Date:
August 11th 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
231/09:30:30
000 0
0 0
0 0
0
010/10:53:48
047 0
0 0
0 184
7
000/00:00:00
000 0
0 0
0 184
2
Coasting Arc #1 (Orbit 1917)
---------------------------------------
Vector Time (GMT): 2007/221/09:30:30
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940310
40 A = 6717052
60 meter
Y = -3048126
57 meter E =
0003488
Z = 4502475
32 I = 51
57535
XDOT = 6181
111640 Wp = 142
07529
YDOT = 3379
728782 meter/sec RA = 188
08120 deg
ZDOT = -3122
749511 TA = 339
06693
MA = 339
08121
Ha = 186
919 n
mi
Hp = 181
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12927527
55 X = 3952230
30
Y = -10000415
25 feet Y = -3003997
75 meter
Z = 14771900
65 Z = 4521645
59
XDOT = 20279
237663 XDOT = 6158
029124
YDOT = 11088
349022 feet/sec YDOT = 3448
720802 meter/sec
ZDOT = -10245
241178 ZDOT = -3092
777780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11961696
93 X = -3645925
22
Y = -11041142
21 feet Y = -3365340
14 meter
Z = 14844167
48 Z = 4524502
25
XDOT = 6817
518203 XDOT = 2077
979548
YDOT = -21000
491066 feet/sec YDOT = -6400
949677 meter/sec
ZDOT = -10131
231527 ZDOT = -3087
999370
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 07221
43832156
00020000 00000-0 20000-3 0 9003
2 25544 51
6307 188
8772 0008525 223
0970 136
9527 15
76177549 19182
Satellite: ISS
Catalog Number: 25544
Epoch time: 07221
43832156 = yrday
fracday
Element set: 900
Inclination: 51
6307 deg
RA of node: 188
8772 deg
Eccentricity:
0008525
Arg of perigee: 223
0970 deg
Mean anomaly: 136
9527 deg
Mean motion: 15
76177549 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1918
Checksum: 307
Coasting Arc #2 (Orbit 1933)
---------------------------------------
Vector Time (GMT): 2007/222/09:35:41
088
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3211105
35 A = 6717089
85 meter
Y = -3769678
20 meter E =
0009425
Z = 4541685
22 I = 51
60350
XDOT = 6760
643506 Wp = 169
77658
YDOT = -2071
776912 meter/sec RA = 182
95306 deg
ZDOT = 3050
281796 TA = 249
81482
MA = 249
91621
Ha = 186
829 n
mi
Hp = 182
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10535122
53 X = -3190775
81
Y = -12367710
64 feet Y = -3805473
45 meter
Z = 14900542
06 Z = 4526134
94
XDOT = 22180
588930 XDOT = 6768
490560
YDOT = -6797
168348 feet/sec YDOT = -1996
132067 meter/sec
ZDOT = 10007
486206 ZDOT = 3083
143125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9963517
36 X = -3036880
09
Y = 12901338
06 feet Y = 3932327
84 meter
Z = 14841126
14 Z = 4523575
25
XDOT = -10192
225671 XDOT = -3106
590384
YDOT = -19564
655709 feet/sec YDOT = -5963
307060 meter/sec
ZDOT = 10131
776848 ZDOT = 3088
165583
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 07222
45275370
00020000 00000-0 20000-3 0 9016
2 25544 51
6301 183
6495 0008506 227
5910 132
4536 15
76172698 19342
Satellite: ISS
Catalog Number: 25544
Epoch time: 07222
45275370 = yrday
fracday
Element set: 901
Inclination: 51
6301 deg
RA of node: 183
6495 deg
Eccentricity:
0008506
Arg of perigee: 227
5910 deg
Mean anomaly: 132
4536 deg
Mean motion: 15
76172698 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1934
Checksum: 290
Coasting Arc #3 (Orbit 1948)
---------------------------------------
Vector Time (GMT): 2007/223/09:40:37
548
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6702958
33 A = 6725768
40 meter
Y = 463641
34 meter E =
0003332
Z = -254128
67 I = 51
66287
XDOT = -556
314283 Wp = 24
61592
YDOT = -4752
963515 meter/sec RA = 177
75716 deg
ZDOT = 6033
210837 TA = 332
62218
MA = 332
63973
Ha = 186
593 n
mi
Hp = 182
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21991333
10 X = -6706410
18
Y = 1521133
01 feet Y = 388665
81 meter
Z = -833755
48 Z = -286699
19
XDOT = -1825
178093 XDOT = -532
432123
YDOT = -15593
712319 feet/sec YDOT = -4759
051553 meter/sec
ZDOT = 19793
998808 ZDOT = 6030
565903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6757412
61 X = 2059659
36
Y = 20977343
52 feet Y = 6393894
30 meter
Z = -957162
04 Z = -291742
99
XDOT = -13142
578535 XDOT = -4005
857938
YDOT = 5132
220283 feet/sec YDOT = 1564
300742 meter/sec
ZDOT = 19783
367248 ZDOT = 6029
970337
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 07223
40377467
00020000 00000-0 20000-3 0 9023
2 25544 51
6304 178
7493 0008571 229
8771 130
1643 15
76239091 19491
Satellite: ISS
Catalog Number: 25544
Epoch time: 07223
40377467 = yrday
fracday
Element set: 902
Inclination: 51
6304 deg
RA of node: 178
7493 deg
Eccentricity:
0008571
Arg of perigee: 229
8771 deg
Mean anomaly: 130
1643 deg
Mean motion: 15
76239091 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1949
Checksum: 306
Coasting Arc #4 (Orbit 1964)
---------------------------------------
Vector Time (GMT): 2007/224/09:45:30
869
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2298887
59 A = 6715943
66 meter
Y = 4118615
73 meter E =
0009395
Z = -4787717
22 I = 51
65810
XDOT = -7193
271813 Wp = 153
34281
YDOT = -1074
617230 meter/sec RA = 172
57092 deg
ZDOT = 2523
172277 TA = 141
39184
MA = 141
32463
Ha = 186
355 n
mi
Hp = 182
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7542282
13 X = -2321514
43
Y = 13512518
79 feet Y = 4092782
07 meter
Z = -15707733
65 Z = -4798939
63
XDOT = -23599
973140 XDOT = -7192
977474
YDOT = -3525
647079 feet/sec YDOT = -1155
054964 meter/sec
ZDOT = 8278
124267 ZDOT = 2488
228887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15050242
72 X = 4587313
98
Y = 3412131
42 feet Y = 1040017
66 meter
Z = -15749750
27 Z = -4800523
88
XDOT = 3422
385991 XDOT = 1043
143250
YDOT = 22598
412122 feet/sec YDOT = 6887
996015 meter/sec
ZDOT = 8145
511999 ZDOT = 2482
752057
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
41818843
00020000 00000-0 20000-3 0 9034
2 25544 51
6304 173
5212 0008452 235
8398 124
1965 15
76179509 19658
Satellite: ISS
Catalog Number: 25544
Epoch time: 07224
41818843 = yrday
fracday
Element set: 903
Inclination: 51
6304 deg
RA of node: 173
5212 deg
Eccentricity:
0008452
Arg of perigee: 235
8398 deg
Mean anomaly: 124
1965 deg
Mean motion: 15
76179509 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1965
Checksum: 304
Coasting Arc #5 (Orbit 1980)
---------------------------------------
Vector Time (GMT): 2007/225/09:50:11
343
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4801976
65 A = 6718587
14 meter
Y = 2262594
21 meter E =
0001698
Z = -4117148
01 I = 51
69610
XDOT = -5223
781483 Wp = 183
01814
YDOT = 4218
441640 meter/sec RA = 167
44971 deg
ZDOT = -3776
016623 TA = 48
33309
MA = 48
31856
Ha = 186
222 n
mi
Hp = 182
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15754516
55 X = 4796318
98
Y = 7423209
34 feet Y = 2316261
14 meter
Z = -13507703
45 Z = -4093834
22
XDOT = -17138
390691 XDOT = -5252
221711
YDOT = 13840
031626 feet/sec YDOT = 4159
867500 meter/sec
ZDOT = -12388
505982 ZDOT = -3801
462068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2087596
09 X = 636299
29
Y = -17359112
08 feet Y = -5291057
36 meter
Z = -13419018
28 Z = -4090116
77
XDOT = 17226
683155 XDOT = 5250
693026
YDOT = 11718
373521 feet/sec YDOT = 3571
760249 meter/sec
ZDOT = -12484
434895 ZDOT = -3805
255756
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
43259286
00020000 00000-0 20000-3 0 9048
2 25544 51
6308 168
2933 0008408 239
8740 120
1591 15
76213498 19814
Satellite: ISS
Catalog Number: 25544
Epoch time: 07225
43259286 = yrday
fracday
Element set: 904
Inclination: 51
6308 deg
RA of node: 168
2933 deg
Eccentricity:
0008408
Arg of perigee: 239
8740 deg
Mean anomaly: 120
1591 deg
Mean motion: 15
76213498 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1981
Checksum: 304
Coasting Arc #6 (Orbit 1996)
---------------------------------------
Vector Time (GMT): 2007/226/09:55:17
216
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6066742
36 A = 6725392
36 meter
Y = -2724761
69 meter E =
0011939
Z = 945579
18 I = 51
74797
XDOT = 2748
151565 Wp = 162
48057
YDOT = 4049
540728 meter/sec RA = 162
24974 deg
ZDOT = -5954
617899 TA = 7
19328
MA = 7
17617
Ha = 185
826 n
mi
Hp = 183
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19904010
35 X = 6092166
80
Y = -8939506
85 feet Y = -2656777
82 meter
Z = 3102293
91 Z = 975112
52
XDOT = 9016
245293 XDOT = 2731
590619
YDOT = 13285
894777 feet/sec YDOT = 4080
179621 meter/sec
ZDOT = -19536
147962 ZDOT = -5941
307803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15345751
18 X = -4677384
96
Y = -15488294
78 feet Y = -4720832
25 meter
Z = 3213920
34 Z = 979602
92
XDOT = 8112
459948 XDOT = 2472
677792
YDOT = -12086
465689 feet/sec YDOT = -3683
954742 meter/sec
ZDOT = -19485
153831 ZDOT = -5939
074888
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
44698724
00020000 00000-0 20000-3 0 9055
2 25544 51
6312 163
0660 0008435 244
9924 115
0365 15
76241781 19975
Satellite: ISS
Catalog Number: 25544
Epoch time: 07226
44698724 = yrday
fracday
Element set: 905
Inclination: 51
6312 deg
RA of node: 163
0660 deg
Eccentricity:
0008435
Arg of perigee: 244
9924 deg
Mean anomaly: 115
0365 deg
Mean motion: 15
76241781 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1997
Checksum: 302
Coasting Arc #7 (Orbit 2012)
---------------------------------------
Vector Time (GMT): 2007/227/09:59:53
989
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 162814
78 A = 6714607
69 meter
Y = -4406972
84 meter E =
0003803
Z = 5066623
17 I = 51
73913
XDOT = 7330
753097 Wp = 268
19188
YDOT = -1660
025191 meter/sec RA = 157
08399 deg
ZDOT = -1680
666250 TA = 197
93675
MA = 197
95017
Ha = 185
686 n
mi
Hp = 183
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 534169
24 X = 187469
76
Y = -14458572
31 feet Y = -4405014
33 meter
Z = 16622779
44 Z = 5067473
98
XDOT = 24051
027220 XDOT = 7356
935151
YDOT = -5446
276874 feet/sec YDOT = -1577
902177 meter/sec
ZDOT = -5513
996884 ZDOT = -1644
990440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13511357
77 X = -4118261
85
Y = 5166304
30 feet Y = 1574689
55 meter
Z = 16625431
04 Z = 5067431
38
XDOT = -13930
921274 XDOT = -4246
144804
YDOT = -19136
269274 feet/sec YDOT = -5832
734875 meter/sec
ZDOT = -5378
935312 ZDOT = -1639
499483
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
46137273
00020000 00000-0 20000-3 0 9066
2 25544 51
6316 157
8390 0008475 248
9071 111
1187 15
76242300 20138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07227
46137273 = yrday
fracday
Element set: 906
Inclination: 51
6316 deg
RA of node: 157
8390 deg
Eccentricity:
0008475
Arg of perigee: 248
9071 deg
Mean anomaly: 111
1187 deg
Mean motion: 15
76242300 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2013
Checksum: 276
Coasting Arc #8 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2007/228/10:04:41
989
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5652309
75 A = 6720024
36 meter
Y = -225769
85 meter E =
0005171
Z = 3627415
38 I = 51
78450
XDOT = 3046
501077 Wp = 132
18965
YDOT = -5542
703049 meter/sec RA = 151
96313 deg
ZDOT = 4394
764364 TA = 271
20640
MA = 271
26564
Ha = 185
436 n
mi
Hp = 183
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18544323
33 X = -5666986
19
Y = -740714
74 feet Y = -289059
23 meter
Z = 11900969
11 Z = 3599921
13
XDOT = 9995
082275 XDOT = 3086
905258
YDOT = -18184
721289 feet/sec YDOT = -5508
409443 meter/sec
ZDOT = 14418
518253 ZDOT = 4409
662238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7152068
12 X = 2179950
36
Y = 17197671
52 feet Y = 5241850
28 meter
Z = 11796680
37 Z = 3595628
18
XDOT = -19413
566225 XDOT = -5917
254985
YDOT = -1871
731392 feet/sec YDOT = -570
503728 meter/sec
ZDOT = 14474
289240 ZDOT = 4411
763360
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
47574654
00020000 00000-0 20000-3 0 9077
2 25544 51
6322 152
6116 0008595 252
5020 107
5205 15
76295128 20295
Satellite: ISS
Catalog Number: 25544
Epoch time: 07228
47574654 = yrday
fracday
Element set: 907
Inclination: 51
6322 deg
RA of node: 152
6116 deg
Eccentricity:
0008595
Arg of perigee: 252
5020 deg
Mean anomaly: 107
5205 deg
Mean motion: 15
76295128 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2029
Checksum: 284
Coasting Arc #9 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2007/229/10:09:38
164
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4595339
05 A = 6724427
91 meter
Y = 4603042
61 meter E =
0005527
Z = -1693043
21 I = 51
82391
XDOT = -4537
707876 Wp = 319
49379
YDOT = -2418
127562 meter/sec RA = 146
76154 deg
ZDOT = 5735
786217 TA = 21
81655
MA = 21
79302
Ha = 185
179 n
mi
Hp = 183
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15076571
70 X = -4638244
99
Y = 15101845
82 feet Y = 4551415
04 meter
Z = -5554603
72 Z = -1715471
42
XDOT = -14887
493031 XDOT = -4538
193973
YDOT = -7933
489375 feet/sec YDOT = -2468
873501 meter/sec
ZDOT = 18818
196249 ZDOT = 5713
741007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20295766
24 X = 6186149
55
Y = 6519607
13 feet Y = 1987176
25 meter
Z = -5639058
37 Z = -1718784
99
XDOT = 237
911423 XDOT = 72
515402
YDOT = 15480
919762 feet/sec YDOT = 4718
584344 meter/sec
ZDOT = 18734
281989 ZDOT = 5710
209150
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
42671555
00020000 00000-0 20000-3 0 9082
2 25544 51
6318 147
7105 0008504 257
2645 102
7569 15
76271875 20448
Satellite: ISS
Catalog Number: 25544
Epoch time: 07229
42671555 = yrday
fracday
Element set: 908
Inclination: 51
6318 deg
RA of node: 147
7105 deg
Eccentricity:
0008504
Arg of perigee: 257
2645 deg
Mean anomaly: 102
7569 deg
Mean motion: 15
76271875 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2044
Checksum: 302
Coasting Arc #10 (Orbit 2059)
---------------------------------------
Vector Time (GMT): 2007/230/10:14:32
147
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1714550
61 A = 6713857
23 meter
Y = 3874000
94 meter E =
0006795
Z = -5214069
68 I = 51
81247
XDOT = -6426
526818 Wp = 117
28544
YDOT = 4132
842083 meter/sec RA = 141
61148 deg
ZDOT = 955
308955 TA = 161
80840
MA = 161
78408
Ha = 184
960 n
mi
Hp = 184
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5625166
04 X = 1696432
43
Y = 12709976
84 feet Y = 3893072
77 meter
Z = -17106527
81 Z = -5205784
39
XDOT = -21084
405570 XDOT = -6476
903938
YDOT = 13559
193185 feet/sec YDOT = 4060
695352 meter/sec
ZDOT = 3134
215732 ZDOT = 923
966695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8284745
18 X = 2525190
33
Y = -11208930
05 feet Y = -3416481
88 meter
Z = -17074606
37 Z = -5204340
02
XDOT = 21333
447199 XDOT = 6502
434706
YDOT = 11163
321756 feet/sec YDOT = 3402
580471 meter/sec
ZDOT = 3015
886836 ZDOT = 919
242307
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
44107191
00020000 00000-0 20000-3 0 9097
2 25544 51
6324 142
4826 0008556 261
4756 98
5439 15
76291035 20600
Satellite: ISS
Catalog Number: 25544
Epoch time: 07230
44107191 = yrday
fracday
Element set: 909
Inclination: 51
6324 deg
RA of node: 142
4826 deg
Eccentricity:
0008556
Arg of perigee: 261
4756 deg
Mean anomaly: 98
5439 deg
Mean motion: 15
76291035 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2060
Checksum: 289
Coasting Arc #11 (Orbit 2075)
---------------------------------------
Vector Time (GMT): 2007/231/09:30:30
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5622085
82 A = 6723652
83 meter
Y = 2992818
07 meter E =
0006222
Z = 2142885
18 I = 51
86638
XDOT = -711
629249 Wp = 49
48712
YDOT = -5307
208343 meter/sec RA = 136
65682 deg
ZDOT = 5538
688138 TA = 334
42994
MA = 334
46070
Ha = 184
657 n
mi
Hp = 184
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18445163
46 X = -5665543
84
Y = 9818956
93 feet Y = 2929705
70 meter
Z = 7030463
18 Z = 2115467
65
XDOT = -2334
741630 XDOT = -679
136262
YDOT = -17412
100864 feet/sec YDOT = -5314
984647 meter/sec
ZDOT = 18171
549008 ZDOT = 5535
309839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15362566
66 X = 4682510
32
Y = 14215256
07 feet Y = 4332810
05 meter
Z = 6926862
43 Z = 2111307
67
XDOT = -14599
553392 XDOT = -4449
943874
YDOT = 6919
234163 feet/sec YDOT = 2108
982573 meter/sec
ZDOT = 18158
055965 ZDOT = 5534
575458
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
45541817
00020000 00000-0 20000-3 0 9108
2 25544 51
6319 137
2547 0008564 265
1377 94
8810 15
76317700 20762
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
45541817 = yrday
fracday
Element set: 910
Inclination: 51
6319 deg
RA of node: 137
2547 deg
Eccentricity:
0008564
Arg of perigee: 265
1377 deg
Mean anomaly: 94
8810 deg
Mean motion: 15
76317700 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2076
Checksum: 292
Coasting Arc #12 (Orbit 2090)
---------------------------------------
Vector Time (GMT): 2007/232/09:35:16
847
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1532695
59 A = 6720823
04 meter
Y = 5647889
75 meter E =
0003892
Z = -3301235
17 I = 51
87724
XDOT = -5969
169242 Wp = 273
27063
YDOT = 1148
495517 meter/sec RA = 131
45777 deg
ZDOT = 4731
716882 TA = 48
08060
MA = 48
04742
Ha = 183
646 n
mi
Hp = 183
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5028528
83 X = -1579700
43
Y = 18529822
01 feet Y = 5630487
60 meter
Z = -10830824
06 Z = -3308794
94
XDOT = -19583
888589 XDOT = -6004
554045
YDOT = 3768
029910 feet/sec YDOT = 1081
546856 meter/sec
ZDOT = 15524
005518 ZDOT = 4702
632791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19063883
25 X = 5810671
61
Y = -2145324
93 feet Y = -653895
04 meter
Z = -10858779
50 Z = -3309755
99
XDOT = 10537
431461 XDOT = 3211
809109
YDOT = 15544
307320 feet/sec YDOT = 4737
904871 meter/sec
ZDOT = 15413
838501 ZDOT = 4698
137975
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
40635946
00020000 00000-0 20000-3 0 9112
2 25544 51
6320 132
3537 0008623 269
5434 90
4743 15
76312931 20912
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
40635946 = yrday
fracday
Element set: 911
Inclination: 51
6320 deg
RA of node: 132
3537 deg
Eccentricity:
0008623
Arg of perigee: 269
5434 deg
Mean anomaly: 90
4743 deg
Mean motion: 15
76312931 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2091
Checksum: 276
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
- 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