Date: January 23rd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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


There are no maneuvers



Coasting Arc #1 (Orbit 2776)
---------------------------------------

Vector Time (GMT): 2007/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         654396
00                 A    =         6715018
71  meter
 Y    =       -5197335
05  meter          E    =           
0030773
 Z    =        4170347
35                 I    =           51
84979
 XDOT =       6422
796474                 Wp   =          106
81626
 YDOT =      -2174
465182  meter/sec      RA   =          135
88507  deg
 ZDOT =      -3704
266869                 TA   =           20
80901
                                          MA   =           20
68401
                                          Ha   =            193
097  n
mi
                                          Hp   =            170
826

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2146968
52                 X    =          692206
42
 Y    =      -17051624
18  feet           Y    =        -5189805
94  meter
 Z    =       13682241
97                 Z    =         4173618
03
 XDOT =      21072
166910                 XDOT =        6464
628509
 YDOT =      -7134
072118  feet/sec       YDOT =       -2102
407897  meter/sec
 ZDOT =     -12153
106524                 ZDOT =       -3672
964156

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15715840
90                 X    =         4790188
31
 Y    =       -6932708
95  feet           Y    =        -2113089
69  meter
 Z    =       13693830
64                 Z    =         4173879
58
 XDOT =      16428
368506                 XDOT =        5007
366721
 YDOT =      13380
086818  feet/sec       YDOT =        4078
250462  meter/sec
 ZDOT =     -12035
954796                 ZDOT =       -3668
559022


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   07022
54102421  
00020000  00000-0  20000-3 0  9009
2 25544  51
6337 136
6096 0022838 120
5622 239
7801 15
77346637 27771


Satellite: ISS
Catalog Number: 25544
Epoch time:      07022
54102421   =   yrday
fracday
Element set:     900
Inclination:       51
6337  deg
RA of node:       136
6096  deg
Eccentricity:     
0022838     
Arg of perigee:   120
5622  deg
Mean anomaly:     239
7801  deg
Mean motion:   15
77346637  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2777
Checksum:              282


Coasting Arc #2 (Orbit 2792)
---------------------------------------

Vector Time (GMT): 2007/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5226939
35                 A    =         6715434
45  meter
 Y    =        1229046
91  meter          E    =           
0033013
 Z    =        4018922
24                 I    =           51
87190
 XDOT =       1520
987710                 Wp   =          117
29434
 YDOT =      -6469
004033  meter/sec      RA   =          130
79026  deg
 ZDOT =       3917
223801                 TA   =          292
32441
                                          MA   =          292
67403
                                          Ha   =            192
915  n
mi
                                          Hp   =            170
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17148751
15                 X    =        -5259817
06
 Y    =        4032306
12  feet           Y    =         1170412
46  meter
 Z    =       13185440
41                 Z    =         3993450
43
 XDOT =       4990
117158                 XDOT =        1574
183199
 YDOT =     -21223
766511  feet/sec       YDOT =       -6451
698138  meter/sec
 ZDOT =      12851
784125                 ZDOT =        3924
741710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12483232
72                 X    =        -3804889
33
 Y    =      -12530557
16  feet           Y    =        -3819313
82  meter
 Z    =       13090035
73                 Z    =         3989842
89
 XDOT =      19726
672186                 XDOT =        6012
689682
 YDOT =      -6062
431582  feet/sec       YDOT =       -1847
829146  meter/sec
 ZDOT =      12879
141837                 ZDOT =        3925
562432


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   07023
55466639  
00020000  00000-0  20000-3 0  9016
2 25544  51
6341 131
3771 0022671 124
4587 235
8724 15
77446193 27933


Satellite: ISS
Catalog Number: 25544
Epoch time:      07023
55466639   =   yrday
fracday
Element set:     901
Inclination:       51
6341  deg
RA of node:       131
3771  deg
Eccentricity:     
0022671     
Arg of perigee:   124
4587  deg
Mean anomaly:     235
8724  deg
Mean motion:   15
77446193  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2793
Checksum:              301


Coasting Arc #3 (Orbit 2807)
---------------------------------------

Vector Time (GMT): 2007/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1902478
90                 A    =         6719768
33  meter
 Y    =        5971174
70  meter          E    =           
0024057
 Z    =       -2460448
67                 I    =           51
90423
 XDOT =      -5490
128921                 Wp   =          115
06480
 YDOT =        447
509859  meter/sec      RA   =          125
59898  deg
 ZDOT =       5361
845902                 TA   =          217
26560
                                          MA   =          217
43276
                                          Ha   =            192
721  n
mi
                                          Hp   =            171
094

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6241728
67                 X    =        -1957155
79
 Y    =       19590468
19  feet           Y    =         5949594
47  meter
 Z    =       -8072338
15                 Z    =        -2469823
44
 XDOT =     -18012
233993                 XDOT =       -5520
771499
 YDOT =       1468
208198  feet/sec       YDOT =         385
944724  meter/sec
 ZDOT =      17591
357947                 ZDOT =        5335
100829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19833439
00                 X    =        -6045232
21
 Y    =        5368784
05  feet           Y    =         1636405
38  meter
 Z    =       -8106732
95                 Z    =        -2470932
20
 XDOT =     -10627
373331                 XDOT =       -3239
223391
 YDOT =     -13000
143295  feet/sec       YDOT =       -3962
443676  meter/sec
 ZDOT =      17491
068985                 ZDOT =        5331
277827


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   07024
50493443  
00020000  00000-0  20000-3 0  9026
2 25544  51
6340 126
4720 0022448 127
5421 232
7788 15
77427292 28086


Satellite: ISS
Catalog Number: 25544
Epoch time:      07024
50493443   =   yrday
fracday
Element set:     902
Inclination:       51
6340  deg
RA of node:       126
4720  deg
Eccentricity:     
0022448     
Arg of perigee:   127
5421  deg
Mean anomaly:     232
7788  deg
Mean motion:   15
77427292  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2808
Checksum:              284


Coasting Arc #4 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2007/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4320576
24                 A    =         6711007
24  meter
 Y    =         584783
13  meter          E    =           
0032651
 Z    =       -5124932
08                 I    =           51
89030
 XDOT =      -2739
949303                 Wp   =          111
87927
 YDOT =       7017
086960  meter/sec      RA   =          120
48890  deg
 ZDOT =      -1528
836750                 TA   =          143
58993
                                          MA   =          143
36741
                                          Ha   =            192
608  n
mi
                                          Hp   =            171
269

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14175118
90                 X    =         4338611
71
 Y    =        1918579
83  feet           Y    =          633199
27  meter
 Z    =      -16814081
64                 Z    =        -5103899
13
 XDOT =      -8989
334983                 XDOT =       -2810
784997
 YDOT =      23021
938845  feet/sec       YDOT =        6986
051321  meter/sec
 ZDOT =      -5015
868603                 ZDOT =       -1542
319044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6317069
81                 X    =         1925442
88
 Y    =       12936761
68  feet           Y    =         3943124
96  meter
 Z    =      -16735086
26                 Z    =        -5100854
29
 XDOT =     -23183
383473                 XDOT =       -7066
295283
 YDOT =       4851
324139  feet/sec       YDOT =        1478
683598  meter/sec
 ZDOT =      -5065
548253                 ZDOT =       -1543
979108


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   07025
51852607  
00020000  00000-0  20000-3 0  9030
2 25544  51
6338 121
2387 0022425 131
5973 228
7118 15
77473423 28244


Satellite: ISS
Catalog Number: 25544
Epoch time:      07025
51852607   =   yrday
fracday
Element set:     903
Inclination:       51
6338  deg
RA of node:       121
2387  deg
Eccentricity:     
0022425     
Arg of perigee:   131
5973  deg
Mean anomaly:     228
7118  deg
Mean motion:   15
77473423  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2824
Checksum:              286


Coasting Arc #5 (Orbit 2839)
---------------------------------------

Vector Time (GMT): 2007/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2761875
46                 A    =         6722192
08  meter
 Y    =       -6108059
60  meter          E    =           
0035133
 Z    =         149543
67                 I    =           51
94128
 XDOT =       4401
058053                 Wp   =          134
51006
 YDOT =       1820
691007  meter/sec      RA   =          115
33180  deg
 ZDOT =      -6075
676948                 TA   =           43
86680
                                          MA   =           43
58834
                                          Ha   =            192
511  n
mi
                                          Hp   =            171
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9061271
18                 X    =         2829244
93
 Y    =      -20039565
62  feet           Y    =        -6076798
10  meter
 Z    =         490628
83                 Z    =          163123
96
 XDOT =      14439
166839                 XDOT =        4409
885970
 YDOT =       5973
395691  feet/sec       YDOT =        1869
955851  meter/sec
 ZDOT =     -19933
323321                 ZDOT =       -6054
275262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21634190
65                 X    =         6594101
31
 Y    =       -3949793
29  feet           Y    =        -1203896
99  meter
 Z    =         540805
30                 Z    =          164837
46
 XDOT =       3075
870517                 XDOT =         937
525334
 YDOT =      13786
643427  feet/sec       YDOT =        4202
168917  meter/sec
 ZDOT =     -19852
781147                 ZDOT =       -6051
127694


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   07026
53209142  
00020000  00000-0  20000-3 0  9044
2 25544  51
6332 116
0058 0022527 135
1091 225
1900 15
77517275 28401


Satellite: ISS
Catalog Number: 25544
Epoch time:      07026
53209142   =   yrday
fracday
Element set:     904
Inclination:       51
6332  deg
RA of node:       116
0058  deg
Eccentricity:     
0022527     
Arg of perigee:   135
1091  deg
Mean anomaly:     225
1900  deg
Mean motion:   15
77517275  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2840
Checksum:              257


Coasting Arc #6 (Orbit 2855)
---------------------------------------

Vector Time (GMT): 2007/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3366249
38                 A    =         6710214
62  meter
 Y    =       -2595986
61  meter          E    =           
0023039
 Z    =        5174310
12                 I    =           51
91377
 XDOT =       3471
316234                 Wp   =          129
20940
 YDOT =      -6799
904225  meter/sec      RA   =          110
18107  deg
 ZDOT =      -1164
095462                 TA   =          331
76904
                                          MA   =          331
89373
                                          Ha   =            192
306  n
mi
                                          Hp   =            171
325

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11044125
28                 X    =        -3362106
07
 Y    =       -8517016
43  feet           Y    =        -2633607
18  meter
 Z    =       16976083
09                 Z    =         5157966
91
 XDOT =      11388
832790                 XDOT =        3552
750631
 YDOT =     -22309
397064  feet/sec       YDOT =       -6760
630606  meter/sec
 ZDOT =      -3819
210832                 ZDOT =       -1147
034819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         427649
67                 X    =          130347
62
 Y    =      -14014961
15  feet           Y    =        -4271760
16  meter
 Z    =       16914421
32                 Z    =         5155515
62
 XDOT =      23756
059902                 XDOT =        7240
847058
 YDOT =      -3765
025334  feet/sec       YDOT =       -1147
579722  meter/sec
 ZDOT =      -3756
048692                 ZDOT =       -1144
843641


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   07027
54562740  
00020000  00000-0  20000-3 0  9053
2 25544  51
6340 110
7724 0022241 138
8623 221
4223 15
77618481 28560


Satellite: ISS
Catalog Number: 25544
Epoch time:      07027
54562740   =   yrday
fracday
Element set:     905
Inclination:       51
6340  deg
RA of node:       110
7724  deg
Eccentricity:     
0022241     
Arg of perigee:   138
8623  deg
Mean anomaly:     221
4223  deg
Mean motion:   15
77618481  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2856
Checksum:              275


Coasting Arc #7 (Orbit 2871)
---------------------------------------

Vector Time (GMT): 2007/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3219780
63                 A    =         6719914
13  meter
 Y    =        5493980
21  meter          E    =           
0029860
 Z    =        2147834
43                 I    =           51
95493
 XDOT =      -3364
999730                 Wp   =          115
54866
 YDOT =      -4164
302581  meter/sec      RA   =          105
06837  deg
 ZDOT =       5535
595842                 TA   =          268
39423
                                          MA   =          268
73628
                                          Ha   =            192
140  n
mi
                                          Hp   =            171
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10563584
74                 X    =        -3291409
42
 Y    =       18024869
44  feet           Y    =         5457574
10  meter
 Z    =        7046700
87                 Z    =         2132019
58
 XDOT =     -11040
025360                 XDOT =       -3345
074305
 YDOT =     -13662
410043  feet/sec       YDOT =       -4201
821063  meter/sec
 ZDOT =      18161
403682                 ZDOT =        5519
296889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20790508
21                 X    =        -6336946
90
 Y    =        2250189
64  feet           Y    =          685857
80  meter
 Z    =        6988036
12                 Z    =         2129953
41
 XDOT =       4477
672561                 XDOT =        1364
794597
 YDOT =     -15577
023099  feet/sec       YDOT =       -4747
876641  meter/sec
 ZDOT =      18099
707456                 ZDOT =        5516
790833


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   07028
55913998  
00020000  00000-0  20000-3 0  9061
2 25544  51
6338 105
5395 0022292 142
3524 217
9206 15
77625060 28729


Satellite: ISS
Catalog Number: 25544
Epoch time:      07028
55913998   =   yrday
fracday
Element set:     906
Inclination:       51
6338  deg
RA of node:       105
5395  deg
Eccentricity:     
0022292     
Arg of perigee:   142
3524  deg
Mean anomaly:     217
9206  deg
Mean motion:   15
77625060  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2872
Checksum:              302


Coasting Arc #8 (Orbit 2886)
---------------------------------------

Vector Time (GMT): 2007/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2535069
73                 A    =         6714110
36  meter
 Y    =        4611589
99  meter          E    =           
0029216
 Z    =       -4200788
39                 I    =           51
94157
 XDOT =      -3890
102727                 Wp   =          136
36308
 YDOT =       5503
419439  meter/sec      RA   =           99
88232  deg
 ZDOT =       3688
529161                 TA   =          171
23341
                                          MA   =          171
18228
                                          Ha   =            191
942  n
mi
                                          Hp   =            171
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8317157
91                 X    =         2503720
10
 Y    =       15129888
42  feet           Y    =         4639763
74  meter
 Z    =      -13782114
14                 Z    =        -4188548
92
 XDOT =     -12762
804222                 XDOT =       -3969
271448
 YDOT =      18055
838055  feet/sec       YDOT =        5459
475078  meter/sec
 ZDOT =      12101
473624                 ZDOT =        3669
439761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6858343
65                 X    =        -2090423
14
 Y    =       15884956
09  feet           Y    =         4841734
62  meter
 Z    =      -13735596
16                 Z    =        -4186609
71
 XDOT =     -20974
687015                 XDOT =       -6393
084602
 YDOT =       1362
500190  feet/sec       YDOT =         415
290058  meter/sec
 ZDOT =      12030
508087                 ZDOT =        3666
898865


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   07029
50928356  
00020000  00000-0  20000-3 0  9072
2 25544  51
6333 100
6333 0022251 145
5407 214
7206 15
77681746 28876


Satellite: ISS
Catalog Number: 25544
Epoch time:      07029
50928356   =   yrday
fracday
Element set:     907
Inclination:       51
6333  deg
RA of node:       100
6333  deg
Eccentricity:     
0022251     
Arg of perigee:   145
5407  deg
Mean anomaly:     214
7206  deg
Mean motion:   15
77681746  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2887
Checksum:              290


Coasting Arc #9 (Orbit 2902)
---------------------------------------

Vector Time (GMT): 2007/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3571190
82                 A    =         6714353
23  meter
 Y    =       -3914301
69  meter          E    =           
0024816
 Z    =       -4128522
43                 I    =           51
94588
 XDOT =       2465
198648                 Wp   =          131
57135
 YDOT =       6227
370943  meter/sec      RA   =           94
79025  deg
 ZDOT =      -3802
497827                 TA   =           99
73940
                                          MA   =           99
45904
                                          Ha   =            191
883  n
mi
                                          Hp   =            171
834

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11716505
32                 X    =         3634750
76
 Y    =      -12842197
16  feet           Y    =        -3874010
84  meter
 Z    =      -13545021
10                 Z    =        -4111020
08
 XDOT =       8087
922072                 XDOT =        2413
851435
 YDOT =      20431
007030  feet/sec       YDOT =        6254
651469  meter/sec
 ZDOT =     -12475
386571                 ZDOT =       -3790
646279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17393171
36                 X    =         5301438
63
 Y    =        1199396
04  feet           Y    =          365575
91  meter
 Z    =      -13479805
67                 Z    =        -4108644
77
 XDOT =     -10786
365509                 XDOT =       -3287
684207
 YDOT =      17855
681002  feet/sec       YDOT =        5442
411569  meter/sec
 ZDOT =     -12430
120333                 ZDOT =       -3788
700677


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   07030
52274503  
00020000  00000-0  20000-3 0  9085
2 25544  51
6332  95
3990 0022152 149
4254 210
8207 15
77677594 29030


Satellite: ISS
Catalog Number: 25544
Epoch time:      07030
52274503   =   yrday
fracday
Element set:     908
Inclination:       51
6332  deg
RA of node:        95
3990  deg
Eccentricity:     
0022152     
Arg of perigee:   149
4254  deg
Mean anomaly:     210
8207  deg
Mean motion:   15
77677594  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2903
Checksum:              287


Coasting Arc #10 (Orbit 2918)
---------------------------------------

Vector Time (GMT): 2007/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1805500
66                 A    =         6719302
76  meter
 Y    =       -6043346
46  meter          E    =           
0033399
 Z    =        2254466
39                 I    =           51
96497
 XDOT =       4278
755456                 Wp   =          135
54209
 YDOT =      -3339
103881  meter/sec      RA   =           89
60319  deg
 ZDOT =      -5499
091014                 TA   =           19
15939
                                          MA   =           19
03408
                                          Ha   =            191
571  n
mi
                                          Hp   =            171
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5923558
60                 X    =        -1748740
37
 Y    =      -19827252
17  feet           Y    =        -6063219
41  meter
 Z    =        7396543
28                 Z    =         2245832
88
 XDOT =      14037
911602                 XDOT =        4342
488543
 YDOT =     -10955
065228  feet/sec       YDOT =       -3290
899622  meter/sec
 ZDOT =     -18041
637185                 ZDOT =       -5478
150957

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11475573
02                 X    =         3497754
66
 Y    =      -17233955
60  feet           Y    =        -5252909
67  meter
 Z    =        7363377
34                 Z    =         2244357
41
 XDOT =      16195
992338                 XDOT =        4936
538465
 YDOT =       3074
049049  feet/sec       YDOT =         936
970150  meter/sec
 ZDOT =     -17963
437601                 ZDOT =       -5475
255781


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   07031
53617918  
00020000  00000-0  20000-3 0  9099
2 25544  51
6338  90
1653 0021920 152
8751 207
3564 15
77760921 29198


Satellite: ISS
Catalog Number: 25544
Epoch time:      07031
53617918   =   yrday
fracday
Element set:     909
Inclination:       51
6338  deg
RA of node:        90
1653  deg
Eccentricity:     
0021920     
Arg of perigee:   152
8751  deg
Mean anomaly:     207
3564  deg
Mean motion:   15
77760921  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2919
Checksum:              299


Coasting Arc #11 (Orbit 2934)
---------------------------------------

Vector Time (GMT): 2007/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3892800
01                 A    =         6709832
73  meter
 Y    =        1770069
22  meter          E    =           
0025557
 Z    =        5164231
47                 I    =           51
93123
 XDOT =      -1693
502770                 Wp   =          151
63997
 YDOT =      -7421
575436  meter/sec      RA   =           84
49181  deg
 ZDOT =       1242
690484                 TA   =          286
41072
                                          MA   =          286
69150
                                          Ha   =            191
502  n
mi
                                          Hp   =            172
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12771653
58                 X    =        -3937389
91
 Y    =        5807313
73  feet           Y    =         1726288
12  meter
 Z    =       16943016
63                 Z    =         5145212
69
 XDOT =      -5556
111449                 XDOT =       -1616
424357
 YDOT =     -24349
000775  feet/sec       YDOT =       -7440
082241  meter/sec
 ZDOT =       4077
068517                 ZDOT =        1234
650464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12780217
14                 X    =        -3895410
18
 Y    =       -5992766
60  feet           Y    =        -1826595
26  meter
 Z    =       16871829
74                 Z    =         5142533
71
 XDOT =      14425
484789                 XDOT =        4396
887764
 YDOT =     -19145
489767  feet/sec       YDOT =       -5835
545281  meter/sec
 ZDOT =       4045
954782                 ZDOT =        1233
207018


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   07032
54958835  
00020000  00000-0  20000-3 0  9109
2 25544  51
6332  84
9316 0021955 156
7170 203
4994 15
77789567 29354


Satellite: ISS
Catalog Number: 25544
Epoch time:      07032
54958835   =   yrday
fracday
Element set:     910
Inclination:       51
6332  deg
RA of node:        84
9316  deg
Eccentricity:     
0021955     
Arg of perigee:   156
7170  deg
Mean anomaly:     203
4994  deg
Mean motion:   15
77789567  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2935
Checksum:              325


Coasting Arc #12 (Orbit 2950)
---------------------------------------

Vector Time (GMT): 2007/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1102145
02                 A    =         6721417
13  meter
 Y    =        6635462
33  meter          E    =           
0020532
 Z    =         184525
44                 I    =           51
96587
 XDOT =      -4706
536188                 Wp   =          124
94259
 YDOT =        599
920626  meter/sec      RA   =           79
33969  deg
 ZDOT =       6054
728044                 TA   =          237
05264
                                          MA   =          237
25025
                                          Ha   =            191
263  n
mi
                                          Hp   =            172
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3615961
36                 X    =         1026968
07
 Y    =       21769889
53  feet           Y    =         6647366
79  meter
 Z    =         605398
42                 Z    =          189697
13
 XDOT =     -15441
391693                 XDOT =       -4742
306553
 YDOT =       1968
243525  feet/sec       YDOT =         547
089279  meter/sec
 ZDOT =      19864
593321                 ZDOT =        6031
777616

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13889958
79                 X    =        -4233659
44
 Y    =       17147809
86  feet           Y    =         5226652
45  meter
 Z    =         625648
10                 Z    =          190697
54
 XDOT =     -10540
990680                 XDOT =       -3212
893959
 YDOT =      -9316
020122  feet/sec       YDOT =       -2839
522933  meter/sec
 ZDOT =      19778
494089                 ZDOT =        6028
484998


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   07033
56297412  
00020000  00000-0  20000-3 0  9110
2 25544  51
6328  79
6967 0021746 159
9391 200
2634 15
77781007 29515


Satellite: ISS
Catalog Number: 25544
Epoch time:      07033
56297412   =   yrday
fracday
Element set:     911
Inclination:       51
6328  deg
RA of node:        79
6967  deg
Eccentricity:     
0021746     
Arg of perigee:   159
9391  deg
Mean anomaly:     200
2634  deg
Mean motion:   15
77781007  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2951
Checksum:              307

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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