Date: October 18th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5112 86 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 3007)
---------------------------------------

Vector Time (GMT): 2007/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         645252
77                 A    =         6715101
34  meter
 Y    =       -4127729
55  meter          E    =           
0004948
 Z    =        5253066
39                 I    =           51
54818
 XDOT =       7567
279160                 Wp   =          101
52044
 YDOT =       1451
920778  meter/sec      RA   =          192
10265  deg
 ZDOT =        210
228720                 TA   =          346
47713
                                          MA   =          346
49039
                                          Ha   =            188
272  n
mi
                                          Hp   =            180
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2116971
03                 X    =          665842
74
 Y    =      -13542419
78  feet           Y    =        -4120398
97  meter
 Z    =       17234469
80                 Z    =         5256251
02
 XDOT =      24827
031364                 XDOT =        7549
459869
 YDOT =       4763
519614  feet/sec       YDOT =        1536
442737  meter/sec
 ZDOT =        689
726773                 ZDOT =         246
948066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3863385
72                 X    =         1177559
97
 Y    =       13135976
27  feet           Y    =         4003845
57  meter
 Z    =       17246043
82                 Z    =         5256594
16
 XDOT =     -23565
994117                 XDOT =       -7182
915007
 YDOT =       5837
053851  feet/sec       YDOT =        1779
134014  meter/sec
 ZDOT =        829
449554                 ZDOT =         252
816224


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   07290
54801102  
00020000  00000-0  20000-3 0  9008
2 25544  51
6365 192
8436 0002483 100
2968 259
8476 15
75760891 30085


Satellite: ISS
Catalog Number: 25544
Epoch time:      07290
54801102   =   yrday
fracday
Element set:     900
Inclination:       51
6365  deg
RA of node:       192
8436  deg
Eccentricity:     
0002483     
Arg of perigee:   100
2968  deg
Mean anomaly:     259
8476  deg
Mean motion:   15
75760891  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3008
Checksum:              295


Coasting Arc #2 (Orbit 3023)
---------------------------------------

Vector Time (GMT): 2007/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6613656
35                 A    =         6727149
55  meter
 Y    =       -1127722
80  meter          E    =           
0014599
 Z    =         402741
87                 I    =           51
61758
 XDOT =       1170
662154                 Wp   =           57
09825
 YDOT =      -4661
873134  meter/sec      RA   =          186
95133  deg
 ZDOT =       6021
135836                 TA   =          307
28579
                                          MA   =          307
41880
                                          Ha   =            188
306  n
mi
                                          Hp   =            180
209

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21698347
62                 X    =        -6602510
92
 Y    =       -3699877
97  feet           Y    =        -1201618
14  meter
 Z    =        1321331
61                 Z    =          370639
24
 XDOT =       3840
755097                 XDOT =        1193
454828
 YDOT =     -15294
859362  feet/sec       YDOT =       -4648
654808  meter/sec
 ZDOT =      19754
382664                 ZDOT =        6026
878280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21145907
11                 X    =         6445272
49
 Y    =       -6137253
76  feet           Y    =        -1870634
95  meter
 Z    =        1199179
85                 Z    =          365510
02
 XDOT =       2867
154454                 XDOT =         873
908677
 YDOT =      13848
202164  feet/sec       YDOT =        4220
932019  meter/sec
 ZDOT =      19775
610228                 ZDOT =        6027
605998


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   07291
56272121  
00020000  00000-0  20000-3 0  9015
2 25544  51
6368 187
6184 0002512 101
6599 258
4847 15
75751133 30242


Satellite: ISS
Catalog Number: 25544
Epoch time:      07291
56272121   =   yrday
fracday
Element set:     901
Inclination:       51
6368  deg
RA of node:       187
6184  deg
Eccentricity:     
0002512     
Arg of perigee:   101
6599  deg
Mean anomaly:     258
4847  deg
Mean motion:   15
75751133  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3024
Checksum:              289


Coasting Arc #3 (Orbit 3038)
---------------------------------------

Vector Time (GMT): 2007/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1424189
24                 A    =         6715399
21  meter
 Y    =        4056733
76  meter          E    =           
0016837
 Z    =       -5173311
02                 I    =           51
60783
 XDOT =      -7514
575885                 Wp   =          100
06422
 YDOT =      -1156
008868  meter/sec      RA   =          181
78667  deg
 ZDOT =       1162
536219                 TA   =          181
05294
                                          MA   =          181
05649
                                          Ha   =            188
200  n
mi
                                          Hp   =            180
095

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4672536
89                 X    =        -1444315
04
 Y    =       13309493
97  feet           Y    =         4040695
19  meter
 Z    =      -16972805
19                 Z    =        -5180278
68
 XDOT =     -24654
120359                 XDOT =       -7506
738188
 YDOT =      -3792
680012  feet/sec       YDOT =       -1239
997295  meter/sec
 ZDOT =       3814
095206                 ZDOT =        1126
048925

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1926317
21                 X    =         -587141
49
 Y    =      -13942113
37  feet           Y    =        -4249556
16  meter
 Z    =      -16998768
29                 Z    =        -5181224
57
 XDOT =      22712
185381                 XDOT =        6922
674104
 YDOT =      -7617
819611  feet/sec       YDOT =       -2321
911417  meter/sec
 ZDOT =       3675
259867                 ZDOT =        1120
219208


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   07292
51399150  
00020000  00000-0  20000-3 0  9024
2 25544  51
6373 182
7198 0002445 105
8936 254
2498 15
75798711 30390


Satellite: ISS
Catalog Number: 25544
Epoch time:      07292
51399150   =   yrday
fracday
Element set:     902
Inclination:       51
6373  deg
RA of node:       182
7198  deg
Eccentricity:     
0002445     
Arg of perigee:   105
8936  deg
Mean anomaly:     254
2498  deg
Mean motion:   15
75798711  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3039
Checksum:              316


Coasting Arc #4 (Orbit 3054)
---------------------------------------

Vector Time (GMT): 2007/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6458913
96                 A    =         6725996
88  meter
 Y    =         911485
57  meter          E    =           
0010203
 Z    =       -1626746
41                 I    =           51
67255
 XDOT =      -2100
549388                 Wp   =          136
63758
 YDOT =       4675
073251  meter/sec      RA   =          176
66222  deg
 ZDOT =      -5749
105587                 TA   =           61
32869
                                          MA   =           61
22614
                                          Ha   =            188
207  n
mi
                                          Hp   =            180
257

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21190662
60                 X    =         6456144
09
 Y    =        2990438
23  feet           Y    =          983697
30  meter
 Z    =       -5337094
53                 Z    =        -1595375
35
 XDOT =      -6891
566232                 XDOT =       -2124
742174
 YDOT =      15338
166835  feet/sec       YDOT =        4651
448399  meter/sec
 ZDOT =     -18861
894970                 ZDOT =       -5759
368991

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20162131
00                 X    =        -6145417
53
 Y    =        7261907
56  feet           Y    =         2213429
42  meter
 Z    =       -5217724
85                 Z    =        -1590362
53
 XDOT =       -630
435591                 XDOT =        -192
156768
 YDOT =     -15261
668467  feet/sec       YDOT =       -4651
756549  meter/sec
 ZDOT =     -18900
307265                 ZDOT =       -5760
813654


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   07293
52866141  
00020000  00000-0  20000-3 0  9036
2 25544  51
6375 177
4946 0002374 113
8747 246
2666 15
75785497 30557


Satellite: ISS
Catalog Number: 25544
Epoch time:      07293
52866141   =   yrday
fracday
Element set:     903
Inclination:       51
6375  deg
RA of node:       177
4946  deg
Eccentricity:     
0002374     
Arg of perigee:   113
8747  deg
Mean anomaly:     246
2666  deg
Mean motion:   15
75785497  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3055
Checksum:              325


Coasting Arc #5 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2007/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2217085
29                 A    =         6716745
37  meter
 Y    =       -4155383
67  meter          E    =           
0008665
 Z    =        4782765
90                 I    =           51
67157
 XDOT =       7221
938022                 Wp   =           71
66908
 YDOT =        937
809150  meter/sec      RA   =          171
48003  deg
 ZDOT =      -2526
592552                 TA   =           43
06217
                                          MA   =           42
99441
                                          Ha   =            187
899  n
mi
                                          Hp   =            180
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7273901
86                 X    =         2240152
52
 Y    =      -13633148
51  feet           Y    =        -4130461
84  meter
 Z    =       15691489
16                 Z    =         4793592
79
 XDOT =      23694
022383                 XDOT =        7223
188437
 YDOT =       3076
801673  feet/sec       YDOT =        1018
575863  meter/sec
 ZDOT =      -8289
345643                 ZDOT =       -2491
504913

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         275205
15                 X    =           83882
53
 Y    =       15408443
65  feet           Y    =         4696493
63  meter
 Z    =       15732111
90                 Z    =         4795147
71
 XDOT =     -21160
187740                 XDOT =       -6449
625223
 YDOT =       8726
461570  feet/sec       YDOT =        2659
825487  meter/sec
 ZDOT =      -8155
832958                 ZDOT =       -2485
897886


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   07294
54330875  
00020000  00000-0  20000-3 0  9040
2 25544  51
6377 172
2692 0002197 112
4025 247
7372 15
75896155 30719


Satellite: ISS
Catalog Number: 25544
Epoch time:      07294
54330875   =   yrday
fracday
Element set:     904
Inclination:       51
6377  deg
RA of node:       172
2692  deg
Eccentricity:     
0002197     
Arg of perigee:   112
4025  deg
Mean anomaly:     247
7372  deg
Mean motion:   15
75896155  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3071
Checksum:              301


Coasting Arc #6 (Orbit 3086)
---------------------------------------

Vector Time (GMT): 2007/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6078511
78                 A    =         6723645
33  meter
 Y    =        -763863
86  meter          E    =           
0015497
 Z    =        2755086
86                 I    =           51
72245
 XDOT =       2963
057386                 Wp   =           84
14388
 YDOT =      -4903
524465  meter/sec      RA   =          166
37675  deg
 ZDOT =       5154
698699                 TA   =          307
35404
                                          MA   =          307
49510
                                          Ha   =            188
043  n
mi
                                          Hp   =            180
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19942623
95                 X    =        -6082902
30
 Y    =       -2506115
02  feet           Y    =         -831861
63  meter
 Z    =        9038998
90                 Z    =         2725546
36
 XDOT =       9721
316882                 XDOT =        2992
628119
 YDOT =     -16087
678691  feet/sec       YDOT =       -4870
224276  meter/sec
 ZDOT =      16911
741137                 ZDOT =        5169
165538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18594819
70                 X    =         5667701
04
 Y    =       -7761510
33  feet           Y    =        -2365708
35  meter
 Z    =        8926589
57                 Z    =         2720824
50
 XDOT =       -923
680709                 XDOT =        -281
537880
 YDOT =      17388
314361  feet/sec       YDOT =        5299
958217  meter/sec
 ZDOT =      16966
106980                 ZDOT =        5171
269407


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   07295
55793949  
00020000  00000-0  20000-3 0  9058
2 25544  51
6374 167
0434 0002209 114
5555 245
5839 15
75869121 30871


Satellite: ISS
Catalog Number: 25544
Epoch time:      07295
55793949   =   yrday
fracday
Element set:     905
Inclination:       51
6374  deg
RA of node:       167
0434  deg
Eccentricity:     
0002209     
Arg of perigee:   114
5555  deg
Mean anomaly:     245
5839  deg
Mean motion:   15
75869121  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3087
Checksum:              321


Coasting Arc #7 (Orbit 3101)
---------------------------------------

Vector Time (GMT): 2007/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2923120
83                 A    =         6719254
67  meter
 Y    =        4434341
64  meter          E    =           
0009925
 Z    =       -4126322
38                 I    =           51
73579
 XDOT =      -6649
476603                 Wp   =          112
59615
 YDOT =       -876
986708  meter/sec      RA   =          161
18423  deg
 ZDOT =       3771
530260                 TA   =          196
01581
                                          MA   =          196
04721
                                          Ha   =            187
825  n
mi
                                          Hp   =            180
115

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9590291
43                 X    =        -2952443
70
 Y    =       14548364
96  feet           Y    =         4401489
43  meter
 Z    =      -13537803
09                 Z    =        -4140594
71
 XDOT =     -21815
868120                 XDOT =       -6657
497594
 YDOT =      -2877
252979  feet/sec       YDOT =        -951
389528  meter/sec
 ZDOT =      12373
786942                 ZDOT =        3739
207006

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         726861
61                 X    =          221547
42
 Y    =      -17367892
90  feet           Y    =        -5293733
76  meter
 Z    =      -13591493
42                 Z    =        -4142687
20
 XDOT =      19007
418335                 XDOT =        5793
461108
 YDOT =      -8782
752808  feet/sec       YDOT =       -2676
983056  meter/sec
 ZDOT =      12250
777158                 ZDOT =        3734
036878


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   07296
50913503  
00020000  00000-0  20000-3 0  9065
2 25544  51
6369 162
1442 0002086 121
2489 238
8880 15
75918046 31024


Satellite: ISS
Catalog Number: 25544
Epoch time:      07296
50913503   =   yrday
fracday
Element set:     906
Inclination:       51
6369  deg
RA of node:       162
1442  deg
Eccentricity:     
0002086     
Arg of perigee:   121
2489  deg
Mean anomaly:     238
8880  deg
Mean motion:   15
75918046  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3102
Checksum:              291


Coasting Arc #8 (Orbit 3117)
---------------------------------------

Vector Time (GMT): 2007/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5489051
43                 A    =         6720531
70  meter
 Y    =         835752
34  meter          E    =           
0007507
 Z    =       -3793044
38                 I    =           51
76595
 XDOT =      -3706
721423                 Wp   =           88
62279
 YDOT =       5271
101888  meter/sec      RA   =          156
09325  deg
 ZDOT =      -4209
658901                 TA   =          137
27774
                                          MA   =          137
21936
                                          Ha   =            187
790  n
mi
                                          Hp   =            180
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18008698
90                 X    =         5497724
38
 Y    =        2741969
63  feet           Y    =          897182
29  meter
 Z    =      -12444371
32                 Z    =        -3766356
83
 XDOT =     -12161
159525                 XDOT =       -3744
937865
 YDOT =      17293
641366  feet/sec       YDOT =        5229
437294  meter/sec
 ZDOT =     -13811
216868                 ZDOT =       -4227
759794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16813226
27                 X    =        -5124671
37
 Y    =        7187833
61  feet           Y    =         2190851
68  meter
 Z    =      -12342790
67                 Z    =        -3762082
60
 XDOT =       1690
944187                 XDOT =         515
399788
 YDOT =     -19838
514298  feet/sec       YDOT =       -6046
779158  meter/sec
 ZDOT =     -13879
361794                 ZDOT =       -4230
429475


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   07297
52372500  
00020000  00000-0  20000-3 0  9075
2 25544  51
6360 156
9184 0002004 127
2453 232
8894 15
75928121 31187


Satellite: ISS
Catalog Number: 25544
Epoch time:      07297
52372500   =   yrday
fracday
Element set:     907
Inclination:       51
6360  deg
RA of node:       156
9184  deg
Eccentricity:     
0002004     
Arg of perigee:   127
2453  deg
Mean anomaly:     232
8894  deg
Mean motion:   15
75928121  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3118
Checksum:              284


Coasting Arc #9 (Orbit 3133)
---------------------------------------

Vector Time (GMT): 2007/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3486607
06                 A    =         6722032
88  meter
 Y    =       -4788979
68  meter          E    =           
0014569
 Z    =        3162663
49                 I    =           51
79803
 XDOT =       5896
734498                 Wp   =           97
79784
 YDOT =       1082
050231  meter/sec      RA   =          150
90138  deg
 ZDOT =      -4845
300633                 TA   =           45
38026
                                          MA   =           45
26152
                                          Ha   =            187
555  n
mi
                                          Hp   =            180
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11438999
53                 X    =         3524534
86
 Y    =      -15711875
58  feet           Y    =        -4749778
27  meter
 Z    =       10376192
57                 Z    =         3179694
31
 XDOT =      19346
241792                 XDOT =        5907
734958
 YDOT =       3550
033565  feet/sec       YDOT =        1148
052167  meter/sec
 ZDOT =     -15896
655621                 ZDOT =       -4816
626678

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1069120
67                 X    =         -325867
98
 Y    =       19370993
64  feet           Y    =         5904278
86  meter
 Z    =       10440340
17                 Z    =         3182215
68
 XDOT =     -16852
938244                 XDOT =       -5136
775577
 YDOT =       7608
598328  feet/sec       YDOT =        2319
100770  meter/sec
 ZDOT =     -15787
486484                 ZDOT =       -4812
025880


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   07298
53829369  
00020000  00000-0  20000-3 0  9088
2 25544  51
6360 151
6920 0001879 126
3933 233
7404 15
76015928 31347


Satellite: ISS
Catalog Number: 25544
Epoch time:      07298
53829369   =   yrday
fracday
Element set:     908
Inclination:       51
6360  deg
RA of node:       151
6920  deg
Eccentricity:     
0001879     
Arg of perigee:   126
3933  deg
Mean anomaly:     233
7404  deg
Mean motion:   15
76015928  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3134
Checksum:              307


Coasting Arc #10 (Orbit 3149)
---------------------------------------

Vector Time (GMT): 2007/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4773199
94                 A    =         6717501
44  meter
 Y    =       -1119803
32  meter          E    =           
0010419
 Z    =        4586573
30                 I    =           51
80516
 XDOT =       4222
656245                 Wp   =          117
72980
 YDOT =      -5712
655516  meter/sec      RA   =          145
80856  deg
 ZDOT =       2989
849024                 TA   =          302
64321
                                          MA   =          302
74369
                                          Ha   =            187
776  n
mi
                                          Hp   =            180
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15660104
78                 X    =        -4782604
92
 Y    =       -3673895
40  feet           Y    =        -1173232
50  meter
 Z    =       15047812
67                 Z    =         4563361
42
 XDOT =      13853
859073                 XDOT =        4271
697509
 YDOT =     -18742
308123  feet/sec       YDOT =       -5665
161162  meter/sec
 ZDOT =       9809
215958                 ZDOT =        3010
482586

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15132966
53                 X    =         4612528
20
 Y    =       -5690571
99  feet           Y    =        -1734486
34  meter
 Z    =       14959404
05                 Z    =         4559626
35
 XDOT =      -1478
078796                 XDOT =        -450
518417
 YDOT =      22146
046845  feet/sec       YDOT =        6750
115078  meter/sec
 ZDOT =       9886
960030                 ZDOT =        3013
545417


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   07299
55284522  
00020000  00000-0  20000-3 0  9098
2 25544  51
6344 146
4649 0001945 129
8567 230
2768 15
75971175 31501


Satellite: ISS
Catalog Number: 25544
Epoch time:      07299
55284522   =   yrday
fracday
Element set:     909
Inclination:       51
6344  deg
RA of node:       146
4649  deg
Eccentricity:     
0001945     
Arg of perigee:   129
8567  deg
Mean anomaly:     230
2768  deg
Mean motion:   15
75971175  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3150
Checksum:              321


Coasting Arc #11 (Orbit 3164)
---------------------------------------

Vector Time (GMT): 2007/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3820502
67                 A    =         6724634
62  meter
 Y    =        5161005
64  meter          E    =           
0006681
 Z    =       -1994083
72                 I    =           51
85207
 XDOT =      -5036
274778                 Wp   =           56
30910
 YDOT =      -1567
232777  meter/sec      RA   =          140
62911  deg
 ZDOT =       5609
839583                 TA   =          281
53552
                                          MA   =          281
61053
                                          Ha   =            187
475  n
mi
                                          Hp   =            180
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12534457
58                 X    =        -3868242
62
 Y    =       16932433
20  feet           Y    =         5118015
75  meter
 Z    =       -6542269
44                 Z    =        -2012760
18
 XDOT =     -16523
211215                 XDOT =       -5045
627979
 YDOT =      -5141
839820  feet/sec       YDOT =       -1623
603726  meter/sec
 ZDOT =      18404
985510                 ZDOT =        5585
349730

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         624879
52                 X    =          190463
28
 Y    =      -21035767
20  feet           Y    =        -6411701
84  meter
 Z    =       -6612657
15                 Z    =        -2015537
90
 XDOT =      15060
045069                 XDOT =        4590
301737
 YDOT =      -5291
617816  feet/sec       YDOT =       -1612
885110  meter/sec
 ZDOT =      18311
655209                 ZDOT =        5581
392508


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   07300
50396522  
00020000  00000-0  20000-3 0  9102
2 25544  51
6333 141
5641 0001873 138
8645 221
2661 15
76028020 31655


Satellite: ISS
Catalog Number: 25544
Epoch time:      07300
50396522   =   yrday
fracday
Element set:     910
Inclination:       51
6333  deg
RA of node:       141
5641  deg
Eccentricity:     
0001873     
Arg of perigee:   138
8645  deg
Mean anomaly:     221
2661  deg
Mean motion:   15
76028020  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3165
Checksum:              259


Coasting Arc #12 (Orbit 3180)
---------------------------------------

Vector Time (GMT): 2007/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 524298
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4015135
28                 A    =         6715006
90  meter
 Y    =        1696819
57  meter          E    =           
0014810
 Z    =       -5120795
48                 I    =           51
84031
 XDOT =      -4484
955912                 Wp   =           85
27626
 YDOT =       6065
829118  meter/sec      RA   =          135
52272  deg
 ZDOT =      -1509
145826                 TA   =          170
29133
                                          MA   =          170
26268
                                          Ha   =            187
437  n
mi
                                          Hp   =            180
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13173016
01                 X    =         4020739
43
 Y    =        5566993
35  feet           Y    =         1741750
73  meter
 Z    =      -16800510
11                 Z    =        -5101275
64
 XDOT =     -14714
422284                 XDOT =       -4545
120209
 YDOT =      19901
014166  feet/sec       YDOT =        6015
339499  meter/sec
 ZDOT =      -4951
265832                 ZDOT =       -1531
080190

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14022038
62                 X    =        -4273917
37
 Y    =        3224635
58  feet           Y    =          982868
93  meter
 Z    =      -16726059
42                 Z    =        -5098102
91
 XDOT =        542
445069                 XDOT =         165
337257
 YDOT =     -23708
944724  feet/sec       YDOT =       -7226
486352  meter/sec
 ZDOT =      -5033
951822                 ZDOT =       -1534
348515


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   07301
51847514  
00020000  00000-0  20000-3 0  9117
2 25544  51
6323 136
3368 0001925 141
3246 218
8056 15
76064256 31815


Satellite: ISS
Catalog Number: 25544
Epoch time:      07301
51847514   =   yrday
fracday
Element set:     911
Inclination:       51
6323  deg
RA of node:       136
3368  deg
Eccentricity:     
0001925     
Arg of perigee:   141
3246  deg
Mean anomaly:     218
8056  deg
Mean motion:   15
76064256  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3181
Checksum:              274

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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