Date: October 29th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 24756 99 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 2616)
---------------------------------------

Vector Time (GMT): 2009/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6494121
43                 A    =         6727405
95  meter
 Y    =         478184
49  meter          E    =           
0012032
 Z    =        1658584
54                 I    =           51
70396
 XDOT =      -1822
703235                 Wp   =          146
00803
 YDOT =      -4807
426525  meter/sec      RA   =            7
39164  deg
 ZDOT =      -5740
569213                 TA   =           15
66120
                                          MA   =           15
62401
                                          Ha   =            187
403  n
mi
                                          Hp   =            184
010

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21306172
67                 X    =        -6507043
17
 Y    =        1568846
76  feet           Y    =          405491
11  meter
 Z    =        5441550
31                 Z    =         1627004
09
 XDOT =      -5979
997491                 XDOT =       -1740
923086
 YDOT =     -15772
396737  feet/sec       YDOT =       -4827
351682  meter/sec
 ZDOT =     -18833
888493                 ZDOT =       -5749
225540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17423762
13                 X    =         5310762
70
 Y    =      -12416378
95  feet           Y    =        -3784512
30  meter
 Z    =        5317028
41                 Z    =         1620630
26
 XDOT =      12298
754789                 XDOT =        3748
660460
 YDOT =       9164
272310  feet/sec       YDOT =        2793
270200  meter/sec
 ZDOT =     -18868
183252                 ZDOT =       -5751
022255


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
53488743  
00016717  00000-0  10270-3 0  9005
2 25544  51
6441   7
7314 0007011 238
2855 121
7626 15
75276209 26172


Satellite: ISS
Catalog Number: 25544
Epoch time:      09296
53488743   =   yrday
fracday
Element set:     900
Inclination:       51
6441  deg
RA of node:         7
7314  deg
Eccentricity:     
0007011     
Arg of perigee:   238
2855  deg
Mean anomaly:     121
7626  deg
Mean motion:   15
75276209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2617
Checksum:              311


Coasting Arc #2 (Orbit 2632)
---------------------------------------

Vector Time (GMT): 2009/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1405477
06                 A    =         6716877
26  meter
 Y    =        4114142
97  meter          E    =           
0006393
 Z    =        5123514
18                 I    =           51
63951
 XDOT =      -7527
087250                 Wp   =          204
50718
 YDOT =        814
416004  meter/sec      RA   =            2
27538  deg
 ZDOT =       1405
763470                 TA   =          232
00098
                                          MA   =          232
05872
                                          Ha   =            186
995  n
mi
                                          Hp   =            184
082

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4611145
22                 X    =         1334478
02
 Y    =       13497844
38  feet           Y    =         4129462
78  meter
 Z    =       16809429
73                 Z    =         5130169
71
 XDOT =     -24695
168143                 XDOT =       -7542
463817
 YDOT =       2671
968516  feet/sec       YDOT =         730
157681  meter/sec
 ZDOT =       4612
084876                 ZDOT =        1369
158925

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11020199
83                 X    =        -3358956
91
 Y    =       -9006778
00  feet           Y    =        -2745265
93  meter
 Z    =       16835811
14                 Z    =         5131555
24
 XDOT =      18824
004348                 XDOT =        5737
556525
 YDOT =     -14649
551173  feet/sec       YDOT =       -4465
183197  meter/sec
 ZDOT =       4467
759757                 ZDOT =        1361
773174


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
54987811  
00016717  00000-0  10270-3 0  9018
2 25544  51
6442   2
5088 0007065 242
8083 117
2361 15
75346599 26331


Satellite: ISS
Catalog Number: 25544
Epoch time:      09297
54987811   =   yrday
fracday
Element set:     901
Inclination:       51
6442  deg
RA of node:         2
5088  deg
Eccentricity:     
0007065     
Arg of perigee:   242
8083  deg
Mean anomaly:     117
2361  deg
Mean motion:   15
75346599  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2633
Checksum:              323


Coasting Arc #3 (Orbit 2647)
---------------------------------------

Vector Time (GMT): 2009/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6614429
45                 A    =         6728113
83  meter
 Y    =        -939376
63  meter          E    =           
0005674
 Z    =        -764351
99                 I    =           51
64662
 XDOT =       1352
268971                 Wp   =            3
96944
 YDOT =       4666
112984  meter/sec      RA   =          357
11099  deg
 ZDOT =       5975
660679                 TA   =          347
69624
                                          MA   =          347
71009
                                          Ha   =            186
676  n
mi
                                          Hp   =            184
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21700884
04                 X    =         6628155
26
 Y    =       -3081944
33  feet           Y    =         -865333
43  meter
 Z    =       -2507716
50                 Z    =         -732185
27
 XDOT =       4436
577988                 XDOT =        1270
962061
 YDOT =      15308
769633  feet/sec       YDOT =        4680
780210  meter/sec
 ZDOT =      19605
185955                 ZDOT =        5982
032628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16472787
28                 X    =        -5020905
56
 Y    =       14480815
03  feet           Y    =         4413752
42  meter
 Z    =       -2380896
11                 Z    =         -725697
14
 XDOT =     -10950
560593                 XDOT =       -3337
730869
 YDOT =      -9233
976813  feet/sec       YDOT =       -2814
516133  meter/sec
 ZDOT =      19630
467810                 ZDOT =        5983
366588


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
50139769  
00016717  00000-0  10270-3 0  9027
2 25544  51
6435 357
6128 0006807 248
4690 111
5748 15
75346437 26484


Satellite: ISS
Catalog Number: 25544
Epoch time:      09298
50139769   =   yrday
fracday
Element set:     902
Inclination:       51
6435  deg
RA of node:       357
6128  deg
Eccentricity:     
0006807     
Arg of perigee:   248
4690  deg
Mean anomaly:     111
5748  deg
Mean motion:   15
75346437  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2648
Checksum:              345


Coasting Arc #4 (Orbit 2663)
---------------------------------------

Vector Time (GMT): 2009/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -924055
82                 A    =         6716046
61  meter
 Y    =       -4082805
50  meter          E    =           
0008744
 Z    =       -5259177
92                 I    =           51
57680
 XDOT =       7577
424527                 Wp   =          100
18887
 YDOT =      -1317
451365  meter/sec      RA   =          351
97246  deg
 ZDOT =       -310
571637                 TA   =          166
87045
                                          MA   =          166
84767
                                          Ha   =            186
382  n
mi
                                          Hp   =            184
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3031679
22                 X    =         -852783
99
 Y    =      -13395031
17  feet           Y    =        -4092740
38  meter
 Z    =      -17254520
73                 Z    =        -5263493
89
 XDOT =      24860
316689                 XDOT =        7593
102044
 YDOT =      -4322
346999  feet/sec       YDOT =       -1232
628483  meter/sec
 ZDOT =      -1018
935818                 ZDOT =        -273
721878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9957581
65                 X    =         3035070
89
 Y    =        9427203
66  feet           Y    =         2873411
68  meter
 Z    =      -17271676
91                 Z    =        -5264407
12
 XDOT =     -17441
246518                 XDOT =       -5316
091939
 YDOT =      16833
597155  feet/sec       YDOT =        5130
880413  meter/sec
 ZDOT =       -873
661781                 ZDOT =        -266
292111


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
51631350  
00016717  00000-0  10270-3 0  9033
2 25544  51
6435 352
3898 0006783 251
5565 108
4862 15
75429871 26643


Satellite: ISS
Catalog Number: 25544
Epoch time:      09299
51631350   =   yrday
fracday
Element set:     903
Inclination:       51
6435  deg
RA of node:       352
3898  deg
Eccentricity:     
0006783     
Arg of perigee:   251
5565  deg
Mean anomaly:     108
4862  deg
Mean motion:   15
75429871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2664
Checksum:              340


Coasting Arc #5 (Orbit 2679)
---------------------------------------

Vector Time (GMT): 2009/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6580883
50                 A    =         6727806
70  meter
 Y    =        1343891
42  meter          E    =           
0010257
 Z    =        -241873
27                 I    =           51
58844
 XDOT =       -747
246250                 Wp   =          170
70469
 YDOT =      -4736
480263  meter/sec      RA   =          346
82202  deg
 ZDOT =      -6031
016749                 TA   =           11
92769
                                          MA   =           11
90342
                                          Ha   =            185
919  n
mi
                                          Hp   =            183
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21590825
13                 X    =        -6594247
02
 Y    =        4409092
60  feet           Y    =         1270225
38  meter
 Z    =        -793547
48                 Z    =         -273876
19
 XDOT =      -2451
595310                 XDOT =        -664
928519
 YDOT =     -15539
633409  feet/sec       YDOT =       -4744
376295  meter/sec
 ZDOT =     -19786
800359                 ZDOT =       -6034
446861

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15094076
71                 X    =         4600674
58
 Y    =      -16048568
11  feet           Y    =        -4891603
56  meter
 Z    =        -919703
77                 Z    =         -280325
71
 XDOT =       9698
551547                 XDOT =        2956
118512
 YDOT =      10249
089753  feet/sec       YDOT =        3123
922557  meter/sec
 ZDOT =     -19800
486818                 ZDOT =       -6035
188382


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
53118935  
00016717  00000-0  10270-3 0  9048
2 25544  51
6441 347
1669 0006556 256
2447 103
7988 15
75525361 26803


Satellite: ISS
Catalog Number: 25544
Epoch time:      09300
53118935   =   yrday
fracday
Element set:     904
Inclination:       51
6441  deg
RA of node:       347
1669  deg
Eccentricity:     
0006556     
Arg of perigee:   256
2447  deg
Mean anomaly:     103
7988  deg
Mean motion:   15
75525361  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2680
Checksum:              325


Coasting Arc #6 (Orbit 2695)
---------------------------------------

Vector Time (GMT): 2009/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         370541
82                 A    =         6715855
66  meter
 Y    =        4234181
33  meter          E    =           
0003574
 Z    =        5202821
30                 I    =           51
51907
 XDOT =      -7451
873693                 Wp   =          280
45219
 YDOT =       1733
518714  meter/sec      RA   =          341
65888  deg
 ZDOT =       -879
933580                 TA   =          177
94129
                                          MA   =          177
93982
                                          Ha   =            185
595  n
mi
                                          Hp   =            183
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1215688
40                 X    =          297892
11
 Y    =       13891671
03  feet           Y    =         4237918
94  meter
 Z    =       17069623
68                 Z    =         5204444
79
 XDOT =     -24448
404506                 XDOT =       -7466
429721
 YDOT =       5687
397355  feet/sec       YDOT =        1650
106047  meter/sec
 ZDOT =      -2886
921194                 ZDOT =        -916
170854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9104653
90                 X    =        -2775098
51
 Y    =      -10551689
14  feet           Y    =        -3216154
85  meter
 Z    =       17076170
77                 Z    =         5204816
85
 XDOT =      15587
594480                 XDOT =        4751
098797
 YDOT =     -18353
786705  feet/sec       YDOT =       -5594
234188  meter/sec
 ZDOT =      -3029
756884                 ZDOT =        -923
469898


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
54602550  
00016717  00000-0  10270-3 0  9052
2 25544  51
6435 341
9439 0006539 260
1489  99
8937 15
75587601 26965


Satellite: ISS
Catalog Number: 25544
Epoch time:      09301
54602550   =   yrday
fracday
Element set:     905
Inclination:       51
6435  deg
RA of node:       341
9439  deg
Eccentricity:     
0006539     
Arg of perigee:   260
1489  deg
Mean anomaly:      99
8937  deg
Mean motion:   15
75587601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2696
Checksum:              341


Coasting Arc #7 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2009/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6385743
13                 A    =         6726853
84  meter
 Y    =       -1641524
90  meter          E    =           
0008795
 Z    =        1306633
54                 I    =           51
52812
 XDOT =         92
149644                 Wp   =           41
30391
 YDOT =       5021
122000  meter/sec      RA   =          336
52319  deg
 ZDOT =       5841
917383                 TA   =          333
07276
                                          MA   =          333
11837
                                          Ha   =            185
427  n
mi
                                          Hp   =            183
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20950600
84                 X    =         6397276
82
 Y    =       -5385580
38  feet           Y    =        -1570051
20  meter
 Z    =        4286855
44                 Z    =         1337684
24
 XDOT =        302
328227                 XDOT =           7
616142
 YDOT =      16473
497376  feet/sec       YDOT =        5021
680101  meter/sec
 ZDOT =      19166
395615                 ZDOT =        5842
159478

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13416685
52                 X    =        -4089405
75
 Y    =       16936955
58  feet           Y    =         5162384
06  meter
 Z    =        4409236
48                 Z    =         1343935
28
 XDOT =      -8872
677411                 XDOT =       -2704
392075
 YDOT =     -12031
553563  feet/sec       YDOT =       -3667
217526  meter/sec
 ZDOT =      19167
524146                 ZDOT =        5842
261360


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   09302
56082508  
00016717  00000-0  10270-3 0  9061
2 25544  51
6433 336
7200 0006274 266
0141  94
0306 15
75596458 27123


Satellite: ISS
Catalog Number: 25544
Epoch time:      09302
56082508   =   yrday
fracday
Element set:     906
Inclination:       51
6433  deg
RA of node:       336
7200  deg
Eccentricity:     
0006274     
Arg of perigee:   266
0141  deg
Mean anomaly:      94
0306  deg
Mean motion:   15
75596458  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              298


Coasting Arc #8 (Orbit 2726)
---------------------------------------

Vector Time (GMT): 2009/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         199788
01                 A    =         6716875
34  meter
 Y    =       -4574639
17  meter          E    =           
0006767
 Z    =       -4920280
39                 I    =           51
46888
 XDOT =       7132
141846                 Wp   =          121
51207
 YDOT =      -1972
808799  meter/sec      RA   =          331
33500  deg
 ZDOT =       2122
480391                 TA   =          169
13213
                                          MA   =          169
11750
                                          Ha   =            185
212  n
mi
                                          Hp   =            183
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         655472
46                 X    =          274830
03
 Y    =      -15008658
71  feet           Y    =        -4571985
69  meter
 Z    =      -16142652
20                 Z    =        -4919127
28
 XDOT =      23399
415505                 XDOT =        7143
361159
 YDOT =      -6472
469812  feet/sec       YDOT =       -1892
990145  meter/sec
 ZDOT =       6963
518342                 ZDOT =        2157
156586

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8685642
49                 X    =         2647383
83
 Y    =       12263389
55  feet           Y    =         3737881
14  meter
 Z    =      -16138264
83                 Z    =        -4918943
12
 XDOT =     -13470
408295                 XDOT =       -4105
780448
 YDOT =      18889
949004  feet/sec       YDOT =        5757
656456  meter/sec
 ZDOT =       7100
177469                 ZDOT =        2164
134092


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   09303
51216000  
00016717  00000-0  10270-3 0  9074
2 25544  51
6442 331
8228 0006392 269
0132  91
0300 15
75675393 27276


Satellite: ISS
Catalog Number: 25544
Epoch time:      09303
51216000   =   yrday
fracday
Element set:     907
Inclination:       51
6442  deg
RA of node:       331
8228  deg
Eccentricity:     
0006392     
Arg of perigee:   269
0132  deg
Mean anomaly:      91
0300  deg
Mean motion:   15
75675393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2727
Checksum:              284


Coasting Arc #9 (Orbit 2742)
---------------------------------------

Vector Time (GMT): 2009/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6033926
69                 A    =         6724617
35  meter
 Y    =        1741047
80  meter          E    =           
0004084
 Z    =       -2396710
17                 I    =           51
46952
 XDOT =        543
052210                 Wp   =          212
92368
 YDOT =      -5501
631278  meter/sec      RA   =          326
21294  deg
 ZDOT =      -5362
851773                 TA   =          354
19204
                                          MA   =          354
19678
                                          Ha   =            185
138  n
mi
                                          Hp   =            183
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19796347
41                 X    =        -6041303
79
 Y    =        5712099
07  feet           Y    =         1673531
52  meter
 Z    =       -7863222
34                 Z    =        -2426041
87
 XDOT =       1781
667355                 XDOT =         630
584611
 YDOT =     -18049
971383  feet/sec       YDOT =       -5495
069352  meter/sec
 ZDOT =     -17594
658049                 ZDOT =       -5360
000693

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11708780
88                 X    =         3568836
41
 Y    =      -16899607
27  feet           Y    =        -5151000
30  meter
 Z    =       -7978811
73                 Z    =        -2431941
82
 XDOT =       8703
399779                 XDOT =        2652
796253
 YDOT =      14333
204060  feet/sec       YDOT =        4368
760597  meter/sec
 ZDOT =     -17583
607802                 ZDOT =       -5359
483658


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   09304
52688032  
00016717  00000-0  10270-3 0  9085
2 25544  51
6435 326
5986 0006282 272
6668  87
3777 15
75751716 27430


Satellite: ISS
Catalog Number: 25544
Epoch time:      09304
52688032   =   yrday
fracday
Element set:     908
Inclination:       51
6435  deg
RA of node:       326
5986  deg
Eccentricity:     
0006282     
Arg of perigee:   272
6668  deg
Mean anomaly:      87
3777  deg
Mean motion:   15
75751716  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2743
Checksum:              349


Coasting Arc #10 (Orbit 2758)
---------------------------------------

Vector Time (GMT): 2009/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -715884
83                 A    =         6718663
95  meter
 Y    =        5058051
13  meter          E    =           
0004881
 Z    =        4363915
93                 I    =           51
42453
 XDOT =      -6655
932317                 Wp   =           34
19297
 YDOT =       1952
259338  meter/sec      RA   =          321
00440  deg
 ZDOT =      -3348
883916                 TA   =           89
62411
                                          MA   =           89
56818
                                          Ha   =            185
196  n
mi
                                          Hp   =            183
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2348703
52                 X    =         -793591
48
 Y    =       16594655
94  feet           Y    =         5049611
30  meter
 Z    =       14317309
49                 Z    =         4360249
17
 XDOT =     -21837
048284                 XDOT =       -6660
999295
 YDOT =       6405
050321  feet/sec       YDOT =        1877
800372  meter/sec
 ZDOT =     -10987
151954                 ZDOT =       -3381
231900

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8838452
99                 X    =        -2693960
47
 Y    =      -14254457
00  feet           Y    =        -4344758
49  meter
 Z    =       14303026
57                 Z    =         4359562
50
 XDOT =      11476
332531                 XDOT =        3497
986156
 YDOT =     -18287
450985  feet/sec       YDOT =       -5574
015060  meter/sec
 ZDOT =     -11114
623449                 ZDOT =       -3387
737227


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   09305
54156022  
00016717  00000-0  10270-3 0  9098
2 25544  51
6423 321
3739 0006219 277
5675  82
4782 15
75838852 27594


Satellite: ISS
Catalog Number: 25544
Epoch time:      09305
54156022   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:       321
3739  deg
Eccentricity:     
0006219     
Arg of perigee:   277
5675  deg
Mean anomaly:      82
4782  deg
Mean motion:   15
75838852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2759
Checksum:              336


Coasting Arc #11 (Orbit 2774)
---------------------------------------

Vector Time (GMT): 2009/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5559637
55                 A    =         6721657
21  meter
 Y    =       -1586947
57  meter          E    =           
0006433
 Z    =        3421772
09                 I    =           51
41208
 XDOT =      -1069
812359                 Wp   =           81
20378
 YDOT =       6112
298518  meter/sec      RA   =          315
88888  deg
 ZDOT =       4566
649169                 TA   =          319
45773
                                          MA   =          319
50563
                                          Ha   =            185
199  n
mi
                                          Hp   =            183
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18240280
67                 X    =         5560346
90
 Y    =       -5206520
91  feet           Y    =        -1524772
48  meter
 Z    =       11226286
40                 Z    =         3448783
52
 XDOT =      -3509
883066                 XDOT =       -1160
266401
 YDOT =      20053
472827  feet/sec       YDOT =        6099
829468  meter/sec
 ZDOT =      14982
444779                 ZDOT =        4561
232139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10266184
63                 X    =        -3129133
08
 Y    =       15875134
64  feet           Y    =         4838741
04  meter
 Z    =       11332729
53                 Z    =         3454215
96
 XDOT =      -9321
986785                 XDOT =       -2841
341572
 YDOT =     -16723
411070  feet/sec       YDOT =       -5097
295694  meter/sec
 ZDOT =      14961
294411                 ZDOT =        4560
202537


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   09306
55620130  
00016717  00000-0  10270-3 0  9108
2 25544  51
6418 316
1487 0006165 281
8581  78
1892 15
75870771 27752


Satellite: ISS
Catalog Number: 25544
Epoch time:      09306
55620130   =   yrday
fracday
Element set:     910
Inclination:       51
6418  deg
RA of node:       316
1487  deg
Eccentricity:     
0006165     
Arg of perigee:   281
8581  deg
Mean anomaly:      78
1892  deg
Mean motion:   15
75870771  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2775
Checksum:              324


Coasting Arc #12 (Orbit 2789)
---------------------------------------

Vector Time (GMT): 2009/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1107506
65                 A    =         6721283
95  meter
 Y    =       -5611719
65  meter          E    =           
0001348
 Z    =       -3527843
30                 I    =           51
39093
 XDOT =       6072
124865                 Wp   =          327
39267
 YDOT =      -1604
134503  meter/sec      RA   =          310
67007  deg
 ZDOT =       4458
257893                 TA   =          350
40247
                                          MA   =          350
40504
                                          Ha   =            185
439  n
mi
                                          Hp   =            183
082

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3633552
00                 X    =         1187313
81
 Y    =      -18411153
72  feet           Y    =        -5598888
52  meter
 Z    =      -11574289
03                 Z    =        -3522269
17
 XDOT =      19921
669506                 XDOT =        6067
953080
 YDOT =      -5262
908476  feet/sec       YDOT =       -1536
255903  meter/sec
 ZDOT =      14626
830359                 ZDOT =        4487
747158

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9600313
75                 X    =         2926175
63
 Y    =       16140358
97  feet           Y    =         4919581
41  meter
 Z    =      -11552499
13                 Z    =        -3521201
74
 XDOT =     -10009
441510                 XDOT =       -3050
877772
 YDOT =      16505
225389  feet/sec       YDOT =        5030
792699  meter/sec
 ZDOT =      14743
044335                 ZDOT =        4493
679913


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   09307
50738909  
00016717  00000-0  10270-3 0  9119
2 25544  51
6422 311
2504 0006168 285
9052  74
1432 15
75929228 27909


Satellite: ISS
Catalog Number: 25544
Epoch time:      09307
50738909   =   yrday
fracday
Element set:     911
Inclination:       51
6422  deg
RA of node:       311
2504  deg
Eccentricity:     
0006168     
Arg of perigee:   285
9052  deg
Mean anomaly:      74
1432  deg
Mean motion:   15
75929228  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2790
Checksum:              312


Coasting Arc #13 (Orbit 2805)
---------------------------------------

Vector Time (GMT): 2009/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5035149
21                 A    =         6718307
02  meter
 Y    =        1120669
11  meter          E    =           
0005829
 Z    =       -4309644
78                 I    =           51
36193
 XDOT =       1441
885353                 Wp   =           26
15081
 YDOT =      -6738
162302  meter/sec      RA   =          305
55050  deg
 ZDOT =      -3433
396693                 TA   =          209
01664
                                          MA   =          209
04905
                                          Ha   =            185
526  n
mi
                                          Hp   =            182
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16519518
40                 X    =        -5026370
32
 Y    =        3676735
92  feet           Y    =         1064412
45  meter
 Z    =      -14139254
54                 Z    =        -4334084
96
 XDOT =       4730
594989                 XDOT =        1533
804867
 YDOT =     -22106
831701  feet/sec       YDOT =       -6721
524135  meter/sec
 ZDOT =     -11264
424845                 ZDOT =       -3426
168904

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9490350
26                 X    =         2892658
76
 Y    =      -13914483
99  feet           Y    =        -4241134
72  meter
 Z    =      -14235581
53                 Z    =        -4339005
25
 XDOT =      10587
104219                 XDOT =        3226
949366
 YDOT =      18727
680295  feet/sec       YDOT =        5708
196954  meter/sec
 ZDOT =     -11236
149151                 ZDOT =       -3424
778261


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   09308
52195048  
00016717  00000-0  10270-3 0  9124
2 25544  51
6411 306
0242 0006149 289
5187  70
5312 15
75994055 28061


Satellite: ISS
Catalog Number: 25544
Epoch time:      09308
52195048   =   yrday
fracday
Element set:     912
Inclination:       51
6411  deg
RA of node:       306
0242  deg
Eccentricity:     
0006149     
Arg of perigee:   289
5187  deg
Mean anomaly:      70
5312  deg
Mean motion:   15
75994055  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2806
Checksum:              309


Coasting Arc #14 (Orbit 2821)
---------------------------------------

Vector Time (GMT): 2009/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1365237
98                 A    =         6723746
76  meter
 Y    =        6128096
79  meter          E    =           
0007831
 Z    =        2397794
43                 I    =           51
36445
 XDOT =      -5470
690507                 Wp   =           99
08446
 YDOT =        880
318686  meter/sec      RA   =          300
33371  deg
 ZDOT =      -5351
083470                 TA   =           53
73806
                                          MA   =           53
66573
                                          Ha   =            185
641  n
mi
                                          Hp   =            182
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4479127
25                 X    =        -1445310
34
 Y    =       20105304
42  feet           Y    =         6112382
00  meter
 Z    =        7866779
61                 Z    =         2390967
88
 XDOT =     -17948
459669                 XDOT =       -5454
132449
 YDOT =       2888
184664  feet/sec       YDOT =         819
235192  meter/sec
 ZDOT =     -17556
048130                 ZDOT =       -5377
620556

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10736509
00                 X    =        -3272487
94
 Y    =      -17590703
05  feet           Y    =        -5361646
29  meter
 Z    =        7840064
33                 Z    =         2389651
61
 XDOT =       9527
615372                 XDOT =        2904
017165
 YDOT =     -13706
428732  feet/sec       YDOT =       -4177
719477  meter/sec
 ZDOT =     -17660
656684                 ZDOT =       -5382
968157


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   09309
53646975  
00016717  00000-0  10270-3 0  9137
2 25544  51
6409 300
7982 0006236 294
6299  65
4215 15
76090165 28221


Satellite: ISS
Catalog Number: 25544
Epoch time:      09309
53646975   =   yrday
fracday
Element set:     913
Inclination:       51
6409  deg
RA of node:       300
7982  deg
Eccentricity:     
0006236     
Arg of perigee:   294
6299  deg
Mean anomaly:      65
4215  deg
Mean motion:   15
76090165  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2822
Checksum:              332


Coasting Arc #15 (Orbit 2837)
---------------------------------------

Vector Time (GMT): 2009/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 745169
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4531711
80                 A    =         6715357
11  meter
 Y    =        -332767
92  meter          E    =           
0000776
 Z    =        4945267
08                 I    =           51
32202
 XDOT =      -1647
012508                 Wp   =          236
58264
 YDOT =       7255
735569  meter/sec      RA   =          295
19855  deg
 ZDOT =       1997
321691                 TA   =          194
01956
                                          MA   =          194
02171
                                          Ha   =            185
610  n
mi
                                          Hp   =            182
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14867820
87                 X    =         4511072
30
 Y    =       -1091758
26  feet           Y    =         -282207
45  meter
 Z    =       16224629
53                 Z    =         4967232
48
 XDOT =      -5403
584344                 XDOT =       -1737
727844
 YDOT =      23804
906723  feet/sec       YDOT =        7236
810327  meter/sec
 ZDOT =       6552
892688                 ZDOT =        1989
100557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9660997
43                 X    =        -2944672
02
 Y    =       11229041
01  feet           Y    =         3422611
70  meter
 Z    =       16311235
51                 Z    =         4971664
58
 XDOT =     -12190
244479                 XDOT =       -3715
586517
 YDOT =     -19960
862169  feet/sec       YDOT =       -6084
070789  meter/sec
 ZDOT =       6520
716831                 ZDOT =        1987
514490


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   09310
55094863  
00016717  00000-0  10270-3 0  9145
2 25544  51
6405 295
5721 0006230 297
8540  62
1992 15
76123073 28385


Satellite: ISS
Catalog Number: 25544
Epoch time:      09310
55094863   =   yrday
fracday
Element set:     914
Inclination:       51
6405  deg
RA of node:       295
5721  deg
Eccentricity:     
0006230     
Arg of perigee:   297
8540  deg
Mean anomaly:      62
1992  deg
Mean motion:   15
76123073  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2838
Checksum:              314

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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