[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 23rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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 3016)
---------------------------------------
Vector Time (GMT): 2011/355/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2230741
76 A = 6776452
91 meter
Y = 6274922
31 meter E =
0032170
Z = 1128935
16 I = 51
35571
XDOT = -4925
349539 Wp = 167
01764
YDOT = -694
550606 meter/sec RA = 297
36019 deg
ZDOT = -5870
231536 TA =
62607
MA =
62206
Ha = 221
036 n
mi
Hp = 203
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7318706
58 X = -2306227
59
Y = 20587015
47 feet Y = 6249554
59 meter
Z = 3703855
51 Z = 1117915
53
XDOT = -16159
283263 XDOT = -4888
700183
YDOT = -2278
709338 feet/sec YDOT = -749
423282 meter/sec
ZDOT = -19259
289817 ZDOT = -5894
070086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21014264
12 X = -6405147
70
Y = 6010378
92 feet Y = 1831963
50 meter
Z = 3658314
65 Z = 1115054
30
XDOT = -7043
271733 XDOT = -2146
789224
YDOT = -12840
625107 feet/sec YDOT = -3913
822533 meter/sec
ZDOT = -19356
604122 ZDOT = -5899
892936
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 11355
63581982
00016717 00000-0 10270-3 0 9004
2 25544 51
6442 297
8640 0024346 190
5081 169
5568 15
58390870 30170
Satellite: ISS
Catalog Number: 25544
Epoch time: 11355
63581982 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 297
8640 deg
Eccentricity:
0024346
Arg of perigee: 190
5081 deg
Mean anomaly: 169
5568 deg
Mean motion: 15
58390870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3017
Checksum: 328
Coasting Arc #2 (Orbit 3032)
---------------------------------------
Vector Time (GMT): 2011/356/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3844511
97 A = 6775114
14 meter
Y = -5237385
99 meter E =
0019511
Z = 1955236
98 I = 51
33914
XDOT = 3032
427988 Wp = 158
81457
YDOT = 4313
211161 meter/sec RA = 292
34882 deg
ZDOT = 5555
696127 TA = 222
84278
MA = 222
99497
Ha = 220
744 n
mi
Hp = 203
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12613228
24 X = 3893293
52
Y = -17183024
90 feet Y = -5194121
82 meter
Z = 6414819
47 Z = 1974031
42
XDOT = 9948
910721 XDOT = 2956
982801
YDOT = 14150
955254 feet/sec YDOT = 4346
699023 meter/sec
ZDOT = 18227
349499 ZDOT = 5570
245040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21291636
85 X = 6489690
91
Y = -139593
55 feet Y = -42548
11 meter
Z = 6492033
14 Z = 1978771
70
XDOT = -5513
708834 XDOT = -1680
578452
YDOT = 14780
934934 feet/sec YDOT = 4505
228968 meter/sec
ZDOT = 18286
417901 ZDOT = 5573
700176
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 11356
66180108
00016717 00000-0 10270-3 0 9014
2 25544 51
6443 292
7157 0024199 194
5047 165
5416 15
58454205 30339
Satellite: ISS
Catalog Number: 25544
Epoch time: 11356
66180108 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 292
7157 deg
Eccentricity:
0024199
Arg of perigee: 194
5047 deg
Mean anomaly: 165
5416 deg
Mean motion: 15
58454205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3033
Checksum: 307
Coasting Arc #3 (Orbit 3047)
---------------------------------------
Vector Time (GMT): 2011/357/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4473819
72 A = 6768258
87 meter
Y = 2534333
70 meter E =
0019742
Z = -4390847
32 I = 51
30703
XDOT = -649
853706 Wp = 176
75440
YDOT = -6889
757348 meter/sec RA = 287
31426 deg
ZDOT = -3334
647099 TA = 59
55175
MA = 59
35687
Ha = 220
313 n
mi
Hp = 203
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14677886
22 X = -4480496
77
Y = 8314743
12 feet Y = 2484268
04 meter
Z = -14405667
05 Z = -4412596
90
XDOT = -2132
065964 XDOT = -556
563714
YDOT = -22604
190774 feet/sec YDOT = -6896
502294 meter/sec
ZDOT = -10940
443238 ZDOT = -3337
578519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15484503
56 X = -4719676
68
Y = -6498576
27 feet Y = -1980766
05 meter
Z = -14494729
94 Z = -4417993
69
XDOT = 16186
625417 XDOT = 4933
683427
YDOT = -14287
498732 feet/sec YDOT = -4354
829613 meter/sec
ZDOT = -10951
844139 ZDOT = -3338
122093
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
62363290
00016717 00000-0 10270-3 0 9027
2 25544 51
6451 287
8893 0024163 198
2913 161
7376 15
58514163 30483
Satellite: ISS
Catalog Number: 25544
Epoch time: 11357
62363290 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 287
8893 deg
Eccentricity:
0024163
Arg of perigee: 198
2913 deg
Mean anomaly: 161
7376 deg
Mean motion: 15
58514163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3048
Checksum: 324
Coasting Arc #4 (Orbit 3063)
---------------------------------------
Vector Time (GMT): 2011/358/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4130016
09 A = 6764458
58 meter
Y = 930271
05 meter E =
0023361
Z = 5281564
95 I = 51
28658
XDOT = -1660
818055 Wp = 196
55091
YDOT = 7489
265806 meter/sec RA = 282
24924 deg
ZDOT = -42
480432 TA = 253
72714
MA = 253
98424
Ha = 220
082 n
mi
Hp = 203
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13549921
55 X = 4093650
02
Y = 3052070
37 feet Y = 976251
29 meter
Z = 17327969
00 Z = 5301540
19
XDOT = -5448
878134 XDOT = -1744
234718
YDOT = 24571
082042 feet/sec YDOT = 7470
227118 meter/sec
ZDOT = -139
371497 ZDOT = -50
750094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5989599
68 X = 1825629
98
Y = 12418049
01 feet Y = 3785021
34 meter
Z = 17409502
34 Z = 5306416
31
XDOT = -21707
052636 XDOT = -6616
309643
YDOT = 10612
588843 feet/sec YDOT = 3234
717079 meter/sec
ZDOT = -173
773935 ZDOT = -52
966295
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
64956022
00016717 00000-0 10270-3 0 9032
2 25544 51
6450 282
7416 0024241 202
2124 157
7983 15
58566591 30643
Satellite: ISS
Catalog Number: 25544
Epoch time: 11358
64956022 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 282
7416 deg
Eccentricity:
0024241
Arg of perigee: 202
2124 deg
Mean anomaly: 157
7983 deg
Mean motion: 15
58566591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3064
Checksum: 309
Coasting Arc #5 (Orbit 3078)
---------------------------------------
Vector Time (GMT): 2011/359/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2938566
51 A = 6768428
94 meter
Y = -4322926
86 meter E =
0024890
Z = -4312945
24 I = 51
29455
XDOT = 3526
103668 Wp = 185
62786
YDOT = -5865
645467 meter/sec RA = 277
18235 deg
ZDOT = 3450
695773 TA = 119
73024
MA = 119
48233
Ha = 219
870 n
mi
Hp = 203
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9640966
24 X = -2869057
08
Y = -14182830
90 feet Y = -4355398
45 meter
Z = -14150082
82 Z = -4327052
37
XDOT = 11568
581589 XDOT = 3574
669804
YDOT = -19244
243658 feet/sec YDOT = -5825
943351 meter/sec
ZDOT = 11321
180359 ZDOT = 3467
942474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4858367
04 X = 1480830
28
Y = -16397334
01 feet Y = -4997907
41 meter
Z = -14207373
90 Z = -4330407
57
XDOT = 20966
198675 XDOT = 6390
497356
YDOT = -3732
348344 feet/sec YDOT = -1137
619775 meter/sec
ZDOT = 11392
122350 ZDOT = 3472
318892
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
61134284
00016717 00000-0 10270-3 0 9049
2 25544 51
6449 277
9144 0024176 205
9645 154
0298 15
58587880 30799
Satellite: ISS
Catalog Number: 25544
Epoch time: 11359
61134284 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 277
9144 deg
Eccentricity:
0024176
Arg of perigee: 205
9645 deg
Mean anomaly: 154
0298 deg
Mean motion: 15
58587880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3079
Checksum: 342
Coasting Arc #6 (Orbit 3094)
---------------------------------------
Vector Time (GMT): 2011/360/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1222542
65 A = 6774960
40 meter
Y = 6390771
57 meter E =
0026823
Z = 1824774
91 I = 51
31341
XDOT = -4607
597543 Wp = 177
93766
YDOT = 2483
246065 meter/sec RA = 272
14803 deg
ZDOT = -5633
705810 TA = 341
82342
MA = 341
91912
Ha = 219
632 n
mi
Hp = 204
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4010966
71 X = 1142124
65
Y = 20967098
33 feet Y = 6403992
93 meter
Z = 5986794
32 Z = 1830519
37
XDOT = -15116
789838 XDOT = -4607
656219
YDOT = 8147
132759 feet/sec YDOT = 2431
721445 meter/sec
ZDOT = -18483
286779 ZDOT = -5656
088956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13358217
57 X = -4071584
72
Y = 16643002
95 feet Y = 5072787
30 meter
Z = 6009762
80 Z = 1831775
70
XDOT = -14726
951178 XDOT = -4488
774719
YDOT = -5140
998174 feet/sec YDOT = -1566
976243 meter/sec
ZDOT = -18574
945019 ZDOT = -5661
643242
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
63721862
00016717 00000-0 10270-3 0 9058
2 25544 51
6447 272
7667 0024222 209
3673 150
6123 15
58591302 30952
Satellite: ISS
Catalog Number: 25544
Epoch time: 11360
63721862 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 272
7667 deg
Eccentricity:
0024222
Arg of perigee: 209
3673 deg
Mean anomaly: 150
6123 deg
Mean motion: 15
58591302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3095
Checksum: 304
Coasting Arc #7 (Orbit 3110)
---------------------------------------
Vector Time (GMT): 2011/361/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 750136
93 A = 6775337
55 meter
Y = -6606464
40 meter E =
0013301
Z = 1348305
80 I = 51
31489
XDOT = 4721
645166 Wp = 186
12250
YDOT = 1717
745369 meter/sec RA = 267
13315 deg
ZDOT = 5782
042094 TA = 188
62751
MA = 188
65040
Ha = 219
288 n
mi
Hp = 204
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2461079
16 X = 817406
28
Y = -21674751
98 feet Y = -6597699
92 meter
Z = 4423575
45 Z = 1352112
62
XDOT = 15490
961832 XDOT = 4673
998503
YDOT = 5635
647537 feet/sec YDOT = 1770
278719 meter/sec
ZDOT = 18969
954378 ZDOT = 5804
863846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17846184
48 X = 5439517
03
Y = -12538863
32 feet Y = -3821845
54 meter
Z = 4439640
73 Z = 1353202
49
XDOT = 5052
347299 XDOT = 1539
955457
YDOT = 13949
439451 feet/sec YDOT = 4251
789145 meter/sec
ZDOT = 19063
082596 ZDOT = 5810
427575
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
66306337
00016717 00000-0 10270-3 0 9069
2 25544 51
6440 267
6169 0024208 213
8555 146
1055 15
58681057 31118
Satellite: ISS
Catalog Number: 25544
Epoch time: 11361
66306337 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 267
6169 deg
Eccentricity:
0024208
Arg of perigee: 213
8555 deg
Mean anomaly: 146
1055 deg
Mean motion: 15
58681057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3111
Checksum: 301
Coasting Arc #8 (Orbit 3125)
---------------------------------------
Vector Time (GMT): 2011/362/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2603972
49 A = 6769073
10 meter
Y = 4754838
33 meter E =
0018668
Z = -4034334
86 I = 51
29566
XDOT = -3876
391728 Wp = 205
19725
YDOT = -5395
167645 meter/sec RA = 262
10227 deg
ZDOT = -3866
709625 TA = 24
71145
MA = 24
62213
Ha = 218
934 n
mi
Hp = 204
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8543216
84 X = -2637350
81
Y = 15599863
30 feet Y = 4725532
80 meter
Z = -13236006
76 Z = -4047065
43
XDOT = -12717
820630 XDOT = -3796
990364
YDOT = -17700
681251 feet/sec YDOT = -5438
071581 meter/sec
ZDOT = -12686
055201 ZDOT = -3885
348341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17219390
99 X = -5248470
38
Y = 4294814
44 feet Y = 1309059
44 meter
Z = -13288389
91 Z = -4050301
24
XDOT = 4829
335230 XDOT = 1471
981378
YDOT = -20021
874295 feet/sec YDOT = -6102
667285 meter/sec
ZDOT = -12761
820771 ZDOT = -3889
802971
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
62477061
00016717 00000-0 10270-3 0 9070
2 25544 51
6431 262
7897 0024257 217
7319 142
2136 15
58690884 31268
Satellite: ISS
Catalog Number: 25544
Epoch time: 11362
62477061 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 262
7897 deg
Eccentricity:
0024257
Arg of perigee: 217
7319 deg
Mean anomaly: 142
2136 deg
Mean motion: 15
58690884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3126
Checksum: 322
Coasting Arc #9 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2011/363/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3973400
58 A = 6764093
53 meter
Y = -1547814
12 meter E =
0023414
Z = 5263674
79 I = 51
28450
XDOT = 2129
668672 Wp = 214
57350
YDOT = 7343
851591 meter/sec RA = 257
03795 deg
ZDOT = 534
103185 TA = 230
19972
MA = 230
40608
Ha = 218
651 n
mi
Hp = 204
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13036091
13 X = 3964843
68
Y = -5078130
33 feet Y = -1503429
28 meter
Z = 17269274
26 Z = 5282956
37
XDOT = 6987
101941 XDOT = 2044
795446
YDOT = 24094
001284 feet/sec YDOT = 7367
192270 meter/sec
ZDOT = 1752
307038 ZDOT = 544
243232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12581189
00 X = 3834746
41
Y = 5891427
14 feet Y = 1795706
99 meter
Z = 17348189
61 Z = 5287728
19
XDOT = -12256
231669 XDOT = -3735
699413
YDOT = 20721
994538 feet/sec YDOT = 6316
063935 meter/sec
ZDOT = 1793
209359 ZDOT = 546
570213
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
65056591
00016717 00000-0 10270-3 0 9086
2 25544 51
6431 257
6404 0024139 221
2631 138
6700 15
58730985 31422
Satellite: ISS
Catalog Number: 25544
Epoch time: 11363
65056591 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 257
6404 deg
Eccentricity:
0024139
Arg of perigee: 221
2631 deg
Mean anomaly: 138
6700 deg
Mean motion: 15
58730985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 302
Coasting Arc #10 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2011/364/14:26:16
688
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4531200
12 A = 6766868
68 meter
Y = -2140682
78 meter E =
0021945
Z = -4550909
39 I = 51
30101
XDOT = 259
569105 Wp = 200
50109
YDOT = -7043
550598 meter/sec RA = 251
96524 deg
ZDOT = 3030
069931 TA = 100
02444
MA = 99
77674
Ha = 218
301 n
mi
Hp = 204
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14866142
13 X = -4484818
63
Y = -7023237
47 feet Y = -2191093
88 meter
Z = -14930805
07 Z = -4572809
10
XDOT = 851
604674 XDOT = 323
592873
YDOT = -23108
761803 feet/sec YDOT = -7040
290115 meter/sec
ZDOT = 9941
174314 ZDOT = 3031
486050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5334706
81 X = -1626018
64
Y = -15465858
43 feet Y = -4713993
65 meter
Z = -15020156
89 Z = -4578143
82
XDOT = 15920
558458 XDOT = 4852
586218
YDOT = -15230
487406 feet/sec YDOT = -4642
252561 meter/sec
ZDOT = 9947
468704 ZDOT = 3031
988461
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
61222325
00016717 00000-0 10270-3 0 9094
2 25544 51
6418 252
8109 0024208 225
1038 134
8153 15
58795117 31571
Satellite: ISS
Catalog Number: 25544
Epoch time: 11364
61222325 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 252
8109 deg
Eccentricity:
0024208
Arg of perigee: 225
1038 deg
Mean anomaly: 134
8153 deg
Mean motion: 15
58795117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3157
Checksum: 299
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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