Date: August 13th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6200 0 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


234/21:22:30 000 0 0 0 0 0 0
013/22:45:48 047 0 0 0 0 184 5
000/00:00:00 000 0 0 0 0 183 9

Coasting Arc #1 (Orbit 1972)
---------------------------------------

Vector Time (GMT): 2007/224/21:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6125407
08                 A    =         6724676
31  meter
 Y    =       -2293898
26  meter          E    =           
0012466
 Z    =        1525485
33                 I    =           51
70156
 XDOT =       2986
386142                 Wp   =          155
17704
 YDOT =       4119
942611  meter/sec      RA   =          170
08292  deg
 ZDOT =      -5790
373638                 TA   =            8
00015
                                          MA   =            7
98029
                                          Ha   =            186
218  n
mi
                                          Hp   =            182
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20096479
91                 X    =         6143192
19
 Y    =       -7525912
92  feet           Y    =        -2225301
14  meter
 Z    =        5004873
12                 Z    =         1555284
90
 XDOT =       9797
854797                 XDOT =        2968
222272
 YDOT =      13516
872084  feet/sec       YDOT =        4153
236803  meter/sec
 ZDOT =     -18997
288839                 ZDOT =       -5775
910040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11163262
97                 X    =         3402562
55
 Y    =       18296141
86  feet           Y    =         5576664
04  meter
 Z    =        5117555
83                 Z    =         1559831
02
 XDOT =     -10080
619854                 XDOT =       -3072
572931
 YDOT =      11454
082888  feet/sec       YDOT =        3491
204464  meter/sec
 ZDOT =     -18941
922412                 ZDOT =       -5773
497951


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   07224
92536503  
00020000  00000-0  20000-3 0  9007
2 25544  51
6297 170
9071 0008640 236
5341 123
4997 15
76267538 19734


Satellite: ISS
Catalog Number: 25544
Epoch time:      07224
92536503   =   yrday
fracday
Element set:     900
Inclination:       51
6297  deg
RA of node:       170
9071  deg
Eccentricity:     
0008640     
Arg of perigee:   236
5341  deg
Mean anomaly:     123
4997  deg
Mean motion:   15
76267538  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1973
Checksum:              303


Coasting Arc #2 (Orbit 1988)
---------------------------------------

Vector Time (GMT): 2007/225/21:27:29
021
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         185797
29                 A    =         6714231
10  meter
 Y    =       -4281161
57  meter          E    =           
0004633
 Z    =        5171990
00                 I    =           51
69434
 XDOT =       7537
005009                 Wp   =          239
94264
 YDOT =      -1077
204985  meter/sec      RA   =          164
92114  deg
 ZDOT =      -1165
474561                 TA   =          221
15778
                                          MA   =          221
19273
                                          Ha   =            186
267  n
mi
                                          Hp   =            182
786

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         609571
15                 X    =          208532
03
 Y    =      -14045805
68  feet           Y    =        -4278956
91  meter
 Z    =       16968471
12                 Z    =         5172947
68
 XDOT =      24727
706723                 XDOT =        7554
151851
 YDOT =      -3534
137089  feet/sec       YDOT =        -992
826041  meter/sec
 ZDOT =      -3823
735435                 ZDOT =       -1128
818989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13798481
02                 X    =         4205777
02
 Y    =       -2674651
86  feet           Y    =         -815233
89  meter
 Z    =       16971546
94                 Z    =         5172927
51
 XDOT =       8843
037308                 XDOT =        2695
357772
 YDOT =      22302
709160  feet/sec       YDOT =        6797
865752  meter/sec
 ZDOT =      -3684
893617                 ZDOT =       -1123
155574


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   07225
93974951  
00020000  00000-0  20000-3 0  9013
2 25544  51
6300 165
6791 0008482 238
1033 121
9306 15
76208518 19896


Satellite: ISS
Catalog Number: 25544
Epoch time:      07225
93974951   =   yrday
fracday
Element set:     901
Inclination:       51
6300  deg
RA of node:       165
6791  deg
Eccentricity:     
0008482     
Arg of perigee:   238
1033  deg
Mean anomaly:     121
9306  deg
Mean motion:   15
76208518  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1989
Checksum:              301


Coasting Arc #3 (Orbit 2004)
---------------------------------------

Vector Time (GMT): 2007/226/21:32:08
464
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5863101
17                 A    =         6721206
62  meter
 Y    =        -561480
96  meter          E    =           
0006267
 Z    =        3237069
46                 I    =           51
74710
 XDOT =       3136
135447                 Wp   =          123
02044
 YDOT =      -5165
415204  meter/sec      RA   =          159
79243  deg
 ZDOT =       4774
342186                 TA   =          274
81084
                                          MA   =          274
88239
                                          Ha   =            185
982  n
mi
                                          Hp   =            182
991

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19235896
24                 X    =        -5872111
66
 Y    =       -1842129
12  feet           Y    =         -627095
87  meter
 Z    =       10620306
61                 Z    =         3208565
14
 XDOT =      10289
158292                 XDOT =        3170
470339
 YDOT =     -16946
900276  feet/sec       YDOT =       -5130
153246  meter/sec
 ZDOT =      15663
852317                 ZDOT =        4789
660592

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3287975
87                 X    =        -1002175
05
 Y    =      -19102040
17  feet           Y    =        -5822301
84  meter
 Z    =       10512151
65                 Z    =         3204103
82
 XDOT =      17637
693914                 XDOT =        5375
969105
 YDOT =       5633
946982  feet/sec       YDOT =        1717
227040  meter/sec
 ZDOT =      15721
263415                 ZDOT =        4791
841089


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   07226
95411939  
00020000  00000-0  20000-3 0  9029
2 25544  51
6310 160
4511 0008649 242
1117 117
9171 15
76287875 20051


Satellite: ISS
Catalog Number: 25544
Epoch time:      07226
95411939   =   yrday
fracday
Element set:     902
Inclination:       51
6310  deg
RA of node:       160
4511  deg
Eccentricity:     
0008649     
Arg of perigee:   242
1117  deg
Mean anomaly:     117
9171  deg
Mean motion:   15
76287875  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2005
Checksum:              282


Coasting Arc #4 (Orbit 2019)
---------------------------------------

Vector Time (GMT): 2007/227/21:36:29
890
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4637589
09                 A    =         6723204
01  meter
 Y    =        4257392
27  meter          E    =           
0003760
 Z    =       -2356004
88                 I    =           51
78189
 XDOT =      -4934
896048                 Wp   =          275
65026
 YDOT =      -2375
484071  meter/sec      RA   =          154
58639  deg
 ZDOT =       5414
325165                 TA   =           57
85474
                                          MA   =           57
81827
                                          Ha   =            185
766  n
mi
                                          Hp   =            183
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15215187
30                 X    =        -4673406
32
 Y    =       13967822
41  feet           Y    =         4205331
87  meter
 Z    =       -7729674
79                 Z    =        -2378620
96
 XDOT =     -16190
603833                 XDOT =       -4934
267711
 YDOT =      -7793
582909  feet/sec       YDOT =       -2430
665355  meter/sec
 ZDOT =      17763
534007                 ZDOT =        5390
353297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17847260
62                 X    =        -5439845
04
 Y    =      -10332125
53  feet           Y    =        -3149231
86  meter
 Z    =       -7814878
79                 Z    =        -2381975
05
 XDOT =       1844
032448                 XDOT =         562
061090
 YDOT =     -16569
228086  feet/sec       YDOT =       -5050
300721  meter/sec
 ZDOT =      17672
324012                 ZDOT =        5386
524359


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   07227
90508503  
00020000  00000-0  20000-3 0  9030
2 25544  51
6321 155
5505 0008557 245
6043 114
4228 15
76285513 20204


Satellite: ISS
Catalog Number: 25544
Epoch time:      07227
90508503   =   yrday
fracday
Element set:     903
Inclination:       51
6321  deg
RA of node:       155
5505  deg
Eccentricity:     
0008557     
Arg of perigee:   245
6043  deg
Mean anomaly:     114
4228  deg
Mean motion:   15
76285513  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2020
Checksum:              266


Coasting Arc #5 (Orbit 2035)
---------------------------------------

Vector Time (GMT): 2007/228/21:41:15
136
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2037892
53                 A    =         6713489
39  meter
 Y    =        3623783
57  meter          E    =           
0007728
 Z    =       -5277349
79                 I    =           51
77504
 XDOT =      -6661
040743                 Wp   =          113
41455
 YDOT =       3861
755636  meter/sec      RA   =          149
44789  deg
 ZDOT =         76
603042                 TA   =          157
32813
                                          MA   =          157
29398
                                          Ha   =            185
519  n
mi
                                          Hp   =            183
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6685999
11                 X    =         2022855
56
 Y    =       11889053
72  feet           Y    =         3646488
36  meter
 Z    =      -17314139
74                 Z    =        -5267486
33
 XDOT =     -21853
808212                 XDOT =       -6704
100526
 YDOT =      12669
801954  feet/sec       YDOT =        3787
027363  meter/sec
 ZDOT =        251
322315                 ZDOT =          44
139419

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8947414
26                 X    =        -2727171
87
 Y    =       10358864
61  feet           Y    =         3157381
93  meter
 Z    =      -17276264
63                 Z    =        -5265805
46
 XDOT =     -18475
985492                 XDOT =       -5631
480378
 YDOT =     -15727
836606  feet/sec       YDOT =       -4793
844598  meter/sec
 ZDOT =        128
718913                 ZDOT =          39
233525


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   07228
91943819  
00020000  00000-0  20000-3 0  9046
2 25544  51
6322 150
3238 0008489 249
7462 110
2790 15
76322116 20361


Satellite: ISS
Catalog Number: 25544
Epoch time:      07228
91943819   =   yrday
fracday
Element set:     904
Inclination:       51
6322  deg
RA of node:       150
3238  deg
Eccentricity:     
0008489     
Arg of perigee:   249
7462  deg
Mean anomaly:     110
2790  deg
Mean motion:   15
76322116  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2036
Checksum:              289


Coasting Arc #6 (Orbit 2051)
---------------------------------------

Vector Time (GMT): 2007/229/21:46:03
412
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5953315
98                 A    =         6722950
63  meter
 Y    =       -1861522
10  meter          E    =           
0007319
 Z    =       -2495041
78                 I    =           51
83107
 XDOT =       -508
511853                 Wp   =          215
50983
 YDOT =       5532
611137  meter/sec      RA   =          144
31044  deg
 ZDOT =      -5339
223625                 TA   =          352
67999
                                          MA   =          352
69067
                                          Ha   =            185
410  n
mi
                                          Hp   =            183
554

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19531876
57                 X    =         5985809
73
 Y    =       -6107355
97  feet           Y    =        -1794767
07  meter
 Z    =       -8185832
60                 Z    =        -2466041
81
 XDOT =      -1668
345974                 XDOT =        -544
403698
 YDOT =      18151
611341  feet/sec       YDOT =        5526
724022  meter/sec
 ZDOT =     -17517
137876                 ZDOT =       -5341
781108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12903623
45                 X    =         3933024
43
 Y    =       15939730
60  feet           Y    =         4858429
89  meter
 Z    =       -8076097
15                 Z    =        -2461594
41
 XDOT =     -16286
664946                 XDOT =       -4964
175476
 YDOT =       4301
354042  feet/sec       YDOT =        1311
052712  meter/sec
 ZDOT =     -17526
119787                 ZDOT =       -5341
961311


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   07229
93378166  
00020000  00000-0  20000-3 0  9057
2 25544  51
6321 145
0950 0008582 253
8777 106
1443 15
76316566 20520


Satellite: ISS
Catalog Number: 25544
Epoch time:      07229
93378166   =   yrday
fracday
Element set:     905
Inclination:       51
6321  deg
RA of node:       145
0950  deg
Eccentricity:     
0008582     
Arg of perigee:   253
8777  deg
Mean anomaly:     106
1443  deg
Mean motion:   15
76316566  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2052
Checksum:              299


Coasting Arc #7 (Orbit 2067)
---------------------------------------

Vector Time (GMT): 2007/230/21:50:25
450
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2510366
72                 A    =         6721355
84  meter
 Y    =       -5401763
69  meter          E    =           
0005487
 Z    =        3106380
83                 I    =           51
84904
 XDOT =       5945
585796                 Wp   =          122
20122
 YDOT =        -56
736047  meter/sec      RA   =          139
10924  deg
 ZDOT =      -4900
088514                 TA   =           21
78298
                                          MA   =           21
75966
                                          Ha   =            185
118  n
mi
                                          Hp   =            183
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8236111
27                 X    =         2555493
27
 Y    =      -17722321
82  feet           Y    =        -5373439
09  meter
 Z    =       10191538
17                 Z    =         3118685
67
 XDOT =      19506
515078                 XDOT =        5969
582017
 YDOT =       -186
141885  feet/sec       YDOT =           9
885105  meter/sec
 ZDOT =     -16076
405887                 ZDOT =       -4871
146653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19515446
56                 X    =         5948308
11
 Y    =         349883
89  feet           Y    =          106644
61  meter
 Z    =       10237509
29                 Z    =         3120392
83
 XDOT =       8086
939723                 XDOT =        2464
899228
 YDOT =      16439
416079  feet/sec       YDOT =        5010
734021  meter/sec
 ZDOT =     -15966
650808                 ZDOT =       -4866
635166


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   07230
94811584  
00020000  00000-0  20000-3 0  9067
2 25544  51
6326 139
8676 0008574 257
5318 102
4887 15
76313816 20687


Satellite: ISS
Catalog Number: 25544
Epoch time:      07230
94811584   =   yrday
fracday
Element set:     906
Inclination:       51
6326  deg
RA of node:       139
8676  deg
Eccentricity:     
0008574     
Arg of perigee:   257
5318  deg
Mean anomaly:     102
4887  deg
Mean motion:   15
76313816  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2068
Checksum:              316


Coasting Arc #8 (Orbit 2083)
---------------------------------------

Vector Time (GMT): 2007/231/21:55:09
183
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3661389
11                 A    =         6713627
63  meter
 Y    =       -2112836
28  meter          E    =           
0006383
 Z    =        5220853
82                 I    =           51
84532
 XDOT =       4765
519733                 Wp   =          242
09562
 YDOT =      -5978
526129  meter/sec      RA   =          133
98645  deg
 ZDOT =        920
527243                 TA   =          199
14849
                                          MA   =          199
17250
                                          Ha   =            184
804  n
mi
                                          Hp   =            183
941

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12012431
47                 X    =        -3662852
87
 Y    =       -6931877
56  feet           Y    =        -2153788
36  meter
 Z    =       17128785
49                 Z    =         5203063
19
 XDOT =      15634
907261                 XDOT =        4827
546567
 YDOT =     -19614
587037  feet/sec       YDOT =       -5924
888622  meter/sec
 ZDOT =       3020
102503                 ZDOT =         943
828567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         942614
82                 X    =          287309
00
 Y    =      -13920384
83  feet           Y    =        -4242933
29  meter
 Z    =       17061040
19                 Z    =         5200205
05
 XDOT =      23452
845289                 XDOT =        7148
427244
 YDOT =       5405
346992  feet/sec       YDOT =        1647
549763  meter/sec
 ZDOT =       3107
715688                 ZDOT =         947
231742


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   07231
96243812  
00020000  00000-0  20000-3 0  9074
2 25544  51
6334 134
6394 0008666 262
5303  97
4877 15
76379874 20844


Satellite: ISS
Catalog Number: 25544
Epoch time:      07231
96243812   =   yrday
fracday
Element set:     907
Inclination:       51
6334  deg
RA of node:       134
6394  deg
Eccentricity:     
0008666     
Arg of perigee:   262
5303  deg
Mean anomaly:      97
4877  deg
Mean motion:   15
76379874  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2084
Checksum:              320


Coasting Arc #9 (Orbit 2099)
---------------------------------------

Vector Time (GMT): 2007/232/21:59:56
852
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5031420
00                 A    =         6724227
28  meter
 Y    =        4113822
34  meter          E    =           
0007028
 Z    =        1707674
50                 I    =           51
90037
 XDOT =      -1942
752009                 Wp   =           37
05196
 YDOT =      -4760
569764  meter/sec      RA   =          128
84027  deg
 ZDOT =       5737
611289                 TA   =          341
78840
                                          MA   =          341
81356
                                          Ha   =            184
388  n
mi
                                          Hp   =            184
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16507283
47                 X    =        -5085342
99
 Y    =       13496792
44  feet           Y    =         4057256
58  meter
 Z    =        5602606
64                 Z    =         1683101
13
 XDOT =      -6373
858298                 XDOT =       -1917
246458
 YDOT =     -15618
667205  feet/sec       YDOT =       -4782
152393  meter/sec
 ZDOT =      18824
184019                 ZDOT =        5728
235126

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19696321
35                 X    =        -6003438
75
 Y    =       -8230354
24  feet           Y    =        -2508611
97  meter
 Z    =        5509919
15                 Z    =         1679423
36
 XDOT =      10124
652258                 XDOT =        3085
994008
 YDOT =     -11636
877439  feet/sec       YDOT =       -3546
920244  meter/sec
 ZDOT =      18788
017145                 ZDOT =        5726
587626


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   07232
97675329  
00020000  00000-0  20000-3 0  9089
2 25544  51
6336 129
4116 0008519 266
6039  93
4150 15
76366938 21004


Satellite: ISS
Catalog Number: 25544
Epoch time:      07232
97675329   =   yrday
fracday
Element set:     908
Inclination:       51
6336  deg
RA of node:       129
4116  deg
Eccentricity:     
0008519     
Arg of perigee:   266
6039  deg
Mean anomaly:      93
4150  deg
Mean motion:   15
76366938  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2100
Checksum:              305


Coasting Arc #10 (Orbit 2114)
---------------------------------------

Vector Time (GMT): 2007/233/22:05:05
949
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -449323
16                 A    =         6719967
64  meter
 Y    =        5690182
90  meter          E    =           
0003450
 Z    =       -3544110
88                 I    =           51
90347
 XDOT =      -5797
075241                 Wp   =          261
33719
 YDOT =       2346
138940  meter/sec      RA   =          123
64530  deg
 ZDOT =       4497
551327                 TA   =           56
57330
                                          MA   =           56
54031
                                          Ha   =            184
421  n
mi
                                          Hp   =            184
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1474157
36                 X    =         -495701
64
 Y    =       18668579
06  feet           Y    =         5684899
23  meter
 Z    =      -11627660
37                 Z    =        -3546405
97
 XDOT =     -19019
275725                 XDOT =       -5844
727484
 YDOT =       7697
306234  feet/sec       YDOT =        2281
046049  meter/sec
 ZDOT =      14755
745825                 ZDOT =        4469
273630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16817536
98                 X    =        -5125985
27
 Y    =        8226391
68  feet           Y    =         2507404
19  meter
 Z    =      -11635652
08                 Z    =        -3546546
75
 XDOT =     -15701
197299                 XDOT =       -4785
724937
 YDOT =     -11359
424800  feet/sec       YDOT =       -3462
352679  meter/sec
 ZDOT =      14648
771988                 ZDOT =        4464
945702


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   07233
92766429  
00020000  00000-0  20000-3 0  9098
2 25544  51
6338 124
5113 0008688 270
7753  89
2415 15
76364715 21159


Satellite: ISS
Catalog Number: 25544
Epoch time:      07233
92766429   =   yrday
fracday
Element set:     909
Inclination:       51
6338  deg
RA of node:       124
5113  deg
Eccentricity:     
0008688     
Arg of perigee:   270
7753  deg
Mean anomaly:      89
2415  deg
Mean motion:   15
76364715  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2115
Checksum:              309


Coasting Arc #11 (Orbit 2130)
---------------------------------------

Vector Time (GMT): 2007/234/21:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4559454
93                 A    =         6714832
50  meter
 Y    =         286790
46  meter          E    =           
0004261
 Z    =        4924834
99                 I    =           51
90131
 XDOT =       1932
033281                 Wp   =          227
79869
 YDOT =      -7122
707760  meter/sec      RA   =          118
70475  deg
 ZDOT =       2201
876885                 TA   =          200
88947
                                          MA   =          200
90689
                                          Ha   =            184
470  n
mi
                                          Hp   =            183
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14958841
64                 X    =        -4586246
80
 Y    =         940913
59  feet           Y    =          235653
91  meter
 Z    =       16157595
12                 Z    =         4902620
24
 XDOT =       6338
691868                 XDOT =        2000
840612
 YDOT =     -23368
463781  feet/sec       YDOT =       -7100
718115  meter/sec
 ZDOT =       7224
005527                 ZDOT =        2211
429257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6196819
94                 X    =        -1888790
72
 Y    =      -13746521
86  feet           Y    =        -4189939
86  meter
 Z    =       16073353
75                 Z    =         4899158
22
 XDOT =      23084
196841                 XDOT =        7036
063197
 YDOT =      -1911
885543  feet/sec       YDOT =        -582
742713  meter/sec
 ZDOT =       7259
356082                 ZDOT =        2212
651734


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   07234
94195923  
00020000  00000-0  20000-3 0  9108
2 25544  51
6341 119
2821 0008607 274
3411  85
6770 15
76421602 21313


Satellite: ISS
Catalog Number: 25544
Epoch time:      07234
94195923   =   yrday
fracday
Element set:     910
Inclination:       51
6341  deg
RA of node:       119
2821  deg
Eccentricity:     
0008607     
Arg of perigee:   274
3411  deg
Mean anomaly:      85
6770  deg
Mean motion:   15
76421602  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2131
Checksum:              273


Coasting Arc #12 (Orbit 2146)
---------------------------------------

Vector Time (GMT): 2007/235/21:26:31
324
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2903008
45                 A    =         6725340
06  meter
 Y    =        6051037
86  meter          E    =           
0009985
 Z    =         312296
18                 I    =           51
94958
 XDOT =      -4164
993174                 Wp   =            6
46346
 YDOT =      -2311
277899  meter/sec      RA   =          113
54230  deg
 ZDOT =       6057
855287                 TA   =          356
92052
                                          MA   =          356
92666
                                          Ha   =            184
851  n
mi
                                          Hp   =            183
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9524305
94                 X    =        -2971973
36
 Y    =       19852486
42  feet           Y    =         6018189
16  meter
 Z    =        1024593
77                 Z    =          298026
44
 XDOT =     -13664
675768                 XDOT =       -4168
266233
 YDOT =      -7582
932738  feet/sec       YDOT =       -2357
871943  meter/sec
 ZDOT =      19874
853304                 ZDOT =        6037
613838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21991965
02                 X    =        -6703150
94
 Y    =       -1137387
29  feet           Y    =         -346675
65  meter
 Z    =         971204
26                 Z    =          296023
06
 XDOT =       1601
326344                 XDOT =         488
084270
 YDOT =     -14031
079219  feet/sec       YDOT =       -4276
672946  meter/sec
 ZDOT =      19797
767486                 ZDOT =        6034
359530


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   07235
95624687  
00020000  00000-0  20000-3 0  9115
2 25544  51
6344 114
0546 0008558 279
4068  80
6128 15
76395614 21474


Satellite: ISS
Catalog Number: 25544
Epoch time:      07235
95624687   =   yrday
fracday
Element set:     911
Inclination:       51
6344  deg
RA of node:       114
0546  deg
Eccentricity:     
0008558     
Arg of perigee:   279
4068  deg
Mean anomaly:      80
6128  deg
Mean motion:   15
76395614  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2147
Checksum:              311

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