Date:
June 12th 2008
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) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 2765)
---------------------------------------
Vector Time (GMT): 2008/163/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3444366
04 A = 6722534
24 meter
Y = 5446598
12 meter E =
0013212
Z = 1884686
85 I = 51
88017
XDOT = -5078
508159 Wp = 42
04191
YDOT = 1246
755637 meter/sec RA = 44
42478 deg
ZDOT = 5665
148539 TA = 338
86169
MA = 338
91624
Ha = 185
350 n
mi
Hp = 180
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11300413
52 X = 3374049
83
Y = 17869416
39 feet Y = 5484721
60 meter
Z = 6183355
79 Z = 1901249
50
XDOT = -16661
772175 XDOT = -5119
592485
YDOT = 4090
405633 feet/sec YDOT = 1189
734447 meter/sec
ZDOT = 18586
445338 ZDOT = 5640
377420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5906250
39 X = 1800225
12
Y = -20281354
87 feet Y = -6181756
96 meter
Z = 6247569
74 Z = 1904259
26
XDOT = 12701
270722 XDOT = 3871
347316
YDOT = 9407
999941 feet/sec YDOT = 2867
558382 meter/sec
ZDOT = 18491
182232 ZDOT = 5636
112344
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 08163
70394161
00020000 00000-0 20000-3 0 9008
2 25544 51
6367 44
6643 0005942 316
1557 43
9135 15
76840170 27660
Satellite: ISS
Catalog Number: 25544
Epoch time: 08163
70394161 = yrday
fracday
Element set: 900
Inclination: 51
6367 deg
RA of node: 44
6643 deg
Eccentricity:
0005942
Arg of perigee: 316
1557 deg
Mean anomaly: 43
9135 deg
Mean motion: 15
76840170 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2766
Checksum: 290
Coasting Arc #2 (Orbit 2780)
---------------------------------------
Vector Time (GMT): 2008/164/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4947764
22 A = 6715305
43 meter
Y = -538142
72 meter E =
0005589
Z = -4512496
14 I = 51
83367
XDOT = 3528
895566 Wp = 78
98364
YDOT = 6077
834069 meter/sec RA = 39
24150 deg
ZDOT = 3148
785513 TA = 222
33016
MA = 222
37331
Ha = 185
562 n
mi
Hp = 180
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16232822
25 X = 4975335
13
Y = -1765560
12 feet Y = -482659
25 meter
Z = -14804777
36 Z = -4488392
83
XDOT = 11577
741358 XDOT = 3445
373654
YDOT = 19940
400489 feet/sec YDOT = 6116
828795 meter/sec
ZDOT = 10330
661131 ZDOT = 3165
726926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12329406
53 X = -3758003
11
Y = -10832596
46 feet Y = -3301775
40 meter
Z = -14712027
12 Z = -4484225
87
XDOT = 6121
499301 XDOT = 1865
832987
YDOT = -21067
576474 feet/sec YDOT = -6421
397309 meter/sec
ZDOT = 10396
378148 ZDOT = 3168
816059
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 08164
65456966
00020000 00000-0 20000-3 0 9016
2 25544 51
6364 39
7608 0005836 320
3032 39
7704 15
76849588 27814
Satellite: ISS
Catalog Number: 25544
Epoch time: 08164
65456966 = yrday
fracday
Element set: 901
Inclination: 51
6364 deg
RA of node: 39
7608 deg
Eccentricity:
0005836
Arg of perigee: 320
3032 deg
Mean anomaly: 39
7704 deg
Mean motion: 15
76849588 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2781
Checksum: 322
Coasting Arc #3 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2008/165/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2585339
40 A = 6718518
06 meter
Y = -5104929
00 meter E =
0005803
Z = -3527384
51 I = 51
82175
XDOT = 6242
442036 Wp = 18
89602
YDOT = -46
271257 meter/sec RA = 34
14736 deg
ZDOT = -4505
006278 TA = 202
98110
MA = 203
00708
Ha = 185
623 n
mi
Hp = 180
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8482084
64 X = -2510927
57
Y = -16748454
74 feet Y = -5133423
18 meter
Z = -11572783
83 Z = -3539764
21
XDOT = 20480
452873 XDOT = 6264
380209
YDOT = -151
808587 feet/sec YDOT = 23
658626 meter/sec
ZDOT = -14780
204323 ZDOT = -4474
626915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6353510
20 X = -1936549
91
Y = 17634469
13 feet Y = 5374986
19 meter
Z = -11620853
15 Z = -3542036
04
XDOT = -12981
686109 XDOT = -3956
817926
YDOT = -14347
188056 feet/sec YDOT = -4373
022920 meter/sec
ZDOT = -14663
252479 ZDOT = -4469
359356
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 08165
66856067
00020000 00000-0 20000-3 0 9025
2 25544 51
6367 34
5316 0005893 325
5036 34
5746 15
76882769 27974
Satellite: ISS
Catalog Number: 25544
Epoch time: 08165
66856067 = yrday
fracday
Element set: 902
Inclination: 51
6367 deg
RA of node: 34
5316 deg
Eccentricity:
0005893
Arg of perigee: 325
5036 deg
Mean anomaly: 34
5746 deg
Mean motion: 15
76882769 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2797
Checksum: 331
Coasting Arc #4 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2008/166/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5889564
82 A = 6719586
09 meter
Y = -371062
83 meter E =
0010587
Z = 3210153
57 I = 51
79988
XDOT = -2275
264307 Wp = 66
46936
YDOT = -5577
521157 meter/sec RA = 28
95029 deg
ZDOT = -4802
499455 TA = 76
08076
MA = 75
96303
Ha = 185
718 n
mi
Hp = 180
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19322719
23 X = -5900572
32
Y = -1217397
72 feet Y = -436985
39 meter
Z = 10531999
90 Z = 3181514
95
XDOT = -7464
777911 XDOT = -2189
396560
YDOT = -18298
953927 feet/sec YDOT = -5602
483557 meter/sec
ZDOT = -15756
231807 ZDOT = -4813
345161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12715227
69 X = 3875601
40
Y = 14679352
11 feet Y = 4474266
52 meter
Z = 10421715
98 Z = 3176539
03
XDOT = -6814
493178 XDOT = -2077
057521
YDOT = 17157
897927 feet/sec YDOT = 5229
727288 meter/sec
ZDOT = -15798
426321 ZDOT = -4815
360343
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 08166
68253949
00020000 00000-0 20000-3 0 9039
2 25544 51
6365 29
3011 0005918 327
2190 32
8607 15
76883644 28133
Satellite: ISS
Catalog Number: 25544
Epoch time: 08166
68253949 = yrday
fracday
Element set: 903
Inclination: 51
6365 deg
RA of node: 29
3011 deg
Eccentricity:
0005918
Arg of perigee: 327
2190 deg
Mean anomaly: 32
8607 deg
Mean motion: 15
76883644 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2813
Checksum: 304
Coasting Arc #5 (Orbit 2828)
---------------------------------------
Vector Time (GMT): 2008/167/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1278861
12 A = 6714222
96 meter
Y = 4616240
48 meter E =
0004245
Z = 4700803
89 I = 51
75584
XDOT = -7160
245864 Wp = 68
92754
YDOT = -805
426291 meter/sec RA = 23
84827 deg
ZDOT = 2738
419684 TA = 354
17604
MA = 354
18097
Ha = 185
783 n
mi
Hp = 180
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4195738
59 X = 1204310
66
Y = 15145145
92 feet Y = 4630123
73 meter
Z = 15422584
93 Z = 4706836
43
XDOT = -23491
620288 XDOT = -7164
010174
YDOT = -2642
474709 feet/sec YDOT = -885
517815 meter/sec
ZDOT = 8984
316547 ZDOT = 2703
625552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7690692
12 X = 2344122
96
Y = -13678630
51 feet Y = -4169246
58 meter
Z = 15446168
31 Z = 4707992
10
XDOT = 13935
193443 XDOT = 4247
446961
YDOT = 17830
620414 feet/sec YDOT = 5434
773102 meter/sec
ZDOT = 8850
299005 ZDOT = 2697
571137
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 08167
69650747
00020000 00000-0 20000-3 0 9049
2 25544 51
6364 24
0707 0005866 331
5936 28
4908 15
76910154 28293
Satellite: ISS
Catalog Number: 25544
Epoch time: 08167
69650747 = yrday
fracday
Element set: 904
Inclination: 51
6364 deg
RA of node: 24
0707 deg
Eccentricity:
0005866
Arg of perigee: 331
5936 deg
Mean anomaly: 28
4908 deg
Mean motion: 15
76910154 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2829
Checksum: 314
Coasting Arc #6 (Orbit 2843)
---------------------------------------
Vector Time (GMT): 2008/168/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6480318
50 A = 6722979
04 meter
Y = 958744
78 meter E =
0012362
Z = -1478898
17 I = 51
75886
XDOT = 577
488789 Wp = 12
85148
YDOT = 5029
962709 meter/sec RA = 18
66407 deg
ZDOT = 5812
356566 TA = 330
86560
MA = 330
93451
Ha = 185
954 n
mi
Hp = 179
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21260887
48 X = 6476300
31
Y = 3145488
13 feet Y = 1031189
24 meter
Z = -4852028
12 Z = -1447426
08
XDOT = 1894
648257 XDOT = 492
964427
YDOT = 16502
502325 feet/sec YDOT = 5035
946748 meter/sec
ZDOT = 19069
411306 ZDOT = 5814
957732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13266108
80 X = -4043509
96
Y = -16943778
59 feet Y = -5164463
71 meter
Z = -4730785
72 Z = -1441943
49
XDOT = 8836
884109 XDOT = 2693
482276
YDOT = -12226
232275 feet/sec YDOT = -3726
555597 meter/sec
ZDOT = 19079
811120 ZDOT = 5815
526429
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 08168
64709190
00020000 00000-0 20000-3 0 9053
2 25544 51
6374 19
1677 0005724 336
0938 23
9960 15
76916849 28442
Satellite: ISS
Catalog Number: 25544
Epoch time: 08168
64709190 = yrday
fracday
Element set: 905
Inclination: 51
6374 deg
RA of node: 19
1677 deg
Eccentricity:
0005724
Arg of perigee: 336
0938 deg
Mean anomaly: 23
9960 deg
Mean motion: 15
76916849 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2844
Checksum: 327
Coasting Arc #7 (Orbit 2859)
---------------------------------------
Vector Time (GMT): 2008/169/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 345887
62 A = 6711790
09 meter
Y = -4182151
81 meter E =
0014547
Z = -5249779
51 I = 51
69355
XDOT = 7554
511364 Wp = 63
12171
YDOT = 1351
831011 meter/sec RA = 13
53209 deg
ZDOT = -573
941387 TA = 201
39432
MA = 201
45519
Ha = 185
977 n
mi
Hp = 179
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1134801
92 X = 418130
00
Y = -13720970
52 feet Y = -4177878
86 meter
Z = -17223686
04 Z = -5247924
59
XDOT = 24785
142271 XDOT = 7541
621624
YDOT = 4435
141111 feet/sec YDOT = 1436
237933 meter/sec
ZDOT = -1883
009801 ZDOT = -537
272402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10186994
45 X = -3104995
91
Y = 9274319
37 feet Y = 2826812
54 meter
Z = -17216861
28 Z = -5247699
32
XDOT = -14590
940676 XDOT = -4447
318718
YDOT = -19292
057669 feet/sec YDOT = -5880
219177 meter/sec
ZDOT = -1741
724473 ZDOT = -530
877619
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 08169
66103680
00020000 00000-0 20000-3 0 9069
2 25544 51
6376 13
9386 0005719 340
9905 19
1046 15
76954243 28605
Satellite: ISS
Catalog Number: 25544
Epoch time: 08169
66103680 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 13
9386 deg
Eccentricity:
0005719
Arg of perigee: 340
9905 deg
Mean anomaly: 19
1046 deg
Mean motion: 15
76954243 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2860
Checksum: 306
Coasting Arc #8 (Orbit 2875)
---------------------------------------
Vector Time (GMT): 2008/170/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6561851
05 A = 6723567
28 meter
Y = -1369203
68 meter E =
0006213
Z = -504783
09 I = 51
70412
XDOT = 1416
738213 Wp = 115
16738
YDOT = -4593
603249 meter/sec RA = 8
37727 deg
ZDOT = -6016
694504 TA = 70
32314
MA = 70
25611
Ha = 186
075 n
mi
Hp = 179
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21528382
70 X = -6543600
56
Y = -4492138
07 feet Y = -1442479
90 meter
Z = -1656112
49 Z = -536616
56
XDOT = 4648
091249 XDOT = 1497
227349
YDOT = -15070
876802 feet/sec YDOT = -4577
309119 meter/sec
ZDOT = -19739
811366 ZDOT = -6009
617477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13119987
56 X = 3998972
21
Y = 17637888
76 feet Y = 5376028
49 meter
Z = -1778786
40 Z = -542174
09
XDOT = -12274
771975 XDOT = -3741
350498
YDOT = 7161
045437 feet/sec YDOT = 2182
686649 meter/sec
ZDOT = -19712
908336 ZDOT = -6008
494461
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 08170
67496891
00020000 00000-0 20000-3 0 9072
2 25544 51
6370 8
7070 0005925 344
0582 16
0395 15
76984217 28760
Satellite: ISS
Catalog Number: 25544
Epoch time: 08170
67496891 = yrday
fracday
Element set: 907
Inclination: 51
6370 deg
RA of node: 8
7070 deg
Eccentricity:
0005925
Arg of perigee: 344
0582 deg
Mean anomaly: 16
0395 deg
Mean motion: 15
76984217 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2876
Checksum: 314
Coasting Arc #9 (Orbit 2891)
---------------------------------------
Vector Time (GMT): 2008/171/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2118061
57 A = 6712760
65 meter
Y = 3883635
61 meter E =
0009288
Z = 5048506
89 I = 51
63850
XDOT = -7306
985441 Wp = 19
74235
YDOT = -1758
848221 meter/sec RA = 3
20190 deg
ZDOT = -1703
069299 TA = 86
68122
MA = 86
57497
Ha = 186
313 n
mi
Hp = 179
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6949020
88 X = -2185856
22
Y = 12741586
65 feet Y = 3859570
08 meter
Z = 16563342
83 Z = 5038053
55
XDOT = -23973
049346 XDOT = -7278
501477
YDOT = -5770
499413 feet/sec YDOT = -1840
399483 meter/sec
ZDOT = -5587
497700 ZDOT = -1738
497721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13637899
28 X = 4156831
70
Y = -5095755
49 feet Y = -1553186
27 meter
Z = 16523384
23 Z = 5036327
51
XDOT = 14057
961764 XDOT = 4284
866746
YDOT = 18961
691575 feet/sec YDOT = 5779
523592 meter/sec
ZDOT = -5724
048965 ZDOT = -1744
690125
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 08171
68889239
00020000 00000-0 20000-3 0 9087
2 25544 51
6377 3
4768 0005767 348
9268 11
1768 15
76934723 28926
Satellite: ISS
Catalog Number: 25544
Epoch time: 08171
68889239 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 3
4768 deg
Eccentricity:
0005767
Arg of perigee: 348
9268 deg
Mean anomaly: 11
1768 deg
Mean motion: 15
76934723 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2892
Checksum: 345
Coasting Arc #10 (Orbit 2907)
---------------------------------------
Vector Time (GMT): 2008/172/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6027074
87 A = 6720984
67 meter
Y = 1706326
31 meter E =
0015597
Z = 2409866
59 I = 51
63912
XDOT = -3391
540371 Wp = 52
87906
YDOT = 4369
472315 meter/sec RA = 358
07943 deg
ZDOT = 5373
931208 TA = 334
37396
MA = 334
45118
Ha = 186
104 n
mi
Hp = 179
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19773867
67 X = 5995839
90
Y = 5598183
43 feet Y = 1773549
37 meter
Z = 7906386
46 Z = 2439070
41
XDOT = -11127
100955 XDOT = -3466
253835
YDOT = 14335
539090 feet/sec YDOT = 4331
127305 meter/sec
ZDOT = 17631
007901 ZDOT = 5357
274647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11634534
00 X = -3546205
96
Y = -16887574
51 feet Y = -5147332
71 meter
Z = 8018970
82 Z = 2444182
31
XDOT = 16556
867762 XDOT = 5046
533294
YDOT = -3042
787720 feet/sec YDOT = -927
441697 meter/sec
ZDOT = 17567
198770 ZDOT = 5354
482185
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 08172
70279913
00020000 00000-0 20000-3 0 9094
2 25544 51
6389 358
2466 0005754 350
9922 9
1139 15
77024338 29081
Satellite: ISS
Catalog Number: 25544
Epoch time: 08172
70279913 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 358
2466 deg
Eccentricity:
0005754
Arg of perigee: 350
9922 deg
Mean anomaly: 9
1139 deg
Mean motion: 15
77024338 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2908
Checksum: 317
Coasting Arc #11 (Orbit 2922)
---------------------------------------
Vector Time (GMT): 2008/173/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3721625
64 A = 6716280
53 meter
Y = -3768008
83 meter E =
0007488
Z = -4133821
27 I = 51
59370
XDOT = 6365
027310 Wp = 63
19428
YDOT = 2192
501582 meter/sec RA = 352
87312 deg
ZDOT = 3740
371825 TA = 245
06699
MA = 245
14482
Ha = 186
404 n
mi
Hp = 179
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12210057
87 X = 3783564
67
Y = -12362233
69 feet Y = -3726044
37 meter
Z = -13562405
75 Z = -4115592
06
XDOT = 20882
635532 XDOT = 6321
867473
YDOT = 7193
246661 feet/sec YDOT = 2263
436927 meter/sec
ZDOT = 12271
561106 ZDOT = 3771
188429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17315556
62 X = -5277781
66
Y = 1993301
02 feet Y = 607558
15 meter
Z = -13492495
50 Z = -4112512
63
XDOT = -11629
598921 XDOT = -3544
701751
YDOT = -17345
043397 feet/sec YDOT = -5286
769227 meter/sec
ZDOT = 12390
397675 ZDOT = 3776
593211
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 08173
65332967
00020000 00000-0 20000-3 0 9100
2 25544 51
6391 353
3440 0005957 354
3978 5
7119 15
76996210 29239
Satellite: ISS
Catalog Number: 25544
Epoch time: 08173
65332967 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 353
3440 deg
Eccentricity:
0005957
Arg of perigee: 354
3978 deg
Mean anomaly: 5
7119 deg
Mean motion: 15
76996210 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2923
Checksum: 311
Coasting Arc #12 (Orbit 2938)
---------------------------------------
Vector Time (GMT): 2008/174/15:27:46
949
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4942682
14 A = 6716521
22 meter
Y = -2178797
58 meter E =
0010671
Z = -4003621
74 I = 51
56647
XDOT = 5059
264170 Wp = 38
62105
YDOT = -4277
003768 meter/sec RA = 347
76138 deg
ZDOT = -3915
754012 TA = 190
85789
MA = 190
88094
Ha = 186
424 n
mi
Hp = 178
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16216148
74 X = -4898502
46
Y = -7148286
04 feet Y = -2233821
78 meter
Z = -13135241
94 Z = -4027526
11
XDOT = 16598
635727 XDOT = 5125
736114
YDOT = -14032
164593 feet/sec YDOT = -4220
055847 meter/sec
ZDOT = -12846
961981 ZDOT = -3891
015624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8420783
58 X = 2566654
84
Y = 15515175
63 feet Y = 4729025
53 meter
Z = -13227463
22 Z = -4031730
79
XDOT = -20639
434499 XDOT = -6290
899635
YDOT = 322
985887 feet/sec YDOT = 98
446098 meter/sec
ZDOT = -12752
026596 ZDOT = -3886
817706
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 08174
66721628
00020000 00000-0 20000-3 0 9119
2 25544 51
6396 348
1133 0005942 358
1451 1
9691 15
77018780 29395
Satellite: ISS
Catalog Number: 25544
Epoch time: 08174
66721628 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 348
1133 deg
Eccentricity:
0005942
Arg of perigee: 358
1451 deg
Mean anomaly: 1
9691 deg
Mean motion: 15
77018780 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2939
Checksum: 306
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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
- 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