[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 26th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 66 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 3049)
---------------------------------------
Vector Time (GMT): 2011/357/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3284107
20 A = 6775066
71 meter
Y = 5581103
73 meter E =
0028560
Z = -1927115
75 I = 51
32644
XDOT = -3480
910083 Wp = 187
05470
YDOT = -3972
364479 meter/sec RA = 286
69410 deg
ZDOT = -5591
381405 TA = 14
37410
MA = 14
29303
Ha = 220
394 n
mi
Hp = 203
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10774629
93 X = -3336910
59
Y = 18310707
78 feet Y = 5544083
88 meter
Z = -6322558
23 Z = -1943197
29
XDOT = -11420
308671 XDOT = -3409
069796
YDOT = -13032
691860 feet/sec YDOT = -4010
887622 meter/sec
ZDOT = -18344
427183 ZDOT = -5608
117705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13292447
83 X = -4051538
10
Y = 16548247
58 feet Y = 5043905
86 meter
Z = -6388720
10 Z = -1947281
89
XDOT = -8079
970961 XDOT = -2462
775149
YDOT = -13574
803063 feet/sec YDOT = -4137
599974 meter/sec
ZDOT = -18412
468228 ZDOT = -5612
120316
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 11357
75186218
00016717 00000-0 10270-3 0 9002
2 25544 51
6432 287
2471 0024357 199
1946 160
8293 15
58490025 30500
Satellite: ISS
Catalog Number: 25544
Epoch time: 11357
75186218 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 287
2471 deg
Eccentricity:
0024357
Arg of perigee: 199
1946 deg
Mean anomaly: 160
8293 deg
Mean motion: 15
58490025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 316
Coasting Arc #2 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2011/358/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4199476
81 A = 6768366
09 meter
Y = -3040784
90 meter E =
0025428
Z = 4366128
46 I = 51
29618
XDOT = 1361
301477 Wp = 180
91270
YDOT = 6748
208786 meter/sec RA = 281
65786 deg
ZDOT = 3365
710182 TA = 234
71669
MA = 234
95481
Ha = 220
121 n
mi
Hp = 203
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13777811
05 X = 4211957
71
Y = -9976328
40 feet Y = -2993754
64 meter
Z = 14324568
44 Z = 4386559
17
XDOT = 4466
212196 XDOT = 1269
390645
YDOT = 22139
792604 feet/sec YDOT = 6762
917285 meter/sec
ZDOT = 11042
356239 ZDOT = 3372
101088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14861998
41 X = 4529937
12
Y = -8128385
74 feet Y = -2477531
97 meter
Z = 14408289
80 Z = 4391646
73
XDOT = 917
249947 XDOT = 279
577784
YDOT = 21438
953752 feet/sec YDOT = 6534
593104 meter/sec
ZDOT = 11067
912624 ZDOT = 3373
499768
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 11358
77777789
00016717 00000-0 10270-3 0 9015
2 25544 51
6427 282
0978 0024152 202
9924 157
0152 15
58533373 30664
Satellite: ISS
Catalog Number: 25544
Epoch time: 11358
77777789 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 282
0978 deg
Eccentricity:
0024152
Arg of perigee: 202
9924 deg
Mean anomaly: 157
0152 deg
Mean motion: 15
58533373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 333
Coasting Arc #3 (Orbit 3080)
---------------------------------------
Vector Time (GMT): 2011/359/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194615
96 A = 6764326
41 meter
Y = -575662
71 meter E =
0022304
Z = -5279242
89 I = 51
27691
XDOT = 933
790682 Wp = 169
20331
YDOT = -7615
662998 meter/sec RA = 276
58930 deg
ZDOT = 66
988121 TA = 101
56311
MA = 101
31263
Ha = 219
772 n
mi
Hp = 203
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13761863
40 X = -4162221
82
Y = -1888657
19 feet Y = -622387
62 meter
Z = -17320350
69 Z = -5299541
42
XDOT = 3063
617722 XDOT = 1018
555727
YDOT = -24985
770991 feet/sec YDOT = -7604
746840 meter/sec
ZDOT = 219
777301 ZDOT = 71
729238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13359983
91 X = -4072123
09
Y = -3404177
66 feet Y = -1037593
35 meter
Z = -17403242
87 Z = -5304508
43
XDOT = 5587
358860 XDOT = 1703
026980
YDOT = -23512
733315 feet/sec YDOT = -7166
681114 meter/sec
ZDOT = 239
762770 ZDOT = 73
079692
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 11359
73954599
00016717 00000-0 10270-3 0 9029
2 25544 51
6413 277
2698 0024265 206
3826 153
6095 15
58612333 30817
Satellite: ISS
Catalog Number: 25544
Epoch time: 11359
73954599 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 277
2698 deg
Eccentricity:
0024265
Arg of perigee: 206
3826 deg
Mean anomaly: 153
6095 deg
Mean motion: 15
58612333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3081
Checksum: 330
Coasting Arc #4 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2011/360/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3354513
28 A = 6768177
39 meter
Y = 3982076
69 meter E =
0018222
Z = 4315952
21 I = 51
28807
XDOT = -2936
142348 Wp = 190
01048
YDOT = 6198
145147 meter/sec RA = 271
52359 deg
ZDOT = -3456
430983 TA = 295
11812
MA = 295
30707
Ha = 219
487 n
mi
Hp = 203
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11005620
98 X = 3288769
86
Y = 13064556
07 feet Y = 4019220
81 meter
Z = 14159948
21 Z = 4332088
93
XDOT = -9633
012952 XDOT = -2988
442611
YDOT = 20335
121872 feet/sec YDOT = 6165
019389 meter/sec
ZDOT = -11339
996663 ZDOT = -3470
820793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9633944
42 X = 2936426
26
Y = 14040321
55 feet Y = 4279490
01 meter
Z = 14225573
36 Z = 4335954
76
XDOT = -10422
167531 XDOT = -3176
676663
YDOT = 18635
344615 feet/sec YDOT = 5680
053039 meter/sec
ZDOT = -11399
284853 ZDOT = -3474
502023
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 11360
76540531
00016717 00000-0 10270-3 0 9032
2 25544 51
6416 272
1219 0024350 210
5230 149
4509 15
58650103 30971
Satellite: ISS
Catalog Number: 25544
Epoch time: 11360
76540531 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 272
1219 deg
Eccentricity:
0024350
Arg of perigee: 210
5230 deg
Mean anomaly: 149
4509 deg
Mean motion: 15
58650103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 277
Coasting Arc #5 (Orbit 3111)
---------------------------------------
Vector Time (GMT): 2011/361/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1807845
31 A = 6774741
67 meter
Y = -6291883
56 meter E =
0016982
Z = -1771563
54 I = 51
30920
XDOT = 4345
301614 Wp = 211
72018
YDOT = -2845
582404 meter/sec RA = 266
48619 deg
ZDOT = 5633
171397 TA = 128
72750
MA = 128
57557
Ha = 219
322 n
mi
Hp = 204
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5931251
02 X = -1728748
08
Y = -20642662
61 feet Y = -6311657
57 meter
Z = -5812216
34 Z = -1780154
37
XDOT = 14256
238890 XDOT = 4349
434133
YDOT = -9335
900276 feet/sec YDOT = -2796
968015 meter/sec
ZDOT = 18481
533456 ZDOT = 5654
290227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4278013
83 X = -1303938
62
Y = -21037922
40 feet Y = -6412358
75 meter
Z = -5846839
80 Z = -1782116
77
XDOT = 13291
012902 XDOT = 4051
100733
YDOT = -7898
375568 feet/sec YDOT = -2407
424873 meter/sec
ZDOT = 18568
054094 ZDOT = 5659
542888
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 11361
72712372
00016717 00000-0 10270-3 0 9044
2 25544 51
6401 267
2930 0024374 213
7178 146
2427 15
58690493 31120
Satellite: ISS
Catalog Number: 25544
Epoch time: 11361
72712372 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 267
2930 deg
Eccentricity:
0024374
Arg of perigee: 213
7178 deg
Mean anomaly: 146
2427 deg
Mean motion: 15
58690493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3112
Checksum: 298
Coasting Arc #6 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2011/362/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -144476
01 A = 6775120
14 meter
Y = 6607760
07 meter E =
0027703
Z = -1402067
92 I = 51
31366
XDOT = -4886
537497 Wp = 200
20209
YDOT = -1336
651468 meter/sec RA = 261
47237 deg
ZDOT = -5787
387122 TA = 355
21534
MA = 355
24176
Ha = 218
878 n
mi
Hp = 204
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -474002
64 X = -211543
69
Y = 21679002
86 feet Y = 6605769
56 meter
Z = -4599960
37 Z = -1402932
18
XDOT = -16031
947169 XDOT = -4843
114059
YDOT = -4385
339462 feet/sec YDOT = -1391
052503 meter/sec
ZDOT = -18987
490557 ZDOT = -5811
020109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1753777
75 X = -534551
46
Y = 21612289
20 feet Y = 6587425
75 meter
Z = -4603987
19 Z = -1403295
30
XDOT = -14046
915199 XDOT = -4281
499753
YDOT = -5211
221535 feet/sec YDOT = -1588
380324 meter/sec
ZDOT = -19083
971904 ZDOT = -5816
794636
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 11362
75292872
00016717 00000-0 10270-3 0 9057
2 25544 51
6400 262
1443 0024219 217
6741 142
2719 15
58742830 31289
Satellite: ISS
Catalog Number: 25544
Epoch time: 11362
75292872 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 262
1443 deg
Eccentricity:
0024219
Arg of perigee: 217
6741 deg
Mean anomaly: 142
2719 deg
Mean motion: 15
58742830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 300
Coasting Arc #7 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2011/363/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2174633
98 A = 6768689
60 meter
Y = -4953402
58 meter E =
0021579
Z = 4088037
05 I = 51
29716
XDOT = 4341
159144 Wp = 195
65726
YDOT = 5046
813938 meter/sec RA = 256
43921 deg
ZDOT = 3790
128144 TA = 214
92611
MA = 215
06787
Ha = 218
700 n
mi
Hp = 204
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7134625
93 X = 2210003
68
Y = -16251320
79 feet Y = -4928886
96 meter
Z = 13412195
04 Z = 4098686
87
XDOT = 14242
648110 XDOT = 4265
990567
YDOT = 16557
788510 feet/sec YDOT = 5094
938933 meter/sec
ZDOT = 12434
803623 ZDOT = 3811
034864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7748356
79 X = 2361699
15
Y = -15930853
72 feet Y = -4855724
22 meter
Z = 13456082
52 Z = 4101413
95
XDOT = 12277
222039 XDOT = 3742
097278
YDOT = 16589
742750 feet/sec YDOT = 5056
553590 meter/sec
ZDOT = 12519
878162 ZDOT = 3816
058864
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 11363
77870584
00016717 00000-0 10270-3 0 9063
2 25544 51
6391 256
9934 0024415 221
4034 138
5271 15
58783647 31440
Satellite: ISS
Catalog Number: 25544
Epoch time: 11363
77870584 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 256
9934 deg
Eccentricity:
0024415
Arg of perigee: 221
4034 deg
Mean anomaly: 138
5271 deg
Mean motion: 15
58783647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 327
Coasting Arc #8 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2011/364/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3859886
42 A = 6763771
15 meter
Y = 1759948
89 meter E =
0016670
Z = -5265235
66 I = 51
28949
XDOT = -2747
556662 Wp = 187
46789
YDOT = -7159
945125 meter/sec RA = 251
37316 deg
ZDOT = -395
191406 TA = 78
84433
MA = 78
65695
Ha = 218
275 n
mi
Hp = 204
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12663669
34 X = -3853702
43
Y = 5774110
52 feet Y = 1716820
11 meter
Z = -17274395
20 Z = -5283971
62
XDOT = -9014
293512 XDOT = -2665
368783
YDOT = -23490
633613 feet/sec YDOT = -7190
210434 meter/sec
ZDOT = -1296
559730 ZDOT = -408
339587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12704604
79 X = -3872363
54
Y = 5444818
10 feet Y = 1659580
56 meter
Z = -17351097
26 Z = -5288614
44
XDOT = -7995
765928 XDOT = -2437
109455
YDOT = -22790
379759 feet/sec YDOT = -6946
507750 meter/sec
ZDOT = -1349
783751 ZDOT = -411
414087
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 11364
74034810
00016717 00000-0 10270-3 0 9076
2 25544 51
6393 252
1653 0024251 224
3928 135
5283 15
58819271 31599
Satellite: ISS
Catalog Number: 25544
Epoch time: 11364
74034810 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 252
1653 deg
Eccentricity:
0024251
Arg of perigee: 224
3928 deg
Mean anomaly: 135
5283 deg
Mean motion: 15
58819271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 309
Coasting Arc #9 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2011/365/17:22:00
768
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4724400
93 A = 6766944
67 meter
Y = 1786757
84 meter E =
0016263
Z = 4505166
89 I = 51
31048
XDOT = 327
350561 Wp = 218
30708
YDOT = 6995
554528 meter/sec RA = 246
30313 deg
ZDOT = -3136
349537 TA = 263
17744
MA = 263
36250
Ha = 218
041 n
mi
Hp = 204
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15500003
04 X = 4682184
87
Y = 5862066
42 feet Y = 1839352
72 meter
Z = 14780731
27 Z = 4528015
34
XDOT = 1073
984779 XDOT = 264
336202
YDOT = 22951
294382 feet/sec YDOT = 6998
862993 meter/sec
ZDOT = -10289
860687 ZDOT = -3134
911982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15358097
11 X = 4681148
00
Y = 5998091
83 feet Y = 1828218
39 meter
Z = 14873993
46 Z = 4533593
21
XDOT = 1371
967778 XDOT = 418
175779
YDOT = 21839
874749 feet/sec YDOT = 6656
793823 meter/sec
ZDOT = -10284
479102 ZDOT = -3134
709230
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 11365
76607247
00016717 00000-0 10270-3 0 9080
2 25544 51
6389 247
0150 0024320 228
3319 131
5754 15
58823226 31756
Satellite: ISS
Catalog Number: 25544
Epoch time: 11365
76607247 = yrday
fracday
Element set: 908
Inclination: 51
6389 deg
RA of node: 247
0150 deg
Eccentricity:
0024320
Arg of perigee: 228
3319 deg
Mean anomaly: 131
5754 deg
Mean motion: 15
58823226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 310
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
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