[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 10th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 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
There are no maneuvers
Coasting Arc #1 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2011/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 965038
51 A = 6771177
67 meter
Y = 6660595
20 meter E =
0016808
Z = -755563
48 I = 51
32205
XDOT = -4867
833548 Wp = 91
84185
YDOT = 45
798491 meter/sec RA = 256
59974 deg
ZDOT = -5928
550947 TA = 96
37435
MA = 96
18291
Ha = 215
692 n
mi
Hp = 200
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3166136
86 X = 894157
06
Y = 21852346
47 feet Y = 6670990
60 meter
Z = -2478882
82 Z = -751046
97
XDOT = -15970
582506 XDOT = -4839
184485
YDOT = 150
257517 feet/sec YDOT = -8
475878 meter/sec
ZDOT = -19450
626467 ZDOT = -5952
128944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12935636
95 X = 3942782
14
Y = -17897146
74 feet Y = -5455050
32 meter
Z = -2460846
23 Z = -750065
93
XDOT = 10175
636657 XDOT = 3101
534053
YDOT = 9990
130193 feet/sec YDOT = 3044
991683 meter/sec
ZDOT = -19546
421493 ZDOT = -5957
749271
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 11220
53065576
00016717 00000-0 10270-3 0 9000
2 25544 51
6391 257
2889 0012595 53
4815 306
7499 15
60307638 9080
Satellite: ISS
Catalog Number: 25544
Epoch time: 11220
53065576 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 257
2889 deg
Eccentricity:
0012595
Arg of perigee: 53
4815 deg
Mean anomaly: 306
7499 deg
Mean motion: 15
60307638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 908
Checksum: 324
Coasting Arc #2 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2011/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1606540
40 A = 6764659
91 meter
Y = -5223073
19 meter E =
0021982
Z = 3965204
02 I = 51
30691
XDOT = 4832
546692 Wp = 77
55465
YDOT = 4494
858322 meter/sec RA = 251
56294 deg
ZDOT = 3948
975314 TA = 331
24902
MA = 331
37001
Ha = 215
734 n
mi
Hp = 200
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5270801
83 X = 1645564
55
Y = -17136066
90 feet Y = -5204890
03 meter
Z = 13009199
54 Z = 3973102
77
XDOT = 15854
811982 XDOT = 4762
742111
YDOT = 14746
910506 feet/sec YDOT = 4548
508159 meter/sec
ZDOT = 12955
955754 ZDOT = 3972
282217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15508105
09 X = -4726870
43
Y = 8948883
15 feet Y = 2727619
59 meter
Z = 13041532
89 Z = 3975059
22
XDOT = -769
485030 XDOT = -234
539037
YDOT = -20418
301457 feet/sec YDOT = -6223
498284 meter/sec
ZDOT = 13050
450548 ZDOT = 3977
777327
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 11221
55541373
00016717 00000-0 10270-3 0 9018
2 25544 51
6378 252
1324 0012732 57
5483 302
6902 15
60304659 9244
Satellite: ISS
Catalog Number: 25544
Epoch time: 11221
55541373 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 252
1324 deg
Eccentricity:
0012732
Arg of perigee: 57
5483 deg
Mean anomaly: 302
6902 deg
Mean motion: 15
60304659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 286
Coasting Arc #3 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2011/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3874610
23 A = 6759422
73 meter
Y = 1714977
48 meter E =
0026612
Z = -5288956
73 I = 51
30099
XDOT = -3070
686395 Wp = 76
56617
YDOT = -7016
794051 meter/sec RA = 246
48303 deg
ZDOT = -19
716998 TA = 193
20990
MA = 193
27973
Ha = 215
748 n
mi
Hp = 200
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12711975
80 X = -3867807
28
Y = 5626566
53 feet Y = 1671687
67 meter
Z = -17352220
23 Z = -5307762
48
XDOT = -10074
430430 XDOT = -2991
899240
YDOT = -23020
977857 feet/sec YDOT = -7050
691814 meter/sec
ZDOT = -64
688314 ZDOT = -34
443212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13120715
62 X = 3999194
12
Y = 4294046
26 feet Y = 1308825
30 meter
Z = -17428715
25 Z = -5312272
41
XDOT = -7675
139936 XDOT = -2339
382653
YDOT = 22868
333404 feet/sec YDOT = 6970
268022 meter/sec
ZDOT = -124
219438 ZDOT = -37
862085
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 11222
51611278
00016717 00000-0 10270-3 0 9028
2 25544 51
6387 247
2983 0012564 60
6054 299
6355 15
60311462 9395
Satellite: ISS
Catalog Number: 25544
Epoch time: 11222
51611278 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 247
2983 deg
Eccentricity:
0012564
Arg of perigee: 60
6054 deg
Mean anomaly: 299
6355 deg
Mean motion: 15
60311462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 307
Coasting Arc #4 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2011/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4919175
10 A = 6764360
60 meter
Y = 2373094
30 meter E =
0023377
Z = 3977455
03 I = 51
32960
XDOT = 15
445688 Wp = 70
84176
YDOT = 6603
097104 meter/sec RA = 241
40257 deg
ZDOT = -3932
293095 TA = 60
22022
MA = 59
98792
Ha = 215
658 n
mi
Hp = 200
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16139025
91 X = 4872951
85
Y = 7785742
46 feet Y = 2427844
84 meter
Z = 13049393
14 Z = 4001239
62
XDOT = 50
674830 XDOT = -39
290715
YDOT = 21663
704408 feet/sec YDOT = 6602
964009 meter/sec
ZDOT = -12901
224064 ZDOT = -3932
350626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6959692
21 X = -2121314
19
Y = -16435303
91 feet Y = -5009480
63 meter
Z = 13145952
77 Z = 4006886
40
XDOT = 12969
603921 XDOT = 3953
135275
YDOT = -15880
619726 feet/sec YDOT = -4840
412893 meter/sec
ZDOT = -12901
738059 ZDOT = -3932
449760
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 11223
54084659
00016717 00000-0 10270-3 0 9030
2 25544 51
6369 242
1408 0012720 64
1331 296
1135 15
60375244 9556
Satellite: ISS
Catalog Number: 25544
Epoch time: 11223
54084659 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 242
1408 deg
Eccentricity:
0012720
Arg of perigee: 64
1331 deg
Mean anomaly: 296
1135 deg
Mean motion: 15
60375244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 290
Coasting Arc #5 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2011/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4215668
90 A = 6770886
89 meter
Y = -5234382
56 meter E =
0022310
Z = -764396
17 I = 51
36762
XDOT = 3344
534693 Wp = 55
68722
YDOT = -3540
908478 meter/sec RA = 236
36798 deg
ZDOT = 5938
144100 TA = 295
99506
MA = 296
22468
Ha = 215
683 n
mi
Hp = 200
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13830934
70 X = -4153110
50
Y = -17173171
14 feet Y = -5281174
93 meter
Z = -2507861
45 Z = -784723
56
XDOT = 10972
882851 XDOT = 3355
035616
YDOT = -11617
153800 feet/sec YDOT = -3503
449355 meter/sec
ZDOT = 19482
100067 ZDOT = 5954
416777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -531722
52 X = -162069
02
Y = 22034285
11 feet Y = 6716050
10 meter
Z = -2590266
77 Z = -789513
31
XDOT = -14182
243924 XDOT = -4322
747948
YDOT = 1904
951313 feet/sec YDOT = 580
629160 meter/sec
ZDOT = 19548
381220 ZDOT = 5958
346596
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 11224
50152508
00016717 00000-0 10270-3 0 9047
2 25544 51
6374 237
3069 0012674 68
3453 291
9052 15
60401578 9708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11224
50152508 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 237
3069 deg
Eccentricity:
0012674
Arg of perigee: 68
3453 deg
Mean anomaly: 291
9052 deg
Mean motion: 15
60401578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 299
Coasting Arc #6 (Orbit 985)
---------------------------------------
Vector Time (GMT): 2011/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1731462
21 A = 6767675
00 meter
Y = 5873281
33 meter E =
0016301
Z = -2898957
79 I = 51
37291
XDOT = -5747
313451 Wp = 83
19254
YDOT = -769
942089 meter/sec RA = 231
34537 deg
ZDOT = -5014
991268 TA = 130
01933
MA = 129
87616
Ha = 215
798 n
mi
Hp = 200
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5680650
30 X = 1679739
58
Y = 19269295
71 feet Y = 5892354
44 meter
Z = -9511016
37 Z = -2890672
12
XDOT = -18856
015259 XDOT = -5713
915394
YDOT = -2526
056723 feet/sec YDOT = -834
025244 meter/sec
ZDOT = -16453
383424 ZDOT = -5042
829850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7736112
36 X = 2357967
05
Y = -18557028
43 feet Y = -5656182
26 meter
Z = -9477565
03 Z = -2888761
82
XDOT = 11581
999116 XDOT = 3530
193331
YDOT = 13251
645586 feet/sec YDOT = 4039
101575 meter/sec
ZDOT = -16566
507671 ZDOT = -5049
471538
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 11225
52623643
00016717 00000-0 10270-3 0 9054
2 25544 51
6362 232
1485 0012683 71
6283 288
6252 15
60371719 9863
Satellite: ISS
Catalog Number: 25544
Epoch time: 11225
52623643 = yrday
fracday
Element set: 905
Inclination: 51
6362 deg
RA of node: 232
1485 deg
Eccentricity:
0012683
Arg of perigee: 71
6283 deg
Mean anomaly: 288
6252 deg
Mean motion: 15
60371719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 986
Checksum: 311
Coasting Arc #7 (Orbit 1001)
---------------------------------------
Vector Time (GMT): 2011/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1660960
21 A = 6760075
31 meter
Y = -4130041
07 meter E =
0016426
Z = 5073213
49 I = 51
36678
XDOT = 6058
366600 Wp = 88
93336
YDOT = 4447
603666 meter/sec RA = 226
28382 deg
ZDOT = 1632
976001 TA = 345
27105
MA = 345
31885
Ha = 215
725 n
mi
Hp = 200
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5449344
54 X = 1682375
55
Y = -13550003
50 feet Y = -4111347
43 meter
Z = 16644401
20 Z = 5081334
27
XDOT = 19876
530840 XDOT = 6000
249854
YDOT = 14591
875545 feet/sec YDOT = 4515
027079 meter/sec
ZDOT = 5357
532813 ZDOT = 1662
265626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12585979
09 X = -3836206
43
Y = 7333896
01 feet Y = 2235371
50 meter
Z = 16677564
02 Z = 5083321
51
XDOT = -6024
526972 XDOT = -1836
275821
YDOT = -22824
298379 feet/sec YDOT = -6956
846146 meter/sec
ZDOT = 5476
428436 ZDOT = 1669
215387
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 11226
55093556
00016717 00000-0 10270-3 0 9063
2 25544 51
6355 226
9908 0012698 74
9996 285
2565 15
60394901 10027
Satellite: ISS
Catalog Number: 25544
Epoch time: 11226
55093556 = yrday
fracday
Element set: 906
Inclination: 51
6355 deg
RA of node: 226
9908 deg
Eccentricity:
0012698
Arg of perigee: 74
9996 deg
Mean anomaly: 285
2565 deg
Mean motion: 15
60394901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1002
Checksum: 334
Coasting Arc #8 (Orbit 1016)
---------------------------------------
Vector Time (GMT): 2011/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4701149
76 A = 6761327
71 meter
Y = 961456
18 meter E =
0023378
Z = -4784116
63 I = 51
39309
XDOT = -3854
079432 Wp = 92
74524
YDOT = -6102
208955 meter/sec RA = 221
20085 deg
ZDOT = 2570
672783 TA = 202
63071
MA = 202
73396
Ha = 215
766 n
mi
Hp = 200
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15423719
69 X = -4688311
68
Y = 3154383
80 feet Y = 908956
74 meter
Z = -15695920
69 Z = -4806923
15
XDOT = -12644
617559 XDOT = -3798
044492
YDOT = -20020
370586 feet/sec YDOT = -6144
994262 meter/sec
ZDOT = 8433
965825 ZDOT = 2552
086304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14111724
24 X = 4301253
55
Y = 6766123
66 feet Y = 2062314
49 meter
Z = -15788666
89 Z = -4812385
67
XDOT = -1515
698653 XDOT = -461
984949
YDOT = 22591
505139 feet/sec YDOT = 6885
890766 meter/sec
ZDOT = 8358
625296 ZDOT = 2547
708990
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 11227
51157946
00016717 00000-0 10270-3 0 9075
2 25544 51
6358 222
1562 0012649 78
1634 282
0940 15
60392088 10177
Satellite: ISS
Catalog Number: 25544
Epoch time: 11227
51157946 = yrday
fracday
Element set: 907
Inclination: 51
6358 deg
RA of node: 222
1562 deg
Eccentricity:
0012649
Arg of perigee: 78
1634 deg
Mean anomaly: 282
0940 deg
Mean motion: 15
60392088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1017
Checksum: 306
Coasting Arc #9 (Orbit 1032)
---------------------------------------
Vector Time (GMT): 2011/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5995877
16 A = 6769115
70 meter
Y = 2346249
53 meter E =
0025785
Z = 2060972
77 I = 51
44304
XDOT = -167
836826 Wp = 96
87500
YDOT = 5334
059994 meter/sec RA = 216
15260 deg
ZDOT = -5527
803809 TA = 60
17975
MA = 59
92364
Ha = 215
653 n
mi
Hp = 200
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19671512
99 X = 5959183
66
Y = 7697669
07 feet Y = 2413093
99 meter
Z = 6761721
70 Z = 2090011
03
XDOT = -550
645756 XDOT = -200
618256
YDOT = 17500
196831 feet/sec YDOT = 5331
999687 meter/sec
ZDOT = -18135
839267 ZDOT = -5528
698927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11277118
69 X = -3437265
78
Y = -17816841
29 feet Y = -5430573
22 meter
Z = 6879692
82 Z = 2096930
37
XDOT = 9405
713373 XDOT = 2866
861436
YDOT = -13027
777002 feet/sec YDOT = -3970
866430 meter/sec
ZDOT = -18139
661378 ZDOT = -5528
968788
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 11228
53625386
00016717 00000-0 10270-3 0 9087
2 25544 51
6355 216
9976 0012662 81
3930 278
8660 15
60459678 10333
Satellite: ISS
Catalog Number: 25544
Epoch time: 11228
53625386 = yrday
fracday
Element set: 908
Inclination: 51
6355 deg
RA of node: 216
9976 deg
Eccentricity:
0012662
Arg of perigee: 81
3930 deg
Mean anomaly: 278
8660 deg
Mean motion: 15
60459678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1033
Checksum: 334
Coasting Arc #10 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2011/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4832235
20 A = 6769776
70 meter
Y = -4437018
47 meter E =
0026010
Z = 1631016
46 I = 51
47062
XDOT = 4395
092692 Wp = 74
43183
YDOT = -2660
688863 meter/sec RA = 211
14034 deg
ZDOT = 5714
308868 TA = 303
53225
MA = 303
78043
Ha = 215
613 n
mi
Hp = 200
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15853790
03 X = -4790183
53
Y = -14557147
22 feet Y = -4490820
30 meter
Z = 5351103
88 Z = 1607644
07
XDOT = 14419
595447 XDOT = 4396
759686
YDOT = -8729
294171 feet/sec YDOT = -2611
530755 meter/sec
ZDOT = 18747
732507 ZDOT = 5735
664061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4564037
73 X = 1391118
70
Y = 21057756
71 feet Y = 6418404
25 meter
Z = 5256229
47 Z = 1602098
74
XDOT = -15184
823779 XDOT = -4628
334288
YDOT = -1467
661360 feet/sec YDOT = -447
343183 meter/sec
ZDOT = 18834
643924 ZDOT = 5740
799468
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 11229
56091456
00016717 00000-0 10270-3 0 9097
2 25544 51
6355 211
8410 0012568 86
4816 273
7777 15
60502445 10495
Satellite: ISS
Catalog Number: 25544
Epoch time: 11229
56091456 = yrday
fracday
Element set: 909
Inclination: 51
6355 deg
RA of node: 211
8410 deg
Eccentricity:
0012568
Arg of perigee: 86
4816 deg
Mean anomaly: 273
7777 deg
Mean motion: 15
60502445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 316
Coasting Arc #11 (Orbit 1063)
---------------------------------------
Vector Time (GMT): 2011/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1459948
35 A = 6762083
04 meter
Y = 4776100
68 meter E =
0022391
Z = -4579775
80 I = 51
47104
XDOT = -7000
253821 Wp = 80
87486
YDOT = -749
614793 meter/sec RA = 206
10139 deg
ZDOT = -3022
463223 TA = 158
88805
MA = 158
79548
Ha = 215
698 n
mi
Hp = 200
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4789856
78 X = 1428680
04
Y = 15669621
66 feet Y = 4792251
76 meter
Z = -15025511
16 Z = -4572759
52
XDOT = -22966
712010 XDOT = -6976
668780
YDOT = -2459
366120 feet/sec YDOT = -827
764114 meter/sec
ZDOT = -9916
217924 ZDOT = -3056
412788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4794074
56 X = 1461233
93
Y = -15695487
87 feet Y = -4783984
70 meter
Z = -14997141
93 Z = -4571128
86
XDOT = 16396
355134 XDOT = 4997
609045
YDOT = 14586
255231 feet/sec YDOT = 4445
890594 meter/sec
ZDOT = -10054
228264 ZDOT = -3064
528775
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 11230
52152544
00016717 00000-0 10270-3 0 9103
2 25544 51
6356 207
0046 0012653 89
0406 271
2199 15
60463505 10648
Satellite: ISS
Catalog Number: 25544
Epoch time: 11230
52152544 = yrday
fracday
Element set: 910
Inclination: 51
6356 deg
RA of node: 207
0046 deg
Eccentricity:
0012653
Arg of perigee: 89
0406 deg
Mean anomaly: 271
2199 deg
Mean motion: 15
60463505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1064
Checksum: 275
Coasting Arc #12 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2011/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2704138
49 A = 6759293
69 meter
Y = -3376681
92 meter E =
0015821
Z = 5180287
01 I = 51
48984
XDOT = 6708
977055 Wp = 84
44200
YDOT = 3574
330350 meter/sec RA = 201
02645 deg
ZDOT = -1167
689098 TA = 16
77216
MA = 16
71990
Ha = 215
533 n
mi
Hp = 200
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8871845
43 X = 2716531
53
Y = -11078352
74 feet Y = -3346373
21 meter
Z = 16995692
28 Z = 5193453
76
XDOT = 22011
079578 XDOT = 6674
181945
YDOT = 11726
805611 feet/sec YDOT = 3649
159659 meter/sec
ZDOT = -3831
000978 ZDOT = -1135
181729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13411222
74 X = -4087740
69
Y = 4444337
13 feet Y = 1354633
96 meter
Z = 17049342
18 Z = 5196639
50
XDOT = -11654
048300 XDOT = -3552
153922
YDOT = -20920
081937 feet/sec YDOT = -6376
440975 meter/sec
ZDOT = -3698
937301 ZDOT = -1127
436089
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 11231
54616167
00016717 00000-0 10270-3 0 9113
2 25544 51
6356 201
8474 0012528 92
4585 267
8005 15
60491681 10803
Satellite: ISS
Catalog Number: 25544
Epoch time: 11231
54616167 = yrday
fracday
Element set: 911
Inclination: 51
6356 deg
RA of node: 201
8474 deg
Eccentricity:
0012528
Arg of perigee: 92
4585 deg
Mean anomaly: 267
8005 deg
Mean motion: 15
60491681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 300
Coasting Arc #13 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2011/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5876893
18 A = 6766342
87 meter
Y = 980388
40 meter E =
0017121
Z = -3222614
83 I = 51
54239
XDOT = -3427
372689 Wp = 92
69246
YDOT = -4924
194659 meter/sec RA = 195
97010 deg
ZDOT = 4773
378904 TA = 229
89552
MA = 230
04570
Ha = 215
583 n
mi
Hp = 200
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19281145
61 X = -5871764
52
Y = 3216497
39 feet Y = 914698
06 meter
Z = -10572883
29 Z = -3251152
12
XDOT = -11244
661052 XDOT = -3395
242707
YDOT = -16155
494289 feet/sec YDOT = -4962
341965 meter/sec
ZDOT = 15660
691942 ZDOT = 4756
806905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17960192
76 X = 5474266
75
Y = 7554588
81 feet Y = 2302638
67 meter
Z = -10688964
22 Z = -3257996
30
XDOT = 1498
157854 XDOT = 456
638514
YDOT = 18404
435213 feet/sec YDOT = 5609
671853 meter/sec
ZDOT = 15593
463215 ZDOT = 4752
887588
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 11232
50674573
00016717 00000-0 10270-3 0 9126
2 25544 51
6357 197
0125 0012578 95
7372 264
5219 15
60497839 10956
Satellite: ISS
Catalog Number: 25544
Epoch time: 11232
50674573 = yrday
fracday
Element set: 912
Inclination: 51
6357 deg
RA of node: 197
0125 deg
Eccentricity:
0012578
Arg of perigee: 95
7372 deg
Mean anomaly: 264
5219 deg
Mean motion: 15
60497839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 326
Coasting Arc #14 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2011/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6554453
86 A = 6770696
64 meter
Y = 1616797
40 meter E =
0022494
Z = -430423
33 I = 51
58721
XDOT = -1500
980426 Wp = 118
03101
YDOT = 4554
286980 meter/sec RA = 190
95868 deg
ZDOT = -5998
552341 TA = 66
62682
MA = 66
39037
Ha = 215
524 n
mi
Hp = 200
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21504113
72 X = 6537978
28
Y = 5304453
41 feet Y = 1690001
19 meter
Z = -1412150
02 Z = -398622
01
XDOT = -4924
476462 XDOT = -1522
656112
YDOT = 14941
886416 feet/sec YDOT = 4537
380957 meter/sec
ZDOT = -19680
289834 ZDOT = -6005
896664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15617940
45 X = -4760348
25
Y = -15715994
57 feet Y = -4790235
14 meter
Z = -1282868
37 Z = -391018
28
XDOT = 10727
476850 XDOT = 3269
734944
YDOT = -9125
030005 feet/sec YDOT = -2781
309146 meter/sec
ZDOT = -19710
309662 ZDOT = -6007
702385
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 11233
53135535
00016717 00000-0 10270-3 0 9131
2 25544 51
6364 191
8540 0012481 99
4835 260
7733 15
60537832 11111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11233
53135535 = yrday
fracday
Element set: 913
Inclination: 51
6364 deg
RA of node: 191
8540 deg
Eccentricity:
0012481
Arg of perigee: 99
4835 deg
Mean anomaly: 260
7733 deg
Mean motion: 15
60537832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 296
Coasting Arc #15 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2011/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4359492
00 A = 6764505
61 meter
Y = -3486040
43 meter E =
0023901
Z = 3804643
27 I = 51
59694
XDOT = 5848
322442 Wp = 100
99389
YDOT = -2722
443479 meter/sec RA = 185
94389 deg
ZDOT = 4180
046490 TA = 304
95324
MA = 305
17749
Ha = 215
454 n
mi
Hp = 200
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14302795
28 X = -4338668
52
Y = -11437140
52 feet Y = -3534674
58 meter
Z = 12482425
44 Z = 3783515
55
XDOT = 19187
409586 XDOT = 5858
024936
YDOT = -8931
901177 feet/sec YDOT = -2656
989801 meter/sec
ZDOT = 13714
063289 ZDOT = 4208
480912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6630972
70 X = 2021120
48
Y = 17133109
94 feet Y = 5222171
91 meter
Z = 12396605
41 Z = 3778485
33
XDOT = -19749
969741 XDOT = -6019
790777
YDOT = -2426
563960 feet/sec YDOT = -739
616695 meter/sec
ZDOT = 13829
809179 ZDOT = 4215
325838
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 11234
55594971
00016717 00000-0 10270-3 0 9148
2 25544 51
6366 186
6973 0012407 104
0451 256
2085 15
60588295 11276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11234
55594971 = yrday
fracday
Element set: 914
Inclination: 51
6366 deg
RA of node: 186
6973 deg
Eccentricity:
0012407
Arg of perigee: 104
0451 deg
Mean anomaly: 256
2085 deg
Mean motion: 15
60588295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 318
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