Date: August 31st 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 2235)
---------------------------------------

Vector Time (GMT): 2007/241/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2265806
78                 A    =         6723400
97  meter
 Y    =       -5953236
99  meter          E    =           
0005645
 Z    =        2147112
03                 I    =           51
96554
 XDOT =       4013
715149                 Wp   =           88
04880
 YDOT =      -3531
477566  meter/sec      RA   =           84
45156  deg
 ZDOT =      -5543
411170                 TA   =           68
02647
                                          MA   =           67
96649
                                          Ha   =            186
138  n
mi
                                          Hp   =            182
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7433749
26                 X    =        -2209498
57
 Y    =      -19531617
44  feet           Y    =        -5978259
58  meter
 Z    =        7044330
81                 Z    =         2136241
94
 XDOT =      13168
356788                 XDOT =        4079
834966
 YDOT =     -11586
212486  feet/sec       YDOT =       -3486
224534  meter/sec
 ZDOT =     -18187
044520                 ZDOT =       -5523
751953

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7371301
95                 X    =         2246772
83
 Y    =       19570348
44  feet           Y    =         5965042
20  meter
 Z    =        7002333
47                 Z    =         2134311
24
 XDOT =     -11903
413608                 XDOT =       -3628
160468
 YDOT =      10979
246377  feet/sec       YDOT =        3346
474296  meter/sec
 ZDOT =     -18112
872324                 ZDOT =       -5520
803484


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   07241
59997297  
00020000  00000-0  20000-3 0  9000
2 25544  51
6315  84
9995 0009077 303
1176  56
9117 15
76389928 22361


Satellite: ISS
Catalog Number: 25544
Epoch time:      07241
59997297   =   yrday
fracday
Element set:     900
Inclination:       51
6315  deg
RA of node:        84
9995  deg
Eccentricity:     
0009077     
Arg of perigee:   303
1176  deg
Mean anomaly:      56
9117  deg
Mean motion:   15
76389928  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2236
Checksum:              333


Coasting Arc #2 (Orbit 2251)
---------------------------------------

Vector Time (GMT): 2007/242/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3601662
63                 A    =         6714258
50  meter
 Y    =        2470125
66  meter          E    =           
0003902
 Z    =        5101796
89                 I    =           51
92934
 XDOT =      -2599
762791                 Wp   =          309
01737
 YDOT =      -7074
108353  meter/sec      RA   =           79
35066  deg
 ZDOT =       1592
938709                 TA   =          125
77206
                                          MA   =          125
73577
                                          Ha   =            186
440  n
mi
                                          Hp   =            182
313

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11816478
44                 X    =        -3653799
78
 Y    =        8104086
83  feet           Y    =         2429558
61  meter
 Z    =       16738178
78                 Z    =         5084173
30
 XDOT =      -8529
405481                 XDOT =       -2528
204019
 YDOT =     -23209
016905  feet/sec       YDOT =       -7102
780174  meter/sec
 ZDOT =       5226
176867                 ZDOT =        1580
483320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11812283
96                 X    =         3600384
15
 Y    =       -8246195
96  feet           Y    =        -2513440
53  meter
 Z    =       16671599
06                 Z    =         5081503
39
 XDOT =       8234
966296                 XDOT =        2510
017727
 YDOT =      22243
400011  feet/sec       YDOT =        6779
788323  meter/sec
 ZDOT =       5178
027927                 ZDOT =        1578
262912


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   07242
61428397  
00020000  00000-0  20000-3 0  9015
2 25544  51
6307  79
7700 0008789 307
3845  52
6519 15
76341622 22522


Satellite: ISS
Catalog Number: 25544
Epoch time:      07242
61428397   =   yrday
fracday
Element set:     901
Inclination:       51
6307  deg
RA of node:        79
7700  deg
Eccentricity:     
0008789     
Arg of perigee:   307
3845  deg
Mean anomaly:      52
6519  deg
Mean motion:   15
76341622  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2252
Checksum:              299


Coasting Arc #3 (Orbit 2266)
---------------------------------------

Vector Time (GMT): 2007/243/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2265427
05                 A    =         6725186
17  meter
 Y    =        6294162
99  meter          E    =           
0013964
 Z    =        -595463
79                 I    =           51
96077
 XDOT =      -4306
113969                 Wp   =            1
83792
 YDOT =       2119
009372  meter/sec      RA   =           74
19850  deg
 ZDOT =       6033
326955                 TA   =          351
69815
                                          MA   =          351
72123
                                          Ha   =            186
403  n
mi
                                          Hp   =            182
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7432503
44                 X    =         2197769
07
 Y    =       20650141
04  feet           Y    =         6319117
95  meter
 Z    =       -1953621
37                 Z    =         -584622
95
 XDOT =     -14127
670502                 XDOT =       -4358
797877
 YDOT =       6952
130484  feet/sec       YDOT =        2070
561667  meter/sec
 ZDOT =      19794
379772                 ZDOT =        6012
279752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8042932
84                 X    =        -2451485
93
 Y    =      -20424095
76  feet           Y    =        -6225264
39  meter
 Z    =       -1911704
14                 Z    =         -582687
42
 XDOT =      12540
297246                 XDOT =        3822
282601
 YDOT =      -6778
138540  feet/sec       YDOT =       -2065
976627  meter/sec
 ZDOT =      19714
760991                 ZDOT =        6009
059150


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   07243
56517827  
00020000  00000-0  20000-3 0  9028
2 25544  51
6313  74
8677 0008716 310
1649  49
8751 15
76408047 22679


Satellite: ISS
Catalog Number: 25544
Epoch time:      07243
56517827   =   yrday
fracday
Element set:     902
Inclination:       51
6313  deg
RA of node:        74
8677  deg
Eccentricity:     
0008716     
Arg of perigee:   310
1649  deg
Mean anomaly:      49
8751  deg
Mean motion:   15
76408047  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2267
Checksum:              309


Coasting Arc #4 (Orbit 2282)
---------------------------------------

Vector Time (GMT): 2007/244/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3969490
45                 A    =         6713156
31  meter
 Y    =       -1213312
16  meter          E    =           
0010445
 Z    =       -5283487
77                 I    =           51
91199
 XDOT =       2557
184933                 Wp   =           58
11121
 YDOT =       7257
183235  meter/sec      RA   =           69
06919  deg
 ZDOT =        260
430293                 TA   =          214
31826
                                          MA   =          214
38579
                                          Ha   =            186
543  n
mi
                                          Hp   =            181
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13023262
64                 X    =         4008429
23
 Y    =       -3980682
95  feet           Y    =        -1168705
47  meter
 Z    =      -17334277
45                 Z    =        -5264109
27
 XDOT =       8389
714347                 XDOT =        2474
578844
 YDOT =      23809
656284  feet/sec       YDOT =        7285
317252  meter/sec
 ZDOT =        854
430096                 ZDOT =         272
652362

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12921694
66                 X    =        -3938532
53
 Y    =        4584786
90  feet           Y    =         1397443
05  meter
 Z    =      -17260878
23                 Z    =        -5261115
69
 XDOT =      -9145
678122                 XDOT =       -2787
602692
 YDOT =     -22452
895265  feet/sec       YDOT =       -6843
642477  meter/sec
 ZDOT =        901
697336                 ZDOT =         274
837348


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   07244
57944756  
00020000  00000-0  20000-3 0  9036
2 25544  51
6319  69
6398 0008619 314
6170  45
4290 15
76447957 22838


Satellite: ISS
Catalog Number: 25544
Epoch time:      07244
57944756   =   yrday
fracday
Element set:     903
Inclination:       51
6319  deg
RA of node:        69
6398  deg
Eccentricity:     
0008619     
Arg of perigee:   314
6170  deg
Mean anomaly:      45
4290  deg
Mean motion:   15
76447957  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2283
Checksum:              326


Coasting Arc #5 (Orbit 2298)
---------------------------------------

Vector Time (GMT): 2007/245/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2146738
23                 A    =         6724541
73  meter
 Y    =       -6283065
36  meter          E    =           
0000905
 Z    =       -1061281
62                 I    =           51
93959
 XDOT =       4855
753231                 Wp   =          172
82751
 YDOT =       -656
068450  meter/sec      RA   =           63
94670  deg
 ZDOT =      -5939
436142                 TA   =           18
73644
                                          MA   =           18
73311
                                          Ha   =            186
651  n
mi
                                          Hp   =            181
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7043104
43                 X    =        -2071164
96
 Y    =      -20613731
49  feet           Y    =        -6306648
84  meter
 Z    =       -3481895
09                 Z    =        -1071527
01
 XDOT =      15930
948922                 XDOT =        4891
581466
 YDOT =      -2152
455543  feet/sec       YDOT =        -601
568312  meter/sec
 ZDOT =     -19486
339048                 ZDOT =       -5915
759737

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8319320
47                 X    =         2535728
88
 Y    =       20125668
97  feet           Y    =         6134303
90  meter
 Z    =       -3521532
99                 Z    =        -1073363
26
 XDOT =     -14403
354097                 XDOT =       -4390
142329
 YDOT =       2560
744445  feet/sec       YDOT =         780
514907  meter/sec
 ZDOT =     -19396
556973                 ZDOT =       -5912
070565


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   07245
59369488  
00020000  00000-0  20000-3 0  9043
2 25544  51
6320  64
4104 0008874 319
2307  40
8192 15
76508943 22994


Satellite: ISS
Catalog Number: 25544
Epoch time:      07245
59369488   =   yrday
fracday
Element set:     904
Inclination:       51
6320  deg
RA of node:        64
4104  deg
Eccentricity:     
0008874     
Arg of perigee:   319
2307  deg
Mean anomaly:      40
8192  deg
Mean motion:   15
76508943  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2299
Checksum:              309


Coasting Arc #6 (Orbit 2314)
---------------------------------------

Vector Time (GMT): 2007/246/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4550849
46                 A    =         6714639
72  meter
 Y    =         -32907
18  meter          E    =           
0010312
 Z    =        4940435
31                 I    =           51
89202
 XDOT =      -2291
855227                 Wp   =             
08812
 YDOT =      -7032
339506  meter/sec      RA   =           58
78366  deg
 ZDOT =      -2147
864970                 TA   =          110
72495
                                          MA   =          110
61440
                                          Ha   =            186
865  n
mi
                                          Hp   =            181
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14930608
48                 X    =        -4574143
08
 Y    =        -107963
19  feet           Y    =          -83927
73  meter
 Z    =       16208777
28                 Z    =         4918270
63
 XDOT =      -7519
210062                 XDOT =       -2202
614250
 YDOT =     -23071
980008  feet/sec       YDOT =       -7057
469290  meter/sec
 ZDOT =      -7046
801084                 ZDOT =       -2158
782280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14981142
30                 X    =         4566252
17
 Y    =       -1104688
29  feet           Y    =         -336708
99  meter
 Z    =       16124646
53                 Z    =         4914792
26
 XDOT =       9236
711913                 XDOT =        2815
349791
 YDOT =      21300
543346  feet/sec       YDOT =        6492
405612  meter/sec
 ZDOT =      -7089
070626                 ZDOT =       -2160
748727


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   07246
60792467  
00020000  00000-0  20000-3 0  9054
2 25544  51
6323  59
1816 0008642 322
6696  37
3867 15
76465637 23151


Satellite: ISS
Catalog Number: 25544
Epoch time:      07246
60792467   =   yrday
fracday
Element set:     905
Inclination:       51
6323  deg
RA of node:        59
1816  deg
Eccentricity:     
0008642     
Arg of perigee:   322
6696  deg
Mean anomaly:      37
3867  deg
Mean motion:   15
76465637  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2315
Checksum:              317


Coasting Arc #7 (Orbit 2330)
---------------------------------------

Vector Time (GMT): 2007/247/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1774361
72                 A    =         6721836
82  meter
 Y    =        5911147
74  meter          E    =           
0013161
 Z    =        2641206
67                 I    =           51
90250
 XDOT =      -5603
358185                 Wp   =           39
88199
 YDOT =       -667
807653  meter/sec      RA   =           53
68704  deg
 ZDOT =       5254
497534                 TA   =          350
11452
                                          MA   =          350
14038
                                          Ha   =            186
814  n
mi
                                          Hp   =            180
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5821396
71                 X    =         1695300
02
 Y    =       19393529
34  feet           Y    =         5930547
49  meter
 Z    =        8665376
20                 Z    =         2649634
71
 XDOT =     -18383
721079                 XDOT =       -5620
999577
 YDOT =      -2190
969989  feet/sec       YDOT =        -730
566425  meter/sec
 ZDOT =      17239
165137                 ZDOT =        5227
233570

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7642468
08                 X    =        -2329424
27
 Y    =      -18735602
81  feet           Y    =        -5710611
74  meter
 Z    =        8698060
33                 Z    =         2651168
79
 XDOT =      17239
770290                 XDOT =        5254
681984
 YDOT =        929
663540  feet/sec       YDOT =         283
361447  meter/sec
 ZDOT =      17135
599474                 ZDOT =        5222
930720


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   07247
62212909  
00020000  00000-0  20000-3 0  9066
2 25544  51
6335  53
9529 0008728 325
7947  34
2654 15
76561290 23315


Satellite: ISS
Catalog Number: 25544
Epoch time:      07247
62212909   =   yrday
fracday
Element set:     906
Inclination:       51
6335  deg
RA of node:        53
9529  deg
Eccentricity:     
0008728     
Arg of perigee:   325
7947  deg
Mean anomaly:      34
2654  deg
Mean motion:   15
76561290  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2331
Checksum:              303


Coasting Arc #8 (Orbit 2345)
---------------------------------------

Vector Time (GMT): 2007/248/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5223139
15                 A    =         6717709
46  meter
 Y    =        1062080
81  meter          E    =           
0005853
 Z    =       -4087376
76                 I    =           51
87080
 XDOT =       1687
922831                 Wp   =           26
47572
 YDOT =       6460
252429  meter/sec      RA   =           48
50180  deg
 ZDOT =       3842
828965                 TA   =          282
84627
                                          MA   =          282
91165
                                          Ha   =            187
122  n
mi
                                          Hp   =            180
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17136283
30                 X    =         5230730
22
 Y    =        3484517
09  feet           Y    =         1120531
51  meter
 Z    =      -13410028
75                 Z    =        -4061984
43
 XDOT =       5537
804563                 XDOT =        1596
890225
 YDOT =      21195
053901  feet/sec       YDOT =        6478
618586  meter/sec
 ZDOT =      12607
706579                 ZDOT =        3850
807995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17497820
35                 X    =        -5333335
64
 Y    =       -1483074
30  feet           Y    =         -452041
05  meter
 Z    =      -13313516
04                 Z    =        -4057959
69
 XDOT =      -7975
127465                 XDOT =       -2430
818851
 YDOT =     -19150
113233  feet/sec       YDOT =       -5836
954513  meter/sec
 ZDOT =      12638
748489                 ZDOT =        3852
290540


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   07248
57292893  
00020000  00000-0  20000-3 0  9072
2 25544  51
6341  49
0517 0008848 330
0564  30
0094 15
76560266 23462


Satellite: ISS
Catalog Number: 25544
Epoch time:      07248
57292893   =   yrday
fracday
Element set:     907
Inclination:       51
6341  deg
RA of node:        49
0517  deg
Eccentricity:     
0008848     
Arg of perigee:   330
0564  deg
Mean anomaly:      30
0094  deg
Mean motion:   15
76560266  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2346
Checksum:              296


Coasting Arc #9 (Orbit 2361)
---------------------------------------

Vector Time (GMT): 2007/249/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1060352
73                 A    =         6717856
01  meter
 Y    =       -5311321
23  meter          E    =           
0010594
 Z    =       -3984288
49                 I    =           51
85184
 XDOT =       6361
187214                 Wp   =           15
07404
 YDOT =       1718
684966  meter/sec      RA   =           43
41326  deg
 ZDOT =      -3976
380996                 TA   =          213
82082
                                          MA   =          213
88844
                                          Ha   =            187
121  n
mi
                                          Hp   =            180
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3478847
53                 X    =         -981527
19
 Y    =      -17425594
59  feet           Y    =        -5322737
84  meter
 Z    =      -13071812
64                 Z    =        -3989248
32
 XDOT =      20870
036790                 XDOT =        6360
812175
 YDOT =       5638
730204  feet/sec       YDOT =        1789
817368  meter/sec
 ZDOT =     -13045
869410                 ZDOT =       -3945
479548

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5676037
04                 X    =         1730056
09
 Y    =       16823422
11  feet           Y    =         5127779
06  meter
 Z    =      -13091259
86                 Z    =        -3990216
00
 XDOT =     -20277
347801                 XDOT =       -6180
535610
 YDOT =      -3238
479472  feet/sec       YDOT =        -987
088543  meter/sec
 ZDOT =     -12928
361702                 ZDOT =       -3940
564647


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   07249
58709322  
00020000  00000-0  20000-3 0  9085
2 25544  51
6342  43
8225 0008915 333
8756  26
1958 15
76600402 23620


Satellite: ISS
Catalog Number: 25544
Epoch time:      07249
58709322   =   yrday
fracday
Element set:     908
Inclination:       51
6342  deg
RA of node:        43
8225  deg
Eccentricity:     
0008915     
Arg of perigee:   333
8756  deg
Mean anomaly:      26
1958  deg
Mean motion:   15
76600402  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2362
Checksum:              297


Coasting Arc #10 (Orbit 2377)
---------------------------------------

Vector Time (GMT): 2007/250/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5846645
10                 A    =         6721506
81  meter
 Y    =       -1859156
88  meter          E    =           
0011492
 Z    =        2745107
17                 I    =           51
84249
 XDOT =       -634
568462                 Wp   =           60
47212
 YDOT =      -5671
454584  meter/sec      RA   =           38
22303  deg
 ZDOT =      -5170
933622                 TA   =           88
23507
                                          MA   =           88
10345
                                          Ha   =            187
251  n
mi
                                          Hp   =            180
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19181906
48                 X    =        -5838756
24
 Y    =       -6099596
08  feet           Y    =        -1924493
28  meter
 Z    =        9006257
11                 Z    =         2716723
71
 XDOT =      -2081
917525                 XDOT =        -545
983137
 YDOT =     -18607
134461  feet/sec       YDOT =       -5678
055347  meter/sec
 ZDOT =     -16965
005321                 ZDOT =       -5173
801179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19926536
40                 X    =         6073608
29
 Y    =        3164949
12  feet           Y    =          964676
49  meter
 Z    =        8898287
47                 Z    =         2712198
02
 XDOT =       4968
537649                 XDOT =        1514
410275
 YDOT =      16650
017595  feet/sec       YDOT =        5074
925363  meter/sec
 ZDOT =     -16976
553470                 ZDOT =       -5174
453498


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   07250
60123569  
00020000  00000-0  20000-3 0  9094
2 25544  51
6345  38
5931 0008909 337
9370  22
1410 15
76627950 23781


Satellite: ISS
Catalog Number: 25544
Epoch time:      07250
60123569   =   yrday
fracday
Element set:     909
Inclination:       51
6345  deg
RA of node:        38
5931  deg
Eccentricity:     
0008909     
Arg of perigee:   337
9370  deg
Mean anomaly:      22
1410  deg
Mean motion:   15
76627950  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2378
Checksum:              297


Coasting Arc #11 (Orbit 2393)
---------------------------------------

Vector Time (GMT): 2007/251/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -43525
38                 A    =         6713968
08  meter
 Y    =        4580666
09  meter          E    =           
0005661
 Z    =        4904660
10                 I    =           51
79556
 XDOT =      -6961
447904                 Wp   =           25
35058
 YDOT =      -2447
660449  meter/sec      RA   =           33
12036  deg
 ZDOT =       2228
271360                 TA   =           43
08737
                                          MA   =           43
04306
                                          Ha   =            187
316  n
mi
                                          Hp   =            179
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -142799
81                 X    =         -118569
44
 Y    =       15028432
04  feet           Y    =         4579759
86  meter
 Z    =       16091404
52                 Z    =         4904266
29
 XDOT =     -22839
396009                 XDOT =       -6944
384794
 YDOT =      -8030
382050  feet/sec       YDOT =       -2525
411843  meter/sec
 ZDOT =       7310
601574                 ZDOT =        2194
494633

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2265277
72                 X    =         -690456
65
 Y    =      -14858449
37  feet           Y    =        -4528855
37  meter
 Z    =       16090446
23                 Z    =         4904368
01
 XDOT =      22812
386039                 XDOT =        6953
215265
 YDOT =       4285
192344  feet/sec       YDOT =        1306
126627  meter/sec
 ZDOT =       7182
085524                 ZDOT =        2189
099668


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   07251
61535372  
00020000  00000-0  20000-3 0  9107
2 25544  51
6355  33
3636 0009059 341
4805  18
6028 15
76708741 23948


Satellite: ISS
Catalog Number: 25544
Epoch time:      07251
61535372   =   yrday
fracday
Element set:     910
Inclination:       51
6355  deg
RA of node:        33
3636  deg
Eccentricity:     
0009059     
Arg of perigee:   341
4805  deg
Mean anomaly:      18
6028  deg
Mean motion:   15
76708741  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2394
Checksum:              287


Coasting Arc #12 (Orbit 2408)
---------------------------------------

Vector Time (GMT): 2007/252/13:32:14
583
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6203118
54                 A    =         6724048
98  meter
 Y    =        2330221
62  meter          E    =           
0017043
 Z    =       -1078742
24                 I    =           51
80480
 XDOT =       -799
754579                 Wp   =           12
37058
 YDOT =       4860
201278  meter/sec      RA   =           27
94783  deg
 ZDOT =       5933
243901                 TA   =          335
83201
                                          MA   =          335
91188
                                          Ha   =            187
574  n
mi
                                          Hp   =            179
501

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20351438
78                 X    =         6181840
89
 Y    =        7645084
07  feet           Y    =         2399469
38  meter
 Z    =       -3539180
59                 Z    =        -1048659
67
 XDOT =      -2623
866730                 XDOT =        -882
864892
 YDOT =      15945
542250  feet/sec       YDOT =        4850
793534  meter/sec
 ZDOT =      19466
023297                 ZDOT =        5929
156661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21425959
92                 X    =        -6530632
58
 Y    =       -3788644
40  feet           Y    =        -1154778
81  meter
 Z    =       -3424702
21                 Z    =        -1043849
23
 XDOT =       -506
814594                 XDOT =        -154
477088
 YDOT =     -14613
918057  feet/sec       YDOT =       -4454
322224  meter/sec
 ZDOT =      19451
078588                 ZDOT =        5928
688754


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   07252
56607122  
00020000  00000-0  20000-3 0  9116
2 25544  51
6360  28
4615 0009234 345
9992  14
0915 15
76693298 24099


Satellite: ISS
Catalog Number: 25544
Epoch time:      07252
56607122   =   yrday
fracday
Element set:     911
Inclination:       51
6360  deg
RA of node:        28
4615  deg
Eccentricity:     
0009234     
Arg of perigee:   345
9992  deg
Mean anomaly:      14
0915  deg
Mean motion:   15
76693298  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2409
Checksum:              297

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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