[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 11th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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
116/12:16:31
617 3
6 6
0 6
0
N/A -2
1 -0
1 214
2
000/00:13:01
235 -4
3 -0
1 212
7
Coasting Arc #1 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2012/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2358856
69 A = 6775225
13 meter
Y = 5917822
59 meter E =
0006230
Z = 2295620
68 I = 51
99847
XDOT = -3936
130000 Wp = 56
58080
YDOT = -3689
110390 meter/sec RA = 95
37973 deg
ZDOT = 5458
227557 TA = 328
90037
MA = 328
93723
Ha = 212
365 n
mi
Hp = 211
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7739031
14 X = -2436007
32
Y = 19415428
45 feet Y = 5891013
05 meter
Z = 7531563
89 Z = 2283973
94
XDOT = -12913
812337 XDOT = -3921
100038
YDOT = -12103
380543 feet/sec YDOT = -3733
042531 meter/sec
ZDOT = 17907
570724 ZDOT = 5439
142474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -927992
37 X = -282852
08
Y = 20897743
92 feet Y = 6369632
35 meter
Z = 7483251
22 Z = 2280894
97
XDOT = -14767
388609 XDOT = -4501
100048
YDOT = -7048
893882 feet/sec YDOT = -2148
502855 meter/sec
ZDOT = 17829
422162 ZDOT = 5434
407875
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 12102
55960230
00016717 00000-0 10270-3 0 9003
2 25544 51
6392 95
8870 0008056 264
5147 95
5089 15
58227188 7632
Satellite: ISS
Catalog Number: 25544
Epoch time: 12102
55960230 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 95
8870 deg
Eccentricity:
0008056
Arg of perigee: 264
5147 deg
Mean anomaly: 95
5089 deg
Mean motion: 15
58227188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 319
Coasting Arc #2 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2012/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3589001
09 A = 6768718
42 meter
Y = -3488613
61 meter E =
0003556
Z = -4559642
26 I = 51
97804
XDOT = 2406
296401 Wp = 22
08742
YDOT = 6575
643437 meter/sec RA = 90
38958 deg
ZDOT = -3134
598271 TA = 216
65758
MA = 216
68192
Ha = 211
864 n
mi
Hp = 211
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11774937
95 X = 3649894
46
Y = -11445582
72 feet Y = -3448138
79 meter
Z = -14959456
23 Z = -4542059
07
XDOT = 7894
673232 XDOT = 2347
814565
YDOT = 21573
633324 feet/sec YDOT = 6602
225087 meter/sec
ZDOT = -10284
115061 ZDOT = -3123
050747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7159836
62 X = 2182318
20
Y = -14850997
65 feet Y = -4526584
08 meter
Z = -14886922
68 Z = -4537534
03
XDOT = 13861
606165 XDOT = 4225
017559
YDOT = 16952
767589 feet/sec YDOT = 5167
203561 meter/sec
ZDOT = -10237
167966 ZDOT = -3120
288796
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 12103
52160629
00016717 00000-0 10270-3 0 9016
2 25544 51
6389 91
0608 0007916 269
1491 90
8757 15
58209837 7789
Satellite: ISS
Catalog Number: 25544
Epoch time: 12103
52160629 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 91
0608 deg
Eccentricity:
0007916
Arg of perigee: 269
1491 deg
Mean anomaly: 90
8757 deg
Mean motion: 15
58209837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 329
Coasting Arc #3 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2012/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4174298
44 A = 6765437
03 meter
Y = 89090
66 meter E =
0005630
Z = 5328186
84 I = 51
96633
XDOT = -446
231871 Wp = 279
34794
YDOT = -7655
292954 meter/sec RA = 85
37277 deg
ZDOT = -220
900432 TA = 172
75123
MA = 172
74309
Ha = 212
062 n
mi
Hp = 211
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13695204
87 X = -4200867
51
Y = 292292
18 feet Y = 42262
68 meter
Z = 17480927
96 Z = 5307843
79
XDOT = -1464
015324 XDOT = -359
522587
YDOT = -25115
790532 feet/sec YDOT = -7659
798183 meter/sec
ZDOT = -724
738950 ZDOT = -222
857346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12754116
14 X = -3887454
60
Y = 5281382
04 feet Y = 1609765
24 meter
Z = 17397311
24 Z = 5302700
47
XDOT = -10088
786128 XDOT = -3075
062012
YDOT = -21944
234023 feet/sec YDOT = -6688
602530 meter/sec
ZDOT = -732
178398 ZDOT = -223
167976
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 12104
54772519
00016717 00000-0 10270-3 0 9027
2 25544 51
6388 85
9135 0008004 273
5260 86
4979 15
58235069 7948
Satellite: ISS
Catalog Number: 25544
Epoch time: 12104
54772519 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 85
9135 deg
Eccentricity:
0008004
Arg of perigee: 273
5260 deg
Mean anomaly: 86
4979 deg
Mean motion: 15
58235069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 329
Coasting Arc #4 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2012/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4004981
11 A = 6769434
64 meter
Y = 3310313
13 meter E =
0001966
Z = -4340358
40 I = 51
97642
XDOT = -1661
144905 Wp = 175
80986
YDOT = 6616
403540 meter/sec RA = 80
35772 deg
ZDOT = 3511
612721 TA = 129
71970
MA = 129
70237
Ha = 212
753 n
mi
Hp = 211
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13139701
82 X = 3988751
29
Y = 10860607
39 feet Y = 3355008
35 meter
Z = -14240021
00 Z = -4320942
02
XDOT = -5449
950476 XDOT = -1752
065989
YDOT = 21707
360697 feet/sec YDOT = 6597
319397 meter/sec
ZDOT = 11521
039112 ZDOT = 3503
321803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16354369
68 X = 4984811
88
Y = 5039653
53 feet Y = 1536086
40 meter
Z = -14160481
62 Z = -4316114
80
XDOT = 3483
053841 XDOT = 1061
634811
YDOT = 20988
515092 feet/sec YDOT = 6397
299400 meter/sec
ZDOT = 11486
433851 ZDOT = 3501
065038
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 12105
50969483
00016717 00000-0 10270-3 0 9033
2 25544 51
6389 81
0878 0007983 277
5451 82
4797 15
58250006 8090
Satellite: ISS
Catalog Number: 25544
Epoch time: 12105
50969483 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 81
0878 deg
Eccentricity:
0007983
Arg of perigee: 277
5451 deg
Mean anomaly: 82
4797 deg
Mean motion: 15
58250006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 337
Coasting Arc #5 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2012/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3037562
74 A = 6775688
12 meter
Y = -5745259
03 meter E =
0006287
Z = 1904143
45 I = 51
99198
XDOT = 3578
495850 Wp = 127
93891
YDOT = -3766
753093 meter/sec RA = 75
37134 deg
ZDOT = -5647
774405 TA = 31
15373
MA = 31
11647
Ha = 212
809 n
mi
Hp = 211
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9965757
01 X = -2982342
21
Y = -18849275
03 feet Y = -5778918
05 meter
Z = 6247189
81 Z = 1889521
65
XDOT = 11740
471950 XDOT = 3647
786060
YDOT = -12358
113821 feet/sec YDOT = -3726
349092 meter/sec
ZDOT = -18529
443585 ZDOT = -5630
221705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16631181
84 X = -5069184
22
Y = -13369996
21 feet Y = -4075174
85 meter
Z = 6187556
43 Z = 1885967
20
XDOT = 5037
305916 XDOT = 1535
370843
YDOT = -14821
386898 feet/sec YDOT = -4517
558727 meter/sec
ZDOT = -18456
993959 ZDOT = -5625
691759
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 12106
53577830
00016717 00000-0 10270-3 0 9049
2 25544 51
6390 75
9399 0008070 281
8613 78
1636 15
58309073 8259
Satellite: ISS
Catalog Number: 25544
Epoch time: 12106
53577830 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 75
9399 deg
Eccentricity:
0008070
Arg of perigee: 281
8613 deg
Mean anomaly: 78
1636 deg
Mean motion: 15
58309073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 322
Coasting Arc #6 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2012/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1351455
05 A = 6776479
87 meter
Y = 6529087
42 meter E =
0010028
Z = 1172419
91 I = 51
98652
XDOT = -4911
366254 Wp = 22
56748
YDOT = -44
281118 meter/sec RA = 70
40525 deg
ZDOT = 5900
344484 TA = 350
13065
MA = 350
15033
Ha = 212
914 n
mi
Hp = 211
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4433907
66 X = 1272649
67
Y = 21420890
47 feet Y = 6543759
69 meter
Z = 3846522
01 Z = 1178793
29
XDOT = -16113
406345 XDOT = -4939
168651
YDOT = -145
279259 feet/sec YDOT = -99
358039 meter/sec
ZDOT = 19358
085576 ZDOT = 5876
417730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12814210
50 X = 3905771
36
Y = 17723206
11 feet Y = 5402033
22 meter
Z = 3872181
82 Z = 1180241
02
XDOT = -13567
355519 XDOT = -4135
329962
YDOT = 5596
145767 feet/sec YDOT = 1705
705230 meter/sec
ZDOT = 19259
746464 ZDOT = 5870
370722
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 12107
56184271
00016717 00000-0 10270-3 0 9057
2 25544 51
6392 70
7920 0008008 284
3350 75
6916 15
58355187 8419
Satellite: ISS
Catalog Number: 25544
Epoch time: 12107
56184271 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 70
7920 deg
Eccentricity:
0008008
Arg of perigee: 284
3350 deg
Mean anomaly: 75
6916 deg
Mean motion: 15
58355187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 310
Coasting Arc #7 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2012/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 807687
77 A = 6770702
38 meter
Y = -5502846
72 meter E =
0004589
Z = -3863416
13 I = 51
95697
XDOT = 5274
574065 Wp = 340
65334
YDOT = 3700
930440 meter/sec RA = 65
42457 deg
ZDOT = -4163
077756 TA = 245
76568
MA = 245
81364
Ha = 213
182 n
mi
Hp = 211
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2649894
25 X = 887929
39
Y = -18053959
05 feet Y = -5493366
33 meter
Z = -12675249
79 Z = -3859297
03
XDOT = 17305
033023 XDOT = 5253
020887
YDOT = 12142
160236 feet/sec YDOT = 3759
793129 meter/sec
ZDOT = -13658
391589 ZDOT = -4137
506651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5225743
63 X = -1592806
66
Y = -17495699
16 feet Y = -5332689
10 meter
Z = -12657861
14 Z = -3858116
07
XDOT = 19627
861988 XDOT = 5982
572334
YDOT = 3956
598497 feet/sec YDOT = 1205
971222 meter/sec
ZDOT = -13553
601098 ZDOT = -4131
137615
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 12108
52376309
00016717 00000-0 10270-3 0 9060
2 25544 51
6400 65
9657 0008081 289
4464 70
5818 15
58364475 8566
Satellite: ISS
Catalog Number: 25544
Epoch time: 12108
52376309 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 65
9657 deg
Eccentricity:
0008081
Arg of perigee: 289
4464 deg
Mean anomaly: 70
5818 deg
Mean motion: 15
58364475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 330
Coasting Arc #8 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2012/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3015354
32 A = 6765255
72 meter
Y = 3021911
92 meter E =
0004712
Z = 5252004
86 I = 51
92605
XDOT = -4427
458894 Wp = 285
02422
YDOT = -6183
075050 meter/sec RA = 60
41213 deg
ZDOT = 1017
627383 TA = 155
28749
MA = 155
26491
Ha = 213
388 n
mi
Hp = 210
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9892894
76 X = -3074435
13
Y = 9914409
19 feet Y = 2987862
45 meter
Z = 17230987
07 Z = 5237212
52
XDOT = -14525
783774 XDOT = -4362
932884
YDOT = -20285
679298 feet/sec YDOT = -6232
224766 meter/sec
ZDOT = 3338
672517 ZDOT = 996
276034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4591540
96 X = -1399501
68
Y = 13311006
20 feet Y = 4057194
69 meter
Z = 17169934
70 Z = 5233396
10
XDOT = -21037
833270 XDOT = -6412
331581
YDOT = -11442
637392 feet/sec YDOT = -3487
715877 meter/sec
ZDOT = 3251
444636 ZDOT = 991
040325
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 12109
54979190
00016717 00000-0 10270-3 0 9071
2 25544 51
6406 60
8183 0008212 292
7375 67
2912 15
58403206 8726
Satellite: ISS
Catalog Number: 25544
Epoch time: 12109
54979190 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 60
8183 deg
Eccentricity:
0008212
Arg of perigee: 292
7375 deg
Mean anomaly: 67
2912 deg
Mean motion: 15
58403206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 311
Coasting Arc #9 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2012/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4710126
61 A = 6766968
98 meter
Y = 118991
55 meter E =
0003821
Z = -4860444
26 I = 51
91602
XDOT = 2378
900450 Wp = 88
37168
YDOT = 6861
352478 meter/sec RA = 55
38706 deg
ZDOT = 2475
084195 TA = 205
81469
MA = 205
83376
Ha = 213
620 n
mi
Hp = 210
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15453171
28 X = 4732057
19
Y = 390392
24 feet Y = 171785
37 meter
Z = -15946339
44 Z = -4837509
13
XDOT = 7804
791502 XDOT = 2289
975053
YDOT = 22510
998942 feet/sec YDOT = 6887
457785 meter/sec
ZDOT = 8120
354969 ZDOT = 2486
424433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14009472
48 X = 4270087
21
Y = -6759034
84 feet Y = -2060153
82 meter
Z = -15852090
68 Z = -4831717
24
XDOT = 16691
943096 XDOT = 5087
704256
YDOT = 15458
474916 feet/sec YDOT = 4711
743154 meter/sec
ZDOT = 8166
366647 ZDOT = 2489
108554
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 12110
51167804
00016717 00000-0 10270-3 0 9082
2 25544 51
6409 55
9916 0008186 296
6143 63
4173 15
58406704 8873
Satellite: ISS
Catalog Number: 25544
Epoch time: 12110
51167804 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 55
9916 deg
Eccentricity:
0008186
Arg of perigee: 296
6143 deg
Mean anomaly: 63
4173 deg
Mean motion: 15
58406704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 319
Coasting Arc #10 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2012/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5364600
07 A = 6773545
37 meter
Y = -3040505
27 meter E =
0006417
Z = 2800174
90 I = 51
92116
XDOT = 528
478623 Wp = 74
38289
YDOT = -5674
199512 meter/sec RA = 50
38552 deg
ZDOT = -5137
294977 TA = 73
93075
MA = 73
86010
Ha = 213
639 n
mi
Hp = 210
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17600393
93 X = -5343804
65
Y = -9975410
99 feet Y = -3100379
11 meter
Z = 9186925
52 Z = 2774164
20
XDOT = 1733
853751 XDOT = 616
845609
YDOT = -18616
140130 feet/sec YDOT = -5667
795951 meter/sec
ZDOT = -16854
642314 ZDOT = -5134
512634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20273688
43 X = -6179420
23
Y = -456091
34 feet Y = -139016
64 meter
Z = 9080298
99 Z = 2767675
13
XDOT = -7205
175432 XDOT = -2196
137472
YDOT = -15799
720278 feet/sec YDOT = -4815
754741 meter/sec
ZDOT = -16842
705442 ZDOT = -5133
656619
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 12111
53767131
00016717 00000-0 10270-3 0 9095
2 25544 51
6418 50
8439 0008195 300
6782 59
3564 15
58445622 9031
Satellite: ISS
Catalog Number: 25544
Epoch time: 12111
53767131 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 50
8439 deg
Eccentricity:
0008195
Arg of perigee: 300
6782 deg
Mean anomaly: 59
3564 deg
Mean motion: 15
58445622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 903
Checksum: 310
Coasting Arc #11 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2012/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4623158
47 A = 6776739
85 meter
Y = 4937655
57 meter E =
0013310
Z = 221894
68 I = 51
91188
XDOT = -3596
313390 Wp = 10
58520
YDOT = 3093
871144 meter/sec RA = 45
41074 deg
ZDOT = 6038
925364 TA = 351
80227
MA = 351
82400
Ha = 213
807 n
mi
Hp = 210
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15167842
74 X = 4566523
06
Y = 16199657
38 feet Y = 4989037
93 meter
Z = 728000
92 Z = 244216
40
XDOT = -11798
928445 XDOT = -3659
978653
YDOT = 10150
495880 feet/sec YDOT = 3053
299224 meter/sec
ZDOT = 19812
747258 ZDOT = 6021
299554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21134886
05 X = 6441913
27
Y = 6757788
02 feet Y = 2059773
79 meter
Z = 819286
97 Z = 249718
67
XDOT = -4969
021695 XDOT = -1514
557813
YDOT = 13131
651623 feet/sec YDOT = 4002
527415 meter/sec
ZDOT = 19740
032894 ZDOT = 6016
762026
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 12112
56364606
00016717 00000-0 10270-3 0 9101
2 25544 51
6418 45
6957 0008237 304
3162 55
7213 15
58462319 9198
Satellite: ISS
Catalog Number: 25544
Epoch time: 12112
56364606 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 45
6957 deg
Eccentricity:
0008237
Arg of perigee: 304
3162 deg
Mean anomaly: 55
7213 deg
Mean motion: 15
58462319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 303
Coasting Arc #12 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2012/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2519899
28 A = 6772286
39 meter
Y = -5424679
53 meter E =
0004695
Z = -3179148
03 I = 51
87649
XDOT = 5948
958089 Wp = 334
55762
YDOT = 77
636020 meter/sec RA = 40
43190 deg
ZDOT = -4841
035534 TA = 242
06893
MA = 242
11647
Ha = 213
895 n
mi
Hp = 209
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8267386
09 X = -2443608
26
Y = -17797505
01 feet Y = -5452432
11 meter
Z = -10430275
69 Z = -3191204
37
XDOT = 19517
579033 XDOT = 5971
164894
YDOT = 254
711353 feet/sec YDOT = 144
284998 meter/sec
ZDOT = -15882
662512 ZDOT = -4812
081295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16032756
11 X = -4886784
06
Y = -11270585
07 feet Y = -3435274
33 meter
Z = -10479320
20 Z = -3194096
80
XDOT = 16266
411294 XDOT = 4958
002162
YDOT = -8461
911054 feet/sec YDOT = -2579
190489 meter/sec
ZDOT = -15763
682598 ZDOT = -4804
770456
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 12113
52547987
00016717 00000-0 10270-3 0 9114
2 25544 51
6429 40
8697 0008229 308
1514 51
8899 15
58506532 9342
Satellite: ISS
Catalog Number: 25544
Epoch time: 12113
52547987 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 40
8697 deg
Eccentricity:
0008229
Arg of perigee: 308
1514 deg
Mean anomaly: 51
8899 deg
Mean motion: 15
58506532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 330
Coasting Arc #13 (Orbit 949)
---------------------------------------
Vector Time (GMT): 2012/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -500876
12 A = 6765727
35 meter
Y = 4496602
90 meter E =
0002665
Z = 5031087
29 I = 51
83091
XDOT = -6808
445251 Wp = 324
14210
YDOT = -2950
105716 meter/sec RA = 35
42012 deg
ZDOT = 1961
505989 TA = 106
90238
MA = 106
87316
Ha = 214
002 n
mi
Hp = 209
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1643294
35 X = -575561
14
Y = 14752634
18 feet Y = 4490584
24 meter
Z = 16506191
90 Z = 5028472
57
XDOT = -22337
418804 XDOT = -6784
479269
YDOT = -9678
824526 feet/sec YDOT = -3026
107946 meter/sec
ZDOT = 6435
387103 ZDOT = 1928
488518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6135432
16 X = 1870079
72
Y = 13530175
99 feet Y = 4123997
64 meter
Z = 16495023
87 Z = 5027683
27
XDOT = -23170
690843 XDOT = -7062
426569
YDOT = 2837
094440 feet/sec YDOT = 864
746385 meter/sec
ZDOT = 6299
981539 ZDOT = 1920
234373
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
55141723
00016717 00000-0 10270-3 0 9127
2 25544 51
6428 35
7216 0008258 310
8522 49
1917 15
58547830 9507
Satellite: ISS
Catalog Number: 25544
Epoch time: 12114
55141723 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 35
7216 deg
Eccentricity:
0008258
Arg of perigee: 310
8522 deg
Mean anomaly: 49
1917 deg
Mean motion: 15
58547830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 950
Checksum: 298
Coasting Arc #14 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2012/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3590781
64 A = 6765382
43 meter
Y = -2573102
06 meter E =
0007953
Z = -5129654
82 I = 51
80469
XDOT = 5741
601404 Wp = 67
58724
YDOT = 4828
096248 meter/sec RA = 30
38622 deg
ZDOT = 1602
248386 TA = 217
79761
MA = 217
85350
Ha = 214
219 n
mi
Hp = 209
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11780779
67 X = 3644206
82
Y = -8441935
88 feet Y = -2532648
96 meter
Z = -16829576
19 Z = -5112080
94
XDOT = 18837
274947 XDOT = 5679
402434
YDOT = 15840
210787 feet/sec YDOT = 4891
954601 meter/sec
ZDOT = 5256
720427 ZDOT = 1629
990223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5575407
96 X = 1699384
35
Y = -13468545
23 feet Y = -4105212
59 meter
Z = -16757111
95 Z = -5107567
72
XDOT = 23366
678077 XDOT = 7122
163478
YDOT = 3011
559691 feet/sec YDOT = 917
923394 meter/sec
ZDOT = 5370
261314 ZDOT = 1636
855648
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
51321839
00016717 00000-0 10270-3 0 9133
2 25544 51
6433 30
8949 0008289 315
1978 44
8507 15
58552062 9655
Satellite: ISS
Catalog Number: 25544
Epoch time: 12115
51321839 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 30
8949 deg
Eccentricity:
0008289
Arg of perigee: 315
1978 deg
Mean anomaly: 44
8507 deg
Mean motion: 15
58552062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 322
Coasting Arc #15 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5844569
87 A = 6771591
92 meter
Y = 202364
12 meter E =
0009336
Z = 3414136
28 I = 51
79842
XDOT = -2894
569829 Wp = 48
82076
YDOT = -5397
112602 meter/sec RA = 25
36766 deg
ZDOT = -4621
034660 TA = 91
26988
MA = 91
16293
Ha = 214
302 n
mi
Hp = 209
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19175098
00 X = -5862983
69
Y = 663924
28 feet Y = 136903
52 meter
Z = 11201234
50 Z = 3385698
51
XDOT = -9496
620175 XDOT = -2811
554845
YDOT = -17707
062343 feet/sec YDOT = -5429
017238 meter/sec
ZDOT = -15160
874870 ZDOT = -4634
894978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15756418
78 X = -4802556
44
Y = 11066400
61 feet Y = 3373038
91 meter
Z = 11084352
84 Z = 3378510
75
XDOT = -16742
150371 XDOT = -5103
007433
YDOT = -8548
429240 feet/sec YDOT = -2605
561232 meter/sec
ZDOT = -15217
309757 ZDOT = -4638
236014
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
53912104
00016717 00000-0 10270-3 0 9148
2 25544 51
6430 25
7467 0008249 318
9024 41
1509 15
58568332 9816
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53912104 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 25
7467 deg
Eccentricity:
0008249
Arg of perigee: 318
9024 deg
Mean anomaly: 41
1509 deg
Mean motion: 15
58568332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 298
Coasting Arc #16 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:23:02
235
Vector Time (MET): N/A
Weight (LBS) : 924784
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2583212
56 A = 6772785
40 meter
Y = -4763665
74 meter E =
0004160
Z = -4065135
94 I = 51
79165
XDOT = 6605
661096 Wp = 351
77627
YDOT = -259
391261 meter/sec RA = 25
33781 deg
ZDOT = -3889
128614 TA = 238
01452
MA = 238
05496
Ha = 214
229 n
mi
Hp = 212
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8475106
83 X = -2510004
52
Y = -15628824
61 feet Y = -4792143
43 meter
Z = -13337060
16 Z = -4077507
49
XDOT = 21672
116457 XDOT = 6626
963471
YDOT = -851
021199 feet/sec YDOT = -185
403506 meter/sec
ZDOT = -12759
608313 ZDOT = -3856
986442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16344740
43 X = -4981876
88
Y = -6898602
80 feet Y = -2102694
13 meter
Z = -13387438
44 Z = -4080491
24
XDOT = 15893
562544 XDOT = 4844
357863
YDOT = -13122
790959 feet/sec YDOT = -3999
826684 meter/sec
ZDOT = -12627
498166 ZDOT = -3848
861441
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
53913757
00016717 00000-0 10270-3 0 9154
2 25544 51
6439 25
7469 0007728 283
2217 76
8075 15
57388024 9816
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53913757 = yrday
fracday
Element set: 915
Inclination: 51
6439 deg
RA of node: 25
7469 deg
Eccentricity:
0007728
Arg of perigee: 283
2217 deg
Mean anomaly: 76
8075 deg
Mean motion: 15
57388024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 334
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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