Date: November 1st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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 966)
---------------------------------------

Vector Time (GMT): 2008/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2470612
88                 A    =         6734254
83  meter
 Y    =       -5692137
05  meter          E    =           
0003268
 Z    =       -2611744
20                 I    =           51
89470
 XDOT =       5608
892393                 Wp   =          175
73531
 YDOT =        -18
550047  meter/sec      RA   =           47
26312  deg
 ZDOT =      -5268
980314                 TA   =           33
80300
                                          MA   =           33
78217
                                          Ha   =            191
457  n
mi
                                          Hp   =            187
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8105685
29                 X    =        -2394091
05
 Y    =      -18674990
31  feet           Y    =        -5719337
01  meter
 Z    =       -8568714
58                 Z    =        -2623560
98
 XDOT =      18401
877931                 XDOT =        5634
279564
 YDOT =        -60
859735  feet/sec       YDOT =          44
313788  meter/sec
 ZDOT =     -17286
680821                 ZDOT =       -5241
669736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17748775
32                 X    =         5409826
72
 Y    =        9931953
33  feet           Y    =         3027259
37  meter
 Z    =       -8614960
49                 Z    =        -2625839
96
 XDOT =     -13929
293779                 XDOT =       -4245
648744
 YDOT =       9999
747215  feet/sec       YDOT =        3047
922951  meter/sec
 ZDOT =     -17180
838009                 ZDOT =       -5236
719425


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   08303
52653525  
00020000  00000-0  20000-3 0  9006
2 25544  51
6430  47
6826 0003812 265
8192  94
2534 15
72220185  9673


Satellite: ISS
Catalog Number: 25544
Epoch time:      08303
52653525   =   yrday
fracday
Element set:     900
Inclination:       51
6430  deg
RA of node:        47
6826  deg
Eccentricity:     
0003812     
Arg of perigee:   265
8192  deg
Mean anomaly:      94
2534  deg
Mean motion:   15
72220185  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             967
Checksum:              281


Coasting Arc #2 (Orbit 982)
---------------------------------------

Vector Time (GMT): 2008/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4535521
01                 A    =         6727037
31  meter
 Y    =        1042670
15  meter          E    =           
0004378
 Z    =        4856934
29                 I    =           51
85009
 XDOT =      -3981
695500                 Wp   =           30
72277
 YDOT =      -6137
198567  meter/sec      RA   =           42
11698  deg
 ZDOT =      -2396
060143                 TA   =           82
61789
                                          MA   =           82
56813
                                          Ha   =            191
570  n
mi
                                          Hp   =            187
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14880318
26                 X    =        -4570438
10
 Y    =        3420833
83  feet           Y    =          991755
99  meter
 Z    =       15934823
78                 Z    =         4834815
21
 XDOT =     -13063
305445                 XDOT =       -3901
132407
 YDOT =     -20135
165903  feet/sec       YDOT =       -6181
273681  meter/sec
 ZDOT =      -7861
089709                 ZDOT =       -2415
208301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9604062
71                 X    =         2927318
31
 Y    =      -11983742
78  feet           Y    =        -3652644
80  meter
 Z    =       15849178
94                 Z    =         4830829
74
 XDOT =      21837
816449                 XDOT =        6656
166454
 YDOT =       6985
651116  feet/sec       YDOT =        2129
226460  meter/sec
 ZDOT =      -7935
774223                 ZDOT =       -2418
823983


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   08304
54351337  
00020000  00000-0  20000-3 0  9016
2 25544  51
6435  42
4743 0003733 272
7181  87
3554 15
72247819  9832


Satellite: ISS
Catalog Number: 25544
Epoch time:      08304
54351337   =   yrday
fracday
Element set:     901
Inclination:       51
6435  deg
RA of node:        42
4743  deg
Eccentricity:     
0003733     
Arg of perigee:   272
7181  deg
Mean anomaly:      87
3554  deg
Mean motion:   15
72247819  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             983
Checksum:              290


Coasting Arc #3 (Orbit 998)
---------------------------------------

Vector Time (GMT): 2008/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4395825
46                 A    =         6736055
35  meter
 Y    =        4851526
41  meter          E    =           
0011184
 Z    =        1558957
12                 I    =           51
85823
 XDOT =      -4550
938409                 Wp   =           51
76346
 YDOT =       2257
508377  meter/sec      RA   =           37
04377  deg
 ZDOT =       5785
832673                 TA   =          325
36624
                                          MA   =          325
43902
                                          Ha   =            191
450  n
mi
                                          Hp   =            187
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14421999
56                 X    =         4333674
83
 Y    =       15917081
40  feet           Y    =         4900335
51  meter
 Z    =        5114688
72                 Z    =         1580161
93
 XDOT =     -14930
900292                 XDOT =       -4603
951391
 YDOT =       7406
523546  feet/sec       YDOT =        2206
320512  meter/sec
 ZDOT =      18982
390660                 ZDOT =        5763
594849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21224869
29                 X    =        -6469340
16
 Y    =       -3162470
60  feet           Y    =         -963921
04  meter
 Z    =        5197239
22                 Z    =         1584118
51
 XDOT =       6688
359292                 XDOT =        2038
611912
 YDOT =     -13722
308467  feet/sec       YDOT =       -4182
559621  meter/sec
 ZDOT =      18896
373763                 ZDOT =        5759
614723


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   08305
56047910  
00020000  00000-0  20000-3 0  9029
2 25544  51
6436  37
2658 0003730 277
2694  82
8044 15
72259110  9994


Satellite: ISS
Catalog Number: 25544
Epoch time:      08305
56047910   =   yrday
fracday
Element set:     902
Inclination:       51
6436  deg
RA of node:        37
2658  deg
Eccentricity:     
0003730     
Arg of perigee:   277
2694  deg
Mean anomaly:      82
8044  deg
Mean motion:   15
72259110  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             999
Checksum:              295


Coasting Arc #4 (Orbit 1013)
---------------------------------------

Vector Time (GMT): 2008/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3262082
28                 A    =         6725466
70  meter
 Y    =       -2781416
38  meter          E    =           
0010520
 Z    =       -5191289
60                 I    =           51
79818
 XDOT =       5920
310127                 Wp   =           97
68013
 YDOT =       4767
894748  meter/sec      RA   =           31
91128  deg
 ZDOT =       1166
244410                 TA   =          183
44281
                                          MA   =          183
45005
                                          Ha   =            191
456  n
mi
                                          Hp   =            187
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10702369
68                 X    =         3318161
13
 Y    =       -9125381
84  feet           Y    =        -2744624
07  meter
 Z    =      -17031790
03                 Z    =        -5175305
89
 XDOT =      19423
589656                 XDOT =        5860
889176
 YDOT =      15642
699305  feet/sec       YDOT =        4833
766775  meter/sec
 ZDOT =       3826
261187                 ZDOT =        1194
861994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2312377
21                 X    =         -704812
57
 Y    =       13948677
79  feet           Y    =         4251556
99  meter
 Z    =      -16970046
60                 Z    =        -5172470
20
 XDOT =     -23896
161010                 XDOT =       -7283
549876
 YDOT =        826
452978  feet/sec       YDOT =         251
902868  meter/sec
 ZDOT =       3937
532423                 ZDOT =        1200
159883


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   08306
51387336  
00020000  00000-0  20000-3 0  9035
2 25544  51
6433  32
3835 0003777 282
4731  77
6008 15
72286100 10145


Satellite: ISS
Catalog Number: 25544
Epoch time:      08306
51387336   =   yrday
fracday
Element set:     903
Inclination:       51
6433  deg
RA of node:        32
3835  deg
Eccentricity:     
0003777     
Arg of perigee:   282
4731  deg
Mean anomaly:      77
6008  deg
Mean motion:   15
72286100  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1014
Checksum:              272


Coasting Arc #5 (Orbit 1029)
---------------------------------------

Vector Time (GMT): 2008/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5812901
17                 A    =         6736947
97  meter
 Y    =       -3361939
34  meter          E    =           
0008232
 Z    =        -480643
50                 I    =           51
81055
 XDOT =       2759
051154                 Wp   =          152
67214
 YDOT =      -3915
924683  meter/sec      RA   =           26
81561  deg
 ZDOT =      -6025
091554                 TA   =           32
53953
                                          MA   =           32
48881
                                          Ha   =            191
509  n
mi
                                          Hp   =            187
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19071198
07                 X    =        -5772540
45
 Y    =      -11029984
71  feet           Y    =        -3426716
86  meter
 Z    =       -1576914
36                 Z    =         -508785
43
 XDOT =       9052
005097                 XDOT =        2831
904123
 YDOT =     -12847
521926  feet/sec       YDOT =       -3884
663682  meter/sec
 ZDOT =     -19767
360740                 ZDOT =       -6011
511019

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21594545
69                 X    =         6582017
53
 Y    =       -4323195
05  feet           Y    =        -1317709
85  meter
 Z    =       -1686237
95                 Z    =         -513965
33
 XDOT =       1299
609484                 XDOT =         396
120971
 YDOT =      14124
241758  feet/sec       YDOT =        4305
068888  meter/sec
 ZDOT =     -19715
010589                 ZDOT =       -6009
135228


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   08307
53081633  
00020000  00000-0  20000-3 0  9040
2 25544  51
6425  27
1748 0003723 286
2198  73
8555 15
72285046 10302


Satellite: ISS
Catalog Number: 25544
Epoch time:      08307
53081633   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:        27
1748  deg
Eccentricity:     
0003723     
Arg of perigee:   286
2198  deg
Mean anomaly:      73
8555  deg
Mean motion:   15
72285046  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1030
Checksum:              284


Coasting Arc #6 (Orbit 1045)
---------------------------------------

Vector Time (GMT): 2008/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1458960
13                 A    =         6724827
81  meter
 Y    =        3901018
18  meter          E    =           
0001803
 Z    =        5280909
21                 I    =           51
74412
 XDOT =      -7174
839780                 Wp   =          315
88070
 YDOT =      -2788
151920  meter/sec      RA   =           21
69810  deg
 ZDOT =         78
700831                 TA   =          133
38083
                                          MA   =          133
36581
                                          Ha   =            191
537  n
mi
                                          Hp   =            187
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4786614
59                 X    =        -1528127
76
 Y    =       12798616
06  feet           Y    =         3884316
20  meter
 Z    =       17325817
63                 Z    =         5273653
65
 XDOT =     -23539
500590                 XDOT =       -7143
511280
 YDOT =      -9147
480054  feet/sec       YDOT =       -2868
209962  meter/sec
 ZDOT =        258
204825                 ZDOT =          43
920649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5013703
37                 X    =        -1528176
79
 Y    =      -12749232
10  feet           Y    =        -3885965
94  meter
 Z    =       17297978
73                 Z    =         5272423
92
 XDOT =      22628
199609                 XDOT =        6897
075241
 YDOT =      -8737
244647  feet/sec       YDOT =       -2663
112168  meter/sec
 ZDOT =        123
191412                 ZDOT =          37
548742


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   08308
54774498  
00020000  00000-0  20000-3 0  9051
2 25544  51
6432  21
9653 0003875 291
0500  69
0247 15
72342253 10462


Satellite: ISS
Catalog Number: 25544
Epoch time:      08308
54774498   =   yrday
fracday
Element set:     905
Inclination:       51
6432  deg
RA of node:        21
9653  deg
Eccentricity:     
0003875     
Arg of perigee:   291
0500  deg
Mean anomaly:      69
0247  deg
Mean motion:   15
72342253  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1046
Checksum:              285


Coasting Arc #7 (Orbit 1060)
---------------------------------------

Vector Time (GMT): 2008/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6544902
62                 A    =         6736912
33  meter
 Y    =        1444414
91  meter          E    =           
0010887
 Z    =        -612742
75                 I    =           51
75590
 XDOT =       -498
839742                 Wp   =           19
80655
 YDOT =       4791
035475  meter/sec      RA   =           16
57736  deg
 ZDOT =       6006
602863                 TA   =          333
53672
                                          MA   =          333
59228
                                          Ha   =            191
789  n
mi
                                          Hp   =            187
645

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21472777
63                 X    =         6531241
15
 Y    =        4738894
06  feet           Y    =         1517527
44  meter
 Z    =       -2010310
86                 Z    =         -580980
13
 XDOT =      -1636
613326                 XDOT =        -581
556341
 YDOT =      15718
620325  feet/sec       YDOT =        4784
994366  meter/sec
 ZDOT =      19706
702307                 ZDOT =        6003
978773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18876069
34                 X    =        -5753425
93
 Y    =       11300953
36  feet           Y    =         3444530
58  meter
 Z    =       -1887089
19                 Z    =         -575184
79
 XDOT =      -8693
266750                 XDOT =       -2649
707705
 YDOT =     -11255
271136  feet/sec       YDOT =       -3430
606642  meter/sec
 ZDOT =      19696
878743                 ZDOT =        6003
608641


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   08309
50110734  
00020000  00000-0  20000-3 0  9066
2 25544  51
6425  17
0821 0003890 299
3299  60
7475 15
72286514 10615


Satellite: ISS
Catalog Number: 25544
Epoch time:      08309
50110734   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:        17
0821  deg
Eccentricity:     
0003890     
Arg of perigee:   299
3299  deg
Mean anomaly:      60
7475  deg
Mean motion:   15
72286514  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1061
Checksum:              283


Coasting Arc #8 (Orbit 1076)
---------------------------------------

Vector Time (GMT): 2008/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -604280
50                 A    =         6725394
04  meter
 Y    =       -4282790
14  meter          E    =           
0011625
 Z    =       -5160138
93                 I    =           51
68844
 XDOT =       7564
196370                 Wp   =           67
42293
 YDOT =        493
248204  meter/sec      RA   =           11
47682  deg
 ZDOT =      -1293
126967                 TA   =          190
18997
                                          MA   =          190
21356
                                          Ha   =            191
750  n
mi
                                          Hp   =            187
512

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1982547
58                 X    =         -531277
28
 Y    =      -14051148
75  feet           Y    =        -4289139
18  meter
 Z    =      -16929589
66                 Z    =        -5162897
40
 XDOT =      24816
917223                 XDOT =        7564
400481
 YDOT =       1618
268386  feet/sec       YDOT =         577
836608  meter/sec
 ZDOT =      -4242
542544                 ZDOT =       -1256
378955

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11168020
29                 X    =         3404012
58
 Y    =        8733149
96  feet           Y    =         2661864
11  meter
 Z    =      -16940593
16                 Z    =        -5163492
80
 XDOT =     -18262
402209                 XDOT =       -5566
380193
 YDOT =      15387
645369  feet/sec       YDOT =        4690
154308  meter/sec
 ZDOT =      -4100
064181                 ZDOT =       -1249
699562


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   08310
51801505  
00020000  00000-0  20000-3 0  9073
2 25544  51
6419  11
8727 0003831 301
8319  58
2470 15
72326888 10775


Satellite: ISS
Catalog Number: 25544
Epoch time:      08310
51801505   =   yrday
fracday
Element set:     907
Inclination:       51
6419  deg
RA of node:        11
8727  deg
Eccentricity:     
0003831     
Arg of perigee:   301
8319  deg
Mean anomaly:      58
2470  deg
Mean motion:   15
72326888  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1077
Checksum:              280


Coasting Arc #9 (Orbit 1092)
---------------------------------------

Vector Time (GMT): 2008/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6504826
79                 A    =         6735653
43  meter
 Y    =         575535
07  meter          E    =           
0010324
 Z    =        1632410
55                 I    =           51
69509
 XDOT =      -1869
864645                 Wp   =          111
99617
 YDOT =      -4772
055554  meter/sec      RA   =            6
33191  deg
 ZDOT =      -5743
473109                 TA   =           50
00215
                                          MA   =           49
91156
                                          Ha   =            191
850  n
mi
                                          Hp   =            187
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21341295
24                 X    =        -6518709
15
 Y    =        1888238
43  feet           Y    =          502716
69  meter
 Z    =        5355677
64                 Z    =         1600775
85
 XDOT =      -6134
726527                 XDOT =       -1788
462540
 YDOT =     -15656
350242  feet/sec       YDOT =       -4792
510200  meter/sec
 ZDOT =     -18843
415713                 ZDOT =       -5752
359436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13685113
07                 X    =         4171222
46
 Y    =      -16523679
38  feet           Y    =        -5036417
48  meter
 Z    =        5233097
55                 Z    =         1595048
13
 XDOT =      14164
895679                 XDOT =        4317
460203
 YDOT =       5726
077335  feet/sec       YDOT =        1745
308372  meter/sec
 ZDOT =     -18878
208257                 ZDOT =       -5754
077877


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   08311
53490993  
00020000  00000-0  20000-3 0  9082
2 25544  51
6425   6
6633 0003871 309
3883  50
6936 15
72393090 10933


Satellite: ISS
Catalog Number: 25544
Epoch time:      08311
53490993   =   yrday
fracday
Element set:     908
Inclination:       51
6425  deg
RA of node:         6
6633  deg
Eccentricity:     
0003871     
Arg of perigee:   309
3883  deg
Mean anomaly:      50
6936  deg
Mean motion:   15
72393090  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1093
Checksum:              297


Coasting Arc #10 (Orbit 1108)
---------------------------------------

Vector Time (GMT): 2008/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2622110
84                 A    =         6726560
99  meter
 Y    =        3879057
93  meter          E    =           
0003254
 Z    =        4827204
89                 I    =           51
63508
 XDOT =      -7089
803789                 Wp   =          107
46742
 YDOT =       1768
299837  meter/sec      RA   =            1
24467  deg
 ZDOT =       2427
868718                 TA   =          318
80757
                                          MA   =          318
83212
                                          Ha   =            191
873  n
mi
                                          Hp   =            187
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8602725
84                 X    =         2555089
57
 Y    =       12726568
03  feet           Y    =         3908005
14  meter
 Z    =       15837286
39                 Z    =         4839780
56
 XDOT =     -23260
511119                 XDOT =       -7120
844640
 YDOT =       5801
508653  feet/sec       YDOT =        1688
843984  meter/sec
 ZDOT =       7965
448551                 ZDOT =        2393
350415

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15081747
95                 X    =        -4596916
78
 Y    =       -2637793
19  feet           Y    =         -803999
36  meter
 Z    =       15886314
60                 Z    =         4842148
69
 XDOT =      11713
291539                 XDOT =        3570
211261
 YDOT =     -19758
700475  feet/sec       YDOT =       -6022
451905  meter/sec
 ZDOT =       7831
780540                 ZDOT =        2387
126709


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   08312
55179365  
00020000  00000-0  20000-3 0  9093
2 25544  51
6423   1
4538 0003806 312
8273  47
2570 15
72396004 11090


Satellite: ISS
Catalog Number: 25544
Epoch time:      08312
55179365   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:         1
4538  deg
Eccentricity:     
0003806     
Arg of perigee:   312
8273  deg
Mean anomaly:      47
2570  deg
Mean motion:   15
72396004  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1109
Checksum:              275


Coasting Arc #11 (Orbit 1123)
---------------------------------------

Vector Time (GMT): 2008/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5712616
86                 A    =         6733846
39  meter
 Y    =       -2444576
92  meter          E    =           
0006242
 Z    =       -2587159
73                 I    =           51
63031
 XDOT =       4046
751675                 Wp   =           13
73909
 YDOT =       3897
797012  meter/sec      RA   =          356
08007  deg
 ZDOT =       5261
044747                 TA   =          316
90298
                                          MA   =          316
95183
                                          Ha   =            192
092  n
mi
                                          Hp   =            187
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18742181
30                 X    =         5752096
17
 Y    =       -8020265
50  feet           Y    =        -2380474
42  meter
 Z    =       -8488056
85                 Z    =        -2559311
30
 XDOT =      13276
744342                 XDOT =        3977
307341
 YDOT =      12788
047938  feet/sec       YDOT =        3942
661891  meter/sec
 ZDOT =      17260
645494                 ZDOT =        5280
535581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6852109
51                 X    =        -2088522
98
 Y    =       19247347
31  feet           Y    =         5866591
46  meter
 Z    =       -8380295
00                 Z    =        -2554313
92
 XDOT =     -16931
265749                 XDOT =       -5160
649800
 YDOT =       1508
372861  feet/sec       YDOT =         459
752048  meter/sec
 ZDOT =      17336
477263                 ZDOT =        5284
158270


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   08313
50511241  
00020000  00000-0  20000-3 0  9104
2 25544  51
6423 356
5699 0003759 318
3352  41
7523 15
72418036 11242


Satellite: ISS
Catalog Number: 25544
Epoch time:      08313
50511241   =   yrday
fracday
Element set:     910
Inclination:       51
6423  deg
RA of node:       356
5699  deg
Eccentricity:     
0003759     
Arg of perigee:   318
3352  deg
Mean anomaly:      41
7523  deg
Mean motion:   15
72418036  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1124
Checksum:              268


Coasting Arc #12 (Orbit 1139)
---------------------------------------

Vector Time (GMT): 2008/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 626690
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4332874
81                 A    =         6728455
91  meter
 Y    =       -2792977
35  meter          E    =           
0008784
 Z    =       -4333103
31                 I    =           51
58386
 XDOT =       5811
881923                 Wp   =           44
54039
 YDOT =      -3680
417388  meter/sec      RA   =          351
00057  deg
 ZDOT =      -3437
353287                 TA   =          190
66676
                                          MA   =          190
68540
                                          Ha   =            192
166  n
mi
                                          Hp   =            186
874

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14215468
52                 X    =        -4280271
25
 Y    =       -9163311
51  feet           Y    =        -2841135
99  meter
 Z    =      -14216218
21                 Z    =        -4354025
16
 XDOT =      19067
854078                 XDOT =        5869
303479
 YDOT =     -12074
860197  feet/sec       YDOT =       -3615
104547  meter/sec
 ZDOT =     -11277
405796                 ZDOT =       -3408
978884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16245767
54                 X    =         4951709
95
 Y    =       -4450040
12  feet           Y    =        -1356372
23  meter
 Z    =      -14297512
49                 Z    =        -4357881
81
 XDOT =      -4045
736590                 XDOT =       -1233
140512
 YDOT =      21131
255692  feet/sec       YDOT =        6440
806735  meter/sec
 ZDOT =     -11167
699241                 ZDOT =       -3403
914729


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   08314
52197392  
00020000  00000-0  20000-3 0  9115
2 25544  51
6430 351
3602 0003758 323
7286  36
3621 15
72417841 11402


Satellite: ISS
Catalog Number: 25544
Epoch time:      08314
52197392   =   yrday
fracday
Element set:     911
Inclination:       51
6430  deg
RA of node:       351
3602  deg
Eccentricity:     
0003758     
Arg of perigee:   323
7286  deg
Mean anomaly:      36
3621  deg
Mean motion:   15
72417841  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1140
Checksum:              269

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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