[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 26th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26909 78 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 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
334/23:22:31
341 2
1 3
3 3
3
N/A 2
3 -0
3 224
4
000/00:01:02
681 0
9 -0
0 198
2
341/20:07:18
799 1
5 2
0 2
0
N/A 0
8 -0
2 223
5
000/00:00:37
598 1
0 -0
0 199
6
Coasting Arc #1 (Orbit 2578)
---------------------------------------
Vector Time (GMT): 2011/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3728049
58 A = 6764757
19 meter
Y = 2100032
57 meter E =
0033466
Z = 5210690
69 I = 51
96298
XDOT = -2426
545693 Wp = 87
74832
YDOT = -7215
574339 meter/sec RA = 78
29951 deg
ZDOT = 1166
823583 TA = 351
13171
MA = 351
19068
Ha = 225
240 n
mi
Hp = 196
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12231133
80 X = -3776568
71
Y = 6889870
64 feet Y = 2058071
68 meter
Z = 17095441
90 Z = 5192461
62
XDOT = -7961
107916 XDOT = -2351
347724
YDOT = -23673
144157 feet/sec YDOT = -7242
289067 meter/sec
ZDOT = 3828
161363 ZDOT = 1155
217412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -125915
22 X = -38378
96
Y = -14127988
80 feet Y = -4306210
99 meter
Z = 17020844
95 Z = 5187953
54
XDOT = 23570
046421 XDOT = 7184
150149
YDOT = 4365
809216 feet/sec YDOT = 1330
698649 meter/sec
ZDOT = 3781
276247 ZDOT = 1152
533000
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 11327
55012637
00016717 00000-0 10270-3 0 9000
2 25544 51
6418 78
7782 0030393 83
6752 276
7864 15
58605346 25791
Satellite: ISS
Catalog Number: 25544
Epoch time: 11327
55012637 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 78
7782 deg
Eccentricity:
0030393
Arg of perigee: 83
6752 deg
Mean anomaly: 276
7864 deg
Mean motion: 15
58605346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2579
Checksum: 335
Coasting Arc #2 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2011/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4455035
50 A = 6766172
54 meter
Y = 1474738
44 meter E =
0041909
Z = -4911012
60 I = 51
96123
XDOT = 222
392943 Wp = 92
53866
YDOT = 7256
577707 meter/sec RA = 73
27674 deg
ZDOT = 2396
658756 TA = 200
83017
MA = 201
00145
Ha = 225
094 n
mi
Hp = 196
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14616258
19 X = 4462070
94
Y = 4838380
72 feet Y = 1524597
12 meter
Z = -16112246
07 Z = -4889352
31
XDOT = 729
635639 XDOT = 129
589116
YDOT = 23807
669643 feet/sec YDOT = 7258
545549 meter/sec
ZDOT = 7863
053662 ZDOT = 2397
514339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11121481
88 X = -3389827
68
Y = 10779470
12 feet Y = 3285582
49 meter
Z = -16023890
58 Z = -4884081
85
XDOT = -20611
530196 XDOT = -6282
394404
YDOT = -9650
102004 feet/sec YDOT = -2941
351091 meter/sec
ZDOT = 7866
012044 ZDOT = 2397
560471
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 11328
51189443
00016717 00000-0 10270-3 0 9018
2 25544 51
6423 73
9525 0030525 87
0398 273
4249 15
58636234 25948
Satellite: ISS
Catalog Number: 25544
Epoch time: 11328
51189443 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 73
9525 deg
Eccentricity:
0030525
Arg of perigee: 87
0398 deg
Mean anomaly: 273
4249 deg
Mean motion: 15
58636234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 320
Coasting Arc #3 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2011/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4142479
63 A = 6773016
72 meter
Y = -4568605
95 meter E =
0043940
Z = 2758616
02 I = 51
97472
XDOT = 2271
151335 Wp = 93
66894
YDOT = -5221
718509 meter/sec RA = 68
27563 deg
ZDOT = -5169
614233 TA = 55
10925
MA = 54
69702
Ha = 225
131 n
mi
Hp = 196
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13590812
43 X = -4104485
80
Y = -14988864
67 feet Y = -4614717
56 meter
Z = 9050577
51 Z = 2738583
27
XDOT = 7451
283907 XDOT = 2354
486359
YDOT = -17131
622406 feet/sec YDOT = -5195
854603 meter/sec
ZDOT = -16960
676617 ZDOT = -5158
378894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19522120
21 X = 5950342
24
Y = -5452633
01 feet Y = -1661962
54 meter
Z = 8969103
39 Z = 2733782
71
XDOT = 11511
835013 XDOT = 3508
807312
YDOT = 13024
510474 feet/sec YDOT = 3969
870792 meter/sec
ZDOT = -16914
388750 ZDOT = -5155
505691
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 11329
53774256
00016717 00000-0 10270-3 0 9024
2 25544 51
6424 68
8030 0030578 90
8137 269
6522 15
58657062 26106
Satellite: ISS
Catalog Number: 25544
Epoch time: 11329
53774256 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 68
8030 deg
Eccentricity:
0030578
Arg of perigee: 90
8137 deg
Mean anomaly: 269
6522 deg
Mean motion: 15
58657062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 314
Coasting Arc #4 (Orbit 2625)
---------------------------------------
Vector Time (GMT): 2011/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2844444
05 A = 6775983
59 meter
Y = 6137327
98 meter E =
0040428
Z = 276188
62 I = 51
97394
XDOT = -4410
410175 Wp = 80
74214
YDOT = 1738
947440 meter/sec RA = 63
30414 deg
ZDOT = 6037
590502 TA = 282
22646
MA = 282
67893
Ha = 224
968 n
mi
Hp = 196
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9332165
52 X = 2774262
14
Y = 20135590
48 feet Y = 6168743
85 meter
Z = 906130
64 Z = 289837
36
XDOT = -14469
849656 XDOT = -4458
857547
YDOT = 5705
208135 feet/sec YDOT = 1689
355937 meter/sec
ZDOT = 19808
367789 ZDOT = 6016
046964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22188159
10 X = -6762950
89
Y = -337182
12 feet Y = -102773
11 meter
Z = 961402
13 Z = 293035
37
XDOT = 1166
779818 XDOT = 355
634489
YDOT = -14002
207213 feet/sec YDOT = -4267
872759 meter/sec
ZDOT = 19720
232943 ZDOT = 6010
727001
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 11330
56355174
00016717 00000-0 10270-3 0 9034
2 25544 51
6432 63
6548 0030520 94
1204 266
3441 15
58719670 26266
Satellite: ISS
Catalog Number: 25544
Epoch time: 11330
56355174 = yrday
fracday
Element set: 903
Inclination: 51
6432 deg
RA of node: 63
6548 deg
Eccentricity:
0030520
Arg of perigee: 94
1204 deg
Mean anomaly: 266
3441 deg
Mean motion: 15
58719670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2626
Checksum: 294
Coasting Arc #5 (Orbit 2640)
---------------------------------------
Vector Time (GMT): 2011/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -527041
25 A = 6771023
97 meter
Y = -5868012
62 meter E =
0035217
Z = -3362645
66 I = 51
94291
XDOT = 5651
312793 Wp = 96
70205
YDOT = 2157
329213 meter/sec RA = 58
32691 deg
ZDOT = -4696
487686 TA = 122
31380
MA = 121
97226
Ha = 224
831 n
mi
Hp = 196
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1729137
96 X = -445049
55
Y = -19252009
91 feet Y = -5873447
49 meter
Z = -11032302
04 Z = -3365007
57
XDOT = 18541
052470 XDOT = 5649
583948
YDOT = 7077
851750 feet/sec YDOT = 2220
516534 meter/sec
ZDOT = -15408
424166 ZDOT = -4669
037346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18181514
65 X = 5541725
66
Y = 6546729
18 feet Y = 1995443
05 meter
Z = -11041483
34 Z = -3365444
12
XDOT = -13747
820934 XDOT = -4190
335821
YDOT = 12636
547400 feet/sec YDOT = 3851
619647 meter/sec
ZDOT = -15296
462302 ZDOT = -4662
361710
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 11331
52521319
00016717 00000-0 10270-3 0 9048
2 25544 51
6426 58
8268 0030454 97
7885 262
6729 15
58776855 26417
Satellite: ISS
Catalog Number: 25544
Epoch time: 11331
52521319 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 58
8268 deg
Eccentricity:
0030454
Arg of perigee: 97
7885 deg
Mean anomaly: 262
6729 deg
Mean motion: 15
58776855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 339
Coasting Arc #6 (Orbit 2656)
---------------------------------------
Vector Time (GMT): 2011/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2088326
85 A = 6764440
99 meter
Y = 3888208
81 meter E =
0035022
Z = 5099223
27 I = 51
90512
XDOT = -5471
720215 Wp = 104
29773
YDOT = -5153
011394 meter/sec RA = 53
31517 deg
ZDOT = 1670
351689 TA = 329
59974
MA = 329
80236
Ha = 224
732 n
mi
Hp = 196
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6851466
04 X = -2156421
54
Y = 12756590
59 feet Y = 3864474
60 meter
Z = 16729735
13 Z = 5088913
14
XDOT = -17951
837976 XDOT = -5421
805840
YDOT = -16906
205361 feet/sec YDOT = -5213
920610 meter/sec
ZDOT = 5480
156460 ZDOT = 1643
890692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8876565
59 X = -2705577
19
Y = -11502074
70 feet Y = -3505832
37 meter
Z = 16687303
22 Z = 5086290
02
XDOT = 21879
057848 XDOT = 6668
736832
YDOT = -9004
568194 feet/sec YDOT = -2744
592386 meter/sec
ZDOT = 5372
474439 ZDOT = 1637
530209
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 11332
55094800
00016717 00000-0 10270-3 0 9053
2 25544 51
6428 53
6775 0030371 101
4073 259
0496 15
58873561 26575
Satellite: ISS
Catalog Number: 25544
Epoch time: 11332
55094800 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 53
6775 deg
Eccentricity:
0030371
Arg of perigee: 101
4073 deg
Mean anomaly: 259
0496 deg
Mean motion: 15
58873561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2657
Checksum: 312
Coasting Arc #7 (Orbit 2671)
---------------------------------------
Vector Time (GMT): 2011/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4468891
48 A = 6764904
99 meter
Y = -921174
75 meter E =
0043141
Z = -5033725
47 I = 51
88703
XDOT = 3602
531380 Wp = 104
37514
YDOT = 6429
268582 meter/sec RA = 48
28365 deg
ZDOT = 2025
851437 TA = 185
28879
MA = 185
33450
Ha = 224
599 n
mi
Hp = 196
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14661717
45 X = 4503313
05
Y = -3022226
88 feet Y = -871007
98 meter
Z = -16514847
35 Z = -5011932
04
XDOT = 11819
328674 XDOT = 3520
529046
YDOT = 21093
400858 feet/sec YDOT = 6469
095625 meter/sec
ZDOT = 6646
494216 ZDOT = 2043
153914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2924702
86 X = -891449
43
Y = 14781108
49 feet Y = 4505281
87 meter
Z = -16425740
22 Z = -5006565
62
XDOT = -22930
669064 XDOT = -6989
267931
YDOT = 2911
651764 feet/sec YDOT = 887
471458 meter/sec
ZDOT = 6716
656643 ZDOT = 2047
236945
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 11333
51254294
00016717 00000-0 10270-3 0 9066
2 25544 51
6421 48
8499 0030424 104
4922 255
9612 15
58901047 26725
Satellite: ISS
Catalog Number: 25544
Epoch time: 11333
51254294 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 48
8499 deg
Eccentricity:
0030424
Arg of perigee: 104
4922 deg
Mean anomaly: 255
9612 deg
Mean motion: 15
58901047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2672
Checksum: 305
Coasting Arc #8 (Orbit 2687)
---------------------------------------
Vector Time (GMT): 2011/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5669984
13 A = 6771595
33 meter
Y = -2127269
01 meter E =
0043488
Z = 2980111
94 I = 51
88915
XDOT = -468
292672 Wp = 104
46750
YDOT = -5830
840954 meter/sec RA = 43
27135 deg
ZDOT = -5003
189808 TA = 41
39615
MA = 41
06743
Ha = 224
548 n
mi
Hp = 196
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18602310
15 X = -5660252
03
Y = -6979229
03 feet Y = -2190620
03 meter
Z = 9777270
16 Z = 2952590
64
XDOT = -1536
393280 XDOT = -378
751643
YDOT = -19130
055624 feet/sec YDOT = -5835
576714 meter/sec
ZDOT = -16414
664723 ZDOT = -5005
247658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13404861
93 X = 4085801
92
Y = -14739329
13 feet Y = -4492547
52 meter
Z = 9665011
42 Z = 2945895
48
XDOT = 17223
633723 XDOT = 5249
763559
YDOT = 4786
716031 feet/sec YDOT = 1458
991046 meter/sec
ZDOT = -16422
593789 ZDOT = -5005
606587
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 11334
53820729
00016717 00000-0 10270-3 0 9072
2 25544 51
6422 43
6988 0030397 108
0532 252
3939 15
58967150 26885
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
53820729 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 43
6988 deg
Eccentricity:
0030397
Arg of perigee: 108
0532 deg
Mean anomaly: 252
3939 deg
Mean motion: 15
58967150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2688
Checksum: 331
Coasting Arc #9 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2011/334/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4296272
87 A = 6766403
65 meter
Y = -1514845
45 meter E =
0040484
Z = -5040115
07 I = 51
85641
XDOT = 4422
992375 Wp = 107
52391
YDOT = 5906
404912 meter/sec RA = 40
90518 deg
ZDOT = 1996
373922 TA = 181
86298
MA = 181
87810
Ha = 224
419 n
mi
Hp = 198
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14095383
43 X = 4337376
85
Y = -4969965
39 feet Y = -1466571
78 meter
Z = -16535810
60 Z = -5019144
00
XDOT = 14511
129840 XDOT = 4346
919024
YDOT = 19377
968872 feet/sec YDOT = 5955
440064 meter/sec
ZDOT = 6549
783208 ZDOT = 2017
676392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2934982
16 X = 894582
56
Y = -14751148
29 feet Y = -4496150
00 meter
Z = -16450012
95 Z = -5013963
95
XDOT = 22968
386671 XDOT = 7000
764257
YDOT = -2825
674803 feet/sec YDOT = -861
265680 meter/sec
ZDOT = 6636
324454 ZDOT = 2022
751694
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 11334
98692477
00016717 00000-0 10270-3 0 9089
2 25544 51
6432 41
4461 0027743 109
1990 251
2171 15
58372542 26958
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
98692477 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 41
4461 deg
Eccentricity:
0027743
Arg of perigee: 109
1990 deg
Mean anomaly: 251
2171 deg
Mean motion: 15
58372542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 321
Coasting Arc #10 (Orbit 2710)
---------------------------------------
Vector Time (GMT): 2011/335/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5853032
10 A = 6772764
22 meter
Y = -1183000
24 meter E =
0040398
Z = 3149036
49 I = 51
85421
XDOT = -1470
346567 Wp = 106
71998
YDOT = -5780
207190 meter/sec RA = 35
89419 deg
ZDOT = -4864
456332 TA = 36
90028
MA = 36
62300
Ha = 224
461 n
mi
Hp = 198
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19202861
21 X = -5854666
03
Y = -3881234
39 feet Y = -1248461
71 meter
Z = 10331484
55 Z = 3120598
36
XDOT = -4823
971677 XDOT = -1381
971150
YDOT = -18963
934351 feet/sec YDOT = -5796
155166 meter/sec
ZDOT = -15959
502402 ZDOT = -4871
384878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12881383
36 X = -3926245
65
Y = 14841457
69 feet Y = 4523676
30 meter
Z = 10215406
43 Z = 3113655
88
XDOT = -17745
663252 XDOT = -5408
878159
YDOT = -4306
818088 feet/sec YDOT = -1312
718153 meter/sec
ZDOT = -15987
327948 ZDOT = -4872
937558
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 11336
01293468
00016717 00000-0 10270-3 0 9093
2 25544 51
6429 36
2978 0027850 112
8793 247
5307 15
58412164 27113
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
01293468 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 36
2978 deg
Eccentricity:
0027850
Arg of perigee: 112
8793 deg
Mean anomaly: 247
5307 deg
Mean motion: 15
58412164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2711
Checksum: 320
Coasting Arc #11 (Orbit 2725)
---------------------------------------
Vector Time (GMT): 2011/336/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5917659
70 A = 6776639
45 meter
Y = 3298515
08 meter E =
0033045
Z = -267319
71 I = 51
84360
XDOT = -2121
876407 Wp = 96
31775
YDOT = 4243
250840 meter/sec RA = 30
91192 deg
ZDOT = 6020
918480 TA = 260
80820
MA = 261
18215
Ha = 224
159 n
mi
Hp = 198
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19414894
01 X = 5881633
83
Y = 10821899
88 feet Y = 3364488
56 meter
Z = -877033
17 Z = -238658
95
XDOT = -6961
536770 XDOT = -2198
416270
YDOT = 13921
426642 feet/sec YDOT = 4219
094540 meter/sec
ZDOT = 19753
669554 ZDOT = 6010
424585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18793613
27 X = 5728293
32
Y = -11876151
28 feet Y = -3619850
91 meter
Z = -760226
90 Z = -231717
16
XDOT = 7972
412902 XDOT = 2429
991452
YDOT = 11508
094440 feet/sec YDOT = 3507
667185 meter/sec
ZDOT = 19710
445857 ZDOT = 6007
743897
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 11336
97478560
00016717 00000-0 10270-3 0 9108
2 25544 51
6435 31
4716 0027661 116
4311 243
9687 15
58491850 27269
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
97478560 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 31
4716 deg
Eccentricity:
0027661
Arg of perigee: 116
4311 deg
Mean anomaly: 243
9687 deg
Mean motion: 15
58491850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2726
Checksum: 321
Coasting Arc #12 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2011/337/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4178059
00 A = 6773149
02 meter
Y = -4514248
87 meter E =
0032162
Z = -2838005
71 I = 51
80574
XDOT = 5416
574221 Wp = 119
43628
YDOT = -1837
246633 meter/sec RA = 25
93013 deg
ZDOT = -5110
601669 TA = 92
77663
MA = 92
40848
Ha = 224
004 n
mi
Hp = 198
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13707542
66 X = -4113482
61
Y = -14810527
79 feet Y = -4560609
32 meter
Z = -9311042
34 Z = -2858146
20
XDOT = 17770
912797 XDOT = 5461
542693
YDOT = -6027
712051 feet/sec YDOT = -1776
423552 meter/sec
ZDOT = -16767
065842 ZDOT = -5084
178564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19449643
93 X = -5928251
47
Y = 5237186
00 feet Y = 1596294
29 meter
Z = -9392933
65 Z = -2862966
18
XDOT = 3317
852771 XDOT = 1011
281525
YDOT = -17213
187131 feet/sec YDOT = -5246
579438 meter/sec
ZDOT = -16658
973135 ZDOT = -5077
655012
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 11338
00072760
00016717 00000-0 10270-3 0 9117
2 25544 51
6436 26
3224 0027528 120
4164 239
9716 15
58498928 27429
Satellite: ISS
Catalog Number: 25544
Epoch time: 11338
00072760 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 26
3224 deg
Eccentricity:
0027528
Arg of perigee: 120
4164 deg
Mean anomaly: 239
9716 deg
Mean motion: 15
58498928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 310
Coasting Arc #13 (Orbit 2757)
---------------------------------------
Vector Time (GMT): 2011/338/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1200557
80 A = 6766359
28 meter
Y = 4547878
89 meter E =
0034505
Z = 4846061
23 I = 51
75593
XDOT = -7257
614921 Wp = 122
56191
YDOT = -715
939438 meter/sec RA = 20
91775 deg
ZDOT = 2439
087367 TA = 303
45404
MA = 303
78347
Ha = 223
900 n
mi
Hp = 198
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3938837
94 X = 1126071
73
Y = 14920862
49 feet Y = 4560887
57 meter
Z = 15899151
02 Z = 4851712
89
XDOT = -23811
072577 XDOT = -7260
918517
YDOT = -2348
882671 feet/sec YDOT = -797
117124 meter/sec
ZDOT = 8002
255141 ZDOT = 2403
821413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15062355
77 X = 4591006
04
Y = 3248044
69 feet Y = 990004
02 meter
Z = 15921847
55 Z = 4852979
13
XDOT = -12549
616607 XDOT = -3825
123142
YDOT = 19181
538990 feet/sec YDOT = 5846
533084 meter/sec
ZDOT = 7858
261766 ZDOT = 2395
198186
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 11339
02663581
00016717 00000-0 10270-3 0 9128
2 25544 51
6437 21
1745 0027596 123
7273 236
6518 15
58570063 27585
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
02663581 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 21
1745 deg
Eccentricity:
0027596
Arg of perigee: 123
7273 deg
Mean anomaly: 236
6518 deg
Mean motion: 15
58570063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2758
Checksum: 317
Coasting Arc #14 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2011/339/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2391101
39 A = 6764762
80 meter
Y = -3611287
45 meter E =
0040444
Z = -5230600
94 I = 51
72175
XDOT = 6968
869503 Wp = 117
39328
YDOT = 2927
978108 meter/sec RA = 15
87676 deg
ZDOT = 1152
925138 TA = 163
74567
MA = 163
61557
Ha = 223
697 n
mi
Hp = 198
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7844820
84 X = 2456715
46
Y = -11848055
93 feet Y = -3584181
51 meter
Z = -17160764
23 Z = -5218825
64
XDOT = 22863
745089 XDOT = 6930
009546
YDOT = 9606
227389 feet/sec YDOT = 3005
690937 meter/sec
ZDOT = 3782
562788 ZDOT = 1186
686143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7246206
19 X = -2208643
65
Y = -12291027
41 feet Y = -3746305
15 meter
Z = -17112352
65 Z = -5215845
09
XDOT = 17643
131653 XDOT = 5377
626528
YDOT = -15911
200973 feet/sec YDOT = -4849
734057 meter/sec
ZDOT = 3920
211478 ZDOT = 1194
880458
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 11339
98839296
00016717 00000-0 10270-3 0 9132
2 25544 51
6432 16
3464 0027405 127
3499 233
0159 15
58635969 27739
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
98839296 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 16
3464 deg
Eccentricity:
0027405
Arg of perigee: 127
3499 deg
Mean anomaly: 233
0159 deg
Mean motion: 15
58635969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 345
Coasting Arc #15 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2011/340/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5313024
84 A = 6770323
77 meter
Y = 1938779
93 meter E =
0036611
Z = 3678753
52 I = 51
71188
XDOT = -4614
455764 Wp = 117
01439
YDOT = -4374
450284 meter/sec RA = 10
84799 deg
ZDOT = -4342
222071 TA = 18
98437
MA = 18
84824
Ha = 223
575 n
mi
Hp = 198
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17431183
85 X = -5352180
76
Y = 6360826
53 feet Y = 1879147
21 meter
Z = 12069401
31 Z = 3652847
50
XDOT = -15139
290564 XDOT = -4544
102799
YDOT = -14351
871010 feet/sec YDOT = -4425
658268 meter/sec
ZDOT = -14246
135403 ZDOT = -4364
468861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1514940
05 X = -461753
73
Y = 18562283
61 feet Y = 5657784
05 meter
Z = 11963415
74 Z = 3646449
12
XDOT = -17967
805447 XDOT = -5476
587100
YDOT = 7809
301058 feet/sec YDOT = 2380
274963 meter/sec
ZDOT = -14336
619455 ZDOT = -4369
801610
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 11341
01423507
00016717 00000-0 10270-3 0 9144
2 25544 51
6434 11
1977 0027295 130
9243 229
4282 15
58715990 27893
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
01423507 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 11
1977 deg
Eccentricity:
0027295
Arg of perigee: 130
9243 deg
Mean anomaly: 229
4282 deg
Mean motion: 15
58715990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 311
Coasting Arc #16 (Orbit 2801)
---------------------------------------
Vector Time (GMT): 2011/341/20:07:37
598
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4608575
18 A = 6769875
94 meter
Y = -2773120
05 meter E =
0032916
Z = -4147801
08 I = 51
68101
XDOT = 5576
568411 Wp = 128
24460
YDOT = 3633
317798 meter/sec RA = 6
51302 deg
ZDOT = 3767
379316 TA = 180
64516
MA = 180
64942
Ha = 223
501 n
mi
Hp = 199
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15119997
30 X = 4659391
79
Y = -9098162
89 feet Y = -2721299
63 meter
Z = -13608271
26 Z = -4125289
12
XDOT = 18295
828119 XDOT = 5517
223956
YDOT = 11920
333982 feet/sec YDOT = 3695
346251 meter/sec
ZDOT = 12360
168360 ZDOT = 3794
326853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11794963
26 X = 3595104
80
Y = -13220080
00 feet Y = -4029480
38 meter
Z = -13516074
12 Z = -4119699
39
XDOT = 19983
544583 XDOT = 6090
984389
YDOT = 5081
791714 feet/sec YDOT = 1548
930115 meter/sec
ZDOT = 12469
913370 ZDOT = 3800
829595
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 11341
84770983
00016717 00000-0 10270-3 0 9159
2 25544 51
6433 7
0136 0025982 134
2561 226
0732 15
58358728 28025
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
84770983 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 7
0136 deg
Eccentricity:
0025982
Arg of perigee: 134
2561 deg
Mean anomaly: 226
0732 deg
Mean motion: 15
58358728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2802
Checksum: 308
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:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
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:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- 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