Date: August 28th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5381 96 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 2203)
---------------------------------------

Vector Time (GMT): 2007/239/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1863239
92                 A    =         6724473
63  meter
 Y    =       -6231504
55  meter          E    =           
0004040
 Z    =       -1698769
62                 I    =           51
96978
 XDOT =       4267
997502                 Wp   =          235
09471
 YDOT =       2844
361332  meter/sec      RA   =           94
85939  deg
 ZDOT =      -5745
301999                 TA   =          323
61794
                                          MA   =          323
64540
                                          Ha   =            185
909  n
mi
                                          Hp   =            183
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6112991
87                 X    =         1941035
21
 Y    =      -20444568
72  feet           Y    =        -6210233
78  meter
 Z    =       -5573391
16                 Z    =        -1689529
17
 XDOT =      14002
616477                 XDOT =        4263
783336
 YDOT =       9331
894134  feet/sec       YDOT =        2892
064886  meter/sec
 ZDOT =     -18849
416008                 ZDOT =       -5724
578717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9572015
57                 X    =        -2917550
35
 Y    =       19081578
94  feet           Y    =         5816065
26  meter
 Z    =       -5539098
47                 Z    =        -1688317
21
 XDOT =     -10899
670854                 XDOT =       -3322
219676
 YDOT =     -10923
440209  feet/sec       YDOT =       -3329
464576  meter/sec
 ZDOT =     -18770
412959                 ZDOT =       -5721
221870


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   07239
57129639  
00020000  00000-0  20000-3 0  9002
2 25544  51
6328  95
4569 0008899 295
5931  64
4313 15
76273086 22047


Satellite: ISS
Catalog Number: 25544
Epoch time:      07239
57129639   =   yrday
fracday
Element set:     900
Inclination:       51
6328  deg
RA of node:        95
4569  deg
Eccentricity:     
0008899     
Arg of perigee:   295
5931  deg
Mean anomaly:      64
4313  deg
Mean motion:   15
76273086  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2204
Checksum:              321


Coasting Arc #2 (Orbit 2219)
---------------------------------------

Vector Time (GMT): 2007/240/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3698790
16                 A    =         6716060
41  meter
 Y    =       -3056686
29  meter          E    =           
0008028
 Z    =        4703275
39                 I    =           51
94251
 XDOT =       2133
760754                 Wp   =          353
96928
 YDOT =      -6859
800306  meter/sec      RA   =           89
69018  deg
 ZDOT =      -2772
787713                 TA   =          123
28244
                                          MA   =          123
20551
                                          Ha   =            186
069  n
mi
                                          Hp   =            182
894

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12135138
31                 X    =        -3687182
24
 Y    =      -10028498
32  feet           Y    =        -3097983
18  meter
 Z    =       15430693
53                 Z    =         4685335
25
 XDOT =       7000
527408                 XDOT =        2223
778965
 YDOT =     -22505
906517  feet/sec       YDOT =       -6835
436168  meter/sec
 ZDOT =      -9097
072549                 ZDOT =       -2762
203181

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10517317
12                 X    =         3205678
26
 Y    =       11803676
09  feet           Y    =         3597760
47  meter
 Z    =       15362224
27                 Z    =         4682405
96
 XDOT =      -9597
832441                 XDOT =       -2925
419328
 YDOT =      20372
016884  feet/sec       YDOT =        6209
390746  meter/sec
 ZDOT =      -9057
757519                 ZDOT =       -2760
804492


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   07240
58564777  
00020000  00000-0  20000-3 0  9012
2 25544  51
6325  90
2278 0008956 299
2098  60
8170 15
76309702 22207


Satellite: ISS
Catalog Number: 25544
Epoch time:      07240
58564777   =   yrday
fracday
Element set:     901
Inclination:       51
6325  deg
RA of node:        90
2278  deg
Eccentricity:     
0008956     
Arg of perigee:   299
2098  deg
Mean anomaly:      60
8170  deg
Mean motion:   15
76309702  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2220
Checksum:              301


Coasting Arc #3 (Orbit 2235)
---------------------------------------

Vector Time (GMT): 2007/241/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1895169
50                 A    =         6721348
43  meter
 Y    =        5653184
78  meter          E    =           
0008141
 Z    =        3090855
40                 I    =           51
95818
 XDOT =      -4260
378643                 Wp   =           42
79828
 YDOT =      -4122
004728  meter/sec      RA   =           84
60309  deg
 ZDOT =       4925
223822                 TA   =          352
96032
                                          MA   =          352
97175
                                          Ha   =            186
200  n
mi
                                          Hp   =            182
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6217747
72                 X    =        -1973258
07
 Y    =       18547194
16  feet           Y    =         5631555
47  meter
 Z    =       10140601
72                 Z    =         3081458
79
 XDOT =     -13977
620220                 XDOT =       -4237
894735
 YDOT =     -13523
637559  feet/sec       YDOT =       -4169
520715  meter/sec
 ZDOT =      16158
870808                 ZDOT =        4904
581948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8776993
37                 X    =         2675227
58
 Y    =      -17502312
81  feet           Y    =        -5334704
94  meter
 Z    =       10105643
70                 Z    =         3080200
20
 XDOT =      10788
438108                 XDOT =        3288
315935
 YDOT =      14697
742886  feet/sec       YDOT =        4479
872032  meter/sec
 ZDOT =      16080
014933                 ZDOT =        4901
188551


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
59998278  
00020000  00000-0  20000-3 0  9022
2 25544  51
6314  84
9984 0008940 302
6107  57
4194 15
76355175 22362


Satellite: ISS
Catalog Number: 25544
Epoch time:      07241
59998278   =   yrday
fracday
Element set:     902
Inclination:       51
6314  deg
RA of node:        84
9984  deg
Eccentricity:     
0008940     
Arg of perigee:   302
6107  deg
Mean anomaly:      57
4194  deg
Mean motion:   15
76355175  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2236
Checksum:              316


Coasting Arc #4 (Orbit 2250)
---------------------------------------

Vector Time (GMT): 2007/242/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3772418
18                 A    =         6719300
42  meter
 Y    =        4072092
09  meter          E    =           
0003982
 Z    =       -3782127
70                 I    =           51
94682
 XDOT =      -2252
698226                 Wp   =          343
39246
 YDOT =       6024
421128  meter/sec      RA   =           79
41955  deg
 ZDOT =       4242
024584                 TA   =          330
95889
                                          MA   =          330
98104
                                          Ha   =            186
403  n
mi
                                          Hp   =            182
333

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12376700
08                 X    =         3744975
89
 Y    =       13359882
18  feet           Y    =         4114123
75  meter
 Z    =      -12408555
43                 Z    =        -3763868
24
 XDOT =      -7390
742211                 XDOT =       -2340
503685
 YDOT =      19765
161182  feet/sec       YDOT =        5998
739477  meter/sec
 ZDOT =      13917
403491                 ZDOT =        4230
867404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10736586
60                 X    =        -3272511
59
 Y    =      -14768965
44  feet           Y    =        -4501580
67  meter
 Z    =      -12338750
86                 Z    =        -3760851
26
 XDOT =       8730
564237                 XDOT =        2661
075979
 YDOT =     -17932
124671  feet/sec       YDOT =       -5465
711600  meter/sec
 ZDOT =      13875
806406                 ZDOT =        4229
345792


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
55090850  
00020000  00000-0  20000-3 0  9039
2 25544  51
6310  80
0959 0008800 306
7577  53
2778 15
76357485 22513


Satellite: ISS
Catalog Number: 25544
Epoch time:      07242
55090850   =   yrday
fracday
Element set:     903
Inclination:       51
6310  deg
RA of node:        80
0959  deg
Eccentricity:     
0008800     
Arg of perigee:   306
7577  deg
Mean anomaly:      53
2778  deg
Mean motion:   15
76357485  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2251
Checksum:              294


Coasting Arc #5 (Orbit 2266)
---------------------------------------

Vector Time (GMT): 2007/243/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2100719
02                 A    =         6717601
20  meter
 Y    =       -4781737
14  meter          E    =           
0008800
 Z    =       -4231320
11                 I    =           51
93514
 XDOT =       4404
967696                 Wp   =            7
87415
 YDOT =       5160
470215  meter/sec      RA   =           74
33826  deg
 ZDOT =      -3637
180074                 TA   =          225
21291
                                          MA   =          225
28451
                                          Ha   =            186
468  n
mi
                                          Hp   =            182
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6892122
78                 X    =         2174588
02
 Y    =      -15688113
98  feet           Y    =        -4757832
88  meter
 Z    =      -13882283
83                 Z    =        -4220935
16
 XDOT =      14451
993752                 XDOT =        4364
603959
 YDOT =      16930
676560  feet/sec       YDOT =        5209
503206  meter/sec
 ZDOT =     -11933
005493                 ZDOT =       -3615
878975

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8563980
60                 X    =        -2610301
29
 Y    =       14877935
98  feet           Y    =         4534794
89  meter
 Z    =      -13843458
32                 Z    =        -4219486
10
 XDOT =     -11594
057885                 XDOT =       -3533
868843
 YDOT =     -17724
603992  feet/sec       YDOT =       -5402
459297  meter/sec
 ZDOT =     -11851
528259                 ZDOT =       -3612
345813


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
56521203  
00020000  00000-0  20000-3 0  9043
2 25544  51
6312  74
8679 0008770 311
7199  48
3214 15
76400249 22671


Satellite: ISS
Catalog Number: 25544
Epoch time:      07243
56521203   =   yrday
fracday
Element set:     904
Inclination:       51
6312  deg
RA of node:        74
8679  deg
Eccentricity:     
0008770     
Arg of perigee:   311
7199  deg
Mean anomaly:      48
3214  deg
Mean motion:   15
76400249  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2267
Checksum:              286


Coasting Arc #6 (Orbit 2282)
---------------------------------------

Vector Time (GMT): 2007/244/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3928119
54                 A    =         6722645
51  meter
 Y    =       -4857751
25  meter          E    =           
0007496
 Z    =        2481512
87                 I    =           51
94340
 XDOT =       2630
763660                 Wp   =           68
93887
 YDOT =      -4870
169294  meter/sec      RA   =           69
15788  deg
 ZDOT =      -5353
830805                 TA   =           83
10249
                                          MA   =           83
01723
                                          Ha   =            186
595  n
mi
                                          Hp   =            181
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12887531
32                 X    =        -3885562
30
 Y    =      -15937504
11  feet           Y    =        -4901439
70  meter
 Z    =        8141446
43                 Z    =         2462533
44
 XDOT =       8631
114369                 XDOT =        2711
035172
 YDOT =     -15978
245716  feet/sec       YDOT =       -4840
301902  meter/sec
 ZDOT =     -17565
061697                 ZDOT =       -5340
855406

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11499292
74                 X    =         3504984
43
 Y    =       17001058
49  feet           Y    =         5181922
63  meter
 Z    =        8068824
43                 Z    =         2459377
69
 XDOT =      -8845
261481                 XDOT =       -2696
035700
 YDOT =      14320
617989  feet/sec       YDOT =        4364
924363  meter/sec
 ZDOT =     -17516
408102                 ZDOT =       -5339
001190


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
57949748  
00020000  00000-0  20000-3 0  9054
2 25544  51
6313  69
6386 0008977 314
4891  45
5539 15
76427152 22836


Satellite: ISS
Catalog Number: 25544
Epoch time:      07244
57949748   =   yrday
fracday
Element set:     905
Inclination:       51
6313  deg
RA of node:        69
6386  deg
Eccentricity:     
0008977     
Arg of perigee:   314
4891  deg
Mean anomaly:      45
5539  deg
Mean motion:   15
76427152  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2283
Checksum:              332


Coasting Arc #7 (Orbit 2298)
---------------------------------------

Vector Time (GMT): 2007/245/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2563081
18                 A    =         6714456
56  meter
 Y    =        3682983
97  meter          E    =           
0003527
 Z    =        4994903
35                 I    =           51
90444
 XDOT =      -4581
697876                 Wp   =          342
93876
 YDOT =      -5869
552248  meter/sec      RA   =           64
06063  deg
 ZDOT =       1980
506646                 TA   =           88
01771
                                          MA   =           87
97732
                                          Ha   =            186
843  n
mi
                                          Hp   =            181
494

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8409058
98                 X    =        -2628338
83
 Y    =       12083280
73  feet           Y    =         3653957
24  meter
 Z    =       16387478
20                 Z    =         4982293
35
 XDOT =     -15031
817179                 XDOT =       -4525
344145
 YDOT =     -19257
061182  feet/sec       YDOT =       -5920
472302  meter/sec
 ZDOT =       6497
725217                 ZDOT =        1958
385482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9322996
79                 X    =         2841649
42
 Y    =      -11460870
59  feet           Y    =        -3493273
36  meter
 Z    =       16340060
10                 Z    =         4980450
32
 XDOT =      12852
599095                 XDOT =        3917
472204
 YDOT =      19581
260829  feet/sec       YDOT =        5968
368301  meter/sec
 ZDOT =       6413
063778                 ZDOT =        1954
701839


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
59376876  
00020000  00000-0  20000-3 0  9064
2 25544  51
6314  64
4095 0008840 319
0868  40
9632 15
76425759 22992


Satellite: ISS
Catalog Number: 25544
Epoch time:      07245
59376876   =   yrday
fracday
Element set:     906
Inclination:       51
6314  deg
RA of node:        64
4095  deg
Eccentricity:     
0008840     
Arg of perigee:   319
0868  deg
Mean anomaly:      40
9632  deg
Mean motion:   15
76425759  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2299
Checksum:              328


Coasting Arc #8 (Orbit 2313)
---------------------------------------

Vector Time (GMT): 2007/246/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4037510
85                 A    =         6724824
10  meter
 Y    =        5284775
23  meter          E    =           
0014855
 Z    =        -928749
48                 I    =           51
92713
 XDOT =      -3309
808541                 Wp   =            3
78928
 YDOT =       3575
302570  meter/sec      RA   =           58
90085  deg
 ZDOT =       5975
500326                 TA   =          346
09196
                                          MA   =          346
13284
                                          Ha   =            186
875  n
mi
                                          Hp   =            181
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13246426
67                 X    =         3982627
34
 Y    =       17338501
42  feet           Y    =         5329618
11  meter
 Z    =       -3047078
35                 Z    =         -909268
35
 XDOT =     -10858
951905                 XDOT =       -3378
570111
 YDOT =      11729
995310  feet/sec       YDOT =        3537
905784  meter/sec
 ZDOT =      19604
659861                 ZDOT =        5959
254304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12333449
32                 X    =        -3759235
35
 Y    =      -18011838
94  feet           Y    =        -5490008
51  meter
 Z    =       -2972511
30                 Z    =         -906021
44
 XDOT =      10256
976807                 XDOT =        3126
326531
 YDOT =     -10237
613100  feet/sec       YDOT =       -3120
424473  meter/sec
 ZDOT =      19543
420854                 ZDOT =        5956
834676


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
54463056  
00020000  00000-0  20000-3 0  9078
2 25544  51
6327  59
5079 0008702 322
6515  37
4044 15
76461569 23144


Satellite: ISS
Catalog Number: 25544
Epoch time:      07246
54463056   =   yrday
fracday
Element set:     907
Inclination:       51
6327  deg
RA of node:        59
5079  deg
Eccentricity:     
0008702     
Arg of perigee:   322
6515  deg
Mean anomaly:      37
4044  deg
Mean motion:   15
76461569  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2314
Checksum:              294


Coasting Arc #9 (Orbit 2329)
---------------------------------------

Vector Time (GMT): 2007/247/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3275316
63                 A    =         6712970
05  meter
 Y    =       -2548725
45  meter          E    =           
0012767
 Z    =       -5285315
96                 I    =           51
87197
 XDOT =       4614
208106                 Wp   =           54
00463
 YDOT =       6160
508467  meter/sec      RA   =           53
77550  deg
 ZDOT =       -104
168231                 TA   =          214
96769
                                          MA   =          215
05160
                                          Ha   =            186
978  n
mi
                                          Hp   =            181
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10745789
46                 X    =         3329248
51
 Y    =       -8361960
12  feet           Y    =        -2511797
24  meter
 Z    =      -17340275
47                 Z    =        -5269273
60
 XDOT =      15138
478037                 XDOT =        4545
483475
 YDOT =      20211
641953  feet/sec       YDOT =        6211
722891  meter/sec
 ZDOT =       -341
759288                 ZDOT =         -81
919103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11132155
81                 X    =        -3393081
09
 Y    =        7972905
97  feet           Y    =         2430141
74  meter
 Z    =      -17279681
68                 Z    =        -5266846
98
 XDOT =     -13834
033251                 XDOT =       -4216
613335
 YDOT =     -19922
994029  feet/sec       YDOT =       -6072
528580  meter/sec
 ZDOT =       -256
584494                 ZDOT =         -78
206954


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
55886654  
00020000  00000-0  20000-3 0  9084
2 25544  51
6332  54
2805 0008679 327
2117  32
8508 15
76506188 23300


Satellite: ISS
Catalog Number: 25544
Epoch time:      07247
55886654   =   yrday
fracday
Element set:     908
Inclination:       51
6332  deg
RA of node:        54
2805  deg
Eccentricity:     
0008679     
Arg of perigee:   327
2117  deg
Mean anomaly:      32
8508  deg
Mean motion:   15
76506188  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2330
Checksum:              306


Coasting Arc #10 (Orbit 2345)
---------------------------------------

Vector Time (GMT): 2007/248/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3945923
62                 A    =         6724665
90  meter
 Y    =       -5391231
71  meter          E    =           
0002295
 Z    =        -765492
50                 I    =           51
89324
 XDOT =       4263
704862                 Wp   =           96
81435
 YDOT =      -2271
726173  meter/sec      RA   =           48
64336  deg
 ZDOT =      -5994
479856                 TA   =           91
50364
                                          MA   =           91
47735
                                          Ha   =            187
097  n
mi
                                          Hp   =            180
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12945943
64                 X    =        -3881626
20
 Y    =      -17687768
09  feet           Y    =        -5434997
72  meter
 Z    =       -2511458
35                 Z    =         -784505
73
 XDOT =      13988
533013                 XDOT =        4317
910675
 YDOT =      -7453
169860  feet/sec       YDOT =       -2223
743690  meter/sec
 ZDOT =     -19666
928663                 ZDOT =       -5973
635335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12607709
61                 X    =         3842829
89
 Y    =       17920080
15  feet           Y    =         5462040
43  meter
 Z    =       -2584261
12                 Z    =         -787682
79
 XDOT =     -12925
311929                 XDOT =       -3939
635076
 YDOT =       6275
962331  feet/sec       YDOT =        1912
913318  meter/sec
 ZDOT =     -19588
068371                 ZDOT =       -5970
443239


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
57308357  
00020000  00000-0  20000-3 0  9097
2 25544  51
6327  49
0505 0008917 331
0799  28
9871 15
76546437 23464


Satellite: ISS
Catalog Number: 25544
Epoch time:      07248
57308357   =   yrday
fracday
Element set:     909
Inclination:       51
6327  deg
RA of node:        49
0505  deg
Eccentricity:     
0008917     
Arg of perigee:   331
0799  deg
Mean anomaly:      28
9871  deg
Mean motion:   15
76546437  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2346
Checksum:              323


Coasting Arc #11 (Orbit 2361)
---------------------------------------

Vector Time (GMT): 2007/249/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4203524
62                 A    =         6714124
69  meter
 Y    =        1461041
35  meter          E    =           
0011175
 Z    =        5029740
93                 I    =           51
83772
 XDOT =      -4332
042130                 Wp   =            4
41966
 YDOT =      -6098
631811  meter/sec      RA   =           43
48151  deg
 ZDOT =      -1837
712744                 TA   =          103
30588
                                          MA   =          103
18124
                                          Ha   =            187
352  n
mi
                                          Hp   =            180
483

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13791091
26                 X    =        -4243983
09
 Y    =        4793442
74  feet           Y    =         1413808
80  meter
 Z    =       16501774
70                 Z    =         5009222
20
 XDOT =     -14212
736646                 XDOT =       -4254
597175
 YDOT =     -20008
634552  feet/sec       YDOT =       -6146
642082  meter/sec
 ZDOT =      -6029
241285                 ZDOT =       -1858
569640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13888339
30                 X    =         4233165
82
 Y    =       -4779581
51  feet           Y    =        -1456816
45  meter
 Z    =       16424052
23                 Z    =         5006051
12
 XDOT =      13810
265995                 XDOT =        4209
369075
 YDOT =      19009
885111  feet/sec       YDOT =        5794
212982  meter/sec
 ZDOT =      -6109
128260                 ZDOT =       -1862
062294


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
58728546  
00020000  00000-0  20000-3 0  9107
2 25544  51
6334  43
8217 0008752 335
3566  24
7179 15
76506321 23621


Satellite: ISS
Catalog Number: 25544
Epoch time:      07249
58728546   =   yrday
fracday
Element set:     910
Inclination:       51
6334  deg
RA of node:        43
8217  deg
Eccentricity:     
0008752     
Arg of perigee:   335
3566  deg
Mean anomaly:      24
7179  deg
Mean motion:   15
76506321  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2362
Checksum:              300


Coasting Arc #12 (Orbit 2377)
---------------------------------------

Vector Time (GMT): 2007/250/13:01:45
256
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3517274
86                 A    =         6722226
85  meter
 Y    =        5189123
13  meter          E    =           
0015618
 Z    =        2398475
82                 I    =           51
84545
 XDOT =      -5383
704603                 Wp   =           40
05077
 YDOT =       1149
214024  meter/sec      RA   =           38
37699  deg
 ZDOT =       5401
082901                 TA   =          346
97764
                                          MA   =          347
01792
                                          Ha   =            187
225  n
mi
                                          Hp   =            180
134

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11539615
68                 X    =         3447336
70
 Y    =       17024682
18  feet           Y    =         5228064
22  meter
 Z    =        7869015
15                 Z    =         2415392
66
 XDOT =     -17663
072845                 XDOT =       -5422
392280
 YDOT =       3770
387218  feet/sec       YDOT =        1088
794048  meter/sec
 ZDOT =      17720
088258                 ZDOT =        5374
835264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11769681
65                 X    =        -3587398
97
 Y    =      -16836052
67  feet           Y    =        -5131628
85  meter
 Z    =        7933842
52                 Z    =         2418235
20
 XDOT =      16471
212335                 XDOT =        5020
425520
 YDOT =      -3199
458329  feet/sec       YDOT =        -975
194899  meter/sec
 ZDOT =      17620
578040                 ZDOT =        5370
752187


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
60146398  
00020000  00000-0  20000-3 0  9112
2 25544  51
6346  38
5928 0008802 338
2059  21
8729 15
76606038 23781


Satellite: ISS
Catalog Number: 25544
Epoch time:      07250
60146398   =   yrday
fracday
Element set:     911
Inclination:       51
6346  deg
RA of node:        38
5928  deg
Eccentricity:     
0008802     
Arg of perigee:   338
2059  deg
Mean anomaly:      21
8729  deg
Mean motion:   15
76606038  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2378
Checksum:              305

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

The following information is a reminder of your current mailing list subscription:

You are subscribed to the following list: [list_name]

using the following email: example@example.com

You may automatically unsubscribe from this list at any time by visiting the following URL:

http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/

If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism

You may also change your subscription by visiting this list's main screen:

http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]

If you're still having trouble, please contact the list owner at:

<mailto:list
admin@aus-city
com>

The following physical address is associated with this mailing list:

http://www aus-city com

Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list