Date: November 18th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6727 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 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 1259)
---------------------------------------

Vector Time (GMT): 2008/322/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3277768
38                 A    =         6735139
33  meter
 Y    =        5639850
27  meter          E    =           
0012711
 Z    =        1659169
52                 I    =           51
41272
 XDOT =      -5017
156479                 Wp   =          101
52077
 YDOT =      -1226
538670  meter/sec      RA   =          311
87398  deg
 ZDOT =      -5707
992741                 TA   =           60
09685
                                          MA   =           59
97065
                                          Ha   =            192
719  n
mi
                                          Hp   =            185
978

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10753833
25                 X    =        -3348650
54
 Y    =       18503445
78  feet           Y    =         5602799
86  meter
 Z    =        5443469
55                 Z    =         1643074
36
 XDOT =     -16460
487137                 XDOT =       -4975
339460
 YDOT =      -4024
077000  feet/sec       YDOT =       -1282
408958  meter/sec
 ZDOT =     -18727
010305                 ZDOT =       -5732
264989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19568613
65                 X    =         5964513
44
 Y    =        8704192
03  feet           Y    =         2653037
73  meter
 Z    =        5381467
91                 Z    =         1640271
42
 XDOT =      -1583
455524                 XDOT =        -482
637244
 YDOT =      15266
872840  feet/sec       YDOT =        4653
342842  meter/sec
 ZDOT =     -18821
190085                 ZDOT =       -5736
698738


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   08322
14744810  
00020000  00000-0  20000-3 0  9003
2 25544  51
6414 312
2896 0003669 357
3653   2
7490 15
72551350 12605


Satellite: ISS
Catalog Number: 25544
Epoch time:      08322
14744810   =   yrday
fracday
Element set:     900
Inclination:       51
6414  deg
RA of node:       312
2896  deg
Eccentricity:     
0003669     
Arg of perigee:   357
3653  deg
Mean anomaly:       2
7490  deg
Mean motion:   15
72551350  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1260
Checksum:              270


Coasting Arc #2 (Orbit 1275)
---------------------------------------

Vector Time (GMT): 2008/323/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4684243
71                 A    =         6725916
44  meter
 Y    =         165451
70  meter          E    =           
0005851
 Z    =        4818643
32                 I    =           51
36487
 XDOT =      -2700
996650                 Wp   =           88
45538
 YDOT =       6806
031926  meter/sec      RA   =          306
76609  deg
 ZDOT =       2389
630981                 TA   =          338
13089
                                          MA   =          338
15586
                                          Ha   =            192
545  n
mi
                                          Hp   =            185
803

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15368253
63                 X    =         4658637
11
 Y    =         542820
55  feet           Y    =          217690
02  meter
 Z    =       15809197
24                 Z    =         4841337
43
 XDOT =      -8861
537564                 XDOT =       -2788
510578
 YDOT =      22329
501069  feet/sec       YDOT =        6775
338291  meter/sec
 ZDOT =       7839
996658                 ZDOT =        2376
297434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1387244
91                 X    =         -422832
25
 Y    =      -15223780
20  feet           Y    =        -4640208
21  meter
 Z    =       15897190
29                 Z    =         4845463
60
 XDOT =      22164
052387                 XDOT =        6755
603168
 YDOT =       6121
623465  feet/sec       YDOT =        1865
870832  meter/sec
 ZDOT =       7788
786911                 ZDOT =        2374
022251


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   08323
16420520  
00020000  00000-0  20000-3 0  9016
2 25544  51
6425 307
0795 0003704    
0558    
0605 15
72613520 12767


Satellite: ISS
Catalog Number: 25544
Epoch time:      08323
16420520   =   yrday
fracday
Element set:     901
Inclination:       51
6425  deg
RA of node:       307
0795  deg
Eccentricity:     
0003704     
Arg of perigee:      
0558  deg
Mean anomaly:        
0605  deg
Mean motion:   15
72613520  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1276
Checksum:              235


Coasting Arc #3 (Orbit 1290)
---------------------------------------

Vector Time (GMT): 2008/324/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1403790
32                 A    =         6733519
60  meter
 Y    =       -6091075
22  meter          E    =           
0008529
 Z    =       -2495685
29                 I    =           51
37370
 XDOT =       5515
047830                 Wp   =           30
54014
 YDOT =       -892
262584  meter/sec      RA   =          301
58224  deg
 ZDOT =       5294
985604                 TA   =          301
12438
                                          MA   =          301
20802
                                          Ha   =            192
849  n
mi
                                          Hp   =            185
713

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4605611
29                 X    =         1483921
09
 Y    =      -19983842
59  feet           Y    =        -6074929
03  meter
 Z    =       -8187943
85                 Z    =        -2488671
36
 XDOT =      18093
988944                 XDOT =        5498
893025
 YDOT =      -2927
370683  feet/sec       YDOT =        -830
680800  meter/sec
 ZDOT =      17372
000014                 ZDOT =        5321
738677

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20444034
94                 X    =        -6231341
85
 Y    =       -1744835
17  feet           Y    =         -531825
76  meter
 Z    =       -8161190
50                 Z    =        -2487530
86
 XDOT =      -5599
386718                 XDOT =       -1706
693072
 YDOT =     -15899
002168  feet/sec       YDOT =       -4846
015861  meter/sec
 ZDOT =      17475
656514                 ZDOT =        5326
580105


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   08324
11740452  
00020000  00000-0  20000-3 0  9022
2 25544  51
6427 302
1955 0003849   4
9568 355
1632 15
72583426 12919


Satellite: ISS
Catalog Number: 25544
Epoch time:      08324
11740452   =   yrday
fracday
Element set:     902
Inclination:       51
6427  deg
RA of node:       302
1955  deg
Eccentricity:     
0003849     
Arg of perigee:     4
9568  deg
Mean anomaly:     355
1632  deg
Mean motion:   15
72583426  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1291
Checksum:              283


Coasting Arc #4 (Orbit 1306)
---------------------------------------

Vector Time (GMT): 2008/325/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4794174
20                 A    =         6727601
21  meter
 Y    =        1706925
44  meter          E    =           
0011761
 Z    =       -4412389
26                 I    =           51
33985
 XDOT =        537
068672                 Wp   =           53
02028
 YDOT =      -6938
927265  meter/sec      RA   =          296
48266  deg
 ZDOT =      -3266
885587                 TA   =          184
00756
                                          MA   =          184
01699
                                          Ha   =            192
847  n
mi
                                          Hp   =            185
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15728917
97                 X    =        -4791470
16
 Y    =        5600149
08  feet           Y    =         1653329
53  meter
 Z    =      -14476342
71                 Z    =        -4435672
99
 XDOT =       1762
036325                 XDOT =         630
491097
 YDOT =     -22765
509400  feet/sec       YDOT =       -6932
398953  meter/sec
 ZDOT =     -10718
128565                 ZDOT =       -3264
049865

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8032788
77                 X    =         2448394
02
 Y    =       14547051
83  feet           Y    =         4433941
40  meter
 Z    =      -14566489
49                 Z    =        -4439866
00
 XDOT =     -21703
086264                 XDOT =       -6615
100693
 YDOT =       1259
201101  feet/sec       YDOT =         383
804496  meter/sec
 ZDOT =     -10707
643388                 ZDOT =       -3263
689705


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   08325
13413552  
00020000  00000-0  20000-3 0  9034
2 25544  51
6428 296
9852 0003733   8
3774 351
7450 15
72609313 13077


Satellite: ISS
Catalog Number: 25544
Epoch time:      08325
13413552   =   yrday
fracday
Element set:     903
Inclination:       51
6428  deg
RA of node:       296
9852  deg
Eccentricity:     
0003733     
Arg of perigee:     8
3774  deg
Mean anomaly:     351
7450  deg
Mean motion:   15
72609313  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1307
Checksum:              283


Coasting Arc #5 (Orbit 1322)
---------------------------------------

Vector Time (GMT): 2008/326/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         448264
71                 A    =         6731641
34  meter
 Y    =        5900704
71  meter          E    =           
0014148
 Z    =        3200073
26                 I    =           51
34136
 XDOT =      -5256
363290                 Wp   =           77
94076
 YDOT =       2993
940322  meter/sec      RA   =          291
28785  deg
 ZDOT =      -4763
637942                 TA   =           64
53173
                                          MA   =           64
38542
                                          Ha   =            192
934  n
mi
                                          Hp   =            185
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1470684
74                 X    =          366703
13
 Y    =       19359267
43  feet           Y    =         5905261
33  meter
 Z    =       10498928
02                 Z    =         3202053
05
 XDOT =     -17245
286384                 XDOT =       -5266
310106
 YDOT =       9822
638852  feet/sec       YDOT =        2935
105174  meter/sec
 ZDOT =     -15628
733406                 ZDOT =       -4789
197805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18803730
72                 X    =         5731377
12
 Y    =       -4815953
46  feet           Y    =        -1467902
61  meter
 Z    =       10507042
50                 Z    =         3202546
55
 XDOT =      12353
725442                 XDOT =        3765
415515
 YDOT =      13773
744843  feet/sec       YDOT =        4198
237428  meter/sec
 ZDOT =     -15727
608086                 ZDOT =       -4793
774945


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   08326
15085271  
00020000  00000-0  20000-3 0  9041
2 25544  51
6426 291
7750 0003758  14
9140 345
2132 15
72626289 13236


Satellite: ISS
Catalog Number: 25544
Epoch time:      08326
15085271   =   yrday
fracday
Element set:     904
Inclination:       51
6426  deg
RA of node:       291
7750  deg
Eccentricity:     
0003758     
Arg of perigee:    14
9140  deg
Mean anomaly:     345
2132  deg
Mean motion:   15
72626289  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1323
Checksum:              279


Coasting Arc #6 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2008/327/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4245490
62                 A    =         6729260
81  meter
 Y    =       -3478147
46  meter          E    =           
0012262
 Z    =        3881948
38                 I    =           51
32501
 XDOT =       1519
066127                 Wp   =           82
01219
 YDOT =       6378
677512  meter/sec      RA   =          286
19113  deg
 ZDOT =       4044
628850                 TA   =          325
69094
                                          MA   =          325
77008
                                          Ha   =            192
784  n
mi
                                          Hp   =            185
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13928775
00                 X    =         4265210
12
 Y    =      -11411244
96  feet           Y    =        -3430561
80  meter
 Z    =       12736051
11                 Z    =         3902621
16
 XDOT =       4983
812754                 XDOT =        1427
977353
 YDOT =      20927
419659  feet/sec       YDOT =        6395
155155  meter/sec
 ZDOT =      13269
779692                 ZDOT =        4051
787564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13881932
93                 X    =        -4231213
16
 Y    =      -11378835
46  feet           Y    =        -3468269
05  meter
 Z    =       12815940
24                 Z    =         3906298
59
 XDOT =      18748
402786                 XDOT =        5714
513169
 YDOT =      -7861
315567  feet/sec       YDOT =       -2396
128985  meter/sec
 ZDOT =      13298
013036                 ZDOT =        4053
234373


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   08327
16755302  
00020000  00000-0  20000-3 0  9053
2 25544  51
6430 286
5638 0003792  17
7320 342
3974 15
72695555 13398


Satellite: ISS
Catalog Number: 25544
Epoch time:      08327
16755302   =   yrday
fracday
Element set:     905
Inclination:       51
6430  deg
RA of node:       286
5638  deg
Eccentricity:     
0003792     
Arg of perigee:    17
7320  deg
Mean anomaly:     342
3974  deg
Mean motion:   15
72695555  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1339
Checksum:              303


Coasting Arc #7 (Orbit 1353)
---------------------------------------

Vector Time (GMT): 2008/328/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2135315
62                 A    =         6729480
70  meter
 Y    =       -5105324
66  meter          E    =           
0007755
 Z    =       -3834023
81                 I    =           51
31867
 XDOT =       4299
822205                 Wp   =           75
68236
 YDOT =      -4878
520854  meter/sec      RA   =          280
99199  deg
 ZDOT =       4110
259923                 TA   =          237
47039
                                          MA   =          237
54534
                                          Ha   =            192
924  n
mi
                                          Hp   =            185
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7005628
67                 X    =        -2059442
91
 Y    =      -16749752
83  feet           Y    =        -5128778
62  meter
 Z    =      -12578818
26                 Z    =        -3844213
32
 XDOT =      14107
028232                 XDOT =        4334
087672
 YDOT =     -16005
645847  feet/sec       YDOT =       -4830
246330  meter/sec
 ZDOT =      13485
104735                 ZDOT =        4131
231996

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14911786
25                 X    =        -4545112
45
 Y    =       10308566
33  feet           Y    =         3142051
02  meter
 Z    =      -12618708
84                 Z    =        -3846182
45
 XDOT =     -17851
705892                 XDOT =       -5441
199956
 YDOT =      -9252
448882  feet/sec       YDOT =       -2820
146419  meter/sec
 ZDOT =      13566
048078                 ZDOT =        4134
931454


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   08328
12069919  
00020000  00000-0  20000-3 0  9063
2 25544  51
6429 281
6796 0003860  20
3100 339
8216 15
72691957 13548


Satellite: ISS
Catalog Number: 25544
Epoch time:      08328
12069919   =   yrday
fracday
Element set:     906
Inclination:       51
6429  deg
RA of node:       281
6796  deg
Eccentricity:     
0003860     
Arg of perigee:    20
3100  deg
Mean anomaly:     339
8216  deg
Mean motion:   15
72691957  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1354
Checksum:              303


Coasting Arc #8 (Orbit 1369)
---------------------------------------

Vector Time (GMT): 2008/329/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3166589
70                 A    =         6731093
54  meter
 Y    =        4944556
60  meter          E    =           
0007131
 Z    =       -3300099
63                 I    =           51
31951
 XDOT =      -3227
280399                 Wp   =           63
03107
 YDOT =      -5183
804787  meter/sec      RA   =          275
89474  deg
 ZDOT =      -4674
788329                 TA   =          155
84470
                                          MA   =          155
81124
                                          Ha   =            193
005  n
mi
                                          Hp   =            185
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10389073
83                 X    =        -3205613
47
 Y    =       16222298
55  feet           Y    =         4908927
95  meter
 Z    =      -10827098
52                 Z    =        -3315577
86
 XDOT =     -10588
190284                 XDOT =       -3146
364502
 YDOT =     -17007
233552  feet/sec       YDOT =       -5219
441422  meter/sec
 ZDOT =     -15337
232051                 ZDOT =       -4690
270612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18146797
92                 X    =         5531144
01
 Y    =        6363533
62  feet           Y    =         1939605
05  meter
 Z    =      -10886737
47                 Z    =        -3318277
58
 XDOT =     -13707
206289                 XDOT =       -4177
956477
 YDOT =      12771
915662  feet/sec       YDOT =        3892
879894  meter/sec
 ZDOT =     -15397
650696                 ZDOT =       -4693
203932


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   08329
13737361  
00020000  00000-0  20000-3 0  9079
2 25544  51
6426 276
4686 0003855  25
0001 335
1348 15
72703759 13708


Satellite: ISS
Catalog Number: 25544
Epoch time:      08329
13737361   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:       276
4686  deg
Eccentricity:     
0003855     
Arg of perigee:    25
0001  deg
Mean anomaly:     335
1348  deg
Mean motion:   15
72703759  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1370
Checksum:              289


Coasting Arc #9 (Orbit 1385)
---------------------------------------

Vector Time (GMT): 2008/330/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3414204
47                 A    =         6727540
45  meter
 Y    =        3858302
02  meter          E    =           
0012828
 Z    =        4320815
37                 I    =           51
30669
 XDOT =      -2804
907597                 Wp   =           58
43574
 YDOT =       6312
086127  meter/sec      RA   =          270
69565  deg
 ZDOT =      -3405
996990                 TA   =           66
14729
                                          MA   =           66
01290
                                          Ha   =            192
962  n
mi
                                          Hp   =            184
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11201458
23                 X    =         3349816
22
 Y    =       12658471
19  feet           Y    =         3896121
29  meter
 Z    =       14175903
44                 Z    =         4337245
93
 XDOT =      -9202
452745                 XDOT =       -2858
735719
 YDOT =      20708
943986  feet/sec       YDOT =        6280
419314  meter/sec
 ZDOT =     -11174
530807                 ZDOT =       -3419
753898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9558249
57                 X    =         2913354
47
 Y    =      -13875550
08  feet           Y    =        -4229267
67  meter
 Z    =       14239900
73                 Z    =         4340321
74
 XDOT =      21302
036413                 XDOT =        6492
860699
 YDOT =       3104
711269  feet/sec       YDOT =         946
315995  meter/sec
 ZDOT =     -11227
395158                 ZDOT =       -3422
110044


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   08330
15403297  
00020000  00000-0  20000-3 0  9082
2 25544  51
6430 271
2574 0004024  28
1522 331
9857 15
72754169 13860


Satellite: ISS
Catalog Number: 25544
Epoch time:      08330
15403297   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:       271
2574  deg
Eccentricity:     
0004024     
Arg of perigee:    28
1522  deg
Mean anomaly:     331
9857  deg
Mean motion:   15
72754169  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1386
Checksum:              284


Coasting Arc #10 (Orbit 1401)
---------------------------------------

Vector Time (GMT): 2008/331/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1654088
72                 A    =         6732672
53  meter
 Y    =       -5961775
87  meter          E    =           
0016728
 Z    =        2632593
95                 I    =           51
32480
 XDOT =       4447
962163                 Wp   =           68
08359
 YDOT =       3539
548966  meter/sec      RA   =          265
59370  deg
 ZDOT =       5200
730798                 TA   =          322
01679
                                          MA   =          322
13464
                                          Ha   =            193
013  n
mi
                                          Hp   =            184
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5426800
25                 X    =         1707842
30
 Y    =      -19559632
13  feet           Y    =        -5942978
60  meter
 Z    =        8637119
27                 Z    =         2640759
74
 XDOT =      14593
051715                 XDOT =        4382
786844
 YDOT =      11612
693459  feet/sec       YDOT =        3588
923739  meter/sec
 ZDOT =      17062
765085                 ZDOT =        5222
181632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20285011
59                 X    =        -6182871
53
 Y    =         -86539
48  feet           Y    =          -26377
23  meter
 Z    =        8668334
03                 Z    =         2642108
21
 XDOT =       7421
613035                 XDOT =        2262
107653
 YDOT =     -15543
815587  feet/sec       YDOT =       -4737
754991  meter/sec
 ZDOT =      17146
207555                 ZDOT =        5226
164063


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   08331
17067847  
00020000  00000-0  20000-3 0  9093
2 25544  51
6429 266
0466 0003964  32
5803 327
5604 15
72764052 14025


Satellite: ISS
Catalog Number: 25544
Epoch time:      08331
17067847   =   yrday
fracday
Element set:     909
Inclination:       51
6429  deg
RA of node:       266
0466  deg
Eccentricity:     
0003964     
Arg of perigee:    32
5803  deg
Mean anomaly:     327
5604  deg
Mean motion:   15
72764052  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1402
Checksum:              290


Coasting Arc #11 (Orbit 1416)
---------------------------------------

Vector Time (GMT): 2008/332/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4224143
86                 A    =         6725842
90  meter
 Y    =       -2271361
32  meter          E    =           
0013257
 Z    =       -4726909
76                 I    =           51
30491
 XDOT =        921
686406                 Wp   =           91
43216
 YDOT =      -7167
517576  meter/sec      RA   =          260
40209  deg
 ZDOT =       2626
488852                 TA   =          204
49118
                                          MA   =          204
55421
                                          Ha   =            193
079  n
mi
                                          Hp   =            184
542

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13858739
69                 X    =        -4175468
10
 Y    =       -7451972
82  feet           Y    =        -2318325
43  meter
 Z    =      -15508234
11                 Z    =        -4747313
22
 XDOT =       3023
905533                 XDOT =         989
006911
 YDOT =     -23515
477611  feet/sec       YDOT =       -7156
834638  meter/sec
 ZDOT =       8617
089410                 ZDOT =        2631
129230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3338026
16                 X    =        -1017430
37
 Y    =       15296683
13  feet           Y    =         4662429
02  meter
 Z    =      -15587525
67                 Z    =        -4751077
82
 XDOT =     -22301
675629                 XDOT =       -6797
550732
 YDOT =       3912
021999  feet/sec       YDOT =        1192
384305  meter/sec
 ZDOT =       8634
545337                 ZDOT =        2631
809419


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   08332
12377121  
00020000  00000-0  20000-3 0  9100
2 25544  51
6421 261
1618 0004108  36
1154 324
0285 15
72789323 14173


Satellite: ISS
Catalog Number: 25544
Epoch time:      08332
12377121   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:       261
1618  deg
Eccentricity:     
0004108     
Arg of perigee:    36
1154  deg
Mean anomaly:     324
0285  deg
Mean motion:   15
72789323  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1417
Checksum:              255


Coasting Arc #12 (Orbit 1432)
---------------------------------------

Vector Time (GMT): 2008/333/02:41:54
689
Vector Time (MET): N/A
Weight (LBS)     : 611774
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          62295
02                 A    =         6733919
73  meter
 Y    =        6439946
59  meter          E    =           
0007341
 Z    =       -1968418
94                 I    =           51
33803
 XDOT =      -5041
791363                 Wp   =          106
95155
 YDOT =      -1648
498091  meter/sec      RA   =          255
29151  deg
 ZDOT =      -5572
090728                 TA   =           95
03148
                                          MA   =           94
94767
                                          Ha   =            193
159  n
mi
                                          Hp   =            184
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         204379
97                 X    =            -159
70
 Y    =       21128433
69  feet           Y    =         6440294
26  meter
 Z    =       -6458067
39                 Z    =        -1968267
18
 XDOT =     -16541
310247                 XDOT =       -4995
914028
 YDOT =      -5408
458304  feet/sec       YDOT =       -1704
621086  meter/sec
 ZDOT =     -18281
137558                 ZDOT =       -5596
473101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20123547
34                 X    =         6133657
23
 Y    =       -6442762
10  feet           Y    =        -1963753
89  meter
 Z    =       -6456994
26                 Z    =        -1968091
85
 XDOT =       -807
052696                 XDOT =        -245
989662
 YDOT =      15832
332275  feet/sec       YDOT =        4825
694878  meter/sec
 ZDOT =     -18375
820355                 ZDOT =       -5600
950044


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   08333
14038991  
00020000  00000-0  20000-3 0  9113
2 25544  51
6419 255
9505 0004140  40
2478 319
8991 15
72796343 14331


Satellite: ISS
Catalog Number: 25544
Epoch time:      08333
14038991   =   yrday
fracday
Element set:     911
Inclination:       51
6419  deg
RA of node:       255
9505  deg
Eccentricity:     
0004140     
Arg of perigee:    40
2478  deg
Mean anomaly:     319
8991  deg
Mean motion:   15
72796343  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1433
Checksum:              296

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

The following information is a reminder of your current mailing list subscription:

You are subscribed to the following list: [list_name]

using the following email: example@example.com

You may automatically unsubscribe from this list at any time by visiting the following URL:

http://www aus-city com/cgi-bin/dada/plugins/scheduled_mailings pl/u/[list]/

If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism

You may also change your subscription by visiting this list's main screen:

<[program_url]/list/[list]>

If you're still having trouble, please contact the list owner at:

<mailto:[list_owner_email]>

The following physical address is associated with this mailing list:

[physical_address]

Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list