Date: October 15th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12109 4 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 2474)
---------------------------------------

Vector Time (GMT): 2009/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1314619
34                 A    =         6725547
26  meter
 Y    =       -5834451
53  meter          E    =           
0008814
 Z    =       -3067378
20                 I    =           51
91722
 XDOT =       5765
157833                 Wp   =          169
15171
 YDOT =       1293
777281  meter/sec      RA   =           53
60524  deg
 ZDOT =      -4942
473186                 TA   =           46
28337
                                          MA   =           46
21040
                                          Ha   =            189
713  n
mi
                                          Hp   =            182
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4313055
57                 X    =        -1234378
85
 Y    =      -19141901
36  feet           Y    =        -5848703
97  meter
 Z    =      -10063576
78                 Z    =        -3073569
33
 XDOT =      18914
559819                 XDOT =        5774
272011
 YDOT =       4244
676120  feet/sec       YDOT =        1358
297254  meter/sec
 ZDOT =     -16215
463210                 ZDOT =       -4914
443712

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11227224
71                 X    =         3422058
09
 Y    =       16076909
81  feet           Y    =         4900242
11  meter
 Z    =      -10088251
07                 Z    =        -3074898
93
 XDOT =     -18019
759758                 XDOT =       -5492
422774
 YDOT =       2500
286404  feet/sec       YDOT =         762
087296  meter/sec
 ZDOT =     -16104
858192                 ZDOT =       -4908
760777


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   09287
52546835  
00001200  00000-0  20000-3 0  9004
2 25544  51
6411  54
0597 0007942 200
2421 159
8428 15
74882219 24755


Satellite: ISS
Catalog Number: 25544
Epoch time:      09287
52546835   =   yrday
fracday
Element set:     900
Inclination:       51
6411  deg
RA of node:        54
0597  deg
Eccentricity:     
0007942     
Arg of perigee:   200
2421  deg
Mean anomaly:     159
8428  deg
Mean motion:   15
74882219  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2475
Checksum:              301


Coasting Arc #2 (Orbit 2490)
---------------------------------------

Vector Time (GMT): 2009/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5209017
00                 A    =         6722352
77  meter
 Y    =       -1002923
31  meter          E    =           
0008543
 Z    =        4119893
43                 I    =           51
88823
 XDOT =      -1758
145008                 Wp   =          123
04968
 YDOT =      -6471
858105  meter/sec      RA   =           48
43200  deg
 ZDOT =      -3797
325222                 TA   =            5
72746
                                          MA   =            5
71770
                                          Ha   =            189
694  n
mi
                                          Hp   =            182
926

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17089950
79                 X    =        -5217429
00
 Y    =       -3290430
79  feet           Y    =        -1061220
28  meter
 Z    =       13516710
72                 Z    =         4094567
28
 XDOT =      -5768
192283                 XDOT =       -1667
197885
 YDOT =     -21233
130266  feet/sec       YDOT =       -6491
010539  meter/sec
 ZDOT =     -12458
416082                 ZDOT =       -3805
644944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17064288
00                 X    =         5201194
98
 Y    =       -3794047
77  feet           Y    =        -1156425
76  meter
 Z    =       13416784
20                 Z    =         4089435
83
 XDOT =      13378
211438                 XDOT =        4077
678846
 YDOT =      15984
597246  feet/sec       YDOT =        4872
105241  meter/sec
 ZDOT =     -12491
507890                 ZDOT =       -3807
411605


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   09288
54071774  
00001200  00000-0  20000-3 0  9013
2 25544  51
6418  48
8394 0007864 203
4501 156
6305 15
74890369 24917


Satellite: ISS
Catalog Number: 25544
Epoch time:      09288
54071774   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:        48
8394  deg
Eccentricity:     
0007864     
Arg of perigee:   203
4501  deg
Mean anomaly:     156
6305  deg
Mean motion:   15
74890369  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2491
Checksum:              312


Coasting Arc #3 (Orbit 2506)
---------------------------------------

Vector Time (GMT): 2009/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1703037
65                 A    =         6723853
34  meter
 Y    =        5446437
48  meter          E    =           
0011353
 Z    =        3556008
59                 I    =           51
87467
 XDOT =      -6181
820695                 Wp   =          131
75808
 YDOT =      -1002
309406  meter/sec      RA   =           43
35743  deg
 ZDOT =       4479
212325                 TA   =          270
48650
                                          MA   =          270
61659
                                          Ha   =            189
219  n
mi
                                          Hp   =            183
036

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5587393
85                 X    =         1624733
24
 Y    =       17868889
38  feet           Y    =         5465044
33  meter
 Z    =       11666694
85                 Z    =         3564091
45
 XDOT =     -20281
563959                 XDOT =       -6191
912919
 YDOT =      -3288
416685  feet/sec       YDOT =       -1071
494217  meter/sec
 ZDOT =      14695
578494                 ZDOT =        4449
155970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12400585
74                 X    =        -3779698
53
 Y    =      -13999695
48  feet           Y    =        -4267107
18  meter
 Z    =       11698801
05                 Z    =         3565794
56
 XDOT =      18888
257908                 XDOT =        5757
141010
 YDOT =      -4504
340818  feet/sec       YDOT =       -1372
923081  meter/sec
 ZDOT =      14577
002485                 ZDOT =        4443
070357


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   09289
55594387  
00001200  00000-0  20000-3 0  9026
2 25544  51
6429  43
6183 0007821 208
4027 151
6711 15
74984071 25077


Satellite: ISS
Catalog Number: 25544
Epoch time:      09289
55594387   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:        43
6183  deg
Eccentricity:     
0007821     
Arg of perigee:   208
4027  deg
Mean anomaly:     151
6711  deg
Mean motion:   15
74984071  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2507
Checksum:              305


Coasting Arc #4 (Orbit 2521)
---------------------------------------

Vector Time (GMT): 2009/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5590391
72                 A    =         6723674
46  meter
 Y    =         726763
70  meter          E    =           
0007499
 Z    =       -3672023
14                 I    =           51
85137
 XDOT =       2085
391703                 Wp   =          169
42789
 YDOT =       5991
291081  meter/sec      RA   =           38
17938  deg
 ZDOT =       4354
830471                 TA   =          146
62226
                                          MA   =          146
57496
                                          Ha   =            189
024  n
mi
                                          Hp   =            183
453

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18341180
18                 X    =         5599687
93
 Y    =        2384395
34  feet           Y    =          789330
47  meter
 Z    =      -12047320
02                 Z    =        -3644841
77
 XDOT =       6841
836297                 XDOT =        1997
085511
 YDOT =      19656
466802  feet/sec       YDOT =        6014
117727  meter/sec
 ZDOT =      14287
501546                 ZDOT =        4364
746640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17658635
69                 X    =        -5382352
16
 Y    =        5729639
44  feet           Y    =         1746394
10  meter
 Z    =      -11940099
20                 Z    =        -3639342
24
 XDOT =     -14107
021445                 XDOT =       -4299
820136
 YDOT =     -13581
430317  feet/sec       YDOT =       -4139
619961  meter/sec
 ZDOT =      14326
850550                 ZDOT =        4366
824048


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   09290
50770372  
00001200  00000-0  20000-3 0  9034
2 25544  51
6433  38
7246 0007649 213
2271 146
8413 15
74964357 25227


Satellite: ISS
Catalog Number: 25544
Epoch time:      09290
50770372   =   yrday
fracday
Element set:     903
Inclination:       51
6433  deg
RA of node:        38
7246  deg
Eccentricity:     
0007649     
Arg of perigee:   213
2271  deg
Mean anomaly:     146
8413  deg
Mean motion:   15
74964357  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2522
Checksum:              293


Coasting Arc #5 (Orbit 2537)
---------------------------------------

Vector Time (GMT): 2009/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1892805
41                 A    =         6722184
64  meter
 Y    =       -5026967
27  meter          E    =           
0004470
 Z    =       -4041045
78                 I    =           51
82311
 XDOT =       6607
344371                 Wp   =          146
40304
 YDOT =        644
698231  meter/sec      RA   =           33
10223  deg
 ZDOT =      -3902
524796                 TA   =           83
48246
                                          MA   =           83
43157
                                          Ha   =            188
826  n
mi
                                          Hp   =            183
422

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6209991
51                 X    =        -1816821
05
 Y    =      -16492674
76  feet           Y    =        -5047709
09  meter
 Z    =      -13258024
21                 Z    =        -4050056
47
 XDOT =      21677
639012                 XDOT =        6618
602491
 YDOT =       2115
151676  feet/sec       YDOT =         718
648195  meter/sec
 ZDOT =     -12803
559043                 ZDOT =       -3870
398050

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12813800
30                 X    =         3905646
33
 Y    =       12059442
59  feet           Y    =         3675718
10  meter
 Z    =      -13293753
70                 Z    =        -4051936
13
 XDOT =     -19552
550048                 XDOT =       -5959
617255
 YDOT =       6821
796223  feet/sec       YDOT =        2079
283489  meter/sec
 ZDOT =     -12676
844209                 ZDOT =       -3863
902115


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   09291
52289374  
00001200  00000-0  20000-3 0  9045
2 25544  51
6438  33
5040 0007657 216
6423 143
4218 15
74998746 25384


Satellite: ISS
Catalog Number: 25544
Epoch time:      09291
52289374   =   yrday
fracday
Element set:     904
Inclination:       51
6438  deg
RA of node:        33
5040  deg
Eccentricity:     
0007657     
Arg of perigee:   216
6423  deg
Mean anomaly:     143
4218  deg
Mean motion:   15
74998746  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2538
Checksum:              311


Coasting Arc #6 (Orbit 2553)
---------------------------------------

Vector Time (GMT): 2009/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5936249
67                 A    =         6725104
67  meter
 Y    =        -364254
84  meter          E    =           
0010775
 Z    =        3124250
57                 I    =           51
80703
 XDOT =      -2232
351931                 Wp   =          129
30271
 YDOT =      -5529
772960  meter/sec      RA   =           27
92211  deg
 ZDOT =      -4881
864789                 TA   =           14
41826
                                          MA   =           14
38754
                                          Ha   =            188
732  n
mi
                                          Hp   =            183
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19475884
75                 X    =        -5946912
82
 Y    =       -1195061
81  feet           Y    =         -430697
01  meter
 Z    =       10250165
91                 Z    =         3095385
49
 XDOT =      -7323
989275                 XDOT =       -2146
635184
 YDOT =     -18142
299736  feet/sec       YDOT =       -5554
257310  meter/sec
 ZDOT =     -16016
616761                 ZDOT =       -4892
501514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17903884
54                 X    =         5457104
01
 Y    =       -7906323
87  feet           Y    =        -2409847
51  meter
 Z    =       10136326
84                 Z    =         3089552
42
 XDOT =      14175
460350                 XDOT =        4320
680315
 YDOT =      11493
271283  feet/sec       YDOT =        3503
149087  meter/sec
 ZDOT =     -16058
767775                 ZDOT =       -4894
712418


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   09292
53806434  
00001200  00000-0  20000-3 0  9050
2 25544  51
6437  28
2839 0007455 219
8984 140
1632 15
75024882 25547


Satellite: ISS
Catalog Number: 25544
Epoch time:      09292
53806434   =   yrday
fracday
Element set:     905
Inclination:       51
6437  deg
RA of node:        28
2839  deg
Eccentricity:     
0007455     
Arg of perigee:   219
8984  deg
Mean anomaly:     140
1632  deg
Mean motion:   15
75024882  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2554
Checksum:              309


Coasting Arc #7 (Orbit 2569)
---------------------------------------

Vector Time (GMT): 2009/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1951564
10                 A    =         6720359
43  meter
 Y    =        4634768
94  meter          E    =           
0009235
 Z    =        4459997
33                 I    =           51
76529
 XDOT =      -6986
347715                 Wp   =          160
17642
 YDOT =       -178
733398  meter/sec      RA   =           22
83685  deg
 ZDOT =       3232
294281                 TA   =          257
46684
                                          MA   =          257
57017
                                          Ha   =            188
279  n
mi
                                          Hp   =            183
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6402769
35                 X    =         1877925
75
 Y    =       15205934
85  feet           Y    =         4656180
78  meter
 Z    =       14632537
16                 Z    =         4469299
40
 XDOT =     -22921
088303                 XDOT =       -6999
532209
 YDOT =       -586
395662  feet/sec       YDOT =        -256
932548  meter/sec
 ZDOT =      10604
640029                 ZDOT =        3198
321569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12773430
81                 X    =        -3893341
71
 Y    =      -10391134
81  feet           Y    =        -3167217
89  meter
 Z    =       14669384
32                 Z    =         4471228
34
 XDOT =      19753
682207                 XDOT =        6020
922337
 YDOT =      -9452
452093  feet/sec       YDOT =       -2881
107398  meter/sec
 ZDOT =      10470
667276                 ZDOT =        3191
459386


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   09293
55321253  
00001200  00000-0  20000-3 0  9065
2 25544  51
6441  23
0624 0007446 224
9858 135
0704 15
75097342 25706


Satellite: ISS
Catalog Number: 25544
Epoch time:      09293
55321253   =   yrday
fracday
Element set:     906
Inclination:       51
6441  deg
RA of node:        23
0624  deg
Eccentricity:     
0007446     
Arg of perigee:   224
9858  deg
Mean anomaly:     135
0704  deg
Mean motion:   15
75097342  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2570
Checksum:              283


Coasting Arc #8 (Orbit 2584)
---------------------------------------

Vector Time (GMT): 2009/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6247568
79                 A    =         6726485
17  meter
 Y    =         -72373
71  meter          E    =           
0001927
 Z    =       -2492013
86                 I    =           51
75714
 XDOT =       2186
896691                 Wp   =          235
64014
 YDOT =       5104
932385  meter/sec      RA   =           17
65775  deg
 ZDOT =       5330
390650                 TA   =           96
21517
                                          MA   =           96
19323
                                          Ha   =            188
068  n
mi
                                          Hp   =            184
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20497272
95                 X    =         6260019
83
 Y    =        -237446
55  feet           Y    =           -2440
07  meter
 Z    =       -8175898
48                 Z    =        -2461632
10
 XDOT =       7174
857911                 XDOT =        2103
755139
 YDOT =      16748
465830  feet/sec       YDOT =        5128
922631  meter/sec
 ZDOT =      17488
158300                 ZDOT =        5340
812975

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17800529
63                 X    =        -5425601
43
 Y    =       10260623
24  feet           Y    =         3127437
96  meter
 Z    =       -8056094
02                 Z    =        -2455497
46
 XDOT =     -13615
700044                 XDOT =       -4150
065373
 YDOT =      -9847
468049  feet/sec       YDOT =       -3001
508261  meter/sec
 ZDOT =      17529
433426                 ZDOT =        5342
971308


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   09294
50489839  
00001200  00000-0  20000-3 0  9077
2 25544  51
6438  18
1683 0007327 230
2206 129
8313 15
75077243 25858


Satellite: ISS
Catalog Number: 25544
Epoch time:      09294
50489839   =   yrday
fracday
Element set:     907
Inclination:       51
6438  deg
RA of node:        18
1683  deg
Eccentricity:     
0007327     
Arg of perigee:   230
2206  deg
Mean anomaly:     129
8313  deg
Mean motion:   15
75077243  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2585
Checksum:              307


Coasting Arc #9 (Orbit 2600)
---------------------------------------

Vector Time (GMT): 2009/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1825381
35                 A    =         6718829
35  meter
 Y    =       -4310140
47  meter          E    =           
0005670
 Z    =       -4824643
99                 I    =           51
70213
 XDOT =       7291
254360                 Wp   =           97
22031
 YDOT =       -353
965725  meter/sec      RA   =           12
56126  deg
 ZDOT =      -2445
534637                 TA   =          148
92002
                                          MA   =          148
88646
                                          Ha   =            187
845  n
mi
                                          Hp   =            184
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5988783
94                 X    =        -1753611
14
 Y    =      -14140880
80  feet           Y    =        -4330151
57  meter
 Z    =      -15828884
47                 Z    =        -4833337
65
 XDOT =      23921
438188                 XDOT =        7306
550802
 YDOT =      -1161
304873  feet/sec       YDOT =        -272
345047  meter/sec
 ZDOT =      -8023
407601                 ZDOT =       -2410
075742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12222708
81                 X    =         3725481
65
 Y    =        9238200
55  feet           Y    =         2815803
53  meter
 Z    =      -15863311
96                 Z    =        -4835137
48
 XDOT =     -19437
964036                 XDOT =       -5924
691438
 YDOT =      12198
033469  feet/sec       YDOT =        3717
960601  meter/sec
 ZDOT =      -7883
589261                 ZDOT =       -2402
918007


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   09295
52001016  
00001200  00000-0  20000-3 0  9088
2 25544  51
6430  12
9472 0007313 233
6136 126
4354 15
75114626 26016


Satellite: ISS
Catalog Number: 25544
Epoch time:      09295
52001016   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:        12
9472  deg
Eccentricity:     
0007313     
Arg of perigee:   233
6136  deg
Mean anomaly:     126
4354  deg
Mean motion:   15
75114626  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2601
Checksum:              256


Coasting Arc #10 (Orbit 2616)
---------------------------------------

Vector Time (GMT): 2009/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6459439
37                 A    =         6727557
95  meter
 Y    =         566977
46  meter          E    =           
0011916
 Z    =        1763623
69                 I    =           51
70228
 XDOT =      -1979
407158                 Wp   =          144
87650
 YDOT =      -4794
669528  meter/sec      RA   =            7
38652  deg
 ZDOT =      -5698
965191                 TA   =           15
58644
                                          MA   =           15
54978
                                          Ha   =            187
599  n
mi
                                          Hp   =            184
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21192386
38                 X    =        -6473866
86
 Y    =        1860162
27  feet           Y    =          494663
50  meter
 Z    =        5786166
95                 Z    =         1732208
07
 XDOT =      -6494
117974                 XDOT =       -1897
960123
 YDOT =     -15730
543072  feet/sec       YDOT =       -4816
348904  meter/sec
 ZDOT =     -18697
392360                 ZDOT =       -5708
383611

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17177014
11                 X    =         5235553
90
 Y    =      -12607368
47  feet           Y    =        -3842725
91  meter
 Z    =        5662298
00                 Z    =         1725868
43
 XDOT =      12703
216161                 XDOT =        3871
940286
 YDOT =       8879
224362  feet/sec       YDOT =        2706
387585  meter/sec
 ZDOT =     -18734
692011                 ZDOT =       -5710
334125


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   09296
53510212  
00001200  00000-0  20000-3 0  9094
2 25544  51
6430   7
7258 0007073 237
9593 122
0884 15
75169769 26172


Satellite: ISS
Catalog Number: 25544
Epoch time:      09296
53510212   =   yrday
fracday
Element set:     909
Inclination:       51
6430  deg
RA of node:         7
7258  deg
Eccentricity:     
0007073     
Arg of perigee:   237
9593  deg
Mean anomaly:     122
0884  deg
Mean motion:   15
75169769  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2617
Checksum:              308


Coasting Arc #11 (Orbit 2632)
---------------------------------------

Vector Time (GMT): 2009/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1594600
99                 A    =         6717437
04  meter
 Y    =        4092201
14  meter          E    =           
0006596
 Z    =        5086297
49                 I    =           51
63890
 XDOT =      -7477
326617                 Wp   =          201
27733
 YDOT =        950
205940  meter/sec      RA   =            2
27325  deg
 ZDOT =       1574
316862                 TA   =          233
57801
                                          MA   =          233
63885
                                          Ha   =            187
248  n
mi
                                          Hp   =            184
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5231630
56                 X    =         1524014
04
 Y    =       13425856
77  feet           Y    =         4109638
16  meter
 Z    =       16687327
72                 Z    =         5093872
80
 XDOT =     -24531
911473                 XDOT =       -7495
044125
 YDOT =       3117
473555  feet/sec       YDOT =         866
490978  meter/sec
 ZDOT =       5165
081569                 ZDOT =        1537
948374

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11507110
89                 X    =        -3507367
40
 Y    =       -8614382
37  feet           Y    =        -2625663
75  meter
 Z    =       16717335
61                 Z    =         5095443
89
 XDOT =      18479
525030                 XDOT =        5632
559229
 YDOT =     -14905
409983  feet/sec       YDOT =       -4543
168963  meter/sec
 ZDOT =       5021
691813                 ZDOT =        1530
611665


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   09297
55017335  
00001200  00000-0  20000-3 0  9107
2 25544  51
6431   2
5037 0007152 242
3873 117
6565 15
75208650 26337


Satellite: ISS
Catalog Number: 25544
Epoch time:      09297
55017335   =   yrday
fracday
Element set:     910
Inclination:       51
6431  deg
RA of node:         2
5037  deg
Eccentricity:     
0007152     
Arg of perigee:   242
3873  deg
Mean anomaly:     117
6565  deg
Mean motion:   15
75208650  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2633
Checksum:              276


Coasting Arc #12 (Orbit 2647)
---------------------------------------

Vector Time (GMT): 2009/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6564587
23                 A    =         6728445
66  meter
 Y    =       -1095916
05  meter          E    =           
0005251
 Z    =        -964428
73                 I    =           51
64498
 XDOT =       1643
089256                 Wp   =          357
84586
 YDOT =       4621
042333  meter/sec      RA   =          357
10671  deg
 ZDOT =       5937
080132                 TA   =          351
61661
                                          MA   =          351
62538
                                          Ha   =            186
985  n
mi
                                          Hp   =            184
471

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21537359
67                 X    =         6581039
14
 Y    =       -3595525
08  feet           Y    =        -1022414
97  meter
 Z    =       -3164136
25                 Z    =         -932497
53
 XDOT =       5390
712783                 XDOT =        1562
452140
 YDOT =      15160
900042  feet/sec       YDOT =        4638
965428  meter/sec
 ZDOT =      19478
609356                 ZDOT =        5944
866534

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16057702
17                 X    =        -4894387
62
 Y    =       14822842
49  feet           Y    =         4518002
39  meter
 Z    =       -3038249
80                 Z    =         -926058
54
 XDOT =     -11643
189945                 XDOT =       -3548
844295
 YDOT =      -8617
165727  feet/sec       YDOT =       -2626
512113  meter/sec
 ZDOT =      19509
467706                 ZDOT =        5946
485757


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   09298
50178655  
00001200  00000-0  20000-3 0  9117
2 25544  51
6424 357
6082 0006938 247
8940 112
1487 15
75179014 26489


Satellite: ISS
Catalog Number: 25544
Epoch time:      09298
50178655   =   yrday
fracday
Element set:     911
Inclination:       51
6424  deg
RA of node:       357
6082  deg
Eccentricity:     
0006938     
Arg of perigee:   247
8940  deg
Mean anomaly:     112
1487  deg
Mean motion:   15
75179014  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2648
Checksum:              318


Coasting Arc #13 (Orbit 2663)
---------------------------------------

Vector Time (GMT): 2009/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1254290
76                 A    =         6716696
64  meter
 Y    =       -4020462
30  meter          E    =           
0008398
 Z    =       -5239320
34                 I    =           51
57600
 XDOT =       7514
783284                 Wp   =           97
29533
 YDOT =      -1549
695970  meter/sec      RA   =          351
97393  deg
 ZDOT =       -611
737899                 TA   =          166
89324
                                          MA   =          166
87141
                                          Ha   =            186
737  n
mi
                                          Hp   =            184
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4115127
18                 X    =        -1183787
99
 Y    =      -13190493
11  feet           Y    =        -4034094
36  meter
 Z    =      -17189371
19                 Z    =        -5245242
48
 XDOT =      24654
800800                 XDOT =        7534
525489
 YDOT =      -5084
304363  feet/sec       YDOT =       -1465
550855  meter/sec
 ZDOT =      -2007
014104                 ZDOT =        -575
182580

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10738664
13                 X    =         3273144
83
 Y    =        8648492
94  feet           Y    =         2636060
65  meter
 Z    =      -17212859
28                 Z    =        -5246479
51
 XDOT =     -16904
302684                 XDOT =       -5152
431458
 YDOT =      17294
318440  feet/sec       YDOT =        5271
308261  meter/sec
 ZDOT =      -1862
908936                 ZDOT =        -567
814644


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   09299
51682149  
00001200  00000-0  20000-3 0  9128
2 25544  51
6424 352
3859 0006919 250
8906 109
1509 15
75231256 26644


Satellite: ISS
Catalog Number: 25544
Epoch time:      09299
51682149   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:       352
3859  deg
Eccentricity:     
0006919     
Arg of perigee:   250
8906  deg
Mean anomaly:     109
1509  deg
Mean motion:   15
75231256  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2664
Checksum:              314


Coasting Arc #14 (Orbit 2679)
---------------------------------------

Vector Time (GMT): 2009/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6526544
72                 A    =         6728488
12  meter
 Y    =        1604551
85  meter          E    =           
0010570
 Z    =          93398
09                 I    =           51
58743
 XDOT =      -1226
135502                 Wp   =          166
64834
 YDOT =      -4628
695150  meter/sec      RA   =          346
81913  deg
 ZDOT =      -6036
140947                 TA   =           12
33555
                                          MA   =           12
30969
                                          Ha   =            186
324  n
mi
                                          Hp   =            184
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21412548
28                 X    =        -6544455
74
 Y    =        5264277
73  feet           Y    =         1531468
04  meter
 Z    =         306424
17                 Z    =           61648
09
 XDOT =      -4022
754273                 XDOT =       -1144
962557
 YDOT =     -15186
007709  feet/sec       YDOT =       -4641
952804  meter/sec
 ZDOT =     -19803
612030                 ZDOT =       -6041
900321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14460564
75                 X    =         4407580
14
 Y    =      -16648211
51  feet           Y    =        -5074374
87  meter
 Z    =         181274
10                 Z    =           55252
35
 XDOT =      10734
512898                 XDOT =        3271
879531
 YDOT =       9100
517434  feet/sec       YDOT =        2773
837714  meter/sec
 ZDOT =     -19826
480167                 ZDOT =       -6043
111155


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   09300
53183630  
00001200  00000-0  20000-3 0  9135
2 25544  51
6430 347
1638 0006718 255
7052 104
3366 15
75298237 26809


Satellite: ISS
Catalog Number: 25544
Epoch time:      09300
53183630   =   yrday
fracday
Element set:     913
Inclination:       51
6430  deg
RA of node:       347
1638  deg
Eccentricity:     
0006718     
Arg of perigee:   255
7052  deg
Mean anomaly:     104
3366  deg
Mean motion:   15
75298237  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2680
Checksum:              286


Coasting Arc #15 (Orbit 2695)
---------------------------------------

Vector Time (GMT): 2009/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 730759
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         883452
75                 A    =         6716392
66  meter
 Y    =        4102029
63  meter          E    =           
0004100
 Z    =        5247793
76                 I    =           51
51732
 XDOT =      -7394
555609                 Wp   =          264
85757
 YDOT =       2110
767144  meter/sec      RA   =          341
66505  deg
 ZDOT =       -405
695866                 TA   =          188
99778
                                          MA   =          189
00513
                                          Ha   =            186
020  n
mi
                                          Hp   =            184
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2898467
03                 X    =          812024
19
 Y    =       13458102
45  feet           Y    =         4111509
74  meter
 Z    =       17217171
13                 Z    =         5251911
99
 XDOT =     -24260
353047                 XDOT =       -7415
638156
 YDOT =       6925
089054  feet/sec       YDOT =        2027
958968  meter/sec
 ZDOT =      -1331
023182                 ZDOT =        -441
670552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10205879
57                 X    =        -3110752
09
 Y    =       -9208547
56  feet           Y    =        -2806765
29  meter
 Z    =       17233551
25                 Z    =         5252786
42
 XDOT =      14810
167562                 XDOT =        4514
139073
 YDOT =     -19166
628711  feet/sec       YDOT =       -5841
988431  meter/sec
 ZDOT =      -1472
810479                 ZDOT =        -448
912634


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   09301
54683166  
00001200  00000-0  20000-3 0  9147
2 25544  51
6424 341
9418 0006705 259
4828 100
5581 15
75324796 26962


Satellite: ISS
Catalog Number: 25544
Epoch time:      09301
54683166   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       341
9418  deg
Eccentricity:     
0006705     
Arg of perigee:   259
4828  deg
Mean anomaly:     100
5581  deg
Mean motion:   15
75324796  rev/day
Decay rate:    1
20000E-05  rev/day^2
Epoch rev:            2696
Checksum:              311

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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