[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 24th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
116/12:21:04
462 6
1 7
0 7
1
N/A -1
3 -0
9 214
6
000/00:16:08
924 -3
3 0
0 212
8
125/08:45:59
093 1
1 8
7 8
7
N/A -5
9 -0
1 216
0
000/00:21:58
187 -6
3 -0
1 215
0
Coasting Arc #1 (Orbit 949)
---------------------------------------
Vector Time (GMT): 2012/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -662124
44 A = 6765227
73 meter
Y = 4425025
26 meter E =
0003200
Z = 5075501
28 I = 51
83071
XDOT = -6790
461914 Wp = 319
10212
YDOT = -3086
282994 meter/sec RA = 35
42532 deg
ZDOT = 1807
899049 TA = 113
47974
MA = 113
44610
Ha = 213
870 n
mi
Hp = 209
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2172324
29 X = -736212
84
Y = 14517799
43 feet Y = 4417206
76 meter
Z = 16651907
08 Z = 5072104
66
XDOT = -22278
418354 XDOT = -6764
228306
YDOT = -10125
600374 feet/sec YDOT = -3162
071445 meter/sec
ZDOT = 5931
427325 ZDOT = 1774
974451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5560436
75 X = 1694821
12
Y = 13603145
01 feet Y = 4146238
60 meter
Z = 16637532
61 Z = 5071119
94
XDOT = -23343
253107 XDOT = -7115
023547
YDOT = 2464
482231 feet/sec YDOT = 751
174184 meter/sec
ZDOT = 5796
416217 ZDOT = 1766
747663
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 12114
55114008
00016717 00000-0 10270-3 0 9000
2 25544 51
6431 35
7296 0008468 310
5327 49
5090 15
58655618 9502
Satellite: ISS
Catalog Number: 25544
Epoch time: 12114
55114008 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 35
7296 deg
Eccentricity:
0008468
Arg of perigee: 310
5327 deg
Mean anomaly: 49
5090 deg
Mean motion: 15
58655618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 950
Checksum: 296
Coasting Arc #2 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2012/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3760179
01 A = 6765259
25 meter
Y = -2426796
34 meter E =
0007352
Z = -5078541
83 I = 51
80584
XDOT = 5600
560971 Wp = 66
78682
YDOT = 4924
720729 meter/sec RA = 30
39026 deg
ZDOT = 1798
281459 TA = 220
53891
MA = 220
59370
Ha = 214
068 n
mi
Hp = 209
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12336545
32 X = 3811707
28
Y = -7961930
25 feet Y = -2384459
55 meter
Z = -16661882
64 Z = -5060149
61
XDOT = 18374
543867 XDOT = 5536
339710
YDOT = 16157
220240 feet/sec YDOT = 4986
990572 meter/sec
ZDOT = 5899
873552 ZDOT = 1825
333205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6300451
99 X = 1920377
77
Y = -13356931
50 feet Y = -4071192
72 meter
Z = -16586069
53 Z = -5055433
99
XDOT = 23148
165010 XDOT = 7055
560695
YDOT = 3475
307897 feet/sec YDOT = 1059
273847 meter/sec
ZDOT = 6010
569346 ZDOT = 1832
021537
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 12115
51287130
00016717 00000-0 10270-3 0 9015
2 25544 51
6436 30
9025 0008488 314
7829 45
2635 15
58671602 9654
Satellite: ISS
Catalog Number: 25544
Epoch time: 12115
51287130 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 30
9025 deg
Eccentricity:
0008488
Arg of perigee: 314
7829 deg
Mean anomaly: 45
2635 deg
Mean motion: 15
58671602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 303
Coasting Arc #3 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5945962
82 A = 6771693
63 meter
Y = 2459
66 meter E =
0009059
Z = 3240648
29 I = 51
80048
XDOT = -2614
844455 Wp = 52
12603
YDOT = -5402
304534 meter/sec RA = 25
37269 deg
ZDOT = -4779
109775 TA = 90
35990
MA = 90
25609
Ha = 214
113 n
mi
Hp = 209
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19507752
03 X = -5961290
95
Y = 8069
74 feet Y = -64117
53 meter
Z = 10632048
19 Z = 3211725
45
XDOT = -8578
886008 XDOT = -2531
024300
YDOT = -17724
096239 feet/sec YDOT = -5431
076603 meter/sec
ZDOT = -15679
494011 ZDOT = -4791
609225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16390391
46 X = -4995791
32
Y = 10696763
72 feet Y = 3260373
58 meter
Z = 10513192
50 Z = 3204421
07
XDOT = -16007
028035 XDOT = -4878
942145
YDOT = -9019
437191 feet/sec YDOT = -2749
124456 meter/sec
ZDOT = -15730
336053 ZDOT = -4794
606429
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 12116
53869022
00016717 00000-0 10270-3 0 9025
2 25544 51
6433 25
7538 0008441 318
3246 41
7265 15
58701725 9812
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53869022 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 25
7538 deg
Eccentricity:
0008441
Arg of perigee: 318
3246 deg
Mean anomaly: 41
7265 deg
Mean motion: 15
58701725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 301
Coasting Arc #4 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 257345
18 A = 6768852
99 meter
Y = -4375680
26 meter E =
0006129
Z = -5162272
83 I = 51
77618
XDOT = 7218
708603 Wp = 38
40482
YDOT = 2145
574081 meter/sec RA = 25
30595 deg
ZDOT = -1455
020464 TA = 217
60029
MA = 217
64316
Ha = 214
619 n
mi
Hp = 212
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 844308
35 X = 331333
29
Y = -14355906
38 feet Y = -4372388
70 meter
Z = -16936590
63 Z = -5160842
99
XDOT = 23683
427174 XDOT = 7201
248098
YDOT = 7039
285042 feet/sec YDOT = 2226
200540 meter/sec
ZDOT = -4773
689185 ZDOT = -1419
994213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8585825
48 X = -2616959
61
Y = -11545642
09 feet Y = -3519111
71 meter
Z = -16930291
09 Z = -5160352
72
XDOT = 21775
874519 XDOT = 6637
286553
YDOT = -9386
061162 feet/sec YDOT = -2860
871442 meter/sec
ZDOT = -4629
960168 ZDOT = -1411
211859
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 12116
53870324
00016717 00000-0 10270-3 0 9033
2 25544 51
6426 25
7521 0010027 282
6747 77
3286 15
57278909 9818
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53870324 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 25
7521 deg
Eccentricity:
0010027
Arg of perigee: 282
6747 deg
Mean anomaly: 77
3286 deg
Mean motion: 15
57278909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 315
Coasting Arc #5 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2012/117/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3146639
11 A = 6768995
28 meter
Y = 3135316
93 meter E =
0008063
Z = 5113891
24 I = 51
74878
XDOT = -6463
412897 Wp = 315
75735
YDOT = -3779
877196 meter/sec RA = 20
28104 deg
ZDOT = -1655
510598 TA = 150
22229
MA = 150
17638
Ha = 214
912 n
mi
Hp = 212
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10323619
13 X = -3206307
38
Y = 10286472
87 feet Y = 3099795
55 meter
Z = 16777858
40 Z = 5098459
97
XDOT = -21205
422890 XDOT = -6412
622984
YDOT = -12401
171903 feet/sec YDOT = -3851
871064 meter/sec
ZDOT = -5431
465218 ZDOT = -1686
786590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1017884
32 X = -310251
14
Y = 14611182
07 feet Y = 4453488
29 meter
Z = 16714138
88 Z = 5094469
53
XDOT = -23017
408861 XDOT = -7015
706221
YDOT = 4771
636958 feet/sec YDOT = 1454
394945 meter/sec
ZDOT = -5559
621100 ZDOT = -1694
572511
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 12117
56545362
00016717 00000-0 10270-3 0 9049
2 25544 51
6424 20
6090 0010224 286
3683 73
6347 15
57331664 9972
Satellite: ISS
Catalog Number: 25544
Epoch time: 12117
56545362 = yrday
fracday
Element set: 904
Inclination: 51
6424 deg
RA of node: 20
6090 deg
Eccentricity:
0010224
Arg of perigee: 286
3683 deg
Mean anomaly: 73
6347 deg
Mean motion: 15
57331664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 305
Coasting Arc #6 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2012/118/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5464935
08 A = 6774315
14 meter
Y = -1528421
30 meter E =
0004837
Z = -3694164
48 I = 51
73798
XDOT = 4244
985923 Wp = 301
16660
YDOT = 4701
055482 meter/sec RA = 15
26708 deg
ZDOT = 4333
037634 TA = 14
81944
MA = 14
80527
Ha = 215
225 n
mi
Hp = 212
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17929577
04 X = 5499565
58
Y = -5014505
59 feet Y = -1467115
34 meter
Z = -12119962
19 Z = -3667531
77
XDOT = 13927
119171 XDOT = 4171
053191
YDOT = 15423
410375 feet/sec YDOT = 4748
112099 meter/sec
ZDOT = 14216
002735 ZDOT = 4353
480222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9917500
35 X = 3022854
11
Y = -15839909
13 feet Y = -4828004
30 meter
Z = -12010368
37 Z = -3660760
28
XDOT = 19465
418830 XDOT = 5933
059659
YDOT = 1340
683745 feet/sec YDOT = 408
640406 meter/sec
ZDOT = 14299
546945 ZDOT = 4358
501909
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 12118
52801088
00016717 00000-0 10270-3 0 9057
2 25544 51
6427 15
7869 0010235 289
9761 70
0291 15
57334604 10127
Satellite: ISS
Catalog Number: 25544
Epoch time: 12118
52801088 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 15
7869 deg
Eccentricity:
0010235
Arg of perigee: 289
9761 deg
Mean anomaly: 70
0291 deg
Mean motion: 15
57334604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 298
Coasting Arc #7 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2012/119/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6654063
74 A = 6779369
75 meter
Y = -187786
43 meter E =
0004038
Z = 1270391
12 I = 51
72528
XDOT = -980
284106 Wp = 143
06769
YDOT = -4866
834257 meter/sec RA = 10
27722 deg
ZDOT = -5847
459079 TA = 23
11730
MA = 23
09913
Ha = 215
306 n
mi
Hp = 212
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21830917
79 X = -6657640
64
Y = -616097
20 feet Y = -262216
29 meter
Z = 4167949
88 Z = 1238057
11
XDOT = -3216
155205 XDOT = -897
383527
YDOT = -15967
303992 feet/sec YDOT = -4877
332848 meter/sec
ZDOT = -19184
577032 ZDOT = -5852
019941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16311215
13 X = -4971658
37
Y = 14560309
12 feet Y = 4437982
22 meter
Z = 4035097
64 Z = 1229897
76
XDOT = -12156
597967 XDOT = -3705
331060
YDOT = -8290
680854 feet/sec YDOT = -2526
999524 meter/sec
ZDOT = -19202
839737 ZDOT = -5853
025552
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 12119
55471459
00016717 00000-0 10270-3 0 9067
2 25544 51
6426 10
6437 0010132 293
0522 66
9564 15
57337982 10284
Satellite: ISS
Catalog Number: 25544
Epoch time: 12119
55471459 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 10
6437 deg
Eccentricity:
0010132
Arg of perigee: 293
0522 deg
Mean anomaly: 66
9564 deg
Mean motion: 15
57337982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1028
Checksum: 305
Coasting Arc #8 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2012/120/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6353771
96 A = 6778800
30 meter
Y = 1787084
40 meter E =
0011660
Z = 1510292
25 I = 51
69407
XDOT = -2593
832084 Wp = 15
12483
YDOT = 4341
609341 meter/sec RA = 5
29587 deg
ZDOT = 5775
877516 TA = 1
38934
MA = 1
38610
Ha = 215
461 n
mi
Hp = 211
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20845708
54 X = 6325979
50
Y = 5863137
80 feet Y = 1857980
82 meter
Z = 4955027
06 Z = 1541091
22
XDOT = -8509
947783 XDOT = -2670
246111
YDOT = 14244
125135 feet/sec YDOT = 4312
176294 meter/sec
ZDOT = 18949
729384 ZDOT = 5763
091094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18982709
47 X = 5785929
85
Y = -10358969
42 feet Y = -3157413
88 meter
Z = 5081410
87 Z = 1548814
03
XDOT = 3035
966353 XDOT = 925
362544
YDOT = 14831
327496 feet/sec YDOT = 4520
588621 meter/sec
ZDOT = 18896
759656 ZDOT = 5759
732343
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 12120
58139111
00016717 00000-0 10270-3 0 9079
2 25544 51
6427 5
4993 0010383 297
6499 62
3601 15
57406011 10445
Satellite: ISS
Catalog Number: 25544
Epoch time: 12120
58139111 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 5
4993 deg
Eccentricity:
0010383
Arg of perigee: 297
6499 deg
Mean anomaly: 62
3601 deg
Mean motion: 15
57406011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 288
Coasting Arc #9 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2012/121/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4613637
45 A = 6773252
98 meter
Y = -3093583
82 meter E =
0007670
Z = -3878984
24 I = 51
64515
XDOT = 5619
909675 Wp = 338
15447
YDOT = -3220
226378 meter/sec RA =
29893 deg
ZDOT = -4106
496233 TA = 248
74039
MA = 248
82232
Ha = 215
654 n
mi
Hp = 211
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15136605
82 X = -4559858
13
Y = -10149553
22 feet Y = -3144875
76 meter
Z = -12726326
26 Z = -3901266
53
XDOT = 18438
023867 XDOT = 5675
449768
YDOT = -10565
047173 feet/sec YDOT = -3157
070616 meter/sec
ZDOT = -13472
756669 ZDOT = -4079
059824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17804744
40 X = -5426886
09
Y = 3576356
43 feet Y = 1090073
44 meter
Z = -12817581
61 Z = -3906798
87
XDOT = 5763
138599 XDOT = 1756
604645
YDOT = -19301
139633 feet/sec YDOT = -5882
987360 meter/sec
ZDOT = -13359
702008 ZDOT = -4072
037172
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 12121
54387869
00016717 00000-0 10270-3 0 9082
2 25544 51
6424
6774 0010529 300
4946 59
5168 15
57431283 10599
Satellite: ISS
Catalog Number: 25544
Epoch time: 12121
54387869 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node:
6774 deg
Eccentricity:
0010529
Arg of perigee: 300
4946 deg
Mean anomaly: 59
5168 deg
Mean motion: 15
57431283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1059
Checksum: 315
Coasting Arc #10 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2012/122/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1786943
76 A = 6768157
41 meter
Y = 3974233
13 meter E =
0006296
Z = 5182636
30 I = 51
59812
XDOT = -7381
419871 Wp = 304
42135
YDOT = 1638
793877 meter/sec RA = 355
27260 deg
ZDOT = 1292
988054 TA = 133
18437
MA = 133
13175
Ha = 215
824 n
mi
Hp = 211
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5862676
37 X = 1717193
96
Y = 13038822
62 feet Y = 3993826
02 meter
Z = 17003399
92 Z = 5191147
71
XDOT = -24217
256793 XDOT = -7405
477690
YDOT = 5376
620330 feet/sec YDOT = 1556
115799 meter/sec
ZDOT = 4242
086792 ZDOT = 1257
070638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13408337
55 X = 4086861
28
Y = 4839538
10 feet Y = 1475091
21 meter
Z = 17037982
09 Z = 5193176
94
XDOT = -12499
405425 XDOT = -3809
818774
YDOT = 20269
209022 feet/sec YDOT = 6178
054910 meter/sec
ZDOT = 4094
346107 ZDOT = 1247
956693
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 12122
57050940
00016717 00000-0 10270-3 0 9094
2 25544 51
6427 355
5332 0010423 304
8943 55
1232 15
57467431 10758
Satellite: ISS
Catalog Number: 25544
Epoch time: 12122
57050940 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 355
5332 deg
Eccentricity:
0010423
Arg of perigee: 304
8943 deg
Mean anomaly: 55
1232 deg
Mean motion: 15
57467431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 286
Coasting Arc #11 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2012/123/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1406135
80 A = 6768686
00 meter
Y = -4298729
28 meter E =
0005382
Z = -5038455
41 I = 51
56906
XDOT = 7434
072284 Wp = 51
71754
YDOT = 233
801001 meter/sec RA = 350
23246 deg
ZDOT = 1879
858164 TA = 236
48524
MA = 236
53667
Ha = 215
964 n
mi
Hp = 211
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4613306
43 X = 1478576
56
Y = -14103442
52 feet Y = -4282600
15 meter
Z = -16530365
53 Z = -5031448
26
XDOT = 24390
000932 XDOT = 7421
773304
YDOT = 767
063653 feet/sec YDOT = 316
864702 meter/sec
ZDOT = 6167
513661 ZDOT = 1915
943145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7171204
86 X = -2185783
24
Y = -13027986
04 feet Y = -3970930
15 meter
Z = -16501153
66 Z = -5029551
64
XDOT = 16125
390579 XDOT = 4915
019049
YDOT = -16856
381419 feet/sec YDOT = -5137
825056 meter/sec
ZDOT = 6315
750386 ZDOT = 1925
040718
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 12123
53295212
00016717 00000-0 10270-3 0 9106
2 25544 51
6416 350
7099 0010579 308
0522 51
9677 15
57529163 10909
Satellite: ISS
Catalog Number: 25544
Epoch time: 12123
53295212 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 350
7099 deg
Eccentricity:
0010579
Arg of perigee: 308
0522 deg
Mean anomaly: 51
9677 deg
Mean motion: 15
57529163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 299
Coasting Arc #12 (Orbit 1105)
---------------------------------------
Vector Time (GMT): 2012/124/12:29:08
924
Vector Time (MET): N/A
Weight (LBS) : 927128
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4256041
91 A = 6774231
40 meter
Y = 3971393
10 meter E =
0008519
Z = 3468389
31 I = 51
55864
XDOT = -5770
699991 Wp = 30
21742
YDOT = -2205
973714 meter/sec RA = 345
20718 deg
ZDOT = -4543
226225 TA = 108
97604
MA = 108
88370
Ha = 216
123 n
mi
Hp = 210
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13963392
10 X = -4316983
47
Y = 13029504
92 feet Y = 3923458
77 meter
Z = 11379230
03 Z = 3447565
13
XDOT = -18932
742751 XDOT = -5723
533080
YDOT = -7237
446569 feet/sec YDOT = -2270
241671 meter/sec
ZDOT = -14905
597850 ZDOT = -4571
145893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 392739
48 X = 119706
99
Y = 19145199
40 feet Y = 5835456
78 meter
Z = 11293285
12 Z = 3442193
31
XDOT = -16543
045785 XDOT = -5042
320355
YDOT = 9222
883855 feet/sec YDOT = 2811
134999 meter/sec
ZDOT = -15020
085238 ZDOT = -4578
121981
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 12124
55953408
00016717 00000-0 10270-3 0 9118
2 25544 51
6419 345
5662 0010783 312
0254 47
9982 15
57595231 11065
Satellite: ISS
Catalog Number: 25544
Epoch time: 12124
55953408 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 345
5662 deg
Eccentricity:
0010783
Arg of perigee: 312
0254 deg
Mean anomaly: 47
9982 deg
Mean motion: 15
57595231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1106
Checksum: 307
Coasting Arc #13 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2012/125/08:56:58
187
Vector Time (MET): N/A
Weight (LBS) : 926158
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110213
32 A = 6775456
10 meter
Y = -2566378
27 meter E =
0003868
Z = -4737756
87 I = 51
51881
XDOT = 5775
969150 Wp = 6
93883
YDOT = -4261
172381 meter/sec RA = 340
97502 deg
ZDOT = -2699
157849 TA = 236
32220
MA = 236
35909
Ha = 216
029 n
mi
Hp = 215
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13484951
85 X = -4058194
62
Y = -8419876
23 feet Y = -2612050
44 meter
Z = -15543821
77 Z = -4757598
14
XDOT = 18950
030019 XDOT = 5836
301342
YDOT = -13980
224348 feet/sec YDOT = -4196
244625 meter/sec
ZDOT = -8855
504753 ZDOT = -2670
951228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12785020
05 X = -3896874
11
Y = -9313902
58 feet Y = -2838877
51 meter
Z = -15625079
79 Z = -4762524
32
XDOT = 19233
117939 XDOT = 5862
254348
YDOT = -11720
644104 feet/sec YDOT = -3572
452323 meter/sec
ZDOT = -8739
204324 ZDOT = -2663
709478
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 12125
39364885
00016717 00000-0 10270-3 0 9127
2 25544 51
6422 341
3872 0010124 271
5042 88
4951 15
55587470 11193
Satellite: ISS
Catalog Number: 25544
Epoch time: 12125
39364885 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 341
3872 deg
Eccentricity:
0010124
Arg of perigee: 271
5042 deg
Mean anomaly: 88
4951 deg
Mean motion: 15
55587470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1119
Checksum: 304
Coasting Arc #14 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2012/126/08:56:58
187
Vector Time (MET): N/A
Weight (LBS) : 926158
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2028780
02 A = 6773026
47 meter
Y = 3711298
68 meter E =
0007785
Z = 5296731
22 I = 51
48213
XDOT = -6893
502026 Wp = 272
28345
YDOT = 3338
968334 meter/sec RA = 335
95168 deg
ZDOT = 301
531610 TA = 174
83879
MA = 174
83076
Ha = 216
391 n
mi
Hp = 214
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6656102
43 X = 1961397
80
Y = 12176176
79 feet Y = 3733608
93 meter
Z = 17377727
09 Z = 5306423
55
XDOT = -22616
476462 XDOT = -6931
791509
YDOT = 10954
620517 feet/sec YDOT = 3261
666837 meter/sec
ZDOT = 989
276935 ZDOT = 267
949522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5920816
82 X = 1804664
97
Y = 12495373
79 feet Y = 3808589
93 meter
Z = 17417173
76 Z = 5308754
56
XDOT = -22240
041282 XDOT = -6778
764583
YDOT = 9355
192560 feet/sec YDOT = 2851
462692 meter/sec
ZDOT = 850
986477 ZDOT = 259
380678
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 12126
42151809
00016717 00000-0 10270-3 0 9133
2 25544 51
6418 336
2512 0010265 275
1418 84
8564 15
55623058 11356
Satellite: ISS
Catalog Number: 25544
Epoch time: 12126
42151809 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 336
2512 deg
Eccentricity:
0010265
Arg of perigee: 275
1418 deg
Mean anomaly: 84
8564 deg
Mean motion: 15
55623058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 293
Coasting Arc #15 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2012/127/08:56:58
187
Vector Time (MET): N/A
Weight (LBS) : 926158
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 213550
95 A = 6774548
12 meter
Y = -4626707
48 meter E =
0002469
Z = -4946015
08 I = 51
46009
XDOT = 7089
166225 Wp = 135
74932
YDOT = -1977
684899 meter/sec RA = 330
92436 deg
ZDOT = 2155
009297 TA = 155
31162
MA = 155
29980
Ha = 216
821 n
mi
Hp = 215
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 700626
48 X = 289299
04
Y = -15179486
47 feet Y = -4623895
66 meter
Z = -16227083
60 Z = -4944793
86
XDOT = 23258
419372 XDOT = 7100
285419
YDOT = -6488
467516 feet/sec YDOT = -1898
347387 meter/sec
ZDOT = 7070
240475 ZDOT = 2189
475863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1312035
48 X = 399908
41
Y = -15144772
06 feet Y = -4616126
52 meter
Z = -16221602
00 Z = -4944344
29
XDOT = 22316
637330 XDOT = 6802
111058
YDOT = -5795
275396 feet/sec YDOT = -1766
399941 meter/sec
ZDOT = 7212
028684 ZDOT = 2198
226343
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 12127
38512684
00016717 00000-0 10270-3 0 9142
2 25544 51
6419 331
4359 0010320 279
2420 80
7566 15
55640816 11508
Satellite: ISS
Catalog Number: 25544
Epoch time: 12127
38512684 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 331
4359 deg
Eccentricity:
0010320
Arg of perigee: 279
2420 deg
Mean anomaly: 80
7566 deg
Mean motion: 15
55640816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1150
Checksum: 294
Coasting Arc #16 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2012/128/08:56:58
187
Vector Time (MET): N/A
Weight (LBS) : 926158
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2310364
53 A = 6778935
31 meter
Y = 5162097
20 meter E =
0003927
Z = 3739290
92 I = 51
44890
XDOT = -6377
514154 Wp = 23
40140
YDOT = 227
567980 meter/sec RA = 325
90677 deg
ZDOT = -4249
507964 TA = 111
75075
MA = 111
70895
Ha = 217
238 n
mi
Hp = 215
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7579936
12 X = -2386081
42
Y = 16936014
43 feet Y = 5135837
64 meter
Z = 12268014
83 Z = 3727883
52
XDOT = -20923
602867 XDOT = -6358
941323
YDOT = 746
614109 feet/sec YDOT = 156
354833 meter/sec
ZDOT = -13941
955262 ZDOT = -4280
445108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7934647
26 X = -2418480
48
Y = 16807312
34 feet Y = 5122868
80 meter
Z = 12220631
29 Z = 3724848
42
XDOT = -19622
275481 XDOT = -5980
869567
YDOT = 978
218000 feet/sec YDOT = 298
160846 meter/sec
ZDOT = -14069
070512 ZDOT = -4288
252692
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 12128
41295470
00016717 00000-0 10270-3 0 9159
2 25544 51
6417 326
3000 0010335 283
7113 76
2890 15
55679042 11667
Satellite: ISS
Catalog Number: 25544
Epoch time: 12128
41295470 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 326
3000 deg
Eccentricity:
0010335
Arg of perigee: 283
7113 deg
Mean anomaly: 76
2890 deg
Mean motion: 15
55679042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1166
Checksum: 290
Coasting Arc #17 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2012/129/08:56:58
187
Vector Time (MET): N/A
Weight (LBS) : 926158
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3980517
71 A = 6783316
90 meter
Y = -5155435
54 meter E =
0010329
Z = -1870121
57 I = 51
43938
XDOT = 4925
012987 Wp = 327
50868
YDOT = 1764
143239 meter/sec RA = 320
90320 deg
ZDOT = 5613
634826 TA = 11
82469
MA = 11
80045
Ha = 217
523 n
mi
Hp = 215
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13059441
30 X = 4046955
75
Y = -16914158
58 feet Y = -5110551
29 meter
Z = -6135569
44 Z = -1850623
20
XDOT = 16158
179090 XDOT = 4877
649794
YDOT = 5787
871519 feet/sec YDOT = 1818
952460 meter/sec
ZDOT = 18417
437093 ZDOT = 5637
445758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13086465
79 X = 3988754
77
Y = -16922323
29 feet Y = -5157924
14 meter
Z = -6054945
73 Z = -1845547
46
XDOT = 14815
242823 XDOT = 4515
686012
YDOT = 4825
165976 feet/sec YDOT = 1470
710590 meter/sec
ZDOT = 18515
079136 ZDOT = 5643
396121
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 12129
37652318
00016717 00000-0 10270-3 0 9164
2 25544 51
6419 321
4838 0010490 287
3107 72
6899 15
55700248 11818
Satellite: ISS
Catalog Number: 25544
Epoch time: 12129
37652318 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 321
4838 deg
Eccentricity:
0010490
Arg of perigee: 287
3107 deg
Mean anomaly: 72
6899 deg
Mean motion: 15
55700248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1181
Checksum: 316
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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