Date: February 4th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9956 62 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 2950)
---------------------------------------

Vector Time (GMT): 2007/033/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1669676
86                 A    =         6716359
44  meter
 Y    =        5544493
64  meter          E    =           
0028841
 Z    =        3406773
56                 I    =           51
94951
 XDOT =      -4480
910934                 Wp   =          135
95263
 YDOT =      -4220
234743  meter/sec      RA   =           79
33982  deg
 ZDOT =       4628
691076                 TA   =          264
13435
                                          MA   =          264
46319
                                          Ha   =            191
320  n
mi
                                          Hp   =            172
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5477942
44                 X    =        -1748101
00
 Y    =       18190595
95  feet           Y    =         5525383
76  meter
 Z    =       11177078
61                 Z    =         3398472
28
 XDOT =     -14701
151357                 XDOT =       -4455
871214
 YDOT =     -13845
914512  feet/sec       YDOT =       -4270
202961  meter/sec
 ZDOT =      15185
994343                 ZDOT =        4606
984215

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16921906
67                 X    =        -5157797
15
 Y    =        8673812
86  feet           Y    =         2643778
16  meter
 Z    =       11146603
31                 Z    =         3397484
69
 XDOT =        294
552917                 XDOT =          89
779729
 YDOT =     -19019
523222  feet/sec       YDOT =       -5797
150678  meter/sec
 ZDOT =      15103
960771                 ZDOT =        4603
687243


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
56319645  
00020000  00000-0  20000-3 0  9001
2 25544  51
6333  79
7080 0021992 160
3479 199
8538 15
77801348 29511


Satellite: ISS
Catalog Number: 25544
Epoch time:      07033
56319645   =   yrday
fracday
Element set:     900
Inclination:       51
6333  deg
RA of node:        79
7080  deg
Eccentricity:     
0021992     
Arg of perigee:   160
3479  deg
Mean anomaly:     199
8538  deg
Mean motion:   15
77801348  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2951
Checksum:              314


Coasting Arc #2 (Orbit 2965)
---------------------------------------

Vector Time (GMT): 2007/034/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3819145
80                 A    =         6717049
31  meter
 Y    =        4605463
12  meter          E    =           
0022443
 Z    =       -3086019
13                 I    =           51
94677
 XDOT =      -2481
884250                 Wp   =          152
06681
 YDOT =       5358
324421  meter/sec      RA   =           74
14565  deg
 ZDOT =       4920
045773                 TA   =          172
33094
                                          MA   =          172
29656
                                          Ha   =            191
061  n
mi
                                          Hp   =            172
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12530005
91                 X    =         3782353
84
 Y    =       15109787
13  feet           Y    =         4647965
27  meter
 Z    =      -10124734
67                 Z    =        -3067555
63
 XDOT =      -8142
664863                 XDOT =       -2565
517246
 YDOT =      17579
804532  feet/sec       YDOT =        5330
102923  meter/sec
 ZDOT =      16141
882458                 ZDOT =        4907
786114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1763194
37                 X    =         -537421
64
 Y    =       19585927
61  feet           Y    =         5969790
74  meter
 Z    =      -10054827
33                 Z    =        -3064711
37
 XDOT =     -16816
324775                 XDOT =       -5125
615791
 YDOT =       6758
142069  feet/sec       YDOT =        2059
881703  meter/sec
 ZDOT =      16096
521264                 ZDOT =        4906
219681


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   07034
51322335  
00020000  00000-0  20000-3 0  9018
2 25544  51
6340  74
8002 0021996 163
8093 196
3780 15
77885645 29662


Satellite: ISS
Catalog Number: 25544
Epoch time:      07034
51322335   =   yrday
fracday
Element set:     901
Inclination:       51
6340  deg
RA of node:        74
8002  deg
Eccentricity:     
0021996     
Arg of perigee:   163
8093  deg
Mean anomaly:     196
3780  deg
Mean motion:   15
77885645  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2966
Checksum:              302


Coasting Arc #3 (Orbit 2981)
---------------------------------------

Vector Time (GMT): 2007/035/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2739445
52                 A    =         6710594
03  meter
 Y    =       -3648132
68  meter          E    =           
0024535
 Z    =       -4929629
54                 I    =           51
91624
 XDOT =       4177
753417                 Wp   =          136
74587
 YDOT =       6081
448746  meter/sec      RA   =           69
04251  deg
 ZDOT =      -2202
783480                 TA   =          112
07223
                                          MA   =          111
81150
                                          Ha   =            190
941  n
mi
                                          Hp   =            172
653

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8987682
17                 X    =         2803982
40
 Y    =      -11968939
24  feet           Y    =        -3617137
85  meter
 Z    =      -16173325
25                 Z    =        -4916164
93
 XDOT =      13706
540081                 XDOT =        4120
139701
 YDOT =      19952
259666  feet/sec       YDOT =        6127
844569  meter/sec
 ZDOT =      -7226
979922                 ZDOT =       -2182
628530

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14842042
13                 X    =         4523854
44
 Y    =       -2316417
77  feet           Y    =         -706044
14  meter
 Z    =      -16123224
90                 Z    =        -4914358
95
 XDOT =      -4120
453588                 XDOT =       -1255
914254
 YDOT =      22822
645452  feet/sec       YDOT =        6956
342334  meter/sec
 ZDOT =      -7150
533914                 ZDOT =       -2179
482737


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   07035
52655681  
00020000  00000-0  20000-3 0  9024
2 25544  51
6343  69
5648 0021884 167
8640 192
3057 15
77886671 29821


Satellite: ISS
Catalog Number: 25544
Epoch time:      07035
52655681   =   yrday
fracday
Element set:     902
Inclination:       51
6343  deg
RA of node:        69
5648  deg
Eccentricity:     
0021884     
Arg of perigee:   167
8640  deg
Mean anomaly:     192
3057  deg
Mean motion:   15
77886671  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2982
Checksum:              327


Coasting Arc #4 (Orbit 2997)
---------------------------------------

Vector Time (GMT): 2007/036/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3381702
49                 A    =         6720849
38  meter
 Y    =       -5747629
92  meter          E    =           
0032899
 Z    =         645122
41                 I    =           51
93877
 XDOT =       3823
973374                 Wp   =          155
07577
 YDOT =      -2936
473931  meter/sec      RA   =           63
87313  deg
 ZDOT =      -6036
146006                 TA   =           17
89962
                                          MA   =           17
78402
                                          Ha   =            190
695  n
mi
                                          Hp   =            172
764

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11094824
45                 X    =        -3320314
15
 Y    =      -18857053
55  feet           Y    =        -5785102
76  meter
 Z    =        2116543
33                 Z    =          628843
73
 XDOT =      12545
844404                 XDOT =        3885
846996
 YDOT =      -9634
100824  feet/sec       YDOT =       -2893
366279  meter/sec
 ZDOT =     -19803
628629                 ZDOT =       -6017
419283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4725163
60                 X    =         1440229
86
 Y    =      -21368537
88  feet           Y    =        -6513130
35  meter
 Z    =        2054695
03                 Z    =          626271
05
 XDOT =      14268
843214                 XDOT =        4349
143412
 YDOT =       1231
452974  feet/sec       YDOT =         375
346866  meter/sec
 ZDOT =     -19733
679529                 ZDOT =       -6014
825521


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   07036
53986075  
00020000  00000-0  20000-3 0  9031
2 25544  51
6334  64
3296 0021834 171
3587 188
7959 15
77936139 29980


Satellite: ISS
Catalog Number: 25544
Epoch time:      07036
53986075   =   yrday
fracday
Element set:     903
Inclination:       51
6334  deg
RA of node:        64
3296  deg
Eccentricity:     
0021834     
Arg of perigee:   171
3587  deg
Mean anomaly:     188
7959  deg
Mean motion:   15
77936139  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2998
Checksum:              343


Coasting Arc #5 (Orbit 3013)
---------------------------------------

Vector Time (GMT): 2007/037/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3941172
84                 A    =         6708921
69  meter
 Y    =        1420822
96  meter          E    =           
0020621
 Z    =        5233842
25                 I    =           51
88483
 XDOT =      -3459
872035                 Wp   =          166
75009
 YDOT =      -6851
587911  meter/sec      RA   =           58
72612  deg
 ZDOT =       -764
439182                 TA   =          290
37552
                                          MA   =          290
59692
                                          Ha   =            190
510  n
mi
                                          Hp   =            172
975

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12930357
09                 X    =        -3982192
29
 Y    =        4661492
64  feet           Y    =         1376521
32  meter
 Z    =       17171398
45                 Z    =         5214596
77
 XDOT =     -11351
286204                 XDOT =       -3379
286032
 YDOT =     -22478
962962  feet/sec       YDOT =       -6889
827567  meter/sec
 ZDOT =      -2508
002567                 ZDOT =        -781
051002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12800729
85                 X    =        -3901662
46
 Y    =       -5247422
92  feet           Y    =        -1599414
50  meter
 Z    =       17099311
12                 Z    =         5211870
03
 XDOT =       6225
303017                 XDOT =        1897
472360
 YDOT =     -23359
955757  feet/sec       YDOT =       -7120
114515  meter/sec
 ZDOT =      -2571
237670                 ZDOT =        -783
713242


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   07037
55313454  
00020000  00000-0  20000-3 0  9040
2 25544  51
6329  59
0945 0021711 175
1706 184
9673 15
77996222 30145


Satellite: ISS
Catalog Number: 25544
Epoch time:      07037
55313454   =   yrday
fracday
Element set:     904
Inclination:       51
6329  deg
RA of node:        59
0945  deg
Eccentricity:     
0021711     
Arg of perigee:   175
1706  deg
Mean anomaly:     184
9673  deg
Mean motion:   15
77996222  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3014
Checksum:              297


Coasting Arc #6 (Orbit 3029)
---------------------------------------

Vector Time (GMT): 2007/038/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2464488
80                 A    =         6718985
32  meter
 Y    =        5941015
79  meter          E    =           
0021228
 Z    =        1966298
17                 I    =           51
90353
 XDOT =      -5249
226572                 Wp   =          140
22279
 YDOT =        301
912794  meter/sec      RA   =           53
60257  deg
 ZDOT =       5617
799986                 TA   =          241
58484
                                          MA   =          241
79895
                                          Ha   =            190
165  n
mi
                                          Hp   =            173
160

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8085593
17                 X    =         2388320
59
 Y    =       19491521
60  feet           Y    =         5968149
23  meter
 Z    =        6451109
48                 Z    =         1978085
34
 XDOT =     -17221
871957                 XDOT =       -5279
502264
 YDOT =        990
527540  feet/sec       YDOT =         243
043827  meter/sec
 ZDOT =      18431
102316                 ZDOT =        5592
226137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6710673
93                 X    =        -2045413
41
 Y    =       19992009
72  feet           Y    =         6093564
56  meter
 Z    =        6496110
20                 Z    =         1980014
39
 XDOT =     -12267
455328                 XDOT =       -3739
120384
 YDOT =     -10127
591523  feet/sec       YDOT =       -3086
889896  meter/sec
 ZDOT =      18335
112771                 ZDOT =        5588
542373


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   07038
56637879  
00020000  00000-0  20000-3 0  9053
2 25544  51
6331  53
8592 0021642 179
2192 180
9010 15
78045240 30300


Satellite: ISS
Catalog Number: 25544
Epoch time:      07038
56637879   =   yrday
fracday
Element set:     905
Inclination:       51
6331  deg
RA of node:        53
8592  deg
Eccentricity:     
0021642     
Arg of perigee:   179
2192  deg
Mean anomaly:     180
9010  deg
Mean motion:   15
78045240  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3030
Checksum:              285


Coasting Arc #7 (Orbit 3044)
---------------------------------------

Vector Time (GMT): 2007/039/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5167541
18                 A    =         6712983
91  meter
 Y    =         823823
96  meter          E    =           
0025186
 Z    =       -4226335
42                 I    =           51
86544
 XDOT =       1950
362476                 Wp   =          164
53638
 YDOT =       6492
316961  meter/sec      RA   =           48
40948  deg
 ZDOT =       3631
405370                 TA   =          142
44591
                                          MA   =          142
26974
                                          Ha   =            189
953  n
mi
                                          Hp   =            173
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16953875
28                 X    =         5178475
49
 Y    =        2702834
53  feet           Y    =          881671
41  meter
 Z    =      -13865929
84                 Z    =        -4201205
30
 XDOT =       6398
827022                 XDOT =        1859
979044
 YDOT =      21300
252496  feet/sec       YDOT =        6513
621664  meter/sec
 ZDOT =      11914
059613                 ZDOT =        3640
660523

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11306708
77                 X    =         3446284
83
 Y    =       13019533
04  feet           Y    =         3968353
67  meter
 Z    =      -13771467
16                 Z    =        -4197543
19
 XDOT =      -7894
416544                 XDOT =       -2406
218163
 YDOT =      19561
383058  feet/sec       YDOT =        5962
309556  meter/sec
 ZDOT =      11949
616107                 ZDOT =        3642
242989


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   07039
51626857  
00020000  00000-0  20000-3 0  9064
2 25544  51
6334  48
9506 0021511 182
8621 177
2425 15
78059899 30455


Satellite: ISS
Catalog Number: 25544
Epoch time:      07039
51626857   =   yrday
fracday
Element set:     906
Inclination:       51
6334  deg
RA of node:        48
9506  deg
Eccentricity:     
0021511     
Arg of perigee:   182
8621  deg
Mean anomaly:     177
2425  deg
Mean motion:   15
78059899  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3045
Checksum:              311


Coasting Arc #8 (Orbit 3060)
---------------------------------------

Vector Time (GMT): 2007/040/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -761108
30                 A    =         6712899
09  meter
 Y    =       -5207716
03  meter          E    =           
0019289
 Z    =       -4158965
20                 I    =           51
84495
 XDOT =       6432
786703                 Wp   =          164
41422
 YDOT =       2027
542936  meter/sec      RA   =           43
30763  deg
 ZDOT =      -3738
217634                 TA   =           67
62836
                                          MA   =           67
42407
                                          Ha   =            189
703  n
mi
                                          Hp   =            173
539

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2497074
47                 X    =         -682615
05
 Y    =      -17085682
50  feet           Y    =        -5215788
25  meter
 Z    =      -13644898
95                 Z    =        -4162472
01
 XDOT =      21104
943251                 XDOT =        6427
795699
 YDOT =       6652
043752  feet/sec       YDOT =        2099
450074  meter/sec
 ZDOT =     -12264
493551                 ZDOT =       -3706
979639

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8876805
69                 X    =         2705650
38
 Y    =      -14798014
59  feet           Y    =        -4510434
85  meter
 Z    =      -13658707
10                 Z    =        -4163173
92
 XDOT =      11181
261498                 XDOT =        3408
048505
 YDOT =      17851
924999  feet/sec       YDOT =        5441
266740  meter/sec
 ZDOT =     -12146
948627                 ZDOT =       -3702
389941


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   07040
52945530  
00020000  00000-0  20000-3 0  9070
2 25544  51
6324  43
7141 0021517 186
6854 173
4027 15
78113599 30610


Satellite: ISS
Catalog Number: 25544
Epoch time:      07040
52945530   =   yrday
fracday
Element set:     907
Inclination:       51
6324  deg
RA of node:        43
7141  deg
Eccentricity:     
0021517     
Arg of perigee:   186
6854  deg
Mean anomaly:     173
4027  deg
Mean motion:   15
78113599  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3061
Checksum:              282


Coasting Arc #9 (Orbit 3076)
---------------------------------------

Vector Time (GMT): 2007/041/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5851076
21                 A    =         6718488
29  meter
 Y    =       -2529027
71  meter          E    =           
0027674
 Z    =        2063466
03                 I    =           51
84242
 XDOT =        330
560587                 Wp   =          160
05480
 YDOT =      -5321
412358  meter/sec      RA   =           38
11089  deg
 ZDOT =      -5588
471921                 TA   =          356
88613
                                          MA   =          356
90332
                                          Ha   =            189
409  n
mi
                                          Hp   =            173
737

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19196444
25                 X    =        -5832385
22
 Y    =       -8297335
00  feet           Y    =        -2594353
25  meter
 Z    =        6769901
66                 Z    =         2035087
17
 XDOT =       1084
516363                 XDOT =         417
188271
 YDOT =     -17458
701961  feet/sec       YDOT =       -5317
231340  meter/sec
 ZDOT =     -18334
881629                 ZDOT =       -5586
655799

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10035807
19                 X    =        -3058914
03
 Y    =      -18386609
13  feet           Y    =        -5604238
46  meter
 Z    =        6663031
39                 Z    =         2030891
97
 XDOT =      10351
355865                 XDOT =        3155
093268
 YDOT =     -12287
501471  feet/sec       YDOT =       -3745
230448  meter/sec
 ZDOT =     -18328
711465                 ZDOT =       -5586
591255


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   07041
54261128  
00020000  00000-0  20000-3 0  9088
2 25544  51
6324  38
4784 0021334 190
6230 169
4487 15
78188295 30771


Satellite: ISS
Catalog Number: 25544
Epoch time:      07041
54261128   =   yrday
fracday
Element set:     908
Inclination:       51
6324  deg
RA of node:        38
4784  deg
Eccentricity:     
0021334     
Arg of perigee:   190
6230  deg
Mean anomaly:     169
4487  deg
Mean motion:   15
78188295  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3077
Checksum:              301


Coasting Arc #10 (Orbit 3092)
---------------------------------------

Vector Time (GMT): 2007/042/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1461136
09                 A    =         6708351
99  meter
 Y    =        3954224
37  meter          E    =           
0022399
 Z    =        5223015
36                 I    =           51
78458
 XDOT =      -6755
320436                 Wp   =          186
16592
 YDOT =      -3611
488532  meter/sec      RA   =           32
98140  deg
 ZDOT =        822
857876                 TA   =          255
89657
                                          MA   =          256
14560
                                          Ha   =            189
149  n
mi
                                          Hp   =            173
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4793753
58                 X    =        -1530616
31
 Y    =       12973177
08  feet           Y    =         3937496
43  meter
 Z    =       17135877
16                 Z    =         5215748
66
 XDOT =     -22163
124790                 XDOT =       -6718
431430
 YDOT =     -11848
715655  feet/sec       YDOT =       -3686
824070  meter/sec
 ZDOT =       2699
664949                 ZDOT =         790
130430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11718639
13                 X    =        -3571841
21
 Y    =        7407761
24  feet           Y    =         2257885
63  meter
 Z    =       17109069
32                 Z    =         5214844
33
 XDOT =     -10020
128991                 XDOT =       -3054
135316
 YDOT =     -21964
899893  feet/sec       YDOT =       -6694
901487  meter/sec
 ZDOT =       2576
332871                 ZDOT =         785
266259


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   07042
55573759  
00020000  00000-0  20000-3 0  9097
2 25544  51
6318  33
2423 0021349 194
6416 165
4133 15
78207193 30934


Satellite: ISS
Catalog Number: 25544
Epoch time:      07042
55573759   =   yrday
fracday
Element set:     909
Inclination:       51
6318  deg
RA of node:        33
2423  deg
Eccentricity:     
0021349     
Arg of perigee:   194
6416  deg
Mean anomaly:     165
4133  deg
Mean motion:   15
78207193  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3093
Checksum:              293


Coasting Arc #11 (Orbit 3108)
---------------------------------------

Vector Time (GMT): 2007/043/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5633332
93                 A    =         6719651
10  meter
 Y    =        3607776
53  meter          E    =           
0013018
 Z    =         713148
17                 I    =           51
79907
 XDOT =      -3121
775011                 Wp   =          161
38079
 YDOT =       3682
182221  meter/sec      RA   =           27
82448  deg
 ZDOT =       5989
702405                 TA   =          206
37164
                                          MA   =          206
43796
                                          Ha   =            188
853  n
mi
                                          Hp   =            173
924

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18482063
40                 X    =         5589107
29
 Y    =       11836537
18  feet           Y    =         3670524
29  meter
 Z    =        2339724
96                 Z    =          740407
20
 XDOT =     -10242
043998                 XDOT =       -3191
814077
 YDOT =      12080
650331  feet/sec       YDOT =        3646
880867  meter/sec
 ZDOT =      19651
254611                 ZDOT =        5974
367152

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7960356
53                 X    =         2426316
67
 Y    =       20440924
40  feet           Y    =         6230393
76  meter
 Z    =        2442524
65                 Z    =          744481
51
 XDOT =     -13988
696127                 XDOT =       -4263
754579
 YDOT =       3090
535411  feet/sec       YDOT =         941
995193  meter/sec
 ZDOT =      19594
110995                 ZDOT =        5972
285031


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   07043
56882960  
00020000  00000-0  20000-3 0  9108
2 25544  51
6318  28
0059 0021567 198
2470 161
7924 15
78324783 31093


Satellite: ISS
Catalog Number: 25544
Epoch time:      07043
56882960   =   yrday
fracday
Element set:     910
Inclination:       51
6318  deg
RA of node:        28
0059  deg
Eccentricity:     
0021567     
Arg of perigee:   198
2470  deg
Mean anomaly:     161
7924  deg
Mean motion:   15
78324783  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3109
Checksum:              303


Coasting Arc #12 (Orbit 3123)
---------------------------------------

Vector Time (GMT): 2007/044/12:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3959126
73                 A    =         6709913
52  meter
 Y    =       -2476037
82  meter          E    =           
0023525
 Z    =       -4830128
45                 I    =           51
73979
 XDOT =       5776
625100                 Wp   =          171
48810
 YDOT =       4476
052313  meter/sec      RA   =           22
63785  deg
 ZDOT =       2419
078190                 TA   =          122
21799
                                          MA   =          121
98971
                                          Ha   =            188
613  n
mi
                                          Hp   =            174
369

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12989260
94                 X    =         4009983
28
 Y    =       -8123483
65  feet           Y    =        -2431480
02  meter
 Z    =      -15846878
13                 Z    =        -4810772
04
 XDOT =      18952
182088                 XDOT =        5714
392727
 YDOT =      14685
211001  feet/sec       YDOT =        4540
301661  meter/sec
 ZDOT =       7936
608235                 ZDOT =        2446
989526

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15370333
24                 X    =         4684877
57
 Y    =         868293
69  feet           Y    =          264655
92  meter
 Z    =      -15774484
30                 Z    =        -4808062
82
 XDOT =       7096
136906                 XDOT =        2162
902529
 YDOT =      21763
595730  feet/sec       YDOT =        6633
543978  meter/sec
 ZDOT =       8041
966744                 ZDOT =        2451
191463


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   07044
51857974  
00020000  00000-0  20000-3 0  9112
2 25544  51
6319  23
0959 0021247 202
2013 157
8235 15
78291198 31243


Satellite: ISS
Catalog Number: 25544
Epoch time:      07044
51857974   =   yrday
fracday
Element set:     911
Inclination:       51
6319  deg
RA of node:        23
0959  deg
Eccentricity:     
0021247     
Arg of perigee:   202
2013  deg
Mean anomaly:     157
8235  deg
Mean motion:   15
78291198  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3124
Checksum:              287

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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