Date: October 6th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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


278/10:08:14 943 0 2 2 2 2 2
N/A -1 5 0 1 193 7
000/00:04:29 885 1 7 -0 1 186 8

Coasting Arc #1 (Orbit 541)
---------------------------------------

Vector Time (GMT): 2008/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1671396
18                 A    =         6725150
91  meter
 Y    =        3971866
83  meter          E    =           
0016755
 Z    =       -5177119
82                 I    =           51
59273
 XDOT =      -7427
886141                 Wp   =          119
26769
 YDOT =      -1592
947480  meter/sec      RA   =          185
08620  deg
 ZDOT =       1170
742159                 TA   =          161
97008
                                          MA   =          161
91058
                                          Ha   =            193
707  n
mi
                                          Hp   =            185
728

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5483583
26                 X    =        -1690535
93
 Y    =       13031059
17  feet           Y    =         3953069
06  meter
 Z    =      -16985301
24                 Z    =        -5185286
32
 XDOT =     -24369
705186                 XDOT =       -7415
208865
 YDOT =      -5226
205642  feet/sec       YDOT =       -1675
939454  meter/sec
 ZDOT =       3841
017581                 ZDOT =        1134
687545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2843597
49                 X    =          866728
51
 Y    =      -13810567
00  feet           Y    =        -4209460
82  meter
 Z    =      -17016487
27                 Z    =        -5186625
32
 XDOT =      23931
703816                 XDOT =        7294
383323
 YDOT =        346
037795  feet/sec       YDOT =         105
472320  meter/sec
 ZDOT =       3701
332818                 ZDOT =        1128
166243


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   08276
51400900  
00020000  00000-0  20000-3 0  9001
2 25544  51
6417 186
0358 0005935 175
5068 184
6148 15
72380225  5429


Satellite: ISS
Catalog Number: 25544
Epoch time:      08276
51400900   =   yrday
fracday
Element set:     900
Inclination:       51
6417  deg
RA of node:       186
0358  deg
Eccentricity:     
0005935     
Arg of perigee:   175
5068  deg
Mean anomaly:     184
6148  deg
Mean motion:   15
72380225  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             542
Checksum:              282


Coasting Arc #2 (Orbit 557)
---------------------------------------

Vector Time (GMT): 2008/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 628687
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6694191
59                 A    =         6736698
20  meter
 Y    =         412864
12  meter          E    =           
0016234
 Z    =        -525460
06                 I    =           51
66082
 XDOT =       -758
453557                 Wp   =          153
27081
 YDOT =       4755
048767  meter/sec      RA   =          179
97687  deg
 ZDOT =      -6012
091501                 TA   =           32
44424
                                          MA   =           32
34454
                                          Ha   =            193
673  n
mi
                                          Hp   =            185
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21962570
85                 X    =         6691630
00
 Y    =        1354541
08  feet           Y    =          487708
10  meter
 Z    =       -1723950
34                 Z    =         -492945
21
 XDOT =      -2488
364689                 XDOT =        -782
362618
 YDOT =      15600
553697  feet/sec       YDOT =        4746
433454  meter/sec
 ZDOT =     -19724
709649                 ZDOT =       -6015
834355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21784315
31                 X    =        -6639859
31
 Y    =        3170341
68  feet           Y    =          966320
14  meter
 Z    =       -1598075
34                 Z    =         -487093
36
 XDOT =       -636
156142                 XDOT =        -193
900392
 YDOT =     -14167
883759  feet/sec       YDOT =       -4318
370970  meter/sec
 ZDOT =     -19738
701028                 ZDOT =       -6016
356073


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   08277
53088143  
00020000  00000-0  20000-3 0  9016
2 25544  51
6417 180
8263 0006048 179
8778 180
2387 15
72378512  5587


Satellite: ISS
Catalog Number: 25544
Epoch time:      08277
53088143   =   yrday
fracday
Element set:     901
Inclination:       51
6417  deg
RA of node:       180
8263  deg
Eccentricity:     
0006048     
Arg of perigee:   179
8778  deg
Mean anomaly:     180
2387  deg
Mean motion:   15
72378512  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             558
Checksum:              315


Coasting Arc #3 (Orbit 572)
---------------------------------------

Vector Time (GMT): 2008/278/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6447898
76                 A    =         6736607
81  meter
 Y    =        -846438
34  meter          E    =           
0012782
 Z    =        1742390
14                 I    =           51
68211
 XDOT =       2165
766200                 Wp   =           81
51698
 YDOT =      -4698
562201  meter/sec      RA   =          175
25478  deg
 ZDOT =       5698
501217                 TA   =          297
74305
                                          MA   =          297
87263
                                          Ha   =            193
698  n
mi
                                          Hp   =            186
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21154523
51                 X    =        -6446418
92
 Y    =       -2777028
68  feet           Y    =         -918534
17  meter
 Z    =        5716503
09                 Z    =         1711069
23
 XDOT =       7105
532152                 XDOT =        2190
462469
 YDOT =     -15415
230317  feet/sec       YDOT =       -4674
205192  meter/sec
 ZDOT =      18695
870133                 ZDOT =        5709
082772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19794824
13                 X    =         6033462
39
 Y    =        8047541
09  feet           Y    =         2452890
52  meter
 Z    =        5595192
66                 Z    =         1705414
72
 XDOT =     -10084
185879                 XDOT =       -3073
659856
 YDOT =      11699
305533  feet/sec       YDOT =        3565
948326  meter/sec
 ZDOT =      18736
340197                 ZDOT =        5710
836492


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   08278
48419981  
00020000  00000-0  20000-3 0  9020
2 25544  51
6398 175
9419 0004102 181
5326 178
5824 15
72004750  5734


Satellite: ISS
Catalog Number: 25544
Epoch time:      08278
48419981   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       175
9419  deg
Eccentricity:     
0004102     
Arg of perigee:   181
5326  deg
Mean anomaly:     178
5824  deg
Mean motion:   15
72004750  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             573
Checksum:              306


Coasting Arc #4 (Orbit 587)
---------------------------------------

Vector Time (GMT): 2008/279/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -734904
03                 A    =         6726247
80  meter
 Y    =        4267762
34  meter          E    =           
0015059
 Z    =       -5159578
96                 I    =           51
67721
 XDOT =      -7570
687336                 Wp   =          115
73142
 YDOT =        275
003911  meter/sec      RA   =          170
11030  deg
 ZDOT =       1302
334060                 TA   =          166
76004
                                          MA   =          166
72047
                                          Ha   =            193
534  n
mi
                                          Hp   =            186
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2411102
45                 X    =         -757507
47
 Y    =       14001844
94  feet           Y    =         4259417
81  meter
 Z    =      -16927752
48                 Z    =        -5163204
10
 XDOT =     -24838
213046                 XDOT =       -7579
526415
 YDOT =        902
243802  feet/sec       YDOT =         190
294699  meter/sec
 ZDOT =       4272
749540                 ZDOT =        1265
533543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5557804
94                 X    =         1694018
94
 Y    =      -13058155
97  feet           Y    =        -3980125
94  meter
 Z    =      -16941347
28                 Z    =        -5163722
65
 XDOT =      23418
928506                 XDOT =        7138
089409
 YDOT =       4594
213890  feet/sec       YDOT =        1400
316394  meter/sec
 ZDOT =       4130
330740                 ZDOT =        1258
924810


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   08279
43774151  
00020000  00000-0  20000-3 0  9030
2 25544  51
6403 171
0591 0004079 185
5431 174
5687 15
72031922  5883


Satellite: ISS
Catalog Number: 25544
Epoch time:      08279
43774151   =   yrday
fracday
Element set:     903
Inclination:       51
6403  deg
RA of node:       171
0591  deg
Eccentricity:     
0004079     
Arg of perigee:   185
5431  deg
Mean anomaly:     174
5687  deg
Mean motion:   15
72031922  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             588
Checksum:              295


Coasting Arc #5 (Orbit 603)
---------------------------------------

Vector Time (GMT): 2008/280/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6575819
65                 A    =         6737657
84  meter
 Y    =       -1329991
50  meter          E    =           
0014177
 Z    =        -527645
75                 I    =           51
74470
 XDOT =        490
191556                 Wp   =          152
24454
 YDOT =       4780
416722  meter/sec      RA   =          165
01055  deg
 ZDOT =      -6017
273751                 TA   =           33
48581
                                          MA   =           33
39626
                                          Ha   =            193
490  n
mi
                                          Hp   =            186
902

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21574211
47                 X    =         6592766
35
 Y    =       -4363489
16  feet           Y    =        -1256362
13  meter
 Z    =       -1731121
24                 Z    =         -495658
79
 XDOT =       1608
240013                 XDOT =         465
930992
 YDOT =      15683
781897  feet/sec       YDOT =        4785
762669  meter/sec
 ZDOT =     -19741
711782                 ZDOT =       -6014
951303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22015141
81                 X    =        -6710215
22
 Y    =        -482829
72  feet           Y    =         -147166
50  meter
 Z    =       -1607428
24                 Z    =         -489944
13
 XDOT =       1729
603202                 XDOT =         527
183056
 YDOT =     -14073
503475  feet/sec       YDOT =       -4289
603859  meter/sec
 ZDOT =     -19732
232941                 ZDOT =       -6014
384600


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   08280
45483664  
00020000  00000-0  20000-3 0  9041
2 25544  51
6407 165
8510 0004163 189
5631 170
5453 15
72041024  6049


Satellite: ISS
Catalog Number: 25544
Epoch time:      08280
45483664   =   yrday
fracday
Element set:     904
Inclination:       51
6407  deg
RA of node:       165
8510  deg
Eccentricity:     
0004163     
Arg of perigee:   189
5631  deg
Mean anomaly:     170
5453  deg
Mean motion:   15
72041024  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             604
Checksum:              272


Coasting Arc #6 (Orbit 619)
---------------------------------------

Vector Time (GMT): 2008/281/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1557631
39                 A    =         6725460
35  meter
 Y    =       -3864038
70  meter          E    =           
0004479
 Z    =        5278649
09                 I    =           51
73222
 XDOT =       7196
763233                 Wp   =          163
61067
 YDOT =      -2733
867706  meter/sec      RA   =          159
89325  deg
 ZDOT =        118
166985                 TA   =          285
24450
                                          MA   =          285
29401
                                          Ha   =            193
239  n
mi
                                          Hp   =            186
945

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5110339
21                 X    =        -1539950
35
 Y    =      -12677292
32  feet           Y    =        -3881358
14  meter
 Z    =       17318402
51                 Z    =         5271125
00
 XDOT =      23611
427931                 XDOT =        7226
224861
 YDOT =      -8969
382236  feet/sec       YDOT =       -2653
224616  meter/sec
 ZDOT =        387
686959                 ZDOT =         153
200862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2530506
40                 X    =          771298
35
 Y    =       13470248
89  feet           Y    =         4105731
86  meter
 Z    =       17288878
08                 Z    =         5269650
04
 XDOT =     -23954
901046                 XDOT =       -7301
453839
 YDOT =       3810
940736  feet/sec       YDOT =        1161
574736  meter/sec
 ZDOT =        523
047444                 ZDOT =         159
424861


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   08281
47191248  
00020000  00000-0  20000-3 0  9059
2 25544  51
6405 160
6429 0004107 195
7019 164
4017 15
72123363  6209


Satellite: ISS
Catalog Number: 25544
Epoch time:      08281
47191248   =   yrday
fracday
Element set:     905
Inclination:       51
6405  deg
RA of node:       160
6429  deg
Eccentricity:     
0004107     
Arg of perigee:   195
7019  deg
Mean anomaly:     164
4017  deg
Mean motion:   15
72123363  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             620
Checksum:              270


Coasting Arc #7 (Orbit 634)
---------------------------------------

Vector Time (GMT): 2008/282/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5794683
82                 A    =         6737301
97  meter
 Y    =        3356109
42  meter          E    =           
0006892
 Z    =        -719561
91                 I    =           51
79972
 XDOT =      -2951
615040                 Wp   =           51
84198
 YDOT =      -3820
958450  meter/sec      RA   =          154
77255  deg
 ZDOT =       5991
055596                 TA   =          300
34424
                                          MA   =          300
41238
                                          Ha   =            193
087  n
mi
                                          Hp   =            187
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19011429
85                 X    =        -5828286
17
 Y    =       11010857
69  feet           Y    =         3291122
03  meter
 Z    =       -2360767
41                 Z    =         -747794
44
 XDOT =      -9683
776379                 XDOT =       -2937
772849
 YDOT =     -12535
952921  feet/sec       YDOT =       -3853
887608  meter/sec
 ZDOT =      19655
694211                 ZDOT =        5976
750201

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20713444
00                 X    =         6313457
73
 Y    =       -7286993
92  feet           Y    =        -2221075
75  meter
 Z    =       -2469743
37                 Z    =         -752777
78
 XDOT =       6763
540559                 XDOT =        2061
527163
 YDOT =      12628
134919  feet/sec       YDOT =        3849
055523  meter/sec
 ZDOT =      19599
913669                 ZDOT =        5974
053686


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   08282
42540833  
00020000  00000-0  20000-3 0  9064
2 25544  51
6411 155
7598 0004023 198
9276 161
1737 15
72112336  6352


Satellite: ISS
Catalog Number: 25544
Epoch time:      08282
42540833   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:       155
7598  deg
Eccentricity:     
0004023     
Arg of perigee:   198
9276  deg
Mean anomaly:     161
1737  deg
Mean motion:   15
72112336  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             635
Checksum:              288


Coasting Arc #8 (Orbit 650)
---------------------------------------

Vector Time (GMT): 2008/283/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3467354
38                 A    =         6726112
86  meter
 Y    =        2649374
47  meter          E    =           
0012024
 Z    =       -5128539
30                 I    =           51
78898
 XDOT =      -5842
069015                 Wp   =           94
54062
 YDOT =       4773
192854  meter/sec      RA   =          149
68182  deg
 ZDOT =      -1487
871877                 TA   =          161
22523
                                          MA   =          161
18084
                                          Ha   =            192
929  n
mi
                                          Hp   =            187
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11375834
59                 X    =         3462384
69
 Y    =        8692173
46  feet           Y    =         2688120
46  meter
 Z    =      -16825916
35                 Z    =        -5111706
91
 XDOT =     -19166
893093                 XDOT =       -5887
781553
 YDOT =      15660
081543  feet/sec       YDOT =        4707
607819  meter/sec
 ZDOT =      -4881
469412                 ZDOT =       -1516
364111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9838288
50                 X    =        -2998710
33
 Y    =      -10505706
04  feet           Y    =        -3202139
20  meter
 Z    =      -16760464
58                 Z    =        -5108589
61
 XDOT =      20743
570277                 XDOT =        6322
640220
 YDOT =     -11483
320152  feet/sec       YDOT =       -3500
115982  meter/sec
 ZDOT =      -4991
316217                 ZDOT =       -1521
353183


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   08283
44245227  
00020000  00000-0  20000-3 0  9077
2 25544  51
6417 150
5513 0003966 203
2167 156
8817 15
72161072  6511


Satellite: ISS
Catalog Number: 25544
Epoch time:      08283
44245227   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:       150
5513  deg
Eccentricity:     
0003966     
Arg of perigee:   203
2167  deg
Mean anomaly:     156
8817  deg
Mean motion:   15
72161072  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             651
Checksum:              280


Coasting Arc #9 (Orbit 666)
---------------------------------------

Vector Time (GMT): 2008/284/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4275148
53                 A    =         6735932
11  meter
 Y    =       -4846691
37  meter          E    =           
0014458
 Z    =        1868558
28                 I    =           51
84638
 XDOT =       4801
765161                 Wp   =          129
63103
 YDOT =       2043
920172  meter/sec      RA   =          144
54358  deg
 ZDOT =      -5664
770407                 TA   =           29
68508
                                          MA   =           29
60311
                                          Ha   =            192
864  n
mi
                                          Hp   =            187
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14026077
85                 X    =         4319950
07
 Y    =      -15901218
39  feet           Y    =        -4798633
58  meter
 Z    =        6130440
55                 Z    =         1889436
25
 XDOT =      15753
822706                 XDOT =        4806
071536
 YDOT =       6705
774844  feet/sec       YDOT =        2097
640039  meter/sec
 ZDOT =     -18585
204748                 ZDOT =       -5641
432863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16245189
01                 X    =        -4951533
61
 Y    =       13589764
60  feet           Y    =         4142160
25  meter
 Z    =        6210800
25                 Z    =         1893051
92
 XDOT =     -13665
521032                 XDOT =       -4165
250811
 YDOT =      -7853
979851  feet/sec       YDOT =       -2393
893058  meter/sec
 ZDOT =     -18494
617391                 ZDOT =       -5637
159381


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   08284
45948055  
00020000  00000-0  20000-3 0  9089
2 25544  51
6415 145
3429 0004049 206
3144 153
7813 15
72137957  6673


Satellite: ISS
Catalog Number: 25544
Epoch time:      08284
45948055   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:       145
3429  deg
Eccentricity:     
0004049     
Arg of perigee:   206
3144  deg
Mean anomaly:     153
7813  deg
Mean motion:   15
72137957  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             667
Checksum:              304


Coasting Arc #10 (Orbit 682)
---------------------------------------

Vector Time (GMT): 2008/285/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4738928
87                 A    =         6727849
23  meter
 Y    =        -812218
71  meter          E    =           
0008523
 Z    =        4704886
63                 I    =           51
84289
 XDOT =       3796
817064                 Wp   =          144
76835
 YDOT =      -6100
572767  meter/sec      RA   =          139
47434  deg
 ZDOT =       2761
841214                 TA   =          278
03698
                                          MA   =          278
13368
                                          Ha   =            192
734  n
mi
                                          Hp   =            187
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15547666
90                 X    =        -4752350
08
 Y    =       -2664759
55  feet           Y    =         -865286
83  meter
 Z    =       15435979
76                 Z    =         4681832
09
 XDOT =      12456
748899                 XDOT =        3851
335773
 YDOT =     -20015
002518  feet/sec       YDOT =       -6057
809525  meter/sec
 ZDOT =       9061
158839                 ZDOT =        2780
419272

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15133116
62                 X    =         4612573
95
 Y    =        4750866
15  feet           Y    =         1448064
00  meter
 Z    =       15346609
16                 Z    =         4677646
47
 XDOT =     -14646
277484                 XDOT =       -4464
185377
 YDOT =      17053
888271  feet/sec       YDOT =        5198
025145  meter/sec
 ZDOT =       9132
488766                 ZDOT =        2783
582576


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   08285
47648949  
00020000  00000-0  20000-3 0  9092
2 25544  51
6417 140
1340 0003916 212
5208 147
5714 15
72186207  6833


Satellite: ISS
Catalog Number: 25544
Epoch time:      08285
47648949   =   yrday
fracday
Element set:     909
Inclination:       51
6417  deg
RA of node:       140
1340  deg
Eccentricity:     
0003916     
Arg of perigee:   212
5208  deg
Mean anomaly:     147
5714  deg
Mean motion:   15
72186207  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             683
Checksum:              297


Coasting Arc #11 (Orbit 697)
---------------------------------------

Vector Time (GMT): 2008/286/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2289673
85                 A    =         6733523
23  meter
 Y    =        5621321
25  meter          E    =           
0002098
 Z    =       -2918285
73                 I    =           51
88361
 XDOT =      -5795
267752                 Wp   =          126
92768
 YDOT =        261
389899  meter/sec      RA   =          134
32306  deg
 ZDOT =       5051
693656                 TA   =          199
65351
                                          MA   =          199
66160
                                          Ha   =            192
397  n
mi
                                          Hp   =            187
375

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7512053
31                 X    =        -2338185
45
 Y    =       18442655
04  feet           Y    =         5595445
30  meter
 Z    =       -9574428
24                 Z    =        -2929527
49
 XDOT =     -19013
345642                 XDOT =       -5822
300571
 YDOT =        857
578408  feet/sec       YDOT =         196
433165  meter/sec
 ZDOT =      16573
798085                 ZDOT =        5023
474084

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9579719
25                 X    =         2919898
43
 Y    =      -17434642
75  feet           Y    =        -5314079
11  meter
 Z    =       -9617398
67                 Z    =        -2931383
11
 XDOT =      17804
510217                 XDOT =        5426
814714
 YDOT =        702
946803  feet/sec       YDOT =         214
258185  meter/sec
 ZDOT =      16464
528509                 ZDOT =        5018
388290


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   08286
42991948  
00020000  00000-0  20000-3 0  9100
2 25544  51
6414 135
2504 0003950 219
4869 140
6006 15
72218129  6987


Satellite: ISS
Catalog Number: 25544
Epoch time:      08286
42991948   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       135
2504  deg
Eccentricity:     
0003950     
Arg of perigee:   219
4869  deg
Mean anomaly:     140
6006  deg
Mean motion:   15
72218129  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             698
Checksum:              299


Coasting Arc #12 (Orbit 713)
---------------------------------------

Vector Time (GMT): 2008/287/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5192561
35                 A    =         6730063
99  meter
 Y    =       -1287249
26  meter          E    =           
0004163
 Z    =       -4086571
89                 I    =           51
89078
 XDOT =      -1416
202689                 Wp   =           96
86095
 YDOT =       6507
050150  meter/sec      RA   =          129
26723  deg
 ZDOT =      -3852
991134                 TA   =          133
62708
                                          MA   =          133
59254
                                          Ha   =            192
304  n
mi
                                          Hp   =            187
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17035962
43                 X    =         5226421
94
 Y    =       -4223258
73  feet           Y    =        -1228994
08  meter
 Z    =      -13407388
10                 Z    =        -4061263
49
 XDOT =      -4646
334281                 XDOT =       -1470
142757
 YDOT =      21348
589730  feet/sec       YDOT =        6490
911417  meter/sec
 ZDOT =     -12641
047026                 ZDOT =       -3860
002802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17451136
43                 X    =        -5319106
38
 Y    =        2476531
38  feet           Y    =          754846
76  meter
 Z    =      -13309493
45                 Z    =        -4056733
60
 XDOT =       6883
403441                 XDOT =        2098
061369
 YDOT =     -19506
091563  feet/sec       YDOT =       -5945
456708  meter/sec
 ZDOT =     -12667
551201                 ZDOT =       -3861
069606


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   08287
44689494  
00020000  00000-0  20000-3 0  9114
2 25544  51
6406 130
0411 0004061 224
9145 135
1689 15
72235966  7143


Satellite: ISS
Catalog Number: 25544
Epoch time:      08287
44689494   =   yrday
fracday
Element set:     911
Inclination:       51
6406  deg
RA of node:       130
0411  deg
Eccentricity:     
0004061     
Arg of perigee:   224
9145  deg
Mean anomaly:     135
1689  deg
Mean motion:   15
72235966  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             714
Checksum:              289


Coasting Arc #13 (Orbit 729)
---------------------------------------

Vector Time (GMT): 2008/288/10:10:29
885
Vector Time (MET): N/A
Weight (LBS)     : 628523
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         183177
45                 A    =         6730756
31  meter
 Y    =       -5558175
63  meter          E    =           
0008492
 Z    =        3783531
40                 I    =           51
91158
 XDOT =       5837
534733                 Wp   =           96
95148
 YDOT =      -2696
612705  meter/sec      RA   =          124
11199  deg
 ZDOT =      -4237
003697                 TA   =           37
43057
                                          MA   =           37
37145
                                          Ha   =            191
996  n
mi
                                          Hp   =            187
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         600975
90                 X    =          226936
02
 Y    =      -18235484
36  feet           Y    =        -5555882
29  meter
 Z    =       12413160
77                 Z    =         3784528
01
 XDOT =      19152
016842                 XDOT =        5887
838019
 YDOT =      -8847
154543  feet/sec       YDOT =       -2631
053074  meter/sec
 ZDOT =     -13900
930763                 ZDOT =       -4208
521754

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2054065
75                 X    =         -626079
24
 Y    =       18127125
64  feet           Y    =         5525147
90  meter
 Z    =       12416470
99                 Z    =         3784540
36
 XDOT =     -18582
492821                 XDOT =       -5663
943812
 YDOT =       7356
485787  feet/sec       YDOT =        2242
256868  meter/sec
 ZDOT =     -13790
878587                 ZDOT =       -4203
459793


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   08288
46385207  
00020000  00000-0  20000-3 0  9123
2 25544  51
6406 124
8317 0003911 230
4383 129
6434 15
72315614  7301


Satellite: ISS
Catalog Number: 25544
Epoch time:      08288
46385207   =   yrday
fracday
Element set:     912
Inclination:       51
6406  deg
RA of node:       124
8317  deg
Eccentricity:     
0003911     
Arg of perigee:   230
4383  deg
Mean anomaly:     129
6434  deg
Mean motion:   15
72315614  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             730
Checksum:              276

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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