[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 13th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 3512)
---------------------------------------
Vector Time (GMT): 2011/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1172741
95 A = 6717746
16 meter
Y = -4023090
40 meter E =
0011821
Z = -5260628
27 I = 51
56039
XDOT = 7481
900616 Wp = 89
14132
YDOT = -1764
969799 meter/sec RA = 348
61178 deg
ZDOT = -318
597640 TA = 177
83073
MA = 177
82560
Ha = 187
673 n
mi
Hp = 183
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3847578
58 X = -1102112
59
Y = -13199115
50 feet Y = -4035809
68 meter
Z = -17259279
11 Z = -5266154
00
XDOT = 24546
918031 XDOT = 7502
628464
YDOT = -5790
583330 feet/sec YDOT = -1681
186741 meter/sec
ZDOT = -1045
267847 ZDOT = -282
200188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12329422
82 X = -3758008
08
Y = -6020008
61 feet Y = -1834898
62 meter
Z = -17281436
73 Z = -5267381
91
XDOT = 11632
766410 XDOT = 3545
667202
YDOT = -21251
346404 feet/sec YDOT = -6477
410384 meter/sec
ZDOT = -897
897503 ZDOT = -273
679159
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 11131
51633707
00016717 00000-0 10270-3 0 9006
2 25544 51
6467 349
0443 0003233 261
6982 98
3807 15
74834115 35139
Satellite: ISS
Catalog Number: 25544
Epoch time: 11131
51633707 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 349
0443 deg
Eccentricity:
0003233
Arg of perigee: 261
6982 deg
Mean anomaly: 98
3807 deg
Mean motion: 15
74834115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3513
Checksum: 299
Coasting Arc #2 (Orbit 3528)
---------------------------------------
Vector Time (GMT): 2011/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6451837
24 A = 6729750
24 meter
Y = 1892637
99 meter E =
0010378
Z = -27713
53 I = 51
57129
XDOT = -1327
772769 Wp = 149
21061
YDOT = -4599
967511 meter/sec RA = 343
46365 deg
ZDOT = -6034
265026 TA = 31
09085
MA = 31
02948
Ha = 187
581 n
mi
Hp = 183
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21167445
01 X = -6472386
93
Y = 6209442
23 feet Y = 1820374
73 meter
Z = -90923
66 Z = -59106
63
XDOT = -4356
209872 XDOT = -1246
922829
YDOT = -15091
756927 feet/sec YDOT = -4614
363338 meter/sec
ZDOT = -19797
457436 ZDOT = -6040
519057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9156303
52 X = -2790841
31
Y = 20068401
30 feet Y = 6116848
72 meter
Z = -218044
29 Z = -66459
90
XDOT = -12721
823049 XDOT = -3877
611665
YDOT = -6004
891185 feet/sec YDOT = -1830
290833 meter/sec
ZDOT = -19822
533488 ZDOT = -6041
908207
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 11132
53162511
00016717 00000-0 10270-3 0 9010
2 25544 51
6469 343
8253 0003308 264
3983 95
6803 15
74852612 35291
Satellite: ISS
Catalog Number: 25544
Epoch time: 11132
53162511 = yrday
fracday
Element set: 901
Inclination: 51
6469 deg
RA of node: 343
8253 deg
Eccentricity:
0003308
Arg of perigee: 264
3983 deg
Mean anomaly: 95
6803 deg
Mean motion: 15
74852612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3529
Checksum: 305
Coasting Arc #3 (Orbit 3544)
---------------------------------------
Vector Time (GMT): 2011/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1136715
76 A = 6717551
06 meter
Y = 4039125
07 meter E =
0001226
Z = 5246652
71 I = 51
50084
XDOT = -7256
893493 Wp = 313
33032
YDOT = 2551
544266 meter/sec RA = 338
30937 deg
ZDOT = -391
284877 TA = 140
39593
MA = 140
38697
Ha = 187
428 n
mi
Hp = 183
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3729382
42 X = 1065977
45
Y = 13251722
68 feet Y = 4051440
92 meter
Z = 17213427
54 Z = 5252003
17
XDOT = -23808
705685 XDOT = -7282
985185
YDOT = 8371
208223 feet/sec YDOT = 2470
247395 meter/sec
ZDOT = -1283
743036 ZDOT = -426
602582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12493940
35 X = 3808153
02
Y = 5716562
11 feet Y = 1742408
13 meter
Z = 17234874
73 Z = 5253189
82
XDOT = -8423
468519 XDOT = -2567
473205
YDOT = 22719
258419 feet/sec YDOT = 6924
829966 meter/sec
ZDOT = -1426
769581 ZDOT = -434
879368
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 11133
54687551
00016717 00000-0 10270-3 0 9029
2 25544 51
6462 338
6043 0003380 269
6304 90
4473 15
74913913 35454
Satellite: ISS
Catalog Number: 25544
Epoch time: 11133
54687551 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 338
6043 deg
Eccentricity:
0003380
Arg of perigee: 269
6304 deg
Mean anomaly: 90
4473 deg
Mean motion: 15
74913913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3545
Checksum: 307
Coasting Arc #4 (Orbit 3560)
---------------------------------------
Vector Time (GMT): 2011/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6191179
29 A = 6729161
99 meter
Y = -2532684
52 meter E =
0011054
Z = 672493
52 I = 51
51120
XDOT = 1263
716489 Wp = 40
10053
YDOT = 4689
213454 meter/sec RA = 333
16661 deg
ZDOT = 5979
915078 TA = 327
24175
MA = 327
31025
Ha = 187
331 n
mi
Hp = 183
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20312268
02 X = 6215773
21
Y = -8309332
41 feet Y = -2463313
50 meter
Z = 2206343
58 Z = 702630
40
XDOT = 4146
051472 XDOT = 1182
137088
YDOT = 15384
558575 feet/sec YDOT = 4702
888793 meter/sec
ZDOT = 19619
143956 ZDOT = 5985
856282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6281497
86 X = 1914600
55
Y = -21014816
61 feet Y = -6405316
10 meter
Z = 2328402
20 Z = 709696
99
XDOT = 12970
483202 XDOT = 3953
403280
YDOT = 6069
235576 feet/sec YDOT = 1849
903004 meter/sec
ZDOT = 19642
946559 ZDOT = 5987
170111
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 11134
56208921
00016717 00000-0 10270-3 0 9033
2 25544 51
6449 333
3827 0003472 274
0789 85
9978 15
74984363 35614
Satellite: ISS
Catalog Number: 25544
Epoch time: 11134
56208921 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 333
3827 deg
Eccentricity:
0003472
Arg of perigee: 274
0789 deg
Mean anomaly: 85
9978 deg
Mean motion: 15
74984363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3561
Checksum: 341
Coasting Arc #5 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2011/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1062992
13 A = 6717609
93 meter
Y = -4182875
91 meter E =
0010864
Z = -5157318
82 I = 51
44474
XDOT = 6896
240743 Wp = 99
54215
YDOT = -3203
708648 meter/sec RA = 327
99408 deg
ZDOT = 1177
312101 TA = 181
73894
MA = 181
74272
Ha = 187
270 n
mi
Hp = 183
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3487507
00 X = -991085
62
Y = -13723346
18 feet Y = -4194360
61 meter
Z = -16920337
32 Z = -5162308
49
XDOT = 22625
461755 XDOT = 6925
833402
YDOT = -10510
855144 feet/sec YDOT = -3126
425299 meter/sec
ZDOT = 3862
572511 ZDOT = 1210
886373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12907678
81 X = -3934260
50
Y = -5762671
39 feet Y = -1756462
24 meter
Z = -16940312
77 Z = -5163407
33
XDOT = 5177
564846 XDOT = 1578
121765
YDOT = -23348
370188 feet/sec YDOT = -7116
583233 meter/sec
ZDOT = 3998
569797 ZDOT = 1218
764074
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 11135
51381926
00016717 00000-0 10270-3 0 9047
2 25544 51
6438 328
4872 0003429 277
5603 82
5171 15
75045967 35765
Satellite: ISS
Catalog Number: 25544
Epoch time: 11135
51381926 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 328
4872 deg
Eccentricity:
0003429
Arg of perigee: 277
5603 deg
Mean anomaly: 82
5171 deg
Mean motion: 15
75045967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3576
Checksum: 326
Coasting Arc #6 (Orbit 3591)
---------------------------------------
Vector Time (GMT): 2011/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5840704
48 A = 6728114
20 meter
Y = 3024179
74 meter E =
0006201
Z = -1400155
47 I = 51
45557
XDOT = -1160
518501 Wp = 163
41501
YDOT = -4923
992718 meter/sec RA = 322
86124 deg
ZDOT = -5806
364250 TA = 32
02424
MA = 31
98658
Ha = 187
178 n
mi
Hp = 183
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19162416
27 X = -5867285
51
Y = 9921849
53 feet Y = 2958716
93 meter
Z = -4593685
92 Z = -1428594
47
XDOT = -3807
475396 XDOT = -1077
164411
YDOT = -16154
831751 feet/sec YDOT = -4936
503795 meter/sec
ZDOT = -19049
751478 ZDOT = -5811
800099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3566553
03 X = -1087085
36
Y = 21256745
22 feet Y = 6479055
94 meter
Z = -4708898
80 Z = -1435272
35
XDOT = -13583
095655 XDOT = -4140
127556
YDOT = -6495
225781 feet/sec YDOT = -1979
744818 meter/sec
ZDOT = -19071
491277 ZDOT = -5812
990541
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 11136
52896185
00016717 00000-0 10270-3 0 9058
2 25544 51
6440 323
2665 0003536 284
0909 75
9862 15
75112183 35928
Satellite: ISS
Catalog Number: 25544
Epoch time: 11136
52896185 = yrday
fracday
Element set: 905
Inclination: 51
6440 deg
RA of node: 323
2665 deg
Eccentricity:
0003536
Arg of perigee: 284
0909 deg
Mean anomaly: 75
9862 deg
Mean motion: 15
75112183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3592
Checksum: 320
Coasting Arc #7 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2011/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 979911
39 A = 6718293
77 meter
Y = 4444226
71 meter E =
0004632
Z = 4942015
60 I = 51
39811
XDOT = -6452
211022 Wp = 20
49444
YDOT = 3685
161949 meter/sec RA = 317
67083 deg
ZDOT = -2029
765160 TA = 89
23786
MA = 89
18478
Ha = 187
157 n
mi
Hp = 183
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3214932
39 X = 906134
55
Y = 14580796
30 feet Y = 4454771
62 meter
Z = 16213961
95 Z = 4946597
38
XDOT = -21168
671332 XDOT = -6483
079265
YDOT = 12090
426341 feet/sec YDOT = 3612
837042 meter/sec
ZDOT = -6659
334513 ZDOT = -2061
185098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13634878
39 X = 4155910
93
Y = 6035850
98 feet Y = 1839727
38 meter
Z = 16232269
32 Z = 4947595
69
XDOT = -2175
161745 XDOT = -662
989300
YDOT = 23207
783156 feet/sec YDOT = 7073
732306 meter/sec
ZDOT = -6786
645327 ZDOT = -2068
569496
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 11137
54406845
00016717 00000-0 10270-3 0 9062
2 25544 51
6434 318
0440 0003552 285
6096 74
4675 15
75130220 36082
Satellite: ISS
Catalog Number: 25544
Epoch time: 11137
54406845 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 318
0440 deg
Eccentricity:
0003552
Arg of perigee: 285
6096 deg
Mean anomaly: 74
4675 deg
Mean motion: 15
75130220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 298
Coasting Arc #8 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2011/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5409898
62 A = 6726664
55 meter
Y = -3358695
64 meter E =
0011500
Z = 2148358
11 I = 51
40501
XDOT = 1096
342048 Wp = 59
63662
YDOT = 5290
146629 meter/sec RA = 312
54475 deg
ZDOT = 5493
660893 TA = 324
50659
MA = 324
58305
Ha = 187
063 n
mi
Hp = 183
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17749011
21 X = 5436617
65
Y = -11019342
66 feet Y = -3298049
76 meter
Z = 7048419
01 Z = 2174704
18
XDOT = 3596
922730 XDOT = 1010
417599
YDOT = 17356
124111 feet/sec YDOT = 5301
925441 meter/sec
ZDOT = 18023
821829 ZDOT = 5498
778968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1115588
37 X = 340031
34
Y = -20825279
16 feet Y = -6347545
09 meter
Z = 7155189
21 Z = 2180901
67
XDOT = 14705
315709 XDOT = 4482
180228
YDOT = 7005
281803 feet/sec YDOT = 2135
209894 meter/sec
ZDOT = 18044
255354 ZDOT = 5499
889032
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 11138
55913681
00016717 00000-0 10270-3 0 9076
2 25544 51
6432 312
8212 0003537 289
6355 70
4427 15
75211208 36249
Satellite: ISS
Catalog Number: 25544
Epoch time: 11138
55913681 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 312
8212 deg
Eccentricity:
0003537
Arg of perigee: 289
6355 deg
Mean anomaly: 70
4427 deg
Mean motion: 15
75211208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 299
Coasting Arc #9 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2011/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -952601
50 A = 6719346
90 meter
Y = -4812205
32 meter E =
0007107
Z = -4598676
97 I = 51
36143
XDOT = 5933
402670 Wp = 107
69046
YDOT = -3949
055133 meter/sec RA = 307
33944 deg
ZDOT = 2904
888189 TA = 191
19572
MA = 191
21154
Ha = 187
117 n
mi
Hp = 182
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3125333
02 X = -876380
01
Y = -15788075
19 feet Y = -4822431
07 meter
Z = -15087522
85 Z = -4603120
26
XDOT = 19466
544194 XDOT = 5963
009261
YDOT = -12956
217629 feet/sec YDOT = -3882
539091 meter/sec
ZDOT = 9530
473061 ZDOT = 2933
784220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14789254
31 X = -4507764
71
Y = -6306634
51 feet Y = -1922262
20 meter
Z = -15105253
69 Z = -4604081
32
XDOT = -357
308758 XDOT = -108
907709
YDOT = -22257
214647 feet/sec YDOT = -6783
999024 meter/sec
ZDOT = 9647
595222 ZDOT = 2940
587024
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 11139
51073002
00016717 00000-0 10270-3 0 9088
2 25544 51
6439 307
9254 0003458 293
8770 66
2032 15
75267513 36398
Satellite: ISS
Catalog Number: 25544
Epoch time: 11139
51073002 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 307
9254 deg
Eccentricity:
0003458
Arg of perigee: 293
8770 deg
Mean anomaly: 66
2032 deg
Mean motion: 15
75267513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 310
Coasting Arc #10 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2011/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4957226
73 A = 6724538
46 meter
Y = 3475104
38 meter E =
0001170
Z = -2928473
96 I = 51
36242
XDOT = -1088
211020 Wp = 82
55066
YDOT = -5758
213492 meter/sec RA = 302
22109 deg
ZDOT = -4992
509571 TA = 131
33133
MA = 131
32126
Ha = 187
126 n
mi
Hp = 182
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16263867
21 X = -4981491
55
Y = 11401261
10 feet Y = 3419534
40 meter
Z = -9607854
20 Z = -2952614
68
XDOT = -3570
246129 XDOT = -999
487943
YDOT = -18891
776547 feet/sec YDOT = -5769
885767 meter/sec
ZDOT = -16379
624578 ZDOT = -4997
581389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 738640
29 X = 225137
56
Y = 19800670
08 feet Y = 6035244
24 meter
Z = -9705713
19 Z = -2958301
38
XDOT = -16293
020694 XDOT = -4966
112708
YDOT = -7428
467591 feet/sec YDOT = -2264
196922 meter/sec
ZDOT = -16399
855535 ZDOT = -4998
675967
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 11140
52572550
00016717 00000-0 10270-3 0 9094
2 25544 51
6442 302
7036 0003563 300
8921 59
1893 15
75345368 36556
Satellite: ISS
Catalog Number: 25544
Epoch time: 11140
52572550 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 302
7036 deg
Eccentricity:
0003563
Arg of perigee: 300
8921 deg
Mean anomaly: 59
1893 deg
Mean motion: 15
75345368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 304
Coasting Arc #11 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2011/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 981631
16 A = 6721056
41 meter
Y = 5252499
59 meter E =
0008524
Z = 4073622
49 I = 51
33467
XDOT = -5417
103350 Wp = 58
62934
YDOT = 3956
964078 meter/sec RA = 297
00429 deg
ZDOT = -3786
505504 TA = 70
43245
MA = 70
34043
Ha = 187
125 n
mi
Hp = 182
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3220574
67 X = 903034
86
Y = 17232610
21 feet Y = 5263036
83 meter
Z = 13364903
18 Z = 4078200
99
XDOT = -17772
648787 XDOT = -5442
554141
YDOT = 12982
165610 feet/sec YDOT = 3896
244908 meter/sec
ZDOT = -12422
918321 ZDOT = -3812
883082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16278288
88 X = 4961622
45
Y = 6470212
10 feet Y = 1972120
65 meter
Z = 13383170
75 Z = 4079190
45
XDOT = 2100
790144 XDOT = 640
320836
YDOT = 20700
905591 feet/sec YDOT = 6309
636024 meter/sec
ZDOT = -12529
853004 ZDOT = -3819
099196
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 11141
54068425
00016717 00000-0 10270-3 0 9100
2 25544 51
6437 297
4808 0003570 302
6232 57
4587 15
75360808 36715
Satellite: ISS
Catalog Number: 25544
Epoch time: 11141
54068425 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 297
4808 deg
Eccentricity:
0003570
Arg of perigee: 302
6232 deg
Mean anomaly: 57
4587 deg
Mean motion: 15
75360808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 309
Coasting Arc #12 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2011/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4512579
33 A = 6722089
68 meter
Y = -3368189
19 meter E =
0008856
Z = 3662853
21 I = 51
32706
XDOT = 1188
526805 Wp = 83
61608
YDOT = 6280
727988 meter/sec RA = 291
88787 deg
ZDOT = 4303
293971 TA = 320
68402
MA = 320
74829
Ha = 186
946 n
mi
Hp = 182
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14805050
29 X = 4532114
26
Y = -11050489
46 feet Y = -3317617
95 meter
Z = 12017234
94 Z = 3684822
34
XDOT = 3899
366157 XDOT = 1097
301611
YDOT = 20606
062953 feet/sec YDOT = 6293
508295 meter/sec
ZDOT = 14118
418541 ZDOT = 4308
846893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1877778
39 X = -572346
85
Y = -18320158
80 feet Y = -5583984
40 meter
Z = 12106299
88 Z = 3690000
20
XDOT = 18289
784101 XDOT = 5574
726194
YDOT = 7486
750277 feet/sec YDOT = 2281
961485 meter/sec
ZDOT = 14140
587972 ZDOT = 4310
051214
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 11142
55560310
00016717 00000-0 10270-3 0 9113
2 25544 51
6445 292
2581 0003650 306
2648 53
8178 15
75459963 36879
Satellite: ISS
Catalog Number: 25544
Epoch time: 11142
55560310 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 292
2581 deg
Eccentricity:
0003650
Arg of perigee: 306
2648 deg
Mean anomaly: 53
8178 deg
Mean motion: 15
75459963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 316
Coasting Arc #13 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2011/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1121568
08 A = 6722906
97 meter
Y = -5699454
04 meter E =
0003258
Z = -3384025
93 I = 51
32052
XDOT = 4948
311529 Wp = 41
75556
YDOT = -3699
624621 meter/sec RA = 286
66727 deg
ZDOT = 4595
907472 TA = 278
09234
MA = 278
12930
Ha = 187
113 n
mi
Hp = 182
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3679685
30 X = -1041313
40
Y = -18698996
19 feet Y = -5711547
07 meter
Z = -11102447
29 Z = -3389280
05
XDOT = 16234
617876 XDOT = 4966
987654
YDOT = -12137
876054 feet/sec YDOT = -3644
185569 meter/sec
ZDOT = 15078
436588 ZDOT = 4619
991342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17997194
05 X = -5485544
74
Y = -6231120
81 feet Y = -1899245
62 meter
Z = -11123444
53 Z = -3390425
89
XDOT = -2881
986400 XDOT = -878
429455
YDOT = -18738
650417 feet/sec YDOT = -5711
540647 meter/sec
ZDOT = 15176
072197 ZDOT = 4625
666806
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 11143
50705637
00016717 00000-0 10270-3 0 9123
2 25544 51
6453 287
3624 0003674 312
1269 47
9583 15
75497505 37028
Satellite: ISS
Catalog Number: 25544
Epoch time: 11143
50705637 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 287
3624 deg
Eccentricity:
0003674
Arg of perigee: 312
1269 deg
Mean anomaly: 47
9583 deg
Mean motion: 15
75497505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 315
Coasting Arc #14 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2011/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4161420
21 A = 6719472
54 meter
Y = 3019130
94 meter E =
0008380
Z = -4335083
40 I = 51
30178
XDOT = -1384
264084 Wp = 44
28450
YDOT = -6771
178609 meter/sec RA = 281
54725 deg
ZDOT = -3384
938312 TA = 191
40176
MA = 191
42076
Ha = 187
160 n
mi
Hp = 182
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13652953
44 X = -4173812
40
Y = 9905285
22 feet Y = 2972526
43 meter
Z = -14222714
56 Z = -4355329
44
XDOT = -4541
548832 XDOT = -1292
001186
YDOT = -22215
152917 feet/sec YDOT = -6786
142182 meter/sec
ZDOT = -11105
440657 ZDOT = -3391
439431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2071383
41 X = 631357
66
Y = 16669910
85 feet Y = 5080988
83 meter
Z = -14304784
70 Z = -4360098
38
XDOT = -20378
460939 XDOT = -6211
354894
YDOT = -7025
452655 feet/sec YDOT = -2141
357969 meter/sec
ZDOT = -11131
444484 ZDOT = -3392
864279
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 11144
52190178
00016717 00000-0 10270-3 0 9135
2 25544 51
6453 282
1398 0003823 316
6111 43
4752 15
75559153 37184
Satellite: ISS
Catalog Number: 25544
Epoch time: 11144
52190178 = yrday
fracday
Element set: 913
Inclination: 51
6453 deg
RA of node: 282
1398 deg
Eccentricity:
0003823
Arg of perigee: 316
6111 deg
Mean anomaly: 43
4752 deg
Mean motion: 15
75559153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 303
Coasting Arc #15 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2011/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1322584
55 A = 6724914
57 meter
Y = 6104339
11 meter E =
0010989
Z = 2482147
41 I = 51
31531
XDOT = -4616
325351 Wp = 92
74724
YDOT = 3161
183366 meter/sec RA = 276
32935 deg
ZDOT = -5294
892782 TA = 59
01656
MA = 58
90865
Ha = 187
177 n
mi
Hp = 182
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4339188
15 X = 1242168
51
Y = 20027359
29 feet Y = 6118679
27 meter
Z = 8143528
24 Z = 2488377
59
XDOT = -15145
424379 XDOT = -4625
609538
YDOT = 10371
336501 feet/sec YDOT = 3109
509233 meter/sec
ZDOT = -17371
695479 ZDOT = -5317
341283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19691544
75 X = 6001982
84
Y = 5635585
81 feet Y = 1717726
55 meter
Z = 8168473
78 Z = 2489750
81
XDOT = 2486
712929 XDOT = 757
950101
YDOT = 16715
385285 feet/sec YDOT = 5094
849435 meter/sec
ZDOT = -17462
682378 ZDOT = -5322
625589
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 11145
53670930
00016717 00000-0 10270-3 0 9147
2 25544 51
6451 276
9160 0003829 320
4244 39
6640 15
75604953 37346
Satellite: ISS
Catalog Number: 25544
Epoch time: 11145
53670930 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 276
9160 deg
Eccentricity:
0003829
Arg of perigee: 320
4244 deg
Mean anomaly: 39
6640 deg
Mean motion: 15
75604953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3734
Checksum: 307
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