[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 3rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12539 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
062/13:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 193
6
000/00:00:00
000 0
0 0
0 184
9
062/13:52:30
677 0
5 0
5 0
5
N/A -0
1 -0
0 193
6
000/00:09:01
353 0
1 0
1 185
1
062/14:16:00
000 0
3 1
6 1
6
N/A 0
8 -0
1 194
5
000/00:26:00
000 1
3 -0
2 185
5
062/14:36:10
564 -0
5 0
5 0
6
N/A 0
2 0
0 194
8
000/00:06:17
128 -0
1 0
1 185
5
062/16:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 194
8
000/00:00:00
000 0
0 0
0 185
6
Coasting Arc #1 (Orbit 2395)
---------------------------------------
Vector Time (GMT): 2011/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6421978
94 A = 6734740
99 meter
Y = 676873
48 meter E =
0018093
Z = 1876370
56 I = 51
61854
XDOT = -2160
603926 Wp = 54
88782
YDOT = 4781
578169 meter/sec RA = 352
71084 deg
ZDOT = 5641
977154 TA = 325
96402
MA = 326
07993
Ha = 193
543 n
mi
Hp = 185
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21069484
71 X = 6404817
93
Y = 2220713
52 feet Y = 748592
10 meter
Z = 6156071
39 Z = 1907525
85
XDOT = -7088
595558 XDOT = -2241
318725
YDOT = 15687
592418 feet/sec YDOT = 4756
966031 meter/sec
ZDOT = 18510
423732 ZDOT = 5631
284922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18696719
03 X = 5698759
96
Y = 9885512
61 feet Y = 3013104
25 meter
Z = 6281823
57 Z = 1914699
82
XDOT = -11797
604094 XDOT = -3595
909728
YDOT = 10521
002376 feet/sec YDOT = 3206
801524 meter/sec
ZDOT = 18467
100975 ZDOT = 5628
772377
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 11060
55979766
00016717 00000-0 10270-3 0 9009
2 25544 51
6456 352
9014 0005189 21
3119 338
8259 15
72543183 23960
Satellite: ISS
Catalog Number: 25544
Epoch time: 11060
55979766 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 352
9014 deg
Eccentricity:
0005189
Arg of perigee: 21
3119 deg
Mean anomaly: 338
8259 deg
Mean motion: 15
72543183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2396
Checksum: 323
Coasting Arc #2 (Orbit 2410)
---------------------------------------
Vector Time (GMT): 2011/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 938024
17 A = 6725097
58 meter
Y = -4330243
49 meter E =
0015440
Z = -5071972
33 I = 51
55671
XDOT = 7500
748792 Wp = 83
20128
YDOT = -308
805725 meter/sec RA = 347
55154 deg
ZDOT = 1656
954756 TA = 202
73746
MA = 202
80592
Ha = 193
590 n
mi
Hp = 185
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3077507
12 X = 1011014
05
Y = -14206835
61 feet Y = -4319346
24 meter
Z = -16640329
17 Z = -5067237
91
XDOT = 24608
755879 XDOT = 7495
595499
YDOT = -1013
142142 feet/sec YDOT = -224
956490 meter/sec
ZDOT = 5436
203268 ZDOT = 1693
379809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8026327
17 X = 2446424
52
Y = -12145930
35 feet Y = -3702079
57 meter
Z = -16621077
92 Z = -5066104
55
XDOT = 22440
876535 XDOT = 6839
979168
YDOT = 7216
500419 feet/sec YDOT = 2199
589328 meter/sec
ZDOT = 5583
257139 ZDOT = 1701
776776
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 11061
51300844
00016717 00000-0 10270-3 0 9012
2 25544 51
6462 348
0171 0005182 24
5152 335
6256 15
72582981 24111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11061
51300844 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 348
0171 deg
Eccentricity:
0005182
Arg of perigee: 24
5152 deg
Mean anomaly: 335
6256 deg
Mean motion: 15
72582981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2411
Checksum: 277
Coasting Arc #3 (Orbit 2426)
---------------------------------------
Vector Time (GMT): 2011/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6544022
13 A = 6735615
30 meter
Y = 1207065
77 meter E =
0008906
Z = -1036910
68 I = 51
56356
XDOT = 20
855034 Wp = 109
89456
YDOT = -4926
008241 meter/sec RA = 342
44540 deg
ZDOT = -5909
978717 TA = 81
44130
MA = 81
34039
Ha = 193
574 n
mi
Hp = 184
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21469888
87 X = -6551996
41
Y = 3960189
52 feet Y = 1133841
86 meter
Z = -3401937
93 Z = -1068720
15
XDOT = 68
422028 XDOT = 104
645863
YDOT = -16161
444360 feet/sec YDOT = -4925
307105 meter/sec
ZDOT = -19389
693954 ZDOT = -5909
673402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21518340
51 X = -6558790
19
Y = -3565086
43 feet Y = -1086638
34 meter
Z = -3530381
18 Z = -1076060
18
XDOT = 5406
070885 XDOT = 1647
770406
YDOT = -13568
449470 feet/sec YDOT = -4135
663398 meter/sec
ZDOT = -19388
308198 ZDOT = -5909
556339
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 11062
52974306
00016717 00000-0 10270-3 0 9025
2 25544 51
6468 342
8072 0005104 28
5774 331
5667 15
72614042 24279
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
52974306 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 342
8072 deg
Eccentricity:
0005104
Arg of perigee: 28
5774 deg
Mean anomaly: 331
5667 deg
Mean motion: 15
72614042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2427
Checksum: 298
Coasting Arc #4 (Orbit 2427)
---------------------------------------
Vector Time (GMT): 2011/062/13:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 1137589
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6501607
92 A = 6736035
31 meter
Y = 1681500
62 meter E =
0010454
Z = -498827
04 I = 51
56369
XDOT = -776
960196 Wp = 111
90284
YDOT = -4753
467608 meter/sec RA = 342
11987 deg
ZDOT = -6000
872161 TA = 73
52365
MA = 73
40880
Ha = 193
573 n
mi
Hp = 184
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21330734
64 X = -6517504
42
Y = 5516734
32 feet Y = 1608706
77 meter
Z = -1636571
66 Z = -530449
76
XDOT = -2549
082007 XDOT = -694
597917
YDOT = -15595
366168 feet/sec YDOT = -4761
696127 meter/sec
ZDOT = -19687
900792 ZDOT = -6004
446008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21037708
54 X = -6412293
56
Y = 6512688
89 feet Y = 1985067
57 meter
Z = -1764275
33 Z = -537751
12
XDOT = -2686
797354 XDOT = -818
935833
YDOT = -13930
523960 feet/sec YDOT = -4246
023703 meter/sec
ZDOT = -19702
179706 ZDOT = -6005
224374
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 11062
59328823
00016717 00000-0 10270-3 0 9030
2 25544 51
6476 342
4818 0005003 29
0198 331
1241 15
72599365 24281
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
59328823 = yrday
fracday
Element set: 903
Inclination: 51
6476 deg
RA of node: 342
4818 deg
Eccentricity:
0005003
Arg of perigee: 29
0198 deg
Mean anomaly: 331
1241 deg
Mean motion: 15
72599365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2428
Checksum: 305
Coasting Arc #5 (Orbit 2427)
---------------------------------------
Vector Time (GMT): 2011/062/13:57:01
353
Vector Time (MET): N/A
Weight (LBS) : 1137434
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1146632
52 A = 6725925
69 meter
Y = -4470220
08 meter E =
0013926
Z = -4904408
73 I = 51
52867
XDOT = 7343
711998 Wp = 85
02335
YDOT = -537
031898 meter/sec RA = 342
00079 deg
ZDOT = 2212
991478 TA = 206
51050
MA = 206
58179
Ha = 193
583 n
mi
Hp = 185
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3761917
71 X = 1220358
23
Y = -14666076
36 feet Y = -4456986
00 meter
Z = -16090579
83 Z = -4898659
03
XDOT = 24093
543300 XDOT = 7338
421371
YDOT = -1761
915676 feet/sec YDOT = -454
939425 meter/sec
ZDOT = 7260
470727 ZDOT = 2248
653453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1392816
38 X = 424530
43
Y = -15101546
93 feet Y = -4602951
51 meter
Z = -16067231
34 Z = -4897292
11
XDOT = 22331
073502 XDOT = 6806
511203
YDOT = -5795
364058 feet/sec YDOT = -1766
426965 meter/sec
ZDOT = 7404
443964 ZDOT = 2256
874520
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 11062
59328724
00016717 00000-0 10270-3 0 9041
2 25544 51
6478 342
4820 0005035 23
4731 336
6661 15
72546678 24287
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
59328724 = yrday
fracday
Element set: 904
Inclination: 51
6478 deg
RA of node: 342
4820 deg
Eccentricity:
0005035
Arg of perigee: 23
4731 deg
Mean anomaly: 336
6661 deg
Mean motion: 15
72546678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2428
Checksum: 312
Coasting Arc #6 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2011/062/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 1137025
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4536491
83 A = 6728877
49 meter
Y = 2224609
44 meter E =
0010913
Z = 4433404
23 I = 51
53452
XDOT = -5370
316676 Wp = 75
15576
YDOT = 4467
838536 meter/sec RA = 341
92813 deg
ZDOT = 3249
415812 TA = 342
23364
MA = 342
27176
Ha = 194
533 n
mi
Hp = 185
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14883503
39 X = 4489742
58
Y = 7298587
40 feet Y = 2275078
29 meter
Z = 14545289
47 Z = 4455328
13
XDOT = -17619
149198 XDOT = -5435
662407
YDOT = 14658
262912 feet/sec YDOT = 4407
419357 meter/sec
ZDOT = 10660
813032 ZDOT = 3223
168365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16305682
14 X = 4969971
92
Y = 2516435
78 feet Y = 767009
62 meter
Z = 14633720
58 Z = 4460358
03
XDOT = -12277
959728 XDOT = -3742
322125
YDOT = 18105
059708 feet/sec YDOT = 5518
422199 meter/sec
ZDOT = 10554
721583 ZDOT = 3217
079138
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 11062
65685288
00016717 00000-0 10270-3 0 9050
2 25544 51
6482 342
1564 0006501 19
9898 340
1518 15
72120264 24298
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
65685288 = yrday
fracday
Element set: 905
Inclination: 51
6482 deg
RA of node: 342
1564 deg
Eccentricity:
0006501
Arg of perigee: 19
9898 deg
Mean anomaly: 340
1518 deg
Mean motion: 15
72120264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 312
Coasting Arc #7 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2011/062/14:39:19
128
Vector Time (MET): N/A
Weight (LBS) : 1136916
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 391158
39 A = 6725894
06 meter
Y = 4229962
15 meter E =
0009495
Z = 5210993
15 I = 51
52354
XDOT = -7455
394153 Wp = 34
00766
YDOT = 1737
841986 meter/sec RA = 341
86042 deg
ZDOT = -842
558920 TA = 64
07440
MA = 63
97657
Ha = 194
808 n
mi
Hp = 185
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1283328
06 X = 318515
71
Y = 13877828
57 feet Y = 4233930
67 meter
Z = 17096434
21 Z = 5212716
48
XDOT = -24459
954571 XDOT = -7470
180044
YDOT = 5701
581318 feet/sec YDOT = 1654
388497 meter/sec
ZDOT = -2764
300917 ZDOT = -878
812319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5872292
61 X = 1789874
79
Y = 12630273
46 feet Y = 3849707
35 meter
Z = 17103259
67 Z = 5213073
55
XDOT = -20080
809453 XDOT = -6120
630721
YDOT = 13315
511818 feet/sec YDOT = 4058
568002 meter/sec
ZDOT = -2910
698564 ZDOT = -887
180922
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 11062
65685524
00016717 00000-0 10270-3 0 9064
2 25544 51
6482 342
1563 0006569 22
3137 337
8310 15
72057989 24291
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
65685524 = yrday
fracday
Element set: 906
Inclination: 51
6482 deg
RA of node: 342
1563 deg
Eccentricity:
0006569
Arg of perigee: 22
3137 deg
Mean anomaly: 337
8310 deg
Mean motion: 15
72057989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 319
Coasting Arc #8 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2011/062/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4718776
31 A = 6729635
96 meter
Y = 2052173
94 meter E =
0011906
Z = 4325307
32 I = 51
53282
XDOT = -5148
657815 Wp = 75
02411
YDOT = 4588
530271 meter/sec RA = 341
60410 deg
ZDOT = 3435
150203 TA = 340
24206
MA = 340
28815
Ha = 194
837 n
mi
Hp = 185
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15481549
58 X = 4674466
81
Y = 6732854
15 feet Y = 2104694
84 meter
Z = 14190640
82 Z = 4348122
68
XDOT = -16891
921966 XDOT = -5216
271861
YDOT = 15054
233171 feet/sec YDOT = 4530
577154 meter/sec
ZDOT = 11270
177833 ZDOT = 3409
974015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16097755
15 X = 4906595
77
Y = -4821975
18 feet Y = -1469738
04 meter
Z = 14282675
65 Z = 4353359
54
XDOT = -3549
797019 XDOT = -1081
978131
YDOT = 21276
572658 feet/sec YDOT = 6485
099346 meter/sec
ZDOT = 11168
407583 ZDOT = 3404
130631
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 11062
72042595
00016717 00000-0 10270-3 0 9078
2 25544 51
6469 341
8302 0006696 22
6817 337
4640 15
71998598 24305
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
72042595 = yrday
fracday
Element set: 907
Inclination: 51
6469 deg
RA of node: 341
8302 deg
Eccentricity:
0006696
Arg of perigee: 22
6817 deg
Mean anomaly: 337
4640 deg
Mean motion: 15
71998598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2430
Checksum: 327
Coasting Arc #9 (Orbit 2444)
---------------------------------------
Vector Time (GMT): 2011/063/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3497172
17 A = 6732418
30 meter
Y = -4564561
24 meter E =
0009608
Z = -3502760
56 I = 51
51308
XDOT = 6113
661122 Wp = 54
53597
YDOT = 1238
899892 meter/sec RA = 336
42519 deg
ZDOT = 4503
585128 TA = 263
81107
MA = 263
92054
Ha = 194
856 n
mi
Hp = 185
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11473661
97 X = 3564969
42
Y = -14975594
62 feet Y = -4525075
06 meter
Z = -11491996
58 Z = -3485606
51
XDOT = 20057
943313 XDOT = 6077
476036
YDOT = 4064
632192 feet/sec YDOT = 1307
064735 meter/sec
ZDOT = 14775
541760 ZDOT = 4533
196562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1207177
96 X = -367947
84
Y = -18869177
59 feet Y = -5751325
33 meter
Z = -11422617
79 Z = -3481613
90
XDOT = 16312
391958 XDOT = 4972
017069
YDOT = -10032
206990 feet/sec YDOT = -3057
816691 meter/sec
ZDOT = 14895
029883 ZDOT = 4540
005108
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 11063
67395358
00016717 00000-0 10270-3 0 9082
2 25544 51
6461 336
9477 0006509 25
1962 334
9517 15
72067798 24458
Satellite: ISS
Catalog Number: 25544
Epoch time: 11063
67395358 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 336
9477 deg
Eccentricity:
0006509
Arg of perigee: 25
1962 deg
Mean anomaly: 334
9517 deg
Mean motion: 15
72067798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2445
Checksum: 344
Coasting Arc #10 (Orbit 2460)
---------------------------------------
Vector Time (GMT): 2011/064/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5747899
13 A = 6732131
45 meter
Y = -49591
89 meter E =
0010509
Z = -3517725
73 I = 51
48408
XDOT = 2788
906086 Wp = 52
68053
YDOT = -5588
189517 meter/sec RA = 331
34628 deg
ZDOT = -4481
152483 TA = 169
16571
MA = 169
14305
Ha = 194
843 n
mi
Hp = 185
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18857936
78 X = -5729829
24
Y = -162703
06 feet Y = -113767
76 meter
Z = -11541094
91 Z = -3545604
58
XDOT = 9149
954351 XDOT = 2872
955217
YDOT = -18333
955109 feet/sec YDOT = -5556
532861 meter/sec
ZDOT = -14701
943843 ZDOT = -4467
399434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14013449
55 X = -4271299
42
Y = 12516450
09 feet Y = 3815013
99 meter
Z = -11653618
87 Z = -3552023
03
XDOT = -4583
102113 XDOT = -1396
929524
YDOT = -18759
061384 feet/sec YDOT = -5717
761910 meter/sec
ZDOT = -14646
269648 ZDOT = -4464
182989
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 11064
69102788
00016717 00000-0 10270-3 0 9099
2 25544 51
6450 331
7402 0006495 29
0013 331
1509 15
72097819 24616
Satellite: ISS
Catalog Number: 25544
Epoch time: 11064
69102788 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 331
7402 deg
Eccentricity:
0006495
Arg of perigee: 29
0013 deg
Mean anomaly: 331
1509 deg
Mean motion: 15
72097819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2461
Checksum: 299
Coasting Arc #11 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2011/065/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1333958
42 A = 6729475
53 meter
Y = 5007556
55 meter E =
0015289
Z = 4287415
62 I = 51
44939
XDOT = -6763
702005 Wp = 55
98020
YDOT = 1194
052713 meter/sec RA = 326
16214 deg
ZDOT = -3481
746365 TA = 69
42276
MA = 69
25881
Ha = 194
800 n
mi
Hp = 185
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4376503
99 X = -1410681
90
Y = 16428991
32 feet Y = 4992210
94 meter
Z = 14066324
22 Z = 4280748
41
XDOT = -22190
623375 XDOT = -6759
637991
YDOT = 3917
495778 feet/sec YDOT = 1118
439215 meter/sec
ZDOT = -11423
052379 ZDOT = -3514
594201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8009256
55 X = 2441221
40
Y = 15022572
43 feet Y = 4578880
08 meter
Z = 14039271
60 Z = 4279169
98
XDOT = -12332
505676 XDOT = -3758
947730
YDOT = 17427
425066 feet/sec YDOT = 5311
879160 meter/sec
ZDOT = -11555
660467 ZDOT = -3522
165310
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 11065
70807693
00016717 00000-0 10270-3 0 9101
2 25544 51
6453 326
5316 0006408 31
7926 328
3622 15
72157119 24773
Satellite: ISS
Catalog Number: 25544
Epoch time: 11065
70807693 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 326
5316 deg
Eccentricity:
0006408
Arg of perigee: 31
7926 deg
Mean anomaly: 328
3622 deg
Mean motion: 15
72157119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 308
Coasting Arc #12 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2011/066/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5852765
87 A = 6734473
65 meter
Y = -2136152
26 meter E =
0019022
Z = 2528653
70 I = 51
44057
XDOT = -244
230811 Wp = 63
92356
YDOT = 5607
043958 meter/sec RA = 321
07286 deg
ZDOT = 5279
581740 TA = 324
82220
MA = 324
94763
Ha = 194
672 n
mi
Hp = 184
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19201987
75 X = 5863934
13
Y = -7008373
56 feet Y = -2070640
36 meter
Z = 8296107
93 Z = 2557113
48
XDOT = -801
282189 XDOT = -332
558662
YDOT = 18395
813510 feet/sec YDOT = 5603
819536 meter/sec
ZDOT = 17321
462402 ZDOT = 5278
180115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8831980
98 X = 2691987
80
Y = -18382322
72 feet Y = -5602931
97 meter
Z = 8411026
31 Z = 2563680
82
XDOT = 10845
695082 XDOT = 3305
767861
YDOT = 13167
082426 feet/sec YDOT = 4013
326723 meter/sec
ZDOT = 17315
647112 ZDOT = 5277
809240
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 11066
72510287
00016717 00000-0 10270-3 0 9115
2 25544 51
6438 321
3227 0006289 36
6609 323
4982 15
72193620 24939
Satellite: ISS
Catalog Number: 25544
Epoch time: 11066
72510287 = yrday
fracday
Element set: 911
Inclination: 51
6438 deg
RA of node: 321
3227 deg
Eccentricity:
0006289
Arg of perigee: 36
6609 deg
Mean anomaly: 323
4982 deg
Mean motion: 15
72193620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 308
Coasting Arc #13 (Orbit 2507)
---------------------------------------
Vector Time (GMT): 2011/067/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -853718
33 A = 6727008
94 meter
Y = -4581765
15 meter E =
0015905
Z = -4864086
22 I = 51
39152
XDOT = 6377
253107 Wp = 85
29435
YDOT = -3622
618152 meter/sec RA = 315
89397 deg
ZDOT = 2300
800230 TA = 207
18617
MA = 207
26954
Ha = 194
810 n
mi
Hp = 184
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2800913
15 X = -778792
05
Y = -15032037
88 feet Y = -4590893
48 meter
Z = -15958288
14 Z = -4868051
11
XDOT = 20922
746413 XDOT = 6406
111156
YDOT = -11885
230158 feet/sec YDOT = -3551
142263 meter/sec
ZDOT = 7548
557184 ZDOT = 2331
851120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12576843
89 X = -3833422
02
Y = -8667376
66 feet Y = -2641816
40 meter
Z = -15974160
92 Z = -4868924
25
XDOT = 5635
562370 XDOT = 1717
719410
YDOT = -22274
004352 feet/sec YDOT = -6789
116526 meter/sec
ZDOT = 7673
968854 ZDOT = 2339
025707
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 11067
67854368
00016717 00000-0 10270-3 0 9122
2 25544 51
6430 316
4388 0006360 41
4209 318
7435 15
72211801 25083
Satellite: ISS
Catalog Number: 25544
Epoch time: 11067
67854368 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 316
4388 deg
Eccentricity:
0006360
Arg of perigee: 41
4209 deg
Mean anomaly: 318
7435 deg
Mean motion: 15
72211801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2508
Checksum: 299
Coasting Arc #14 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2011/068/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5125413
65 A = 6736077
43 meter
Y = 4106048
90 meter E =
0009677
Z = -1501199
88 I = 51
40173
XDOT = -2055
283447 Wp = 101
04609
YDOT = -4660
552345 meter/sec RA = 310
78774 deg
ZDOT = -5763
519243 TA = 95
52044
MA = 95
41005
Ha = 194
794 n
mi
Hp = 184
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16815661
57 X = -5163654
82
Y = 13471289
06 feet Y = 4048519
48 meter
Z = -4925196
44 Z = -1526192
20
XDOT = -6743
055930 XDOT = -1975
017558
YDOT = -15290
526065 feet/sec YDOT = -4683
087460 meter/sec
ZDOT = -18909
183869 ZDOT = -5773
308389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1891474
58 X = -576521
45
Y = 21439674
02 feet Y = 6534812
64 meter
Z = -5026167
99 Z = -1531976
00
XDOT = -14063
106026 XDOT = -4286
434717
YDOT = -5657
798490 feet/sec YDOT = -1724
496980 meter/sec
ZDOT = -18948
559433 ZDOT = -5775
520915
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 11068
69552208
00016717 00000-0 10270-3 0 9134
2 25544 51
6430 311
2303 0006468 44
1247 316
0431 15
72270715 25248
Satellite: ISS
Catalog Number: 25544
Epoch time: 11068
69552208 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 311
2303 deg
Eccentricity:
0006468
Arg of perigee: 44
1247 deg
Mean anomaly: 316
0431 deg
Mean motion: 15
72270715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 276
Coasting Arc #15 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2011/069/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2640245
16 A = 6725510
47 meter
Y = 3401671
97 meter E =
0010175
Z = 5160394
22 I = 51
34605
XDOT = -5123
408259 Wp = 51
63273
YDOT = 5648
012005 meter/sec RA = 305
62206 deg
ZDOT = -1094
095393 TA = 48
88946
MA = 48
80166
Ha = 194
788 n
mi
Hp = 184
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8662221
65 X = 2576942
68
Y = 11160341
11 feet Y = 3430843
20 meter
Z = 16930427
22 Z = 5173066
45
XDOT = -16809
082214 XDOT = -5180
869733
YDOT = 18530
223114 feet/sec YDOT = 5590
397591 meter/sec
ZDOT = -3589
551814 ZDOT = -1119
124707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14005667
43 X = 4268927
43
Y = 1302882
40 feet Y = 397118
56 meter
Z = 16981473
45 Z = 5175953
11
XDOT = 2283
337661 XDOT = 695
961319
YDOT = 23886
302820 feet/sec YDOT = 7280
545100 meter/sec
ZDOT = -3690
712854 ZDOT = -1124
929278
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 11069
71247818
00016717 00000-0 10270-3 0 9147
2 25544 51
6424 306
0206 0006328 49
5625 310
6088 15
72247830 25407
Satellite: ISS
Catalog Number: 25544
Epoch time: 11069
71247818 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 306
0206 deg
Eccentricity:
0006328
Arg of perigee: 49
5625 deg
Mean anomaly: 310
6088 deg
Mean motion: 15
72247830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2540
Checksum: 298
Coasting Arc #16 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2011/070/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3682583
53 A = 6736887
94 meter
Y = -5615959
40 meter E =
0019267
Z = 404893
42 I = 51
36846
XDOT = 3824
302181 Wp = 50
54856
YDOT = 2952
990960 meter/sec RA = 300
49248 deg
ZDOT = 5998
323591 TA = 313
86985
MA = 314
02886
Ha = 194
759 n
mi
Hp = 184
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12081966
97 X = 3743141
67
Y = -18425063
64 feet Y = -5574439
90 meter
Z = 1328390
49 Z = 422930
67
XDOT = 12546
923165 XDOT = 3761
858501
YDOT = 9688
290551 feet/sec YDOT = 2995
407814 meter/sec
ZDOT = 19679
539342 ZDOT = 6016
750064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5680983
04 X = -1731563
63
Y = -21283425
88 feet Y = -6487188
21 meter
Z = 1401332
10 Z = 427126
02
XDOT = 13956
215350 XDOT = 4253
854439
YDOT = -2388
225140 feet/sec YDOT = -727
931023 meter/sec
ZDOT = 19753
821551 ZDOT = 6020
964809
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 11070
72940781
00016717 00000-0 10270-3 0 9150
2 25544 51
6426 300
8110 0006273 53
6522 306
5219 15
72320822 25566
Satellite: ISS
Catalog Number: 25544
Epoch time: 11070
72940781 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 300
8110 deg
Eccentricity:
0006273
Arg of perigee: 53
6522 deg
Mean anomaly: 306
5219 deg
Mean motion: 15
72320822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2556
Checksum: 280
Coasting Arc #17 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2011/071/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3865835
56 A = 6724781
04 meter
Y = -1675657
51 meter E =
0020734
Z = -5258858
45 I = 51
31401
XDOT = 3199
213945 Wp = 79
84386
YDOT = -6984
338062 meter/sec RA = 295
34578 deg
ZDOT = -123
129545 TA = 188
96119
MA = 188
99826
Ha = 194
778 n
mi
Hp = 184
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12683187
53 X = -3821264
41
Y = -5497564
01 feet Y = -1718638
66 meter
Z = -17253472
61 Z = -5277530
14
XDOT = 10496
108743 XDOT = 3277
674501
YDOT = -22914
494953 feet/sec YDOT = -6948
123823 meter/sec
ZDOT = -403
968324 ZDOT = -107
397028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12385438
92 X = -3775081
78
Y = 5923089
14 feet Y = 1805357
57 meter
Z = -17328782
15 Z = -5281812
80
XDOT = -10041
305890 XDOT = -3060
590035
YDOT = -22022
836548 feet/sec YDOT = -6712
560580 meter/sec
ZDOT = -340
294358 ZDOT = -103
721720
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 11071
68275810
00016717 00000-0 10270-3 0 9161
2 25544 51
6431 295
9279 0006357 58
0158 302
1622 15
72363063 25710
Satellite: ISS
Catalog Number: 25544
Epoch time: 11071
68275810 = yrday
fracday
Element set: 916
Inclination: 51
6431 deg
RA of node: 295
9279 deg
Eccentricity:
0006357
Arg of perigee: 58
0158 deg
Mean anomaly: 302
1622 deg
Mean motion: 15
72363063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2571
Checksum: 305
Coasting Arc #18 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2011/072/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1855831
09 A = 6736509
63 meter
Y = 6442917
93 meter E =
0016521
Z = 602750
05 I = 51
34151
XDOT = -4790
970740 Wp = 107
74273
YDOT = -809
380880 meter/sec RA = 290
19258 deg
ZDOT = -5970
139611 TA = 65
67324
MA = 65
50082
Ha = 194
668 n
mi
Hp = 184
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6088684
68 X = -1930667
10
Y = 21138182
19 feet Y = 6421746
50 meter
Z = 1977526
41 Z = 593552
49
XDOT = -15718
407939 XDOT = -4752
562569
YDOT = -2655
449083 feet/sec YDOT = -862
741928 meter/sec
ZDOT = -19587
072213 ZDOT = -5993
320482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12320248
14 X = 3755211
63
Y = 18227791
22 feet Y = 5555830
76 meter
Z = 1940245
13 Z = 591386
72
XDOT = -10706
363650 XDOT = -3263
299640
YDOT = 9377
404346 feet/sec YDOT = 2858
232845 meter/sec
ZDOT = -19680
606577 ZDOT = -5998
648885
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 11072
69963952
00016717 00000-0 10270-3 0 9175
2 25544 51
6425 290
7175 0006286 59
3257 300
8524 15
72425608 25873
Satellite: ISS
Catalog Number: 25544
Epoch time: 11072
69963952 = yrday
fracday
Element set: 917
Inclination: 51
6425 deg
RA of node: 290
7175 deg
Eccentricity:
0006286
Arg of perigee: 59
3257 deg
Mean anomaly: 300
8524 deg
Mean motion: 15
72425608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2587
Checksum: 332
Coasting Arc #19 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2011/073/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4334950
25 A = 6725091
91 meter
Y = -306410
99 meter E =
0009050
Z = 5124505
73 I = 51
29406
XDOT = -972
871923 Wp = 87
61954
YDOT = 7537
356404 meter/sec RA = 285
06292 deg
ZDOT = 1272
098986 TA = 350
15833
MA = 350
17604
Ha = 194
558 n
mi
Hp = 184
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14222277
73 X = 4313160
94
Y = -1005285
39 feet Y = -258056
53 meter
Z = 16812682
84 Z = 5145511
63
XDOT = -3191
837019 XDOT = -1063
263285
YDOT = 24728
859593 feet/sec YDOT = 7525
971818 meter/sec
ZDOT = 4173
553103 ZDOT = 1267
152930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8078135
71 X = 2462215
77
Y = -11626232
97 feet Y = -3543675
81 meter
Z = 16897470
73 Z = 5150349
08
XDOT = 16389
497400 XDOT = 4995
518808
YDOT = 17431
689560 feet/sec YDOT = 5313
178978 meter/sec
ZDOT = 4153
412746 ZDOT = 1265
960205
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 11073
71649894
00016717 00000-0 10270-3 0 9186
2 25544 51
6428 285
5081 0006266 64
1867 295
9941 15
72431650 26033
Satellite: ISS
Catalog Number: 25544
Epoch time: 11073
71649894 = yrday
fracday
Element set: 918
Inclination: 51
6428 deg
RA of node: 285
5081 deg
Eccentricity:
0006266
Arg of perigee: 64
1867 deg
Mean anomaly: 295
9941 deg
Mean motion: 15
72431650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2603
Checksum: 333
Coasting Arc #20 (Orbit 2617)
---------------------------------------
Vector Time (GMT): 2011/074/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -158018
58 A = 6735425
23 meter
Y = -6537863
25 meter E =
0013800
Z = -1597352
42 I = 51
32339
XDOT = 4916
260580 Wp = 50
92241
YDOT = -1507
838043 meter/sec RA = 279
89049 deg
ZDOT = 5726
806858 TA = 291
38357
MA = 291
53077
Ha = 194
662 n
mi
Hp = 183
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -518433
65 X = -77139
72
Y = -21449682
59 feet Y = -6539178
20 meter
Z = -5240657
56 Z = -1597923
19
XDOT = 16129
463845 XDOT = 4904
936907
YDOT = -4946
975206 feet/sec YDOT = -1452
924383 meter/sec
ZDOT = 18788
736410 ZDOT = 5750
662146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17230343
45 X = -5251808
68
Y = -12784766
99 feet Y = -3896796
98 meter
Z = -5242818
51 Z = -1598011
08
XDOT = 4997
037528 XDOT = 1523
097038
YDOT = -14423
042897 feet/sec YDOT = -4396
143475 meter/sec
ZDOT = 18885
054332 ZDOT = 5756
164560
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 11074
66978054
00016717 00000-0 10270-3 0 9195
2 25544 51
6439 280
6247 0006281 68
4707 291
7125 15
72467931 26187
Satellite: ISS
Catalog Number: 25544
Epoch time: 11074
66978054 = yrday
fracday
Element set: 919
Inclination: 51
6439 deg
RA of node: 280
6247 deg
Eccentricity:
0006281
Arg of perigee: 68
4707 deg
Mean anomaly: 291
7125 deg
Mean motion: 15
72467931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2618
Checksum: 336
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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