Date: March 14th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7104 18 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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


075/02:53:16 462 -2 3 8 7 8 7
N/A 5 4 -0 3 186 2
000/00:12:32 924 -6 4 0 0 178 5

Coasting Arc #1 (Orbit 3581)
---------------------------------------

Vector Time (GMT): 2007/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5114696
53                 A    =         6709340
97  meter
 Y    =       -1173158
84  meter          E    =           
0014080
 Z    =       -4166935
41                 I    =           51
37279
 XDOT =      -1445
777579                 Wp   =          331
55214
 YDOT =      -6643
337627  meter/sec      RA   =          232
30300  deg
 ZDOT =       3652
164133                 TA   =          335
69700
                                          MA   =          335
76334
                                          Ha   =            185
498  n
mi
                                          Hp   =            173
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16780500
43                 X    =        -5080956
10
 Y    =       -3848946
31  feet           Y    =        -1230165
64  meter
 Z    =      -13671047
93                 Z    =        -4191700
20
 XDOT =      -4743
364760                 XDOT =       -1389
124618
 YDOT =     -21795
727124  feet/sec       YDOT =       -6659
188302  meter/sec
 ZDOT =      11982
165791                 ZDOT =        3645
278378

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15895793
33                 X    =        -4845037
81
 Y    =       -6416025
18  feet           Y    =        -1955604
47  meter
 Z    =      -13764283
83                 Z    =        -4195353
71
 XDOT =      -1806
924698                 XDOT =        -550
750648
 YDOT =     -21120
932572  feet/sec       YDOT =       -6437
660248  meter/sec
 ZDOT =      11955
368232                 ZDOT =        3643
996237


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   07073
50929144  
00020000  00000-0  20000-3 0  9000
2 25544  51
6307 233
1680 0021018 316
4053  43
5451 15
79321604 35829


Satellite: ISS
Catalog Number: 25544
Epoch time:      07073
50929144   =   yrday
fracday
Element set:     900
Inclination:       51
6307  deg
RA of node:       233
1680  deg
Eccentricity:     
0021018     
Arg of perigee:   316
4053  deg
Mean anomaly:      43
5451  deg
Mean motion:   15
79321604  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3582
Checksum:              261


Coasting Arc #2 (Orbit 3597)
---------------------------------------

Vector Time (GMT): 2007/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -57686
38                 A    =         6708519
49  meter
 Y    =        5084879
91  meter          E    =           
0020148
 Z    =       -4382548
62                 I    =           51
38921
 XDOT =      -6312
777045                 Wp   =          346
69963
 YDOT =      -2933
576996  meter/sec      RA   =          227
15822  deg
 ZDOT =      -3298
257813                 TA   =          249
96439
                                          MA   =          250
18141
                                          Ha   =            185
839  n
mi
                                          Hp   =            173
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -189259
79                 X    =          -93252
75
 Y    =       16682676
88  feet           Y    =         5084035
82  meter
 Z    =      -14378440
35                 Z    =        -4382915
42
 XDOT =     -20711
210779                 XDOT =       -6263
482172
 YDOT =      -9624
596445  feet/sec       YDOT =       -3003
894491  meter/sec
 ZDOT =     -10821
055818                 ZDOT =       -3328
804829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2435642
49                 X    =         -742383
83
 Y    =       16504422
16  feet           Y    =         5030547
88  meter
 Z    =      -14379108
76                 Z    =        -4382752
35
 XDOT =     -17902
406276                 XDOT =       -5456
653433
 YDOT =     -12233
821993  feet/sec       YDOT =       -3728
868944  meter/sec
 ZDOT =     -10936
281002                 ZDOT =       -3333
378450


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   07074
52168518  
00020000  00000-0  20000-3 0  9014
2 25544  51
6310 227
9272 0021099 320
6748  39
2884 15
79379565 35986


Satellite: ISS
Catalog Number: 25544
Epoch time:      07074
52168518   =   yrday
fracday
Element set:     901
Inclination:       51
6310  deg
RA of node:       227
9272  deg
Eccentricity:     
0021099     
Arg of perigee:   320
6748  deg
Mean anomaly:      39
2884  deg
Mean motion:   15
79379565  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3598
Checksum:              322


Coasting Arc #3 (Orbit 3607)
---------------------------------------

Vector Time (GMT): 2007/075/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4198424
04                 A    =         6721335
03  meter
 Y    =        5153124
84  meter          E    =           
0005661
 Z    =       -1005069
12                 I    =           51
43031
 XDOT =      -4330
860188                 Wp   =          298
43526
 YDOT =       2370
728042  meter/sec      RA   =          223
90372  deg
 ZDOT =      -5908
217667                 TA   =          252
58898
                                          MA   =          252
65089
                                          Ha   =            186
229  n
mi
                                          Hp   =            178
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13774357
07                 X    =         4145371
36
 Y    =       16906577
57  feet           Y    =         5199777
29  meter
 Z    =       -3297470
87                 Z    =         -984802
73
 XDOT =     -14208
858886                 XDOT =       -4328
347676
 YDOT =       7777
979139  feet/sec       YDOT =        2322
311690  meter/sec
 ZDOT =     -19383
916231                 ZDOT =       -5929
250563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21232939
43                 X    =        -6471799
94
 Y    =       -5022829
42  feet           Y    =        -1530958
41  meter
 Z    =       -3220568
25                 Z    =         -981629
20
 XDOT =       6089
883559                 XDOT =        1856
196509
 YDOT =     -13204
584023  feet/sec       YDOT =       -4024
757210  meter/sec
 ZDOT =     -19462
641900                 ZDOT =       -5932
213251


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   07075
15445816  
00020000  00000-0  20000-3 0  9024
2 25544  51
6325 224
6558 0015260 313
3331  46
6561 15
77667967 36083


Satellite: ISS
Catalog Number: 25544
Epoch time:      07075
15445816   =   yrday
fracday
Element set:     902
Inclination:       51
6325  deg
RA of node:       224
6558  deg
Eccentricity:     
0015260     
Arg of perigee:   313
3331  deg
Mean anomaly:      46
6561  deg
Mean motion:   15
77667967  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3608
Checksum:              299


Coasting Arc #4 (Orbit 3623)
---------------------------------------

Vector Time (GMT): 2007/076/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4574893
71                 A    =         6711597
03  meter
 Y    =       -1209755
10  meter          E    =           
0015487
 Z    =        4768875
62                 I    =           51
41949
 XDOT =       4205
047408                 Wp   =          344
65961
 YDOT =       5938
481589  meter/sec      RA   =          218
69469  deg
 ZDOT =      -2514
682631                 TA   =          130
10610
                                          MA   =          129
97026
                                          Ha   =            186
388  n
mi
                                          Hp   =            178
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15009493
79                 X    =         4564915
46
 Y    =       -3969012
78  feet           Y    =        -1158651
49  meter
 Z    =       15645917
40                 Z    =         4791075
88
 XDOT =      13796
087296                 XDOT =        4150
545563
 YDOT =      19483
207313  feet/sec       YDOT =        5985
199847  meter/sec
 ZDOT =      -8250
271100                 ZDOT =       -2494
387768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9214095
99                 X    =        -2808456
46
 Y    =       12390539
61  feet           Y    =         3776636
47  meter
 Z    =       15729197
71                 Z    =         4794259
46
 XDOT =     -22054
188464                 XDOT =       -6722
116644
 YDOT =      -5971
683953  feet/sec       YDOT =       -1820
169269  meter/sec
 ZDOT =      -8173
137483                 ZDOT =       -2491
172305


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   07076
16791058  
00020000  00000-0  20000-3 0  9039
2 25544  51
6323 219
4217 0015347 317
5309  42
4668 15
77719211 36242


Satellite: ISS
Catalog Number: 25544
Epoch time:      07076
16791058   =   yrday
fracday
Element set:     903
Inclination:       51
6323  deg
RA of node:       219
4217  deg
Eccentricity:     
0015347     
Arg of perigee:   317
5309  deg
Mean anomaly:      42
4668  deg
Mean motion:   15
77719211  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3624
Checksum:              293


Coasting Arc #5 (Orbit 3639)
---------------------------------------

Vector Time (GMT): 2007/077/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2942378
56                 A    =         6716935
49  meter
 Y    =       -5070439
06  meter          E    =           
0012968
 Z    =        3262372
47                 I    =           51
46155
 XDOT =       6074
428203                 Wp   =           14
85323
 YDOT =       -488
760368  meter/sec      RA   =          213
56080  deg
 ZDOT =       4727
190109                 TA   =           23
58566
                                          MA   =           23
52625
                                          Ha   =            186
668  n
mi
                                          Hp   =            177
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9653472
96                 X    =        -2901309
27
 Y    =      -16635298
74  feet           Y    =        -5103112
41  meter
 Z    =       10703321
74                 Z    =         3248178
89
 XDOT =      19929
226389                 XDOT =        6056
478642
 YDOT =      -1603
544514  feet/sec       YDOT =        -420
932584  meter/sec
 ZDOT =      15509
153902                 ZDOT =        4756
655678

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18070832
57                 X    =         5507989
77
 Y    =        6672520
78  feet           Y    =         2033784
33  meter
 Z    =       10649238
34                 Z    =         3245887
84
 XDOT =     -13815
404838                 XDOT =       -4210
935395
 YDOT =      12529
747958  feet/sec       YDOT =        3819
067178  meter/sec
 ZDOT =      15619
851581                 ZDOT =        4760
930762


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   07077
18133772  
00020000  00000-0  20000-3 0  9046
2 25544  51
6330 214
1867 0015392 321
7211  38
2860 15
77744817 36407


Satellite: ISS
Catalog Number: 25544
Epoch time:      07077
18133772   =   yrday
fracday
Element set:     904
Inclination:       51
6330  deg
RA of node:       214
1867  deg
Eccentricity:     
0015392     
Arg of perigee:   321
7211  deg
Mean anomaly:      38
2860  deg
Mean motion:   15
77744817  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3640
Checksum:              285


Coasting Arc #6 (Orbit 3654)
---------------------------------------

Vector Time (GMT): 2007/078/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5878006
65                 A    =         6716734
51  meter
 Y    =        -256354
00  meter          E    =           
0013824
 Z    =       -3221992
27                 I    =           51
48730
 XDOT =      -2364
845513                 Wp   =          342
85106
 YDOT =      -5584
494351  meter/sec      RA   =          208
33326  deg
 ZDOT =       4766
447814                 TA   =          339
28071
                                          MA   =          339
33670
                                          Ha   =            186
683  n
mi
                                          Hp   =            177
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19284798
71                 X    =        -5859051
47
 Y    =        -841056
43  feet           Y    =         -321979
55  meter
 Z    =      -10570840
77                 Z    =        -3250501
30
 XDOT =      -7758
679503                 XDOT =       -2325
377479
 YDOT =     -18321
831860  feet/sec       YDOT =       -5610
718156  meter/sec
 ZDOT =      15637
952145                 ZDOT =        4755
056001

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15177853
99                 X    =         4626209
90
 Y    =      -11830699
36  feet           Y    =        -3605997
16  meter
 Z    =      -10678052
85                 Z    =        -3254670
51
 XDOT =      16993
062842                 XDOT =        5179
485554
 YDOT =       7748
761023  feet/sec       YDOT =        2361
822360  meter/sec
 ZDOT =      15594
322489                 ZDOT =        4753
149495


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   07078
13140106  
00020000  00000-0  20000-3 0  9052
2 25544  51
6339 209
2795 0015462 325
3093  34
7062 15
77803066 36550


Satellite: ISS
Catalog Number: 25544
Epoch time:      07078
13140106   =   yrday
fracday
Element set:     905
Inclination:       51
6339  deg
RA of node:       209
2795  deg
Eccentricity:     
0015462     
Arg of perigee:   325
3093  deg
Mean anomaly:      34
7062  deg
Mean motion:   15
77803066  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3655
Checksum:              284


Coasting Arc #7 (Orbit 3670)
---------------------------------------

Vector Time (GMT): 2007/079/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         999481
62                 A    =         6711176
97  meter
 Y    =        4587456
19  meter          E    =           
0017359
 Z    =       -4804864
29                 I    =           51
49533
 XDOT =      -7235
389198                 Wp   =           11
50291
 YDOT =       -992
109287  meter/sec      RA   =          203
20324  deg
 ZDOT =      -2437
046834                 TA   =          234
55643
                                          MA   =          234
71860
                                          Ha   =            186
981  n
mi
                                          Hp   =            177
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3279139
17                 X    =          971450
86
 Y    =       15050709
30  feet           Y    =         4598475
72  meter
 Z    =      -15763990
44                 Z    =        -4800077
39
 XDOT =     -23738
153538                 XDOT =       -7211
918828
 YDOT =      -3254
951728  feet/sec       YDOT =       -1072
888488  meter/sec
 ZDOT =      -7995
560478                 ZDOT =       -2472
139167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12482877
51                 X    =        -3804781
07
 Y    =       -9057716
69  feet           Y    =        -2760792
05  meter
 Z    =      -15745333
79                 Z    =        -4799177
74
 XDOT =      19258
664081                 XDOT =        5870
040812
 YDOT =     -12325
752315  feet/sec       YDOT =       -3756
889306  meter/sec
 ZDOT =      -8127
631443                 ZDOT =       -2477
302064


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   07079
14477685  
00020000  00000-0  20000-3 0  9060
2 25544  51
6346 204
0454 0015577 329
4896  30
5362 15
77858225 36718


Satellite: ISS
Catalog Number: 25544
Epoch time:      07079
14477685   =   yrday
fracday
Element set:     906
Inclination:       51
6346  deg
RA of node:       204
0454  deg
Eccentricity:     
0015577     
Arg of perigee:   329
4896  deg
Mean anomaly:      30
5362  deg
Mean motion:   15
77858225  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3671
Checksum:              320


Coasting Arc #8 (Orbit 3686)
---------------------------------------

Vector Time (GMT): 2007/080/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6521096
65                 A    =         6720869
10  meter
 Y    =        1385313
58  meter          E    =           
0007230
 Z    =         878947
20                 I    =           51
55491
 XDOT =       -232
728170                 Wp   =           35
27987
 YDOT =       4885
555853  meter/sec      RA   =          198
00133  deg
 ZDOT =      -5943
432324                 TA   =          135
11287
                                          MA   =          135
05439
                                          Ha   =            187
146  n
mi
                                          Hp   =            177
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21394674
06                 X    =         6500851
44
 Y    =        4544992
05  feet           Y    =         1458123
01  meter
 Z    =        2883685
03                 Z    =          910577
48
 XDOT =       -763
543866                 XDOT =        -258
469655
 YDOT =      16028
726552  feet/sec       YDOT =        4882
808939  meter/sec
 ZDOT =     -19499
449883                 ZDOT =       -5944
625850

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18849431
14                 X    =        -5745306
61
 Y    =       11062856
62  feet           Y    =         3371958
70  meter
 Z    =        3002801
90                 Z    =          915254
02
 XDOT =      -9520
356029                 XDOT =       -2901
804518
 YDOT =     -10901
754743  feet/sec       YDOT =       -3322
854846  meter/sec
 ZDOT =     -19503
236192                 ZDOT =       -5944
586391


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   07080
15812748  
00020000  00000-0  20000-3 0  9077
2 25544  51
6344 198
8106 0015507 333
1810  26
8552 15
77851071 36879


Satellite: ISS
Catalog Number: 25544
Epoch time:      07080
15812748   =   yrday
fracday
Element set:     907
Inclination:       51
6344  deg
RA of node:       198
8106  deg
Eccentricity:     
0015507     
Arg of perigee:   333
1810  deg
Mean anomaly:      26
8552  deg
Mean motion:   15
77851071  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3687
Checksum:              298


Coasting Arc #9 (Orbit 3702)
---------------------------------------

Vector Time (GMT): 2007/081/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1471025
48                 A    =         6708942
28  meter
 Y    =       -3931314
73  meter          E    =           
0015830
 Z    =        5237783
58                 I    =           51
54336
 XDOT =       7399
098245                 Wp   =          346
88730
 YDOT =       2088
995840  meter/sec      RA   =          192
83375  deg
 ZDOT =       -495
215216                 TA   =          107
90739
                                          MA   =          107
73472
                                          Ha   =            187
210  n
mi
                                          Hp   =            176
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4826199
07                 X    =         1489432
35
 Y    =      -12898014
21  feet           Y    =        -3914761
72  meter
 Z    =       17184329
33                 Z    =         5244974
76
 XDOT =      24275
256710                 XDOT =        7377
594553
 YDOT =       6853
660891  feet/sec       YDOT =        2171
616437  meter/sec
 ZDOT =      -1624
721836                 ZDOT =        -459
322581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5424450
91                 X    =         1653372
64
 Y    =       12622028
49  feet           Y    =         3847194
28  meter
 Z    =       17210806
82                 Z    =         5245853
92
 XDOT =     -21433
403646                 XDOT =       -6532
901431
 YDOT =      11308
665941  feet/sec       YDOT =        3446
881379  meter/sec
 ZDOT =      -1489
471548                 ZDOT =        -453
990928


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   07081
17144876  
00020000  00000-0  20000-3 0  9081
2 25544  51
6345 193
5755 0015738 336
9444  23
1014 15
77948783 37031


Satellite: ISS
Catalog Number: 25544
Epoch time:      07081
17144876   =   yrday
fracday
Element set:     908
Inclination:       51
6345  deg
RA of node:       193
5755  deg
Eccentricity:     
0015738     
Arg of perigee:   336
9444  deg
Mean anomaly:      23
1014  deg
Mean motion:   15
77948783  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3703
Checksum:              314


Coasting Arc #10 (Orbit 3718)
---------------------------------------

Vector Time (GMT): 2007/082/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6098273
06                 A    =         6719735
15  meter
 Y    =       -2194922
63  meter          E    =           
0022489
 Z    =        1716211
57                 I    =           51
60760
 XDOT =       3104
429443                 Wp   =           20
00035
 YDOT =      -4153
228409  meter/sec      RA   =          187
68341  deg
 ZDOT =       5718
258659                 TA   =          359
06165
                                          MA   =          359
06586
                                          Ha   =            187
531  n
mi
                                          Hp   =            176
310

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20007457
55                 X    =        -6081612
95
 Y    =       -7201189
72  feet           Y    =        -2263023
74  meter
 Z    =        5630615
40                 Z    =         1686626
60
 XDOT =      10185
135967                 XDOT =        3122
862365
 YDOT =     -13626
077457  feet/sec       YDOT =       -4118
409751  meter/sec
 ZDOT =      18760
691140                 ZDOT =        5733
384886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19358130
22                 X    =         5900358
09
 Y    =       -8869166
76  feet           Y    =        -2703322
03  meter
 Z    =        5519057
54                 Z    =         1682208
74
 XDOT =       1679
631407                 XDOT =         511
951653
 YDOT =      15377
655913  feet/sec       YDOT =        4687
109522  meter/sec
 ZDOT =      18816
981000                 ZDOT =        5735
415809


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   07082
18474653  
00020000  00000-0  20000-3 0  9093
2 25544  51
6341 188
3403 0015896 341
1766  18
8810 15
77950749 37196


Satellite: ISS
Catalog Number: 25544
Epoch time:      07082
18474653   =   yrday
fracday
Element set:     909
Inclination:       51
6341  deg
RA of node:       188
3403  deg
Eccentricity:     
0015896     
Arg of perigee:   341
1766  deg
Mean anomaly:      18
8810  deg
Mean motion:   15
77950749  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3719
Checksum:              321


Coasting Arc #11 (Orbit 3733)
---------------------------------------

Vector Time (GMT): 2007/083/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3846515
54                 A    =         6712286
11  meter
 Y    =        3313481
87  meter          E    =           
0012838
 Z    =       -4388061
10                 I    =           51
61149
 XDOT =      -6305
215316                 Wp   =           21
12014
 YDOT =      -2919
206680  meter/sec      RA   =          182
47508  deg
 ZDOT =       3337
515698                 TA   =          282
33991
                                          MA   =          282
48360
                                          Ha   =            187
518  n
mi
                                          Hp   =            175
946

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12619801
63                 X    =        -3861965
10
 Y    =       10871003
50  feet           Y    =         3270381
58  meter
 Z    =      -14396525
93                 Z    =        -4406785
00
 XDOT =     -20686
401956                 XDOT =       -6288
316746
 YDOT =      -9577
449737  feet/sec       YDOT =       -2989
620628  meter/sec
 ZDOT =      10949
854653                 ZDOT =        3306
926045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1073317
82                 X    =          327147
27
 Y    =      -16561014
68  feet           Y    =        -5047797
27  meter
 Z    =      -14466473
34                 Z    =        -4409381
07
 XDOT =      20183
914294                 XDOT =        6152
057077
 YDOT =      -8113
863483  feet/sec       YDOT =       -2473
105589  meter/sec
 ZDOT =      10834
405203                 ZDOT =        3302
326706


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   07083
13468714  
00020000  00000-0  20000-3 0  9102
2 25544  51
6337 183
4324 0015932 344
4301  15
6372 15
78006514 37349


Satellite: ISS
Catalog Number: 25544
Epoch time:      07083
13468714   =   yrday
fracday
Element set:     910
Inclination:       51
6337  deg
RA of node:       183
4324  deg
Eccentricity:     
0015932     
Arg of perigee:   344
4301  deg
Mean anomaly:      15
6372  deg
Mean motion:   15
78006514  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3734
Checksum:              273


Coasting Arc #12 (Orbit 3749)
---------------------------------------

Vector Time (GMT): 2007/084/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4616909
43                 A    =         6714090
08  meter
 Y    =        2902276
03  meter          E    =           
0017841
 Z    =       -3932797
83                 I    =           51
64560
 XDOT =      -5592
267784                 Wp   =           10
36534
 YDOT =       3437
544770  meter/sec      RA   =          177
35805  deg
 ZDOT =      -4013
822323                 TA   =          217
87161
                                          MA   =          217
99724
                                          Ha   =            187
729  n
mi
                                          Hp   =            175
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15147340
66                 X    =         4603217
35
 Y    =        9521902
98  feet           Y    =         2953828
35  meter
 Z    =      -12902880
02                 Z    =        -3910402
25
 XDOT =     -18347
335248                 XDOT =       -5610
792956
 YDOT =      11278
034021  feet/sec       YDOT =        3374
905337  meter/sec
 ZDOT =     -13168
708409                 ZDOT =       -4041
034399

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17394471
72                 X    =        -5301834
98
 Y    =        4440493
53  feet           Y    =         1353462
43  meter
 Z    =      -12818238
93                 Z    =        -3906999
23
 XDOT =       4775
398261                 XDOT =        1455
541390
 YDOT =     -19738
927313  feet/sec       YDOT =       -6016
425045  meter/sec
 ZDOT =     -13270
573515                 ZDOT =       -4044
870807


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   07084
14793212  
00020000  00000-0  20000-3 0  9119
2 25544  51
6330 178
1970 0015977 348
0424  12
0360 15
78028527 37509


Satellite: ISS
Catalog Number: 25544
Epoch time:      07084
14793212   =   yrday
fracday
Element set:     911
Inclination:       51
6330  deg
RA of node:       178
1970  deg
Eccentricity:     
0015977     
Arg of perigee:   348
0424  deg
Mean anomaly:      12
0360  deg
Mean motion:   15
78028527  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3750
Checksum:              280


Coasting Arc #13 (Orbit 3765)
---------------------------------------

Vector Time (GMT): 2007/085/02:59:32
924
Vector Time (MET): N/A
Weight (LBS)     : 478706
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5696376
04                 A    =         6718027
23  meter
 Y    =       -2672123
42  meter          E    =           
0016576
 Z    =        2365142
83                 I    =           51
68876
 XDOT =       4012
899798                 Wp   =           43
36262
 YDOT =       3749
227379  meter/sec      RA   =          172
14580  deg
 ZDOT =      -5394
996577                 TA   =          109
99456
                                          MA   =          109
81599
                                          Ha   =            187
822  n
mi
                                          Hp   =            175
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18688897
78                 X    =         5714343
42
 Y    =       -8766809
13  feet           Y    =        -2608322
89  meter
 Z    =        7759654
96                 Z    =         2392859
20
 XDOT =      13165
681752                 XDOT =        3996
884811
 YDOT =      12300
614759  feet/sec       YDOT =        3794
012315  meter/sec
 ZDOT =     -17700
120003                 ZDOT =       -5375
541010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6188186
24                 X    =        -1886159
17
 Y    =       19652359
17  feet           Y    =         5990039
08  meter
 Z    =        7863537
21                 Z    =         2396806
14
 XDOT =     -16601
127814                 XDOT =       -5060
023758
 YDOT =       1869
656676  feet/sec       YDOT =         569
871355  meter/sec
 ZDOT =     -17626
408664                 ZDOT =       -5372
529361


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   07085
16115068  
00020000  00000-0  20000-3 0  9120
2 25544  51
6333 172
9611 0016104 352
5528   7
5395 15
78101589 37668


Satellite: ISS
Catalog Number: 25544
Epoch time:      07085
16115068   =   yrday
fracday
Element set:     912
Inclination:       51
6333  deg
RA of node:       172
9611  deg
Eccentricity:     
0016104     
Arg of perigee:   352
5528  deg
Mean anomaly:       7
5395  deg
Mean motion:   15
78101589  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3766
Checksum:              290

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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