Date: August 1st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7265 64 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 3535)
---------------------------------------

Vector Time (GMT): 2008/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6184039
93                 A    =         6735587
28  meter
 Y    =        2532074
15  meter          E    =           
0022018
 Z    =         732448
28                 I    =           51
80834
 XDOT =      -1201
003422                 Wp   =           34
98182
 YDOT =      -4688
826197  meter/sec      RA   =          152
78654  deg
 ZDOT =       5998
629093                 TA   =          332
98684
                                          MA   =          333
10127
                                          Ha   =            194
692  n
mi
                                          Hp   =            184
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20288844
90                 X    =        -6215452
41
 Y    =        8307329
88  feet           Y    =         2462744
91  meter
 Z    =        2403045
53                 Z    =          702330
89
 XDOT =      -3940
299942                 XDOT =       -1177
622651
 YDOT =     -15383
288049  feet/sec       YDOT =       -4702
126728  meter/sec
 ZDOT =      19680
541644                 ZDOT =        5992
850779

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18996616
28                 X    =         5790168
64
 Y    =       10969127
76  feet           Y    =         3343390
14  meter
 Z    =        2287004
83                 Z    =          697079
07
 XDOT =      -8883
796637                 XDOT =       -2707
781215
 YDOT =      11235
895164  feet/sec       YDOT =        3424
700846  meter/sec
 ZDOT =      19657
776542                 ZDOT =        5991
690290


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   08212
56220515  
00020000  00000-0  20000-3 0  9008
2 25544  51
6397 153
4413 0010125  11
0908 349
0476 15
72734210 35364


Satellite: ISS
Catalog Number: 25544
Epoch time:      08212
56220515   =   yrday
fracday
Element set:     900
Inclination:       51
6397  deg
RA of node:       153
4413  deg
Eccentricity:     
0010125     
Arg of perigee:    11
0908  deg
Mean anomaly:     349
0476  deg
Mean motion:   15
72734210  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3536
Checksum:              254


Coasting Arc #2 (Orbit 3550)
---------------------------------------

Vector Time (GMT): 2008/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1863623
13                 A    =         6723729
68  meter
 Y    =        3740390
65  meter          E    =           
0019729
 Z    =       -5281862
88                 I    =           51
79502
 XDOT =      -6644
444059                 Wp   =           62
75579
 YDOT =       3844
857199  meter/sec      RA   =          147
66217  deg
 ZDOT =        388
314944                 TA   =          210
87218
                                          MA   =          210
98834
                                          Ha   =            194
785  n
mi
                                          Hp   =            183
946

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6114249
12                 X    =         1847316
69
 Y    =       12271622
88  feet           Y    =         3761140
29  meter
 Z    =      -17328946
44                 Z    =        -5272848
72
 XDOT =     -21799
357148                 XDOT =       -6688
830356
 YDOT =      12614
360889  feet/sec       YDOT =        3770
306982  meter/sec
 ZDOT =       1273
999159                 ZDOT =         355
929709

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5686024
37                 X    =         1733100
23
 Y    =      -12524523
85  feet           Y    =        -3817474
87  meter
 Z    =      -17293773
00                 Z    =        -5271142
01
 XDOT =      22570
141955                 XDOT =        6879
379268
 YDOT =       8704
801191  feet/sec       YDOT =        2653
223403  meter/sec
 ZDOT =       1149
313742                 ZDOT =         350
310829


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   08213
51531176  
00020000  00000-0  20000-3 0  9013
2 25544  51
6407 148
5559 0010159  14
4217 345
7233 15
72743238 35510


Satellite: ISS
Catalog Number: 25544
Epoch time:      08213
51531176   =   yrday
fracday
Element set:     901
Inclination:       51
6407  deg
RA of node:       148
5559  deg
Eccentricity:     
0010159     
Arg of perigee:    14
4217  deg
Mean anomaly:     345
7233  deg
Mean motion:   15
72743238  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3551
Checksum:              275


Coasting Arc #3 (Orbit 3566)
---------------------------------------

Vector Time (GMT): 2008/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5330503
81                 A    =         6735709
81  meter
 Y    =       -4118482
70  meter          E    =           
0012143
 Z    =          36364
03                 I    =           51
86049
 XDOT =       2937
652501                 Wp   =           85
52702
 YDOT =       3733
513835  meter/sec      RA   =          142
55228  deg
 ZDOT =      -6049
648801                 TA   =           94
07973
                                          MA   =           93
94092
                                          Ha   =            194
846  n
mi
                                          Hp   =            183
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17488529
57                 X    =         5375984
53
 Y    =      -13512082
35  feet           Y    =        -4058619
65  meter
 Z    =         119304
58                 Z    =           62369
00
 XDOT =       9637
967522                 XDOT =        2925
072755
 YDOT =      12249
061138  feet/sec       YDOT =        3766
294635  meter/sec
 ZDOT =     -19847
929138                 ZDOT =       -6035
408229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21567896
07                 X    =        -6573894
72
 Y    =       -4818404
43  feet           Y    =        -1468649
67  meter
 Z    =         219334
03                 Z    =           66853
01
 XDOT =       2840
331587                 XDOT =         865
733068
 YDOT =     -13754
920148  feet/sec       YDOT =       -4192
499661  meter/sec
 ZDOT =     -19792
565250                 ZDOT =       -6032
773888


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   08214
53194929  
00020000  00000-0  20000-3 0  9028
2 25544  51
6416 143
3449 0010143  18
5144 341
6385 15
72757036 35679


Satellite: ISS
Catalog Number: 25544
Epoch time:      08214
53194929   =   yrday
fracday
Element set:     902
Inclination:       51
6416  deg
RA of node:       143
3449  deg
Eccentricity:     
0010143     
Arg of perigee:    18
5144  deg
Mean anomaly:     341
6385  deg
Mean motion:   15
72757036  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3567
Checksum:              289


Coasting Arc #4 (Orbit 3582)
---------------------------------------

Vector Time (GMT): 2008/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3200337
66                 A    =         6723549
17  meter
 Y    =       -2678414
89  meter          E    =           
0010409
 Z    =        5265694
64                 I    =           51
84256
 XDOT =       5392
500095                 Wp   =           36
92746
 YDOT =      -5480
882003  meter/sec      RA   =          137
44656  deg
 ZDOT =        497
184423                 TA   =           48
40993
                                          MA   =           48
32076
                                          Ha   =            194
885  n
mi
                                          Hp   =            183
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10499795
47                 X    =        -3195728
50
 Y    =       -8787450
42  feet           Y    =        -2714177
51  meter
 Z    =       17275901
06                 Z    =         5250158
79
 XDOT =      17691
929447                 XDOT =        5450
972240
 YDOT =     -17981
896335  feet/sec       YDOT =       -5420
253069  meter/sec
 ZDOT =       1631
182489                 ZDOT =         523
522169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         249188
31                 X    =           75952
60
 Y    =       13765234
65  feet           Y    =         4195643
52  meter
 Z    =       17215631
49                 Z    =         5247324
48
 XDOT =     -24159
521992                 XDOT =       -7363
822303
 YDOT =      -1697
757822  feet/sec       YDOT =        -517
476584  meter/sec
 ZDOT =       1732
369472                 ZDOT =         528
026215


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   08215
54857465  
00020000  00000-0  20000-3 0  9032
2 25544  51
6416 138
1342 0010099  21
4202 338
7381 15
72819470 35833


Satellite: ISS
Catalog Number: 25544
Epoch time:      08215
54857465   =   yrday
fracday
Element set:     903
Inclination:       51
6416  deg
RA of node:       138
1342  deg
Eccentricity:     
0010099     
Arg of perigee:    21
4202  deg
Mean anomaly:     338
7381  deg
Mean motion:   15
72819470  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3583
Checksum:              287


Coasting Arc #5 (Orbit 3597)
---------------------------------------

Vector Time (GMT): 2008/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3986713
90                 A    =         6735329
60  meter
 Y    =        5351052
13  meter          E    =           
0020317
 Z    =        -835990
40                 I    =           51
90265
 XDOT =      -4283
854233                 Wp   =           32
40309
 YDOT =      -2269
064253  meter/sec      RA   =          132
32425  deg
 ZDOT =       5988
416373                 TA   =          318
50834
                                          MA   =          318
66241
                                          Ha   =            194
981  n
mi
                                          Hp   =            183
349

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13079770
03                 X    =        -4042192
92
 Y    =       17555945
32  feet           Y    =         5306160
25  meter
 Z    =       -2742750
64                 Z    =         -855491
94
 XDOT =     -14054
639873                 XDOT =       -4287
252838
 YDOT =      -7444
436524  feet/sec       YDOT =       -2316
988067  meter/sec
 ZDOT =      19647
035344                 ZDOT =        5967
597484

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21798898
93                 X    =         6644304
39
 Y    =       -1919297
07  feet           Y    =         -585001
75  meter
 Z    =       -2817549
52                 Z    =         -858789
10
 XDOT =       3722
051674                 XDOT =        1134
481350
 YDOT =      13941
001203  feet/sec       YDOT =        4249
217167  meter/sec
 ZDOT =      19566
395230                 ZDOT =        5963
837266


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   08216
50165464  
00020000  00000-0  20000-3 0  9041
2 25544  51
6417 133
2486 0010234  25
2766 334
8896 15
72780734 35981


Satellite: ISS
Catalog Number: 25544
Epoch time:      08216
50165464   =   yrday
fracday
Element set:     904
Inclination:       51
6417  deg
RA of node:       133
2486  deg
Eccentricity:     
0010234     
Arg of perigee:    25
2766  deg
Mean anomaly:     334
8896  deg
Mean motion:   15
72780734  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3598
Checksum:              304


Coasting Arc #6 (Orbit 3613)
---------------------------------------

Vector Time (GMT): 2008/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4149914
35                 A    =         6724099
35  meter
 Y    =        1234059
73  meter          E    =           
0022048
 Z    =       -5163188
04                 I    =           51
88458
 XDOT =      -3674
535767                 Wp   =           58
81612
 YDOT =       6607
562636  meter/sec      RA   =          127
23530  deg
 ZDOT =      -1367
255786                 TA   =          198
07213
                                          MA   =          198
15063
                                          Ha   =            195
022  n
mi
                                          Hp   =            183
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13615204
56                 X    =         4160887
89
 Y    =        4048752
39  feet           Y    =         1280527
99  meter
 Z    =      -16939593
31                 Z    =        -5143001
39
 XDOT =     -12055
563539                 XDOT =       -3741
507716
 YDOT =      21678
355104  feet/sec       YDOT =        6566
097452  meter/sec
 ZDOT =      -4485
747328                 ZDOT =       -1385
268829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6316936
90                 X    =        -1925402
37
 Y    =      -12825846
27  feet           Y    =        -3909317
94  meter
 Z    =      -16861494
24                 Z    =        -5139383
45
 XDOT =      23157
458640                 XDOT =        7058
393394
 YDOT =      -5387
840458  feet/sec       YDOT =       -1642
213772  meter/sec
 ZDOT =      -4554
676725                 ZDOT =       -1388
265466


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   08217
51826164  
00020000  00000-0  20000-3 0  9055
2 25544  51
6423 128
0371 0010232  29
4986 330
6752 15
72826822 36144


Satellite: ISS
Catalog Number: 25544
Epoch time:      08217
51826164   =   yrday
fracday
Element set:     905
Inclination:       51
6423  deg
RA of node:       128
0371  deg
Eccentricity:     
0010232     
Arg of perigee:    29
4986  deg
Mean anomaly:     330
6752  deg
Mean motion:   15
72826822  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3614
Checksum:              281


Coasting Arc #7 (Orbit 3629)
---------------------------------------

Vector Time (GMT): 2008/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2399920
43                 A    =         6734508
54  meter
 Y    =       -6097941
78  meter          E    =           
0018154
 Z    =        1542098
55                 I    =           51
93592
 XDOT =       5040
340698                 Wp   =           83
84527
 YDOT =        503
315824  meter/sec      RA   =          122
10166  deg
 ZDOT =      -5793
956585                 TA   =           79
24053
                                          MA   =           79
03620
                                          Ha   =            195
083  n
mi
                                          Hp   =            183
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7873754
71                 X    =         2460439
08
 Y    =      -20006370
68  feet           Y    =        -6070766
16  meter
 Z    =        5059378
46                 Z    =         1553904
04
 XDOT =      16536
550846                 XDOT =        5062
483593
 YDOT =       1651
298635  feet/sec       YDOT =         559
803799  meter/sec
 ZDOT =     -19009
043915                 ZDOT =       -5769
417099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19889828
38                 X    =        -6062419
69
 Y    =        8135611
47  feet           Y    =         2479734
38  meter
 Z    =        5104384
83                 Z    =         1555816
50
 XDOT =      -9702
749448                 XDOT =       -2957
398032
 YDOT =     -11731
922597  feet/sec       YDOT =       -3575
890008  meter/sec
 ZDOT =     -18914
199297                 ZDOT =       -5765
047946


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   08218
53485885  
00020000  00000-0  20000-3 0  9060
2 25544  51
6420 122
8254 0010165  33
2916 326
8884 15
72813737 36306


Satellite: ISS
Catalog Number: 25544
Epoch time:      08218
53485885   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       122
8254  deg
Eccentricity:     
0010165     
Arg of perigee:    33
2916  deg
Mean anomaly:     326
8884  deg
Mean motion:   15
72813737  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3630
Checksum:              298


Coasting Arc #8 (Orbit 3645)
---------------------------------------

Vector Time (GMT): 2008/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4541468
86                 A    =         6724956
27  meter
 Y    =         397082
71  meter          E    =           
0012368
 Z    =        4932610
59                 I    =           51
91864
 XDOT =       1743
605995                 Wp   =           67
79654
 YDOT =      -7183
939517  meter/sec      RA   =          117
02695  deg
 ZDOT =       2183
912084                 TA   =            1
10861
                                          MA   =            1
10587
                                          Ha   =            195
239  n
mi
                                          Hp   =            182
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14899832
23                 X    =        -4569533
11
 Y    =        1302764
80  feet           Y    =          346140
30  meter
 Z    =       16183105
62                 Z    =         4910480
16
 XDOT =       5720
492111                 XDOT =        1813
199400
 YDOT =     -23569
355372  feet/sec       YDOT =       -7164
052476  meter/sec
 ZDOT =       7165
065892                 ZDOT =        2192
551230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11461638
00                 X    =         3493507
26
 Y    =        9751490
53  feet           Y    =         2972254
31  meter
 Z    =       16097651
72                 Z    =         4906564
24
 XDOT =     -20049
436343                 XDOT =       -6111
068197
 YDOT =      11684
977394  feet/sec       YDOT =        3561
581110  meter/sec
 ZDOT =       7197
742624                 ZDOT =        2193
871952


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   08219
55144457  
00020000  00000-0  20000-3 0  9071
2 25544  51
6421 117
6137 0010186  36
7360 323
4499 15
72851306 36469


Satellite: ISS
Catalog Number: 25544
Epoch time:      08219
55144457   =   yrday
fracday
Element set:     907
Inclination:       51
6421  deg
RA of node:       117
6137  deg
Eccentricity:     
0010186     
Arg of perigee:    36
7360  deg
Mean anomaly:     323
4499  deg
Mean motion:   15
72851306  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3646
Checksum:              292


Coasting Arc #9 (Orbit 3660)
---------------------------------------

Vector Time (GMT): 2008/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -626796
83                 A    =         6733161
38  meter
 Y    =        6306571
43  meter          E    =           
0016135
 Z    =       -2260876
61                 I    =           51
95916
 XDOT =      -5204
916094                 Wp   =           41
38845
 YDOT =       1437
917033  meter/sec      RA   =          111
88379  deg
 ZDOT =       5487
888233                 TA   =          293
35796
                                          MA   =          293
52762
                                          Ha   =            195
134  n
mi
                                          Hp   =            182
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2056420
03                 X    =         -686288
46
 Y    =       20690851
16  feet           Y    =         6299229
71  meter
 Z    =       -7417574
18                 Z    =        -2264065
76
 XDOT =     -17076
496370                 XDOT =       -5247
267293
 YDOT =       4717
575566  feet/sec       YDOT =        1379
475598  meter/sec
 ZDOT =      18004
882654                 ZDOT =        5462
500089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15908978
07                 X    =         4849056
52
 Y    =      -13381728
23  feet           Y    =        -4078750
77  meter
 Z    =       -7429290
53                 Z    =        -2264447
75
 XDOT =      14603
232228                 XDOT =        4451
065183
 YDOT =       7481
253526  feet/sec       YDOT =        2280
286075  meter/sec
 ZDOT =      17906
938598                 ZDOT =        5458
034885


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   08220
50448512  
00020000  00000-0  20000-3 0  9088
2 25544  51
6425 112
7278 0010196  39
7911 320
3998 15
72869598 36610


Satellite: ISS
Catalog Number: 25544
Epoch time:      08220
50448512   =   yrday
fracday
Element set:     908
Inclination:       51
6425  deg
RA of node:       112
7278  deg
Eccentricity:     
0010196     
Arg of perigee:    39
7911  deg
Mean anomaly:     320
3998  deg
Mean motion:   15
72869598  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3661
Checksum:              310


Coasting Arc #10 (Orbit 3676)
---------------------------------------

Vector Time (GMT): 2008/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4423723
48                 A    =         6726123
72  meter
 Y    =       -2072144
19  meter          E    =           
0020156
 Z    =       -4643241
49                 I    =           51
94535
 XDOT =        249
225554                 Wp   =           56
83296
 YDOT =       7098
223028  meter/sec      RA   =          106
82048  deg
 ZDOT =      -2928
637219                 TA   =          184
20439
                                          MA   =          184
22135
                                          Ha   =            195
145  n
mi
                                          Hp   =            182
670

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14513528
47                 X    =         4469121
67
 Y    =       -6798373
32  feet           Y    =        -2022421
43  meter
 Z    =      -15233731
93                 Z    =        -4621641
00
 XDOT =        817
669141                 XDOT =         184
060294
 YDOT =      23288
133293  feet/sec       YDOT =        7100
645846  meter/sec
 ZDOT =      -9608
389826                 ZDOT =       -2927
584306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15280612
56                 X    =        -4657530
71
 Y    =       -5088515
43  feet           Y    =        -1550979
50  meter
 Z    =      -15150474
16                 Z    =        -4617864
53
 XDOT =      14991
698027                 XDOT =        4569
469558
 YDOT =     -16409
487457  feet/sec       YDOT =       -5001
611777  meter/sec
 ZDOT =      -9603
651516                 ZDOT =       -2927
192982


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   08221
52105138  
00020000  00000-0  20000-3 0  9096
2 25544  51
6427 107
5159 0010189  42
8811 317
3144 15
72888086 36777


Satellite: ISS
Catalog Number: 25544
Epoch time:      08221
52105138   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:       107
5159  deg
Eccentricity:     
0010189     
Arg of perigee:    42
8811  deg
Mean anomaly:     317
3144  deg
Mean motion:   15
72888086  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3677
Checksum:              295


Coasting Arc #11 (Orbit 3692)
---------------------------------------

Vector Time (GMT): 2008/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1040411
77                 A    =         6731825
24  meter
 Y    =       -6001545
04  meter          E    =           
0021361
 Z    =        2855100
35                 I    =           51
97180
 XDOT =       4750
592549                 Wp   =           76
86660
 YDOT =      -3268
701995  meter/sec      RA   =          101
67048  deg
 ZDOT =      -5103
301737                 TA   =           70
53082
                                          MA   =           70
30016
                                          Ha   =            195
247  n
mi
                                          Hp   =            182
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3413424
43                 X    =         -987093
70
 Y    =      -19690108
41  feet           Y    =        -6012881
64  meter
 Z    =        9367127
12                 Z    =         2850175
07
 XDOT =      15585
933561                 XDOT =        4811
581416
 YDOT =     -10724
087910  feet/sec       YDOT =       -3215
236716  meter/sec
 ZDOT =     -16743
115936                 ZDOT =       -5080
075596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10717084
53                 X    =        -3266567
37
 Y    =       16877870
92  feet           Y    =         5144375
06  meter
 Z    =        9347538
63                 Z    =         2849129
77
 XDOT =     -17580
563295                 XDOT =       -5358
555692
 YDOT =      -1873
418287  feet/sec       YDOT =        -571
017894  meter/sec
 ZDOT =     -16653
680226                 ZDOT =       -5076
041733


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   08222
53760889  
00020000  00000-0  20000-3 0  9100
2 25544  51
6426 102
3040 0010253  47
1266 313
0756 15
72888368 36935


Satellite: ISS
Catalog Number: 25544
Epoch time:      08222
53760889   =   yrday
fracday
Element set:     910
Inclination:       51
6426  deg
RA of node:       102
3040  deg
Eccentricity:     
0010253     
Arg of perigee:    47
1266  deg
Mean anomaly:     313
0756  deg
Mean motion:   15
72888368  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3693
Checksum:              287


Coasting Arc #12 (Orbit 3708)
---------------------------------------

Vector Time (GMT): 2008/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3759616
76                 A    =         6727578
27  meter
 Y    =        3601816
62  meter          E    =           
0017880
 Z    =        4243308
79                 I    =           51
96236
 XDOT =      -2102
432506                 Wp   =           78
14888
 YDOT =      -6472
943849  meter/sec      RA   =           96
61416  deg
 ZDOT =       3622
460719                 TA   =          335
18469
                                          MA   =          335
27057
                                          Ha   =            195
391  n
mi
                                          Hp   =            182
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12334700
66                 X    =        -3820226
51
 Y    =       11816983
67  feet           Y    =         3559435
14  meter
 Z    =       13921616
76                 Z    =         4224897
81
 XDOT =      -6897
744442                 XDOT =       -2047
491896
 YDOT =     -21236
692418  feet/sec       YDOT =       -6496
147609  meter/sec
 ZDOT =      11884
713646                 ZDOT =        3612
380012

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17126879
45                 X    =         5220272
86
 Y    =        -650000
71  feet           Y    =         -198120
22  meter
 Z    =       13850807
04                 Z    =         4221725
99
 XDOT =      -8871
869809                 XDOT =       -2704
145918
 YDOT =      19285
038726  feet/sec       YDOT =        5878
079804  meter/sec
 ZDOT =      11845
167374                 ZDOT =        3610
407016


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   08223
55415561  
00020000  00000-0  20000-3 0  9118
2 25544  51
6428  97
0920 0010261  50
3169 309
8897 15
72888995 37094


Satellite: ISS
Catalog Number: 25544
Epoch time:      08223
55415561   =   yrday
fracday
Element set:     911
Inclination:       51
6428  deg
RA of node:        97
0920  deg
Eccentricity:     
0010261     
Arg of perigee:    50
3169  deg
Mean anomaly:     309
8897  deg
Mean motion:   15
72888995  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3709
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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