[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 3rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 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 2508)
---------------------------------------
Vector Time (GMT): 2012/214/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3612551
55 A = 6784089
30 meter
Y = 5092565
81 meter E =
0013180
Z = 2639622
96 I = 51
30926
XDOT = -2972
707268 Wp = 96
14276
YDOT = 4807
731253 meter/sec RA = 254
43953 deg
ZDOT = -5186
071523 TA = 53
93120
MA = 53
80919
Ha = 219
777 n
mi
Hp = 213
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11852203
23 X = 3542514
57
Y = 16707893
09 feet Y = 5132571
84 meter
Z = 8660180
31 Z = 2657002
35
XDOT = -9752
976601 XDOT = -3001
055243
YDOT = 15773
396500 feet/sec YDOT = 4774
330431 meter/sec
ZDOT = -17014
670351 ZDOT = -5200
580978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11415631
73 X = -3479484
55
Y = -16972725
44 feet Y = -5173286
71 meter
Z = 8731384
74 Z = 2661326
07
XDOT = 8767
671522 XDOT = 2672
386280
YDOT = -14716
116853 feet/sec YDOT = -4485
472417 meter/sec
ZDOT = -17074
983824 ZDOT = -5204
455070
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 12214
67328089
00016717 00000-0 10270-3 0 9000
2 25544 51
6378 255
1479 0001494 354
3794 5
7342 15
54898034 25092
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
67328089 = yrday
fracday
Element set: 900
Inclination: 51
6378 deg
RA of node: 255
1479 deg
Eccentricity:
0001494
Arg of perigee: 354
3794 deg
Mean anomaly: 5
7342 deg
Mean motion: 15
54898034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2509
Checksum: 326
Coasting Arc #2 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2012/215/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2959240
59 A = 6786714
13 meter
Y = -6047740
68 meter E =
0011288
Z = -808158
83 I = 51
32683
XDOT = 4026
343405 Wp = 35
79868
YDOT = -2754
237038 meter/sec RA = 249
43982 deg
ZDOT = 5918
600097 TA = 315
42094
MA = 315
51168
Ha = 219
799 n
mi
Hp = 213
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9708794
59 X = -2887467
82
Y = -19841668
88 feet Y = -6080431
40 meter
Z = -2651439
73 Z = -822360
25
XDOT = 13209
788075 XDOT = 4028
092105
YDOT = -9036
210753 feet/sec YDOT = -2709
202430 meter/sec
ZDOT = 19417
979320 ZDOT = 5938
163535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9581852
07 X = 2920548
51
Y = 19895466
42 feet Y = 6064138
17 meter
Z = -2709460
44 Z = -825843
54
XDOT = -11690
116170 XDOT = -3563
147409
YDOT = 8263
257455 feet/sec YDOT = 2518
640872 meter/sec
ZDOT = 19498
943719 ZDOT = 5943
278045
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 12215
63734196
00016717 00000-0 10270-3 0 9018
2 25544 51
6371 250
3365 0001286 3
6881 356
4282 15
54928107 25247
Satellite: ISS
Catalog Number: 25544
Epoch time: 12215
63734196 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 250
3365 deg
Eccentricity:
0001286
Arg of perigee: 3
6881 deg
Mean anomaly: 356
4282 deg
Mean motion: 15
54928107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 299
Coasting Arc #3 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2012/216/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2004769
86 A = 6786450
64 meter
Y = 6372948
02 meter E =
0008181
Z = -1175726
32 I = 51
33740
XDOT = -4946
119902 Wp = 134
86345
YDOT = 484
471873 meter/sec RA = 244
44347 deg
ZDOT = -5838
408826 TA = 57
96123
MA = 57
88178
Ha = 219
877 n
mi
Hp = 213
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6577328
95 X = 1939068
53
Y = 20908622
10 feet Y = 6394999
27 meter
Z = -3857369
80 Z = -1166146
92
XDOT = -16227
427499 XDOT = -4922
808741
YDOT = 1589
474650 feet/sec YDOT = 429
291738 meter/sec
ZDOT = -19154
884599 ZDOT = -5862
379670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6843663
62 X = -2085948
67
Y = -20830143
61 feet Y = -6349027
77 meter
Z = -3818431
81 Z = -1163858
02
XDOT = 14571
502013 XDOT = 4441
393814
YDOT = -1276
569013 feet/sec YDOT = -389
098235 meter/sec
ZDOT = -19253
823424 ZDOT = -5868
565380
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 12216
66565931
00016717 00000-0 10270-3 0 9022
2 25544 51
6370 245
2024 0001566 3
6632 356
4532 15
54920106 25403
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
66565931 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 245
2024 deg
Eccentricity:
0001566
Arg of perigee: 3
6632 deg
Mean anomaly: 356
4532 deg
Mean motion: 15
54920106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2540
Checksum: 279
Coasting Arc #4 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2012/217/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -804924
60 A = 6783136
69 meter
Y = -6037326
52 meter E =
0013476
Z = 2970281
43 I = 51
34073
XDOT = 5606
703101 Wp = 76
85326
YDOT = 1698
535639 meter/sec RA = 239
44330 deg
ZDOT = 4955
796673 TA = 317
29439
MA = 317
39904
Ha = 219
736 n
mi
Hp = 213
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2640828
76 X = -751782
83
Y = -19807501
70 feet Y = -6046030
56 meter
Z = 9745017
80 Z = 2966500
28
XDOT = 18394
695213 XDOT = 5563
219354
YDOT = 5572
623488 feet/sec YDOT = 1760
990136 meter/sec
ZDOT = 16259
175436 ZDOT = 4982
927634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3270380
80 X = 996812
07
Y = 19720775
35 feet Y = 6010892
33 meter
Z = 9729958
93 Z = 2965691
48
XDOT = -17010
014172 XDOT = -5184
652320
YDOT = -5282
276312 feet/sec YDOT = -1610
037820 meter/sec
ZDOT = 16370
960481 ZDOT = 4989
868755
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 12217
69396034
00016717 00000-0 10270-3 0 9033
2 25544 51
6369 240
0696 0001406 1
2226 358
8930 15
54975080 25561
Satellite: ISS
Catalog Number: 25544
Epoch time: 12217
69396034 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 240
0696 deg
Eccentricity:
0001406
Arg of perigee: 1
2226 deg
Mean anomaly: 358
8930 deg
Mean motion: 15
54975080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2556
Checksum: 308
Coasting Arc #5 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2012/218/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -636160
48 A = 6778766
64 meter
Y = 5139549
45 meter E =
0009834
Z = -4384289
40 I = 51
34262
XDOT = -5873
146720 Wp = 61
45672
YDOT = -3592
152660 meter/sec RA = 234
42987 deg
ZDOT = -3359
904640 TA = 174
37884
MA = 174
36780
Ha = 219
877 n
mi
Hp = 213
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2087140
67 X = -672287
14
Y = 16862038
89 feet Y = 5132233
49 meter
Z = -14384151
57 Z = -4387467
57
XDOT = -19268
854069 XDOT = -5816
220622
YDOT = -11785
277756 feet/sec YDOT = -3657
511569 meter/sec
ZDOT = -11023
309186 ZDOT = -3388
297377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1221002
03 X = 372161
42
Y = -16935264
70 feet Y = -5161868
68 meter
Z = -14397718
28 Z = -4388424
53
XDOT = 18488
283505 XDOT = 5635
228812
YDOT = 10800
710841 feet/sec YDOT = 3292
056664 meter/sec
ZDOT = -11140
141065 ZDOT = -3395
514997
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 12218
65798242
00016717 00000-0 10270-3 0 9048
2 25544 51
6372 235
2563 0001622 9
1570 350
9612 15
54955882 25718
Satellite: ISS
Catalog Number: 25544
Epoch time: 12218
65798242 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 235
2563 deg
Eccentricity:
0001622
Arg of perigee: 9
1570 deg
Mean anomaly: 350
9612 deg
Mean motion: 15
54955882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2571
Checksum: 310
Coasting Arc #6 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2012/219/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2177060
15 A = 6775419
93 meter
Y = -3804864
00 meter E =
0003845
Z = 5163116
35 I = 51
35079
XDOT = 5663
917973 Wp = 102
56059
YDOT = 5009
639442 meter/sec RA = 229
40622 deg
ZDOT = 1301
893328 TA = 334
88188
MA = 334
90058
Ha = 219
720 n
mi
Hp = 213
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7142585
80 X = 2194364
17
Y = -12483149
59 feet Y = -3780421
97 meter
Z = 16939358
12 Z = 5173734
34
XDOT = 18582
408047 XDOT = 5601
153969
YDOT = 16435
824942 feet/sec YDOT = 5072
625970 meter/sec
ZDOT = 4271
303571 ZDOT = 1329
255567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6235932
23 X = -1900712
14
Y = 12901985
09 feet Y = 3932525
06 meter
Z = 16983501
97 Z = 5176571
40
XDOT = -18616
824393 XDOT = -5674
408075
YDOT = -14775
733934 feet/sec YDOT = -4503
643703 meter/sec
ZDOT = 4383
770027 ZDOT = 1336
173104
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 12219
68625599
00016717 00000-0 10270-3 0 9057
2 25544 51
6376 230
1236 0001664 7
2137 352
9040 15
54993458 25872
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
68625599 = yrday
fracday
Element set: 905
Inclination: 51
6376 deg
RA of node: 230
1236 deg
Eccentricity:
0001664
Arg of perigee: 7
2137 deg
Mean anomaly: 352
9040 deg
Mean motion: 15
54993458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2587
Checksum: 323
Coasting Arc #7 (Orbit 2601)
---------------------------------------
Vector Time (GMT): 2012/220/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3695631
98 A = 6775120
57 meter
Y = 2234627
21 meter E =
0014694
Z = -5233025
97 I = 51
37079
XDOT = -4872
290373 Wp = 90
78528
YDOT = -5832
304981 meter/sec RA = 224
37666 deg
ZDOT = 952
467267 TA = 188
36217
MA = 188
38668
Ha = 219
856 n
mi
Hp = 213
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12124776
84 X = -3694924
76
Y = 7331454
10 feet Y = 2193304
32 meter
Z = -17168720
38 Z = -5250977
29
XDOT = -15985
204635 XDOT = -4811
337043
YDOT = -19134
858861 feet/sec YDOT = -5886
449154 meter/sec
ZDOT = 3124
892609 ZDOT = 928
946170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11391655
44 X = 3472176
58
Y = -8272538
80 feet Y = -2521469
83 meter
Z = -17242989
31 Z = -5255663
14
XDOT = 16886
667969 XDOT = 5147
056397
YDOT = 16956
008447 feet/sec YDOT = 5168
191375 meter/sec
ZDOT = 3028
336475 ZDOT = 923
036958
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 12220
65024966
00016717 00000-0 10270-3 0 9068
2 25544 51
6379 225
3106 0001706 12
3880 347
7315 15
54993923 26028
Satellite: ISS
Catalog Number: 25544
Epoch time: 12220
65024966 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 225
3106 deg
Eccentricity:
0001706
Arg of perigee: 12
3880 deg
Mean anomaly: 347
7315 deg
Mean motion: 15
54993923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2602
Checksum: 300
Coasting Arc #8 (Orbit 2617)
---------------------------------------
Vector Time (GMT): 2012/221/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4998566
53 A = 6777854
09 meter
Y = -582852
24 meter E =
0009794
Z = 4535633
42 I = 51
40336
XDOT = 3520
828330 Wp = 58
80619
YDOT = 6076
374147 meter/sec RA = 219
35377 deg
ZDOT = -3089
410048 TA = 62
25568
MA = 62
15639
Ha = 219
722 n
mi
Hp = 213
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16399496
49 X = 4982679
69
Y = -1912244
88 feet Y = -527044
05 meter
Z = 14880687
09 Z = 4559877
44
XDOT = 11551
274048 XDOT = 3467
626921
YDOT = 19935
610719 feet/sec YDOT = 6115
448815 meter/sec
ZDOT = -10135
859736 ZDOT = -3072
435300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16044190
51 X = -4890269
27
Y = 3492130
19 feet Y = 1064401
28 meter
Z = 14980787
41 Z = 4566144
00
XDOT = -13246
583826 XDOT = -4037
558750
YDOT = -17537
841160 feet/sec YDOT = -5345
533985 meter/sec
ZDOT = -10066
329250 ZDOT = -3068
217155
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 12221
67849447
00016717 00000-0 10270-3 0 9071
2 25544 51
6384 220
1777 0001735 15
0324 345
0880 15
55028295 26183
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
67849447 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 220
1777 deg
Eccentricity:
0001735
Arg of perigee: 15
0324 deg
Mean anomaly: 345
0880 deg
Mean motion: 15
55028295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2618
Checksum: 308
Coasting Arc #9 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2012/222/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5902630
05 A = 6782231
09 meter
Y = -936026
29 meter E =
0005596
Z = -3208229
03 I = 51
44215
XDOT = -1677
851543 Wp = 65
44862
YDOT = -5756
544878 meter/sec RA = 214
34451 deg
ZDOT = 4775
346500 TA = 257
33366
MA = 257
39623
Ha = 219
808 n
mi
Hp = 212
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19365584
14 X = -5876139
78
Y = -3070952
38 feet Y = -1001884
96 meter
Z = -10525685
81 Z = -3236839
20
XDOT = -5504
762280 XDOT = -1636
553344
YDOT = -18886
302094 feet/sec YDOT = -5775
076871 meter/sec
ZDOT = 15667
147310 ZDOT = 4767
295797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19525721
30 X = 5951439
85
Y = 839543
45 feet Y = 255892
84 meter
Z = -10643685
16 Z = -3244195
24
XDOT = 7788
996585 XDOT = 2374
086159
YDOT = 16695
239475 feet/sec YDOT = 5088
708992 meter/sec
ZDOT = 15634
411544 ZDOT = 4765
368639
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 12222
64245974
00016717 00000-0 10270-3 0 9085
2 25544 51
6382 215
3653 0001790 16
7105 343
4107 15
55033346 26330
Satellite: ISS
Catalog Number: 25544
Epoch time: 12222
64245974 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 215
3653 deg
Eccentricity:
0001790
Arg of perigee: 16
7105 deg
Mean anomaly: 343
4107 deg
Mean motion: 15
55033346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 289
Coasting Arc #10 (Orbit 2648)
---------------------------------------
Vector Time (GMT): 2012/223/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6244523
17 A = 6785754
55 meter
Y = 2253131
54 meter E =
0013763
Z = 1377982
07 I = 51
48068
XDOT = -516
616398 Wp = 112
28453
YDOT = 5000
425708 meter/sec RA = 209
35060 deg
ZDOT = -5793
785221 TA = 52
65934
MA = 52
53403
Ha = 219
841 n
mi
Hp = 212
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20487280
74 X = 6212170
21
Y = 7392163
84 feet Y = 2322780
73 meter
Z = 4520938
53 Z = 1408238
91
XDOT = -1694
935688 XDOT = -544
349137
YDOT = 16405
596156 feet/sec YDOT = 4994
493732 meter/sec
ZDOT = -19008
481697 ZDOT = -5796
362078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21254495
47 X = -6478370
22
Y = -4634235
24 feet Y = -1412514
90 meter
Z = 4645635
55 Z = 1415989
72
XDOT = -932
949406 XDOT = -284
362979
YDOT = -14919
515980 feet/sec YDOT = -4547
468471 meter/sec
ZDOT = -19019
542242 ZDOT = -5797
156475
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 12223
67067458
00016717 00000-0 10270-3 0 9099
2 25544 51
6390 210
2316 0001772 22
7088 337
4143 15
55066762 26494
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
67067458 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 210
2316 deg
Eccentricity:
0001772
Arg of perigee: 22
7088 deg
Mean anomaly: 337
4143 deg
Mean motion: 15
55066762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2649
Checksum: 307
Coasting Arc #11 (Orbit 2664)
---------------------------------------
Vector Time (GMT): 2012/224/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5926887
54 A = 6786381
99 meter
Y = -3230275
69 meter E =
0014697
Z = 625492
67 I = 51
50953
XDOT = 2786
732727 Wp = 48
49890
YDOT = -3942
771109 meter/sec RA = 204
36567 deg
ZDOT = 5962
645790 TA = 318
27117
MA = 318
38317
Ha = 219
817 n
mi
Hp = 212
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19445169
11 X = -5893363
90
Y = -10598017
34 feet Y = -3296366
41 meter
Z = 2052141
31 Z = 596781
71
XDOT = 9142
823908 XDOT = 2801
649608
YDOT = -12935
600752 feet/sec YDOT = -3911
524986 meter/sec
ZDOT = 19562
486189 ZDOT = 5976
219531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20816953
67 X = 6345007
48
Y = 7586722
31 feet Y = 2312432
96 meter
Z = 1933892
88 Z = 589450
55
XDOT = -6446
134404 XDOT = -1964
781766
YDOT = 12614
284326 feet/sec YDOT = 3844
833863 meter/sec
ZDOT = 19618
852426 ZDOT = 5979
826220
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 12224
69887276
00016717 00000-0 10270-3 0 9102
2 25544 51
6385 205
0982 0001786 23
9934 336
1302 15
55093620 26651
Satellite: ISS
Catalog Number: 25544
Epoch time: 12224
69887276 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 205
0982 deg
Eccentricity:
0001786
Arg of perigee: 23
9934 deg
Mean anomaly: 336
1302 deg
Mean motion: 15
55093620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2665
Checksum: 317
Coasting Arc #12 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2012/225/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4912137
45 A = 6783658
35 meter
Y = 3902631
36 meter E =
0005151
Z = -2581940
26 I = 51
52969
XDOT = -4894
604950 Wp = 109
31554
YDOT = 2696
922257 meter/sec RA = 199
37917 deg
ZDOT = -5245
775664 TA = 99
76869
MA = 99
71051
Ha = 219
833 n
mi
Hp = 212
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16115936
51 X = 4880674
66
Y = 12803908
66 feet Y = 3957386
13 meter
Z = -8470932
62 Z = -2558153
87
XDOT = -16058
415190 XDOT = -4898
916253
YDOT = 8848
170133 feet/sec YDOT = 2642
163878 meter/sec
ZDOT = -17210
550079 ZDOT = -5269
563472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18065352
68 X = -5506319
50
Y = -9947620
69 feet Y = -3032034
79 meter
Z = -8373055
68 Z = -2552107
37
XDOT = 13541
117982 XDOT = 4127
332761
YDOT = -10050
658461 feet/sec YDOT = -3063
440699 meter/sec
ZDOT = -17308
986356 ZDOT = -5275
779041
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 12225
66279361
00016717 00000-0 10270-3 0 9111
2 25544 51
6393 200
2852 0001818 27
7674 332
3576 15
55127848 26800
Satellite: ISS
Catalog Number: 25544
Epoch time: 12225
66279361 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 200
2852 deg
Eccentricity:
0001818
Arg of perigee: 27
7674 deg
Mean anomaly: 332
3576 deg
Mean motion: 15
55127848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2680
Checksum: 315
Coasting Arc #13 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2012/226/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3300418
25 A = 6779186
52 meter
Y = -4233541
07 meter E =
0011194
Z = 4131327
97 I = 51
54367
XDOT = 6536
142389 Wp = 95
28993
YDOT = -1411
291669 meter/sec RA = 194
38229 deg
ZDOT = 3765
558287 TA = 315
86550
MA = 315
95477
Ha = 219
875 n
mi
Hp = 212
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10828143
88 X = -3272901
37
Y = -13889570
42 feet Y = -4270294
71 meter
Z = 13554225
62 Z = 4115361
60
XDOT = 21444
036710 XDOT = 6533
146025
YDOT = -4630
222011 feet/sec YDOT = -1338
217375 meter/sec
ZDOT = 12354
193856 ZDOT = 3797
302726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13263804
78 X = 4042807
70
Y = 11662490
34 feet Y = 3554727
06 meter
Z = 13488650
79 Z = 4111340
76
XDOT = -19312
811994 XDOT = -5886
545096
YDOT = 7486
783593 feet/sec YDOT = 2281
971639 meter/sec
ZDOT = 12485
387914 ZDOT = 3805
546236
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 12226
69096012
00016717 00000-0 10270-3 0 9126
2 25544 51
6390 195
1514 0001775 32
3836 327
7426 15
55146263 26969
Satellite: ISS
Catalog Number: 25544
Epoch time: 12226
69096012 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 195
1514 deg
Eccentricity:
0001775
Arg of perigee: 32
3836 deg
Mean anomaly: 327
7426 deg
Mean motion: 15
55146263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 309
Coasting Arc #14 (Orbit 2710)
---------------------------------------
Vector Time (GMT): 2012/227/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1238967
82 A = 6775290
80 meter
Y = 4304416
79 meter E =
0014721
Z = -5096739
37 I = 51
56163
XDOT = -7466
518656 Wp = 72
54698
YDOT = 135
440396 meter/sec RA = 189
37248 deg
ZDOT = -1700
394284 TA = 180
98566
MA = 180
98857
Ha = 219
792 n
mi
Hp = 212
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4064855
05 X = 1215501
20
Y = 14122102
34 feet Y = 4318140
65 meter
Z = -16721585
85 Z = -5090777
50
XDOT = -24496
452282 XDOT = -7459
218274
YDOT = 444
358255 feet/sec YDOT = 51
986014 meter/sec
ZDOT = -5578
721403 ZDOT = -1736
647876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6900601
03 X = -2103303
19
Y = -13005747
19 feet Y = -3964151
74 meter
Z = -16697320
14 Z = -5089343
18
XDOT = 22933
095776 XDOT = 6990
007593
YDOT = -4812
352581 feet/sec YDOT = -1466
805067 meter/sec
ZDOT = -5728
447214 ZDOT = -1746
030711
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 12227
65485080
00016717 00000-0 10270-3 0 9131
2 25544 51
6398 190
3381 0001838 35
2970 324
8305 15
55186024 27118
Satellite: ISS
Catalog Number: 25544
Epoch time: 12227
65485080 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 190
3381 deg
Eccentricity:
0001838
Arg of perigee: 35
2970 deg
Mean anomaly: 324
8305 deg
Mean motion: 15
55186024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2711
Checksum: 303
Coasting Arc #15 (Orbit 2726)
---------------------------------------
Vector Time (GMT): 2012/228/15:15:28
272
Vector Time (MET): N/A
Weight (LBS) : 939998
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1016650
26 A = 6774241
15 meter
Y = -4119519
27 meter E =
0004407
Z = 5277870
43 I = 51
58893
XDOT = 7572
915853 Wp = 54
68452
YDOT = 1070
349564 meter/sec RA = 184
35692 deg
ZDOT = -620
436924 TA = 41
25499
MA = 41
22170
Ha = 219
638 n
mi
Hp = 212
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3335466
73 X = 1037001
84
Y = -13515483
18 feet Y = -4108036
73 meter
Z = 17315847
85 Z = 5282858
55
XDOT = 24845
524452 XDOT = 7563
398028
YDOT = 3511
645550 feet/sec YDOT = 1154
981409 meter/sec
ZDOT = -2035
554211 ZDOT = -583
671909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -229327
55 X = -69899
04
Y = 13893001
53 feet Y = 4234586
87 meter
Z = 17336785
40 Z = 5284252
19
XDOT = -24015
424725 XDOT = -7319
901456
YDOT = 1966
030197 feet/sec YDOT = 599
246004 meter/sec
ZDOT = -1883
796304 ZDOT = -574
181113
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 12228
68298324
00016717 00000-0 10270-3 0 9149
2 25544 51
6397 185
2041 0001723 33
8543 326
2720 15
55232730 27276
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
68298324 = yrday
fracday
Element set: 914
Inclination: 51
6397 deg
RA of node: 185
2041 deg
Eccentricity:
0001723
Arg of perigee: 33
8543 deg
Mean anomaly: 326
2720 deg
Mean motion: 15
55232730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2727
Checksum: 299
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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