[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 13th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
292/16:08:51
107 -2
4 5
2 5
2
N/A -4
4 0
0 215
0
000/00:01:38
214 -1
2 0
1 204
3
299/12:44:31
303 -2
4 3
3 3
3
N/A -2
2 -0
0 216
3
000/00:01:02
605 0
3 0
0 203
6
Coasting Arc #1 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2011/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4581051
67 A = 6761200
92 meter
Y = 1724798
80 meter E =
0015913
Z = -4670913
04 I = 51
30168
XDOT = 165
264771 Wp = 358
61038
YDOT = -7147
354025 meter/sec RA = 289
51194 deg
ZDOT = -2785
492928 TA = 243
58699
MA = 243
75039
Ha = 213
282 n
mi
Hp = 204
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15029697
08 X = -4577307
35
Y = 5658788
72 feet Y = 1673591
16 meter
Z = -15324517
84 Z = -4693159
27
XDOT = 542
207253 XDOT = 258
707284
YDOT = -23449
324229 feet/sec YDOT = -7144
983735 meter/sec
ZDOT = -9138
756326 ZDOT = -2784
462395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12114828
70 X = 3692599
79
Y = -10409494
45 feet Y = -3172813
91 meter
Z = -15415183
49 Z = -4698547
93
XDOT = 6670
402641 XDOT = 2033
138725
YDOT = 21366
325446 feet/sec YDOT = 6512
455996 meter/sec
ZDOT = -9134
170407 ZDOT = -2784
095140
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 11285
52090073
00016717 00000-0 10270-3 0 9000
2 25544 51
6382 290
0832 0016267 319
3456 40
6484 15
60585804 19237
Satellite: ISS
Catalog Number: 25544
Epoch time: 11285
52090073 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 290
0832 deg
Eccentricity:
0016267
Arg of perigee: 319
3456 deg
Mean anomaly: 40
6484 deg
Mean motion: 15
60585804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 301
Coasting Arc #2 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2011/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3547023
58 A = 6759240
14 meter
Y = 2658228
65 meter E =
0016825
Z = 5111579
55 I = 51
28570
XDOT = -3005
881665 Wp = 339
28336
YDOT = 6899
761331 meter/sec RA = 284
41966 deg
ZDOT = -1488
340215 TA = 125
19201
MA = 125
03433
Ha = 213
442 n
mi
Hp = 203
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11637216
46 X = 3492203
46
Y = 8721222
62 feet Y = 2697587
54 meter
Z = 16770274
10 Z = 5128677
97
XDOT = -9861
816487 XDOT = -3075
582508
YDOT = 22637
012242 feet/sec YDOT = 6865
757882 meter/sec
ZDOT = -4883
005956 ZDOT = -1503
112954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13888991
25 X = -4233364
53
Y = -4030584
17 feet Y = -1228522
05 meter
Z = 16839742
80 Z = 5132753
61
XDOT = 811
828920 XDOT = 247
445455
YDOT = -23642
267035 feet/sec YDOT = -7206
162992 meter/sec
ZDOT = -4943
524472 ZDOT = -1506
786259
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 11286
54545722
00016717 00000-0 10270-3 0 9010
2 25544 51
6375 284
9241 0016290 323
2121 36
7916 15
60634344 19391
Satellite: ISS
Catalog Number: 25544
Epoch time: 11286
54545722 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 284
9241 deg
Eccentricity:
0016290
Arg of perigee: 323
2121 deg
Mean anomaly: 36
7916 deg
Mean motion: 15
60634344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1939
Checksum: 305
Coasting Arc #3 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2011/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1391261
11 A = 6766711
37 meter
Y = -5933023
67 meter E =
0016201
Z = -2917207
40 I = 51
30472
XDOT = 4641
793774 Wp = 343
25242
YDOT = -3542
503145 meter/sec RA = 279
35044 deg
ZDOT = 4999
351701 TA = 343
15912
MA = 343
21284
Ha = 213
594 n
mi
Hp = 203
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4564504
97 X = -1310641
90
Y = -19465300
75 feet Y = -5948131
02 meter
Z = -9570890
41 Z = -2923770
09
XDOT = 15228
982197 XDOT = 4656
775275
YDOT = -11622
385647 feet/sec YDOT = -3490
511683 meter/sec
ZDOT = 16402
072509 ZDOT = 5021
938632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11440588
30 X = 3487091
31
Y = 16381072
98 feet Y = 4992951
04 meter
Z = -9597289
70 Z = -2925253
90
XDOT = -8510
079873 XDOT = -2593
872345
YDOT = 15591
053463 feet/sec YDOT = 4752
153096 meter/sec
ZDOT = 16494
222918 ZDOT = 5027
439145
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 11287
50595029
00016717 00000-0 10270-3 0 9023
2 25544 51
6376 280
0887 0016282 327
1679 32
8464 15
60670611 19546
Satellite: ISS
Catalog Number: 25544
Epoch time: 11287
50595029 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 280
0887 deg
Eccentricity:
0016282
Arg of perigee: 327
1679 deg
Mean anomaly: 32
8464 deg
Mean motion: 15
60670611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 323
Coasting Arc #4 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2011/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1149982
27 A = 6769898
06 meter
Y = 6626539
35 meter E =
0006473
Z = -808325
30 I = 51
31187
XDOT = -4635
020581 Wp = 347
64569
YDOT = -1527
759108 meter/sec RA = 274
32208 deg
ZDOT = -5915
223727 TA = 201
14787
MA = 201
17464
Ha = 213
780 n
mi
Hp = 203
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3772907
72 X = -1220069
29
Y = 21740614
65 feet Y = 6613287
63 meter
Z = -2651985
89 Z = -814082
58
XDOT = -15206
760437 XDOT = -4588
856699
YDOT = -5012
333033 feet/sec YDOT = -1579
332899 meter/sec
ZDOT = -19406
901992 ZDOT = -5937
628922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4991800
62 X = -1521500
83
Y = -21490563
26 feet Y = -6550323
68 meter
Z = -2675781
09 Z = -815578
07
XDOT = 14284
234209 XDOT = 4353
834587
YDOT = -884
150328 feet/sec YDOT = -269
489020 meter/sec
ZDOT = -19498
042683 ZDOT = -5943
003410
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 11288
53044518
00016717 00000-0 10270-3 0 9030
2 25544 51
6373 274
9295 0016308 331
1214 28
9038 15
60735407 19703
Satellite: ISS
Catalog Number: 25544
Epoch time: 11288
53044518 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 274
9295 deg
Eccentricity:
0016308
Arg of perigee: 331
1214 deg
Mean anomaly: 28
9038 deg
Mean motion: 15
60735407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 307
Coasting Arc #5 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2011/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3250364
22 A = 6762656
75 meter
Y = -4253412
55 meter E =
0012418
Z = 4121592
68 I = 51
28682
XDOT = 3074
708177 Wp = 13
51040
YDOT = 5966
520248 meter/sec RA = 269
27975 deg
ZDOT = 3742
178210 TA = 37
91922
MA = 37
83183
Ha = 213
734 n
mi
Hp = 203
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10663924
62 X = 3277662
81
Y = -13954765
58 feet Y = -4216912
22 meter
Z = 13522285
71 Z = 4137449
70
XDOT = 10087
625254 XDOT = 2989
581680
YDOT = 19575
197663 feet/sec YDOT = 6000
427666 meter/sec
ZDOT = 12277
487566 ZDOT = 3756
908463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4031374
70 X = -1228763
01
Y = 17042487
33 feet Y = 5194550
14 meter
Z = 13587075
66 Z = 4141340
66
XDOT = -15834
866317 XDOT = -4826
467253
YDOT = -13556
470388 feet/sec YDOT = -4132
012174 meter/sec
ZDOT = 12337
148556 ZDOT = 3760
362880
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 11289
55490596
00016717 00000-0 10270-3 0 9045
2 25544 51
6371 269
7708 0016310 334
1850 25
8490 15
60798516 19869
Satellite: ISS
Catalog Number: 25544
Epoch time: 11289
55490596 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 269
7708 deg
Eccentricity:
0016310
Arg of perigee: 334
1850 deg
Mean anomaly: 25
8490 deg
Mean motion: 15
60798516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 338
Coasting Arc #6 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2011/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4245835
96 A = 6758005
89 meter
Y = -22773
15 meter E =
0016811
Z = -5264461
58 I = 51
27284
XDOT = -448
323969 Wp = 31
68355
YDOT = -7649
911146 meter/sec RA = 264
19091 deg
ZDOT = 409
334854 TA = 242
15181
MA = 242
32223
Ha = 213
932 n
mi
Hp = 202
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13929908
00 X = -4219691
52
Y = -74715
07 feet Y = -70106
63 meter
Z = -17271855
59 Z = -5285024
68
XDOT = -1470
879164 XDOT = -364
736343
YDOT = -25098
133682 feet/sec YDOT = -7654
457206 meter/sec
ZDOT = 1342
962119 ZDOT = 407
360077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12576918
65 X = 3833444
81
Y = -5741921
86 feet Y = -1750137
78 meter
Z = -17355586
00 Z = -5289982
61
XDOT = 11471
416140 XDOT = 3496
487639
YDOT = 21235
195358 feet/sec YDOT = 6472
487545 meter/sec
ZDOT = 1335
320092 ZDOT = 407
005564
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 11290
51530927
00016717 00000-0 10270-3 0 9057
2 25544 51
6371 264
9342 0016270 338
3639 21
6828 15
60814249 20016
Satellite: ISS
Catalog Number: 25544
Epoch time: 11290
51530927 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 264
9342 deg
Eccentricity:
0016270
Arg of perigee: 338
3639 deg
Mean anomaly: 21
6828 deg
Mean motion: 15
60814249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 297
Coasting Arc #7 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2011/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3768362
63 A = 6764155
79 meter
Y = 4319798
36 meter E =
0017730
Z = 3599884
01 I = 51
29821
XDOT = -2452
401104 Wp = 22
73217
YDOT = 5804
379750 meter/sec RA = 259
10825 deg
ZDOT = -4374
656148 TA = 114
31054
MA = 114
12529
Ha = 214
080 n
mi
Hp = 202
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12363394
45 X = 3702289
90
Y = 14172566
80 feet Y = 4361569
15 meter
Z = 11810643
09 Z = 3618030
36
XDOT = -8045
935380 XDOT = -2495
872985
YDOT = 19043
240649 feet/sec YDOT = 5776
712334 meter/sec
ZDOT = -14352
546417 ZDOT = -4386
675794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17240099
01 X = -5254782
18
Y = -7399218
39 feet Y = -2255281
77 meter
Z = 11884318
04 Z = 3622340
14
XDOT = -1675
194180 XDOT = -510
599186
YDOT = -19350
511761 feet/sec YDOT = -5898
035985 meter/sec
ZDOT = -14401
789934 ZDOT = -4389
665572
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 11291
53970473
00016717 00000-0 10270-3 0 9065
2 25544 51
6370 259
7750 0016360 341
9294 18
1279 15
60887840 20172
Satellite: ISS
Catalog Number: 25544
Epoch time: 11291
53970473 = yrday
fracday
Element set: 906
Inclination: 51
6370 deg
RA of node: 259
7750 deg
Eccentricity:
0016360
Arg of perigee: 341
9294 deg
Mean anomaly: 18
1279 deg
Mean motion: 15
60887840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 321
Coasting Arc #8 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2011/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1861315
72 A = 6769599
19 meter
Y = -6491649
38 meter E =
0024637
Z = -10699
26 I = 51
32369
XDOT = 4619
065913 Wp = 10
96735
YDOT = -1330
516391 meter/sec RA = 254
07376 deg
ZDOT = 6005
028888 TA = 348
91637
MA = 348
97055
Ha = 214
061 n
mi
Hp = 202
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6106678
86 X = -1788534
50
Y = -21298062
27 feet Y = -6512056
81 meter
Z = -35102
55 Z = -19564
64
XDOT = 15154
415726 XDOT = 4604
429066
YDOT = -4365
211257 feet/sec YDOT = -1278
944827 meter/sec
ZDOT = 19701
538345 ZDOT = 6027
433021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15059865
85 X = 4590247
11
Y = 16251019
39 feet Y = 4953310
71 meter
Z = -70883
07 Z = -21605
16
XDOT = -10263
148034 XDOT = -3128
207521
YDOT = 9580
963716 feet/sec YDOT = 2920
277741 meter/sec
ZDOT = 19792
845930 ZDOT = 6032
859439
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 11292
50004434
00016717 00000-0 10270-3 0 9079
2 25544 51
6369 254
9384 0016162 345
7612 14
3087 15
60944736 20326
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
50004434 = yrday
fracday
Element set: 907
Inclination: 51
6369 deg
RA of node: 254
9384 deg
Eccentricity:
0016162
Arg of perigee: 345
7612 deg
Mean anomaly: 14
3087 deg
Mean motion: 15
60944736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 299
Coasting Arc #9 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2011/292/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3393895
26 A = 6761192
71 meter
Y = 2886142
95 meter E =
0018236
Z = -5094687
41 I = 51
29128
XDOT = -3341
218129 Wp = 17
65349
YDOT = -6724
261719 meter/sec RA = 253
21098 deg
ZDOT = -1567
886856 TA = 237
07338
MA = 237
24891
Ha = 215
009 n
mi
Hp = 204
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11134826
95 X = -3401167
12
Y = 9468972
94 feet Y = 2848149
52 meter
Z = -16714853
70 Z = -5111192
86
XDOT = -10962
001737 XDOT = -3258
161197
YDOT = -22061
226112 feet/sec YDOT = -6761
160920 meter/sec
ZDOT = -5143
985748 ZDOT = -1583
916690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9354343
56 X = -2851203
92
Y = -11130391
45 feet Y = -3392543
31 meter
Z = -16782216
68 Z = -5115219
64
XDOT = 21360
914371 XDOT = 6510
806700
YDOT = -10021
540943 feet/sec YDOT = -3054
565679 meter/sec
ZDOT = -5208
934447 ZDOT = -1587
683219
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 11292
69211249
00016717 00000-0 10270-3 0 9084
2 25544 51
6405 253
9723 0016511 331
8485 28
1776 15
59987899 20351
Satellite: ISS
Catalog Number: 25544
Epoch time: 11292
69211249 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 253
9723 deg
Eccentricity:
0016511
Arg of perigee: 331
8485 deg
Mean anomaly: 28
1776 deg
Mean motion: 15
59987899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 339
Coasting Arc #10 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2011/293/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622261
75 A = 6762257
33 meter
Y = 1205205
84 meter E =
0018620
Z = 4794483
62 I = 51
30487
XDOT = 734
930562 Wp = 357
93535
YDOT = 7213
645161 meter/sec RA = 248
12543 deg
ZDOT = -2503
851007 TA = 116
88100
MA = 116
69057
Ha = 215
095 n
mi
Hp = 203
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15164900
75 X = 4585150
43
Y = 3954087
41 feet Y = 1256687
52 meter
Z = 15729933
14 Z = 4816848
55
XDOT = 2411
189508 XDOT = 666
374895
YDOT = 23666
814834 feet/sec YDOT = 7221
480175 meter/sec
ZDOT = -8214
734274 ZDOT = -2500
447539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3850284
10 X = -1173566
59
Y = 15096761
95 feet Y = 4601493
04 meter
Z = 15820964
24 Z = 4822229
90
XDOT = -22547
897594 XDOT = -6872
599187
YDOT = 2905
542334 feet/sec YDOT = 885
609303 meter/sec
ZDOT = -8201
220063 ZDOT = -2499
731875
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 11293
71707566
00016717 00000-0 10270-3 0 9091
2 25544 51
6401 248
8168 0016568 335
2976 24
7385 15
60049564 20514
Satellite: ISS
Catalog Number: 25544
Epoch time: 11293
71707566 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 248
8168 deg
Eccentricity:
0016568
Arg of perigee: 335
2976 deg
Mean anomaly: 24
7385 deg
Mean motion: 15
60049564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 329
Coasting Arc #11 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2011/294/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4382871
13 A = 6769839
47 meter
Y = -4613584
56 meter E =
0019630
Z = -2273178
08 I = 51
34323
XDOT = 2367
383608 Wp = 354
75802
YDOT = -4911
512842 meter/sec RA = 243
07235 deg
ZDOT = 5419
290843 TA = 339
72467
MA = 339
80252
Ha = 215
168 n
mi
Hp = 203
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14379498
46 X = -4319912
59
Y = -15136432
27 feet Y = -4662244
63 meter
Z = -7457933
33 Z = -2294317
02
XDOT = 7767
006588 XDOT = 2395
803002
YDOT = -16113
887276 feet/sec YDOT = -4884
880060 meter/sec
ZDOT = 17779
825600 ZDOT = 5430
861033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14786452
57 X = 4506910
74
Y = -14695371
35 feet Y = -4479149
19 meter
Z = -7543819
24 Z = -2299356
10
XDOT = 15221
557551 XDOT = 4639
530741
YDOT = 6190
211306 feet/sec YDOT = 1886
776406 meter/sec
ZDOT = 17827
181490 ZDOT = 5433
724918
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 11294
67794896
00016717 00000-0 10270-3 0 9101
2 25544 51
6404 243
9832 0016491 338
8331 21
2141 15
60073914 20664
Satellite: ISS
Catalog Number: 25544
Epoch time: 11294
67794896 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 243
9832 deg
Eccentricity:
0016491
Arg of perigee: 338
8331 deg
Mean anomaly: 21
2141 deg
Mean motion: 15
60073914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 309
Coasting Arc #12 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2011/295/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2558573
46 A = 6771292
16 meter
Y = 6130263
10 meter E =
0008546
Z = -1341880
12 I = 51
36281
XDOT = -4957
698126 Wp = 2
62262
YDOT = 799
789270 meter/sec RA = 238
05345 deg
ZDOT = -5792
194398 TA = 192
06162
MA = 192
08210
Ha = 215
345 n
mi
Hp = 203
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8394269
89 X = 2496352
17
Y = 20112411
74 feet Y = 6158526
63 meter
Z = -4402493
85 Z = -1329602
08
XDOT = -16265
413800 XDOT = -4938
135322
YDOT = 2623
980545 feet/sec YDOT = 744
458160 meter/sec
ZDOT = -19003
262459 ZDOT = -5816
231694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19747008
60 X = -6018888
22
Y = 9244672
26 feet Y = 2817776
10 meter
Z = -4352759
03 Z = -1326720
95
XDOT = -2614
104241 XDOT = -796
778973
YDOT = -14588
257008 feet/sec YDOT = -4446
500736 meter/sec
ZDOT = -19101
210351 ZDOT = -5822
048915
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 11295
70284693
00016717 00000-0 10270-3 0 9116
2 25544 51
6404 238
8275 0016330 342
1857 17
8724 15
60090939 20823
Satellite: ISS
Catalog Number: 25544
Epoch time: 11295
70284693 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 238
8275 deg
Eccentricity:
0016330
Arg of perigee: 342
1857 deg
Mean anomaly: 17
8724 deg
Mean motion: 15
60090939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 313
Coasting Arc #13 (Orbit 2097)
---------------------------------------
Vector Time (GMT): 2011/296/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 438615
77 A = 6763830
68 meter
Y = -5169178
52 meter E =
0013949
Z = 4327713
31 I = 51
35543
XDOT = 5986
188237 Wp = 22
50194
YDOT = 3378
726532 meter/sec RA = 233
01335 deg
ZDOT = 3437
977542 TA = 32
60031
MA = 32
51427
Ha = 215
429 n
mi
Hp = 203
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1439028
13 X = 475362
39
Y = -16959247
10 feet Y = -5164067
78 meter
Z = 14198534
47 Z = 4329933
87
XDOT = 19639
725186 XDOT = 5931
260419
YDOT = 11085
060799 feet/sec YDOT = 3445
360959 meter/sec
ZDOT = 11279
453878 ZDOT = 3466
925131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17008665
23 X = 5184241
16
Y = 358788
81 feet Y = 109358
83 meter
Z = 14207808
52 Z = 4330540
04
XDOT = -9895
406047 XDOT = -3016
119763
YDOT = 18946
071173 feet/sec YDOT = 5774
762493 meter/sec
ZDOT = 11397
222638 ZDOT = 3473
873460
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 11296
72770998
00016717 00000-0 10270-3 0 9128
2 25544 51
6404 233
6707 0016439 346
5922 13
4795 15
60154349 20980
Satellite: ISS
Catalog Number: 25544
Epoch time: 11296
72770998 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 233
6707 deg
Eccentricity:
0016439
Arg of perigee: 346
5922 deg
Mean anomaly: 13
4795 deg
Mean motion: 15
60154349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2098
Checksum: 332
Coasting Arc #14 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2011/297/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3541455
20 A = 6759702
12 meter
Y = 2355394
76 meter E =
0019135
Z = -5262945
04 I = 51
36136
XDOT = -4783
126783 Wp = 38
19669
YDOT = -5970
812910 meter/sec RA = 227
93428 deg
ZDOT = 562
248734 TA = 237
09547
MA = 237
27971
Ha = 215
414 n
mi
Hp = 202
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11618947
51 X = -3541963
53
Y = 7727673
09 feet Y = 2315788
71 meter
Z = -17266880
05 Z = -5280151
22
XDOT = -15692
673172 XDOT = -4718
735836
YDOT = -19589
281201 feet/sec YDOT = -6023
940685 meter/sec
ZDOT = 1844
648076 ZDOT = 539
168800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8575964
87 X = -2613954
09
Y = -10896819
18 feet Y = -3321350
49 meter
Z = -17337075
23 Z = -5284340
53
XDOT = 17550
120260 XDOT = 5349
276655
YDOT = -16515
458321 feet/sec YDOT = -5033
911696 meter/sec
ZDOT = 1750
888205 ZDOT = 533
670725
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 11297
68848612
00016717 00000-0 10270-3 0 9134
2 25544 51
6402 228
8365 0016428 349
5424 10
5388 15
60241282 21139
Satellite: ISS
Catalog Number: 25544
Epoch time: 11297
68848612 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 228
8365 deg
Eccentricity:
0016428
Arg of perigee: 349
5424 deg
Mean anomaly: 10
5388 deg
Mean motion: 15
60241282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 307
Coasting Arc #15 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2011/298/16:09:40
214
Vector Time (MET): N/A
Weight (LBS) : 870952
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5573017
37 A = 6765609
09 meter
Y = 1194988
31 meter E =
0019965
Z = 3652320
60 I = 51
40361
XDOT = 1538
272855 Wp = 29
54721
YDOT = 6142
807831 meter/sec RA = 222
86424 deg
ZDOT = -4329
875399 TA = 106
79729
MA = 106
57818
Ha = 215
486 n
mi
Hp = 202
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18284177
71 X = 5541497
81
Y = 3920565
31 feet Y = 1257133
24 meter
Z = 11982679
14 Z = 3679318
34
XDOT = 5046
826952 XDOT = 1490
502714
YDOT = 20153
568999 feet/sec YDOT = 6159
742319 meter/sec
ZDOT = -14205
627949 ZDOT = -4322
518782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2214006
27 X = -674829
11
Y = 18496850
51 feet Y = 5637840
04 meter
Z = 12092612
77 Z = 3685828
37
XDOT = -18240
704078 XDOT = -5559
766603
YDOT = 7142
184797 feet/sec YDOT = 2176
937926 meter/sec
ZDOT = -14175
925272 ZDOT = -4320
822023
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 11298
71328080
00016717 00000-0 10270-3 0 9142
2 25544 51
6407 223
6801 0016494 353
1385 6
9542 15
60317066 21294
Satellite: ISS
Catalog Number: 25544
Epoch time: 11298
71328080 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 223
6801 deg
Eccentricity:
0016494
Arg of perigee: 353
1385 deg
Mean anomaly: 6
9542 deg
Mean motion: 15
60317066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2129
Checksum: 300
Coasting Arc #16 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2011/299/12:45:02
605
Vector Time (MET): N/A
Weight (LBS) : 870646
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3346754
09 A = 6761348
13 meter
Y = 2678023
66 meter E =
0018549
Z = -5236841
35 I = 51
40267
XDOT = -5515
914515 Wp = 36
76077
YDOT = -5263
152842 meter/sec RA = 218
55246 deg
ZDOT = 849
767313 TA = 241
29418
MA = 241
48074
Ha = 216
330 n
mi
Hp = 203
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10980164
34 X = -3351011
20
Y = 8786166
86 feet Y = 2640574
13 meter
Z = -17181238
03 Z = -5253110
81
XDOT = -18096
832397 XDOT = -5460
779071
YDOT = -17267
561818 feet/sec YDOT = -5324
526857 meter/sec
ZDOT = 2787
950501 ZDOT = 823
104459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1475089
46 X = 449607
27
Y = -13903191
53 feet Y = -4237692
78 meter
Z = -17247639
07 Z = -5257080
39
XDOT = 24003
985817 XDOT = 7316
414877
YDOT = -711
924186 feet/sec YDOT = -216
994492 meter/sec
ZDOT = 2679
553492 ZDOT = 816
727904
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 11299
54590465
00016717 00000-0 10270-3 0 9153
2 25544 51
6403 219
4905 0016882 348
1185 11
9570 15
59714939 21421
Satellite: ISS
Catalog Number: 25544
Epoch time: 11299
54590465 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 219
4905 deg
Eccentricity:
0016882
Arg of perigee: 348
1185 deg
Mean anomaly: 11
9570 deg
Mean motion: 15
59714939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 328
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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