Date: October 11th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 3390 63 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 2865)
---------------------------------------

Vector Time (GMT): 2007/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4930762
34                 A    =         6719655
13  meter
 Y    =        1418216
94  meter          E    =           
0012235
 Z    =        4331843
11                 I    =           51
35008
 XDOT =       1016
880505                 Wp   =           70
39019
 YDOT =       6847
931094  meter/sec      RA   =          238
51664  deg
 ZDOT =      -3387
636582                 TA   =           53
91571
                                          MA   =           53
80246
                                          Ha   =            188
670  n
mi
                                          Hp   =            180
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16177041
81                 X    =         4893493
64
 Y    =        4652942
73  feet           Y    =         1473147
49  meter
 Z    =       14212083
70                 Z    =         4355706
35
 XDOT =       3336
222130                 XDOT =         956
687025
 YDOT =      22466
965533  feet/sec       YDOT =        6858
965594  meter/sec
 ZDOT =     -11114
293248                 ZDOT =       -3382
843296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16755769
15                 X    =        -5107158
44
 Y    =         -35140
20  feet           Y    =          -10710
73  meter
 Z    =       14302896
42                 Z    =         4359522
83
 XDOT =      -9463
065856                 XDOT =       -2884
342473
 YDOT =     -19437
718340  feet/sec       YDOT =       -5924
616550  meter/sec
 ZDOT =     -11095
203700                 ZDOT =       -3381
818088


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   07281
54160763  
00020000  00000-0  20000-3 0  9009
2 25544  51
6326 239
2005 0002757  70
4427 289
7034 15
75488250 28661


Satellite: ISS
Catalog Number: 25544
Epoch time:      07281
54160763   =   yrday
fracday
Element set:     900
Inclination:       51
6326  deg
RA of node:       239
2005  deg
Eccentricity:     
0002757     
Arg of perigee:    70
4427  deg
Mean anomaly:     289
7034  deg
Mean motion:   15
75488250  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2866
Checksum:              292


Coasting Arc #2 (Orbit 2881)
---------------------------------------

Vector Time (GMT): 2007/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -926954
37                 A    =         6722938
11  meter
 Y    =       -5743669
44  meter          E    =           
0015257
 Z    =        3355011
82                 I    =           51
37848
 XDOT =       5909
340895                 Wp   =           87
48896
 YDOT =       1758
558433  meter/sec      RA   =          233
40010  deg
 ZDOT =       4625
877712                 TA   =          312
25797
                                          MA   =          312
38726
                                          Ha   =            188
709  n
mi
                                          Hp   =            180
471

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3041188
89                 X    =         -878957
19
 Y    =      -18844059
84  feet           Y    =        -5753766
52  meter
 Z    =       11007256
63                 Z    =         3350625
68
 XDOT =      19387
601363                 XDOT =        5866
765219
 YDOT =       5769
548664  feet/sec       YDOT =        1824
402363  meter/sec
 ZDOT =      15176
764148                 ZDOT =        4654
482148

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8473259
27                 X    =         2582649
42
 Y    =       17115319
12  feet           Y    =         5216749
27  meter
 Z    =       10989852
07                 Z    =         3349706
91
 XDOT =     -18897
294143                 XDOT =       -5759
895255
 YDOT =       -496
262402  feet/sec       YDOT =        -151
260780  meter/sec
 ZDOT =      15285
630846                 ZDOT =        4659
060282


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   07282
55647504  
00020000  00000-0  20000-3 0  9015
2 25544  51
6335 233
9766 0002685  76
8019 283
3444 15
75531040 28822


Satellite: ISS
Catalog Number: 25544
Epoch time:      07282
55647504   =   yrday
fracday
Element set:     901
Inclination:       51
6335  deg
RA of node:       233
9766  deg
Eccentricity:     
0002685     
Arg of perigee:    76
8019  deg
Mean anomaly:     283
3444  deg
Mean motion:   15
75531040  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2882
Checksum:              299


Coasting Arc #3 (Orbit 2896)
---------------------------------------

Vector Time (GMT): 2007/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5390841
80                 A    =         6721878
74  meter
 Y    =       -1612664
67  meter          E    =           
0008413
 Z    =       -3684991
68                 I    =           51
39336
 XDOT =      -1042
075900                 Wp   =           94
49179
 YDOT =      -6303
041028  meter/sec      RA   =          228
18256  deg
 ZDOT =       4290
631717                 TA   =          220
99417
                                          MA   =          221
05744
                                          Ha   =            188
720  n
mi
                                          Hp   =            180
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17686488
85                 X    =        -5354506
70
 Y    =       -5290894
59  feet           Y    =        -1672745
25  meter
 Z    =      -12089867
71                 Z    =        -3711092
52
 XDOT =      -3418
884186                 XDOT =        -992
360427
 YDOT =     -20679
268464  feet/sec       YDOT =       -6314
415800  meter/sec
 ZDOT =      14076
875713                 ZDOT =        4285
690469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18391041
82                 X    =         5605589
55
 Y    =        -403853
57  feet           Y    =         -123094
57  meter
 Z    =      -12189209
89                 Z    =        -3715271
17
 XDOT =       9678
947164                 XDOT =        2950
143096
 YDOT =      17249
736034  feet/sec       YDOT =        5257
719543  meter/sec
 ZDOT =      14057
287941                 ZDOT =        4284
661364


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   07283
50790204  
00020000  00000-0  20000-3 0  9028
2 25544  51
6336 229
0787 0002714  76
3032 283
8434 15
75507980 28971


Satellite: ISS
Catalog Number: 25544
Epoch time:      07283
50790204   =   yrday
fracday
Element set:     902
Inclination:       51
6336  deg
RA of node:       229
0787  deg
Eccentricity:     
0002714     
Arg of perigee:    76
3032  deg
Mean anomaly:     283
8434  deg
Mean motion:   15
75507980  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2897
Checksum:              301


Coasting Arc #4 (Orbit 2912)
---------------------------------------

Vector Time (GMT): 2007/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         823384
50                 A    =         6720410
86  meter
 Y    =        5260476
14  meter          E    =           
0010404
 Z    =       -4111036
54                 I    =           51
40991
 XDOT =      -6437
419214                 Wp   =           73
26232
 YDOT =      -1920
036901  meter/sec      RA   =          223
06955  deg
 ZDOT =      -3751
079079                 TA   =          158
17003
                                          MA   =          158
12567
                                          Ha   =            188
696  n
mi
                                          Hp   =            180
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2701392
70                 X    =          784471
02
 Y    =       17258779
98  feet           Y    =         5269465
84  meter
 Z    =      -13487652
69                 Z    =        -4107131
32
 XDOT =     -21120
141778                 XDOT =       -6397
248124
 YDOT =      -6299
333666  feet/sec       YDOT =       -1991
799410  meter/sec
 ZDOT =     -12306
689892                 ZDOT =       -3782
255101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8233775
24                 X    =        -2509654
69
 Y    =      -15420320
93  feet           Y    =        -4700113
82  meter
 Z    =      -13472135
37                 Z    =        -4106306
86
 XDOT =      20830
716677                 XDOT =        6349
202443
 YDOT =       -281
133428  feet/sec       YDOT =         -85
689469  meter/sec
 ZDOT =     -12425
351688                 ZDOT =       -3787
247195


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   07284
52274238  
00020000  00000-0  20000-3 0  9036
2 25544  51
6346 223
8542 0002758  80
0156 280
1319 15
75558934 29136


Satellite: ISS
Catalog Number: 25544
Epoch time:      07284
52274238   =   yrday
fracday
Element set:     903
Inclination:       51
6346  deg
RA of node:       223
8542  deg
Eccentricity:     
0002758     
Arg of perigee:    80
0156  deg
Mean anomaly:     280
1319  deg
Mean motion:   15
75558934  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2913
Checksum:              294


Coasting Arc #5 (Orbit 2928)
---------------------------------------

Vector Time (GMT): 2007/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5851792
91                 A    =         6724117
06  meter
 Y    =        1688652
44  meter          E    =           
0016095
 Z    =        2833170
93                 I    =           51
44524
 XDOT =        807
858109                 Wp   =           96
45202
 YDOT =       5747
139603  meter/sec      RA   =          217
85795  deg
 ZDOT =      -5071
255535                 TA   =           50
90903
                                          MA   =           50
76600
                                          Ha   =            188
596  n
mi
                                          Hp   =            180
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19198795
64                 X    =         5818711
82
 Y    =        5540198
30  feet           Y    =         1753905
68  meter
 Z    =        9295180
22                 Z    =         2861519
26
 XDOT =       2650
453114                 XDOT =         768
168596
 YDOT =      18855
444892  feet/sec       YDOT =        5755
951354  meter/sec
 ZDOT =     -16637
977477                 ZDOT =       -5067
427559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19887674
07                 X    =        -6061763
06
 Y    =        1323065
14  feet           Y    =          403270
25  meter
 Z    =        9403076
36                 Z    =         2866057
67
 XDOT =      -8914
746882                 XDOT =       -2717
214850
 YDOT =     -15338
422772  feet/sec       YDOT =       -4675
151261  meter/sec
 ZDOT =     -16622
691310                 ZDOT =       -5066
596311


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   07285
53756821  
00020000  00000-0  20000-3 0  9042
2 25544  51
6350 218
6303 0002722  83
4798 276
6676 15
75577371 29297


Satellite: ISS
Catalog Number: 25544
Epoch time:      07285
53756821   =   yrday
fracday
Element set:     904
Inclination:       51
6350  deg
RA of node:       218
6303  deg
Eccentricity:     
0002722     
Arg of perigee:    83
4798  deg
Mean anomaly:     276
6676  deg
Mean motion:   15
75577371  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2929
Checksum:              321


Coasting Arc #6 (Orbit 2944)
---------------------------------------

Vector Time (GMT): 2007/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -534406
39                 A    =         6718016
20  meter
 Y    =       -4780505
60  meter          E    =           
0010256
 Z    =        4683026
15                 I    =           51
44854
 XDOT =       6958
093672                 Wp   =          110
95039
 YDOT =       1896
070259  meter/sec      RA   =          212
74191  deg
 ZDOT =       2721
171147                 TA   =          312
17170
                                          MA   =          312
25876
                                          Ha   =            188
575  n
mi
                                          Hp   =            180
333

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1753301
80                 X    =         -503660
28
 Y    =      -15684073
49  feet           Y    =        -4786309
57  meter
 Z    =       15364259
03                 Z    =         4680504
77
 XDOT =      22828
391313                 XDOT =        6923
155051
 YDOT =       6220
702951  feet/sec       YDOT =        1973
684339  meter/sec
 ZDOT =       8927
726861                 ZDOT =        2754
889592

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7321142
04                 X    =         2231484
09
 Y    =       13992080
32  feet           Y    =         4264786
08  meter
 Z    =       15354063
03                 Z    =         4679918
41
 XDOT =     -22476
732304                 XDOT =       -6850
908006
 YDOT =       1792
800081  feet/sec       YDOT =         546
445465  meter/sec
 ZDOT =       9056
054600                 ZDOT =        2760
285442


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   07286
55237823  
00020000  00000-0  20000-3 0  9052
2 25544  51
6350 213
4064 0002625  89
5761 270
5704 15
75618711 29450


Satellite: ISS
Catalog Number: 25544
Epoch time:      07286
55237823   =   yrday
fracday
Element set:     905
Inclination:       51
6350  deg
RA of node:       213
4064  deg
Eccentricity:     
0002625     
Arg of perigee:    89
5761  deg
Mean anomaly:     270
5704  deg
Mean motion:   15
75618711  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2945
Checksum:              294


Coasting Arc #7 (Orbit 2959)
---------------------------------------

Vector Time (GMT): 2007/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6260444
54                 A    =         6726010
88  meter
 Y    =       -1581385
74  meter          E    =           
0008932
 Z    =       -1876752
62                 I    =           51
50045
 XDOT =       -357
870458                 Wp   =           52
56342
 YDOT =      -5238
981155  meter/sec      RA   =          207
54348  deg
 ZDOT =       5631
856475                 TA   =          286
54344
                                          MA   =          286
64154
                                          Ha   =            188
553  n
mi
                                          Hp   =            180
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20539516
21                 X    =        -6233178
77
 Y    =       -5188273
44  feet           Y    =        -1651241
15  meter
 Z    =       -6157324
87                 Z    =        -1907100
47
 XDOT =      -1174
115677                 XDOT =        -326
620101
 YDOT =     -17188
258384  feet/sec       YDOT =       -5242
808259  meter/sec
 ZDOT =      18477
219407                 ZDOT =        5630
193872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20959238
22                 X    =         6388375
81
 Y    =       -2839834
57  feet           Y    =         -865581
58  meter
 Z    =       -6272816
73                 Z    =        -1911954
54
 XDOT =       7394
015542                 XDOT =        2253
695937
 YDOT =      13940
834907  feet/sec       YDOT =        4249
166480  meter/sec
 ZDOT =      18470
228501                 ZDOT =        5629
725647


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   07287
50375106  
00020000  00000-0  20000-3 0  9066
2 25544  51
6348 208
5084 0002635  90
0401 270
1065 15
75606075 29606


Satellite: ISS
Catalog Number: 25544
Epoch time:      07287
50375106   =   yrday
fracday
Element set:     906
Inclination:       51
6348  deg
RA of node:       208
5084  deg
Eccentricity:     
0002635     
Arg of perigee:    90
0401  deg
Mean anomaly:     270
1065  deg
Mean motion:   15
75606075  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2960
Checksum:              274


Coasting Arc #8 (Orbit 2975)
---------------------------------------

Vector Time (GMT): 2007/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          26546
37                 A    =         6716208
47  meter
 Y    =        4394451
99  meter          E    =           
0016410
 Z    =       -5093424
12                 I    =           51
49447
 XDOT =      -7340
783655                 Wp   =           81
07985
 YDOT =      -1717
992378  meter/sec      RA   =          202
41559  deg
 ZDOT =      -1522
155214                 TA   =          174
28030
                                          MA   =          174
26154
                                          Ha   =            188
542  n
mi
                                          Hp   =            180
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          87094
39                 X    =            2148
57
 Y    =       14417493
42  feet           Y    =         4394612
46  meter
 Z    =      -16710709
04                 Z    =        -5093354
39
 XDOT =     -24083
935875                 XDOT =       -7313
632665
 YDOT =      -5636
457934  feet/sec       YDOT =       -1799
929359  meter/sec
 ZDOT =      -4993
947552                 ZDOT =       -1557
751748

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5777359
61                 X    =        -1760939
21
 Y    =      -13210659
20  feet           Y    =        -4026608
92  meter
 Z    =      -16709880
25                 Z    =        -5093171
50
 XDOT =      23389
376791                 XDOT =        7129
082046
 YDOT =      -3747
600832  feet/sec       YDOT =       -1142
268734  meter/sec
 ZDOT =      -5129
408221                 ZDOT =       -1563
443626


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   07288
51853316  
00020000  00000-0  20000-3 0  9073
2 25544  51
6354 203
2837 0002713  93
9613 266
1861 15
75652840 29762


Satellite: ISS
Catalog Number: 25544
Epoch time:      07288
51853316   =   yrday
fracday
Element set:     907
Inclination:       51
6354  deg
RA of node:       203
2837  deg
Eccentricity:     
0002713     
Arg of perigee:    93
9613  deg
Mean anomaly:     266
1861  deg
Mean motion:   15
75652840  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2976
Checksum:              307


Coasting Arc #9 (Orbit 2991)
---------------------------------------

Vector Time (GMT): 2007/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6530077
31                 A    =         6727225
12  meter
 Y    =        1390981
05  meter          E    =           
0015954
 Z    =         764359
26                 I    =           51
55876
 XDOT =       -326
940391                 Wp   =          122
52118
 YDOT =       4860
474273  meter/sec      RA   =          197
23876  deg
 ZDOT =      -5970
325299                 TA   =           49
12897
                                          MA   =           48
99083
                                          Ha   =            188
528  n
mi
                                          Hp   =            180
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21424138
16                 X    =         6510324
61
 Y    =        4563586
13  feet           Y    =         1463893
61  meter
 Z    =        2507740
36                 Z    =          796035
18
 XDOT =      -1072
639079                 XDOT =        -352
263189
 YDOT =      15946
437904  feet/sec       YDOT =        4856
676758  meter/sec
 ZDOT =     -19587
681428                 ZDOT =       -5971
975040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21423815
78                 X    =        -6529979
05
 Y    =        4496783
06  feet           Y    =         1370619
48  meter
 Z    =        2628276
15                 Z    =          801098
57
 XDOT =      -5249
384356                 XDOT =       -1600
012352
 YDOT =     -13408
121085  feet/sec       YDOT =       -4086
795307  meter/sec
 ZDOT =     -19593
327722                 ZDOT =       -5972
046290


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   07289
53330082  
00020000  00000-0  20000-3 0  9087
2 25544  51
6352 198
0590 0002671  99
3537 260
7929 15
75645397 29927


Satellite: ISS
Catalog Number: 25544
Epoch time:      07289
53330082   =   yrday
fracday
Element set:     908
Inclination:       51
6352  deg
RA of node:       198
0590  deg
Eccentricity:     
0002671     
Arg of perigee:    99
3537  deg
Mean anomaly:     260
7929  deg
Mean motion:   15
75645397  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2992
Checksum:              326


Coasting Arc #10 (Orbit 3007)
---------------------------------------

Vector Time (GMT): 2007/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         618972
90                 A    =         6715220
36  meter
 Y    =       -4132920
86  meter          E    =           
0004984
 Z    =        5252301
97                 I    =           51
54676
 XDOT =       7570
246789                 Wp   =          103
10288
 YDOT =       1432
360220  meter/sec      RA   =          192
09421  deg
 ZDOT =        233
657516                 TA   =          344
67119
                                          MA   =          344
68628
                                          Ha   =            188
336  n
mi
                                          Hp   =            180
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2030750
97                 X    =          639626
58
 Y    =      -13559451
65  feet           Y    =        -4125883
80  meter
 Z    =       17231961
84                 Z    =         5255359
07
 XDOT =      24836
767680                 XDOT =        7552
532191
 YDOT =       4699
344553  feet/sec       YDOT =        1516
915949  meter/sec
 ZDOT =        766
592901                 ZDOT =         270
391533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3948758
09                 X    =         1203581
46
 Y    =       13115170
68  feet           Y    =         3997504
02  meter
 Z    =       17243050
63                 Z    =         5255681
83
 XDOT =     -23548
959744                 XDOT =       -7177
722930
 YDOT =       5892
964413  feet/sec       YDOT =        1796
175553  meter/sec
 ZDOT =        906
368942                 ZDOT =         276
261253


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
54805129  
00020000  00000-0  20000-3 0  9090
2 25544  51
6350 192
8343 0002499 102
4327 257
7117 15
75720701 30081


Satellite: ISS
Catalog Number: 25544
Epoch time:      07290
54805129   =   yrday
fracday
Element set:     909
Inclination:       51
6350  deg
RA of node:       192
8343  deg
Eccentricity:     
0002499     
Arg of perigee:   102
4327  deg
Mean anomaly:     257
7117  deg
Mean motion:   15
75720701  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3008
Checksum:              283


Coasting Arc #11 (Orbit 3023)
---------------------------------------

Vector Time (GMT): 2007/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6620649
08                 A    =         6727296
11  meter
 Y    =       -1099728
60  meter          E    =           
0014479
 Z    =         367875
38                 I    =           51
61619
 XDOT =       1119
574057                 Wp   =           57
10015
 YDOT =      -4670
587269  meter/sec      RA   =          186
94251  deg
 ZDOT =       6023
843432                 TA   =          306
90364
                                          MA   =          307
03623
                                          Ha   =            188
380  n
mi
                                          Hp   =            180
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21721289
62                 X    =        -6609646
78
 Y    =       -3608033
47  feet           Y    =        -1173702
94  meter
 Z    =        1206940
22                 Z    =          335738
42
 XDOT =       3673
143233                 XDOT =        1142
454819
 YDOT =     -15323
449044  feet/sec       YDOT =       -4657
939746  meter/sec
 ZDOT =      19763
265852                 ZDOT =        6029
337899

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21125914
79                 X    =         6439178
83
 Y    =       -6229628
09  feet           Y    =        -1898790
64  meter
 Z    =        1084661
61                 Z    =          330604
86
 XDOT =       3023
760296                 XDOT =         921
642138
 YDOT =      13802
263729  feet/sec       YDOT =        4206
929985  meter/sec
 ZDOT =      19783
549859                 ZDOT =        6030
025997


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
56279009  
00020000  00000-0  20000-3 0  9107
2 25544  51
6353 187
6092 0002527 103
6320 256
5125 15
75703198 30240


Satellite: ISS
Catalog Number: 25544
Epoch time:      07291
56279009   =   yrday
fracday
Element set:     910
Inclination:       51
6353  deg
RA of node:       187
6092  deg
Eccentricity:     
0002527     
Arg of perigee:   103
6320  deg
Mean anomaly:     256
5125  deg
Mean motion:   15
75703198  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3024
Checksum:              279


Coasting Arc #12 (Orbit 3038)
---------------------------------------

Vector Time (GMT): 2007/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1358545
48                 A    =         6715517
76  meter
 Y    =        4066973
12  meter          E    =           
0016913
 Z    =       -5183139
56                 I    =           51
60625
 XDOT =      -7530
375760                 Wp   =           99
95270
 YDOT =      -1108
962493  meter/sec      RA   =          181
77890  deg
 ZDOT =       1103
800297                 TA   =          180
59725
                                          MA   =          180
59927
                                          Ha   =            188
289  n
mi
                                          Hp   =            180
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4457170
21                 X    =        -1378742
91
 Y    =       13343087
67  feet           Y    =         4051668
21  meter
 Z    =      -17005051
06                 Z    =        -5189788
49
 XDOT =     -24705
957217                 XDOT =       -7522
777635
 YDOT =      -3638
328390  feet/sec       YDOT =       -1193
128943  meter/sec
 ZDOT =       3621
392050                 ZDOT =        1067
235665

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2133804
78                 X    =         -650383
70
 Y    =      -13874756
16  feet           Y    =        -4229025
68  meter
 Z    =      -17029801
38                 Z    =        -5190683
46
 XDOT =      22692
680528                 XDOT =        6916
729025
 YDOT =      -7763
326419  feet/sec       YDOT =       -2366
261892  meter/sec
 ZDOT =       3482
268781                 ZDOT =        1061
395524


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
51409224  
00020000  00000-0  20000-3 0  9118
2 25544  51
6358 182
7107 0002467 107
7041 252
4393 15
75742342 30398


Satellite: ISS
Catalog Number: 25544
Epoch time:      07292
51409224   =   yrday
fracday
Element set:     911
Inclination:       51
6358  deg
RA of node:       182
7107  deg
Eccentricity:     
0002467     
Arg of perigee:   107
7041  deg
Mean anomaly:     252
4393  deg
Mean motion:   15
75742342  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3039
Checksum:              278

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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