 XDOT =      20471
090563                 XDOT =        6239
588404
 YDOT =     -11180
476726  feet/sec       YDOT =       -3407
809306  meter/sec
 ZDOT =       6778
112762                 ZDOT =        2065
968770


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   09236
55118030  
00010596  00000-0  82463-4 0  9148
2 25544  51
6420 315
8954 0008536  10
9601 349
1746 15
73757324 16728


Satellite: ISS
Catalog Number: 25544
Epoch time:      09236
55118030   =   yrday
fracday
Element set:     914
Inclination:       51
6420  deg
RA of node:       315
8954  deg
Eccentricity:     
0008536     
Arg of perigee:    10
9601  deg
Mean anomaly:     349
1746  deg
Mean motion:   15
73757324  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1672
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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