[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 26th 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
125/08:45:59
600 1
6 8
7 8
7
N/A -5
9 -0
1 216
0
000/00:21:59
201 -6
2 -0
0 214
8
Coasting Arc #1 (Orbit 981)
---------------------------------------
Vector Time (GMT): 2012/116/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3573006
13 A = 6775048
92 meter
Y = 4639764
96 meter E =
0003485
Z = 3402356
12 I = 51
79776
XDOT = -5992
017452 Wp = 50
07663
YDOT = 1213
737902 meter/sec RA = 25
19194 deg
ZDOT = 4636
436252 TA = 349
66098
MA = 349
66815
Ha = 214
566 n
mi
Hp = 212
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11722461
04 X = 3504329
68
Y = 15222325
97 feet Y = 4679336
48 meter
Z = 11162585
69 Z = 3419547
11
XDOT = -19658
849907 XDOT = -6027
667430
YDOT = 3982
079732 feet/sec YDOT = 1146
532055 meter/sec
ZDOT = 15211
405025 ZDOT = 4607
240340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19147133
90 X = 5836046
41
Y = 974945
47 feet Y = 297163
38 meter
Z = 11232780
82 Z = 3423751
59
XDOT = -9681
877049 XDOT = -2951
036124
YDOT = 16234
597182 feet/sec YDOT = 4948
305221 meter/sec
ZDOT = 15091
309757 ZDOT = 4599
831214
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
60284961
00016717 00000-0 10270-3 0 9004
2 25544 51
6436 25
4314 0009981 283
4503 76
5539 15
57329581 9828
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
60284961 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 25
4314 deg
Eccentricity:
0009981
Arg of perigee: 283
4503 deg
Mean anomaly: 76
5539 deg
Mean motion: 15
57329581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 982
Checksum: 316
Coasting Arc #2 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2012/117/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -826931
46 A = 6769195
09 meter
Y = -4498603
32 meter E =
0006791
Z = -4994281
14 I = 51
75090
XDOT = 7323
997167 Wp = 22
46320
YDOT = 955
381145 meter/sec RA = 20
18336 deg
ZDOT = -2068
032300 TA = 227
42853
MA = 227
48586
Ha = 214
778 n
mi
Hp = 212
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2713029
73 X = -752304
37
Y = -14759197
25 feet Y = -4507433
23 meter
Z = -16385436
81 Z = -4998117
19
XDOT = 24028
862097 XDOT = 7322
815698
YDOT = 3134
452576 feet/sec YDOT = 1037
276041 meter/sec
ZDOT = -6784
882874 ZDOT = -2032
455139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13068775
36 X = -3983362
73
Y = -7341602
33 feet Y = -2237720
39 meter
Z = -16400760
93 Z = -4998951
93
XDOT = 17154
360613 XDOT = 5228
649115
YDOT = -15667
664198 feet/sec YDOT = -4775
504047 meter/sec
ZDOT = -6638
775746 ZDOT = -2023
498847
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
56537578
00016717 00000-0 10270-3 0 9016
2 25544 51
6437 20
6098 0010138 286
9992 73
0051 15
57401701 9973
Satellite: ISS
Catalog Number: 25544
Epoch time: 12117
56537578 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 20
6098 deg
Eccentricity:
0010138
Arg of perigee: 286
9992 deg
Mean anomaly: 73
0051 deg
Mean motion: 15
57401701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 313
Coasting Arc #3 (Orbit 1012)
---------------------------------------
Vector Time (GMT): 2012/118/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2251129
88 A = 6768119
42 meter
Y = 3667124
50 meter E =
0008544
Z = 5230611
15 I = 51
71872
XDOT = -7060
472036 Wp = 311
12616
YDOT = -2792
569599 meter/sec RA = 15
15537 deg
ZDOT = -1076
470824 TA = 149
20024
MA = 149
15008
Ha = 215
013 n
mi
Hp = 212
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7385596
71 X = -2317378
41
Y = 12031248
35 feet Y = 3641580
48 meter
Z = 17160797
73 Z = 5219514
31
XDOT = -23164
278334 XDOT = -7023
490911
YDOT = -9161
973751 feet/sec YDOT = -2871
317376 meter/sec
ZDOT = -3531
728425 ZDOT = -1110
680746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4781851
91 X = 1457508
46
Y = 13341934
72 feet Y = 4066621
70 meter
Z = 17114836
39 Z = 5216602
13
XDOT = -20578
022566 XDOT = -6272
181278
YDOT = 12104
098923 feet/sec YDOT = 3689
329352 meter/sec
ZDOT = -3672
035227 ZDOT = -1119
236337
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
59204633
00016717 00000-0 10270-3 0 9024
2 25544 51
6438 15
4661 0010241 290
3675 69
6379 15
57448326 10132
Satellite: ISS
Catalog Number: 25544
Epoch time: 12118
59204633 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 15
4661 deg
Eccentricity:
0010241
Arg of perigee: 290
3675 deg
Mean anomaly: 69
6379 deg
Mean motion: 15
57448326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1013
Checksum: 300
Coasting Arc #4 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2012/119/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4910176
60 A = 6772867
67 meter
Y = -2351097
77 meter E =
0003511
Z = -4025188
19 I = 51
70459
XDOT = 5176
538864 Wp = 306
05581
YDOT = 4079
054211 meter/sec RA = 10
13414 deg
ZDOT = 3931
734379 TA = 4
69843
MA = 4
69513
Ha = 215
300 n
mi
Hp = 212
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16109503
27 X = 4955655
68
Y = -7713575
36 feet Y = -2295934
83 meter
Z = -13205997
99 Z = -4001224
18
XDOT = 16983
395223 XDOT = 5111
441734
YDOT = 13382
723789 feet/sec YDOT = 4136
577474 meter/sec
ZDOT = 12899
391008 ZDOT = 3956
723809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3703164
31 X = 1128724
48
Y = -17547057
46 feet Y = -5348343
11 meter
Z = -13107290
80 Z = -3995102
24
XDOT = 19619
464936 XDOT = 5980
012912
YDOT = -5572
373760 feet/sec YDOT = -1698
459522 meter/sec
ZDOT = 13001
678746 ZDOT = 3962
911682
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
55452840
00016717 00000-0 10270-3 0 9037
2 25544 51
6434 10
6434 0010339 293
9782 66
0290 15
57457289 10286
Satellite: ISS
Catalog Number: 25544
Epoch time: 12119
55452840 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 10
6434 deg
Eccentricity:
0010339
Arg of perigee: 293
9782 deg
Mean anomaly: 66
0290 deg
Mean motion: 15
57457289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1028
Checksum: 307
Coasting Arc #5 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2012/120/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6517478
70 A = 6778445
94 meter
Y = 758209
17 meter E =
0003760
Z = 1694813
26 I = 51
69343
XDOT = -2033
283634 Wp = 112
10151
YDOT = -4707
183477 meter/sec RA = 5
13768 deg
ZDOT = -5704
485666 TA = 49
31374
MA = 49
28108
Ha = 215
388 n
mi
Hp = 211
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21382804
13 X = -6533705
81
Y = 2487562
89 feet Y = 685235
97 meter
Z = 5560410
97 Z = 1663112
07
XDOT = -6670
878065 XDOT = -1952
784591
YDOT = -15443
515344 feet/sec YDOT = -4729
470861 meter/sec
ZDOT = -18715
504152 ZDOT = -5714
167748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10709331
31 X = -3264204
18
Y = 18712429
62 feet Y = 5703548
55 meter
Z = 5430069
25 Z = 1655085
11
XDOT = -14957
110014 XDOT = -4558
927132
YDOT = -3109
225941 feet/sec YDOT = -947
692067 meter/sec
ZDOT = -18754
826440 ZDOT = -5716
471099
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
58115206
00016717 00000-0 10270-3 0 9045
2 25544 51
6435 5
4999 0010210 297
7418 62
2701 15
57476739 10445
Satellite: ISS
Catalog Number: 25544
Epoch time: 12120
58115206 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 5
4999 deg
Eccentricity:
0010210
Arg of perigee: 297
7418 deg
Mean anomaly: 62
2701 deg
Mean motion: 15
57476739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 294
Coasting Arc #6 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2012/121/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6615525
28 A = 6778841
14 meter
Y = 902905
50 meter E =
0012975
Z = 1119426
33 I = 51
66465
XDOT = -1630
854515 Wp = 11
30553
YDOT = 4651
107271 meter/sec RA =
15339 deg
ZDOT = 5887
358645 TA =
86368
MA =
86144
Ha = 215
463 n
mi
Hp = 211
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21704479
28 X = 6599499
17
Y = 2962288
37 feet Y = 976794
81 meter
Z = 3672658
58 Z = 1151525
51
XDOT = -5350
572556 XDOT = -1711
342569
YDOT = 15259
538292 feet/sec YDOT = 4632
420139 meter/sec
ZDOT = 19315
481119 ZDOT = 5879
240374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14981223
60 X = 4566276
95
Y = -15951080
26 feet Y = -4861889
26 meter
Z = 3804467
37 Z = 1159601
65
XDOT = 8103
248132 XDOT = 2469
870031
YDOT = 12208
709790 feet/sec YDOT = 3721
214744 meter/sec
ZDOT = 19281
665378 ZDOT = 5877
051607
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
60774822
00016717 00000-0 10270-3 0 9055
2 25544 51
6430
3548 0010433 301
1951 58
8180 15
57547354 10605
Satellite: ISS
Catalog Number: 25544
Epoch time: 12121
60774822 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node:
3548 deg
Eccentricity:
0010433
Arg of perigee: 301
1951 deg
Mean anomaly: 58
8180 deg
Mean motion: 15
57547354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 274
Coasting Arc #7 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2012/122/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5180422
24 A = 6773713
44 meter
Y = -2440242
42 meter E =
0007588
Z = -3621777
39 I = 51
61635
XDOT = 4920
945441 Wp = 334
63098
YDOT = -3910
085108 meter/sec RA = 355
15686 deg
ZDOT = -4394
073760 TA = 248
36237
MA = 248
44321
Ha = 215
698 n
mi
Hp = 211
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16996135
95 X = -5135155
99
Y = -8006044
68 feet Y = -2497920
13 meter
Z = -11882471
76 Z = -3646833
85
XDOT = 16144
834124 XDOT = 4985
648682
YDOT = -12828
363216 feet/sec YDOT = -3854
694420 meter/sec
ZDOT = -14416
252493 ZDOT = -4370
010519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16173973
83 X = -4929827
22
Y = 9429550
30 feet Y = 2874126
93 meter
Z = -11985185
67 Z = -3653084
59
XDOT = -713
565808 XDOT = -217
494858
YDOT = -19463
036892 feet/sec YDOT = -5932
333645 meter/sec
ZDOT = -14316
996164 ZDOT = -4363
820431
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
57016226
00016717 00000-0 10270-3 0 9060
2 25544 51
6421 355
5325 0010518 304
6057 55
4105 15
57553932 10757
Satellite: ISS
Catalog Number: 25544
Epoch time: 12122
57016226 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 355
5325 deg
Eccentricity:
0010518
Arg of perigee: 304
6057 deg
Mean anomaly: 55
4105 deg
Mean motion: 15
57553932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 281
Coasting Arc #8 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2012/123/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2516154
10 A = 6768195
03 meter
Y = 3671224
38 meter E =
0005538
Z = 5101646
98 I = 51
56774
XDOT = -7046
161888 Wp = 311
62821
YDOT = 2550
536137 meter/sec RA = 350
12985 deg
ZDOT = 1644
547501 TA = 122
51715
MA = 122
46363
Ha = 215
876 n
mi
Hp = 211
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8255098
74 X = 2450131
73
Y = 12044699
42 feet Y = 3698992
62 meter
Z = 16737686
93 Z = 5113709
99
XDOT = -23117
329030 XDOT = -7082
147758
YDOT = 8367
900712 feet/sec YDOT = 2471
540448 meter/sec
ZDOT = 5395
497051 ZDOT = 1610
229602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14544607
23 X = 4433196
28
Y = -162381
56 feet Y = -49493
90 meter
Z = 16786888
81 Z = 5116643
71
XDOT = -5791
019643 XDOT = -1765
102787
YDOT = 22867
157450 feet/sec YDOT = 6969
909591 meter/sec
ZDOT = 5254
247374 ZDOT = 1601
494600
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
59671396
00016717 00000-0 10270-3 0 9079
2 25544 51
6422 350
3875 0010455 309
0258 50
9965 15
57568840 10919
Satellite: ISS
Catalog Number: 25544
Epoch time: 12123
59671396 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 350
3875 deg
Eccentricity:
0010455
Arg of perigee: 309
0258 deg
Mean anomaly: 50
9965 deg
Mean motion: 15
57568840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 322
Coasting Arc #9 (Orbit 1105)
---------------------------------------
Vector Time (GMT): 2012/124/13:05:59
799
Vector Time (MET): N/A
Weight (LBS) : 927841
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 665710
91 A = 6767989
52 meter
Y = -4383834
13 meter E =
0006839
Z = -5116850
94 I = 51
53639
XDOT = 7475
409514 Wp = 52
12882
YDOT = -696
410545 meter/sec RA = 345
08600 deg
ZDOT = 1574
758903 TA = 233
03896
MA = 233
10160
Ha = 215
955 n
mi
Hp = 210
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2184090
90 X = 739539
31
Y = -14382657
90 feet Y = -4375977
10 meter
Z = -16787568
70 Z = -5113437
42
XDOT = 24525
621765 XDOT = 7474
991360
YDOT = -2284
811499 feet/sec YDOT = -612
818178 meter/sec
ZDOT = 5166
531834 ZDOT = 1611
073772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10908279
17 X = -3324843
49
Y = -9650165
54 feet Y = -2941370
46 meter
Z = -16773112
86 Z = -5112444
80
XDOT = 10517
357814 XDOT = 3205
690662
YDOT = -21096
327911 feet/sec YDOT = -6430
160747 meter/sec
ZDOT = 5315
795628 ZDOT = 1620
254508
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
55908173
00016717 00000-0 10270-3 0 9083
2 25544 51
6408 345
5635 0010509 312
0112 48
0147 15
57646251 11066
Satellite: ISS
Catalog Number: 25544
Epoch time: 12124
55908173 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 345
5635 deg
Eccentricity:
0010509
Arg of perigee: 312
0112 deg
Mean anomaly: 48
0147 deg
Mean motion: 15
57646251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1106
Checksum: 283
Coasting Arc #10 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2012/125/08:56:59
201
Vector Time (MET): N/A
Weight (LBS) : 926871
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3850861
00 A = 6774752
38 meter
Y = -2750343
12 meter E =
0004068
Z = -4850418
69 I = 51
51820
XDOT = 6000
133384 Wp = 13
78047
YDOT = -4111
802237 meter/sec RA = 340
96944 deg
ZDOT = -2428
671718 TA = 232
33650
MA = 232
37341
Ha = 216
030 n
mi
Hp = 214
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12634058
38 X = -3796257
14
Y = -9023435
42 feet Y = -2793100
59 meter
Z = -15913447
16 Z = -4868993
73
XDOT = 19685
476981 XDOT = 6057
464639
YDOT = -13490
164820 feet/sec YDOT = -4044
384513 meter/sec
ZDOT = -7968
083063 ZDOT = -2399
383385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11893465
97 X = -3625128
43
Y = -9857051
00 feet Y = -3004429
15 meter
Z = -15989485
03 Z = -4873595
04
XDOT = 19887
544911 XDOT = 6061
723689
YDOT = -11248
448556 feet/sec YDOT = -3428
527120 meter/sec
ZDOT = -7847
353534 ZDOT = -2391
873357
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
39314903
00016717 00000-0 10270-3 0 9099
2 25544 51
6431 341
3859 0010393 272
3498 87
6466 15
55672800 11194
Satellite: ISS
Catalog Number: 25544
Epoch time: 12125
39314903 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 341
3859 deg
Eccentricity:
0010393
Arg of perigee: 272
3498 deg
Mean anomaly: 87
6466 deg
Mean motion: 15
55672800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1119
Checksum: 317
Coasting Arc #11 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2012/126/08:56:59
201
Vector Time (MET): N/A
Weight (LBS) : 926871
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1689648
02 A = 6772748
79 meter
Y = 3868297
64 meter E =
0008184
Z = 5303384
71 I = 51
48297
XDOT = -7009
087230 Wp = 278
18302
YDOT = 3103
238925 meter/sec RA = 335
94441 deg
ZDOT = -29
323653 TA = 172
10356
MA = 172
09067
Ha = 216
394 n
mi
Hp = 214
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5543464
65 X = 1620503
09
Y = 12691265
24 feet Y = 3886805
65 meter
Z = 17399556
14 Z = 5311425
24
XDOT = -22995
693013 XDOT = -7043
124890
YDOT = 10181
230070 feet/sec YDOT = 3024
668661 meter/sec
ZDOT = -96
206211 ZDOT = -63
456938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4784208
14 X = 1458226
64
Y = 12952701
42 feet Y = 3947983
39 meter
Z = 17432201
41 Z = 5313334
99
XDOT = -22538
709541 XDOT = -6869
798668
YDOT = 8648
363332 feet/sec YDOT = 2636
021144 meter/sec
ZDOT = -236
737499 ZDOT = -72
157590
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
42096229
00016717 00000-0 10270-3 0 9104
2 25544 51
6427 336
2496 0010557 276
0317 83
9633 15
55711531 11350
Satellite: ISS
Catalog Number: 25544
Epoch time: 12126
42096229 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 336
2496 deg
Eccentricity:
0010557
Arg of perigee: 276
0317 deg
Mean anomaly: 83
9633 deg
Mean motion: 15
55711531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1135
Checksum: 298
Coasting Arc #12 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2012/127/08:56:59
201
Vector Time (MET): N/A
Weight (LBS) : 926871
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 591606
05 A = 6774830
88 meter
Y = -4723520
54 meter E =
0001811
Z = -4821617
54 I = 51
46276
XDOT = 7061
926216 Wp = 161
66749
YDOT = -1658
550632 meter/sec RA = 330
91722 deg
ZDOT = 2489
865249 TA = 132
86195
MA = 132
84674
Ha = 216
797 n
mi
Hp = 214
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1940964
74 X = 667804
32
Y = -15497114
62 feet Y = -4716478
56 meter
Z = -15818955
19 Z = -4818558
61
XDOT = 23169
049266 XDOT = 7067
852119
YDOT = -5441
439082 feet/sec YDOT = -1579
546787 meter/sec
ZDOT = 8168
849242 ZDOT = 2524
186881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2558755
51 X = 779908
68
Y = -15420541
03 feet Y = -4700180
91 meter
Z = -15805914
52 Z = -4817642
75
XDOT = 22164
790613 XDOT = 6755
828179
YDOT = -4844
660116 feet/sec YDOT = -1476
652403 meter/sec
ZDOT = 8310
009984 ZDOT = 2532
891043
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
38451879
00016717 00000-0 10270-3 0 9117
2 25544 51
6428 331
4341 0010602 280
0851 79
9106 15
55723706 11500
Satellite: ISS
Catalog Number: 25544
Epoch time: 12127
38451879 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 331
4341 deg
Eccentricity:
0010602
Arg of perigee: 280
0851 deg
Mean anomaly: 79
9106 deg
Mean motion: 15
55723706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1150
Checksum: 291
Coasting Arc #13 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2012/128/08:56:59
201
Vector Time (MET): N/A
Weight (LBS) : 926871
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2675784
60 A = 6779494
37 meter
Y = 5164195
97 meter E =
0003497
Z = 3484287
03 I = 51
45243
XDOT = -6192
027320 Wp = 35
49355
YDOT = -156
054871 meter/sec RA = 325
90153 deg
ZDOT = -4518
843668 TA = 103
42823
MA = 103
38924
Ha = 217
186 n
mi
Hp = 214
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8778820
88 X = -2750259
02
Y = 16942900
15 feet Y = 5133857
02 meter
Z = 11431387
90 Z = 3471107
42
XDOT = -20315
050263 XDOT = -6167
870129
YDOT = -511
991046 feet/sec YDOT = -225
162546 meter/sec
ZDOT = -14825
602585 ZDOT = -4548
866172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9127125
69 X = -2781947
91
Y = 16794997
00 feet Y = 5119115
09 meter
Z = 11376723
76 Z = 3467625
40
XDOT = -18988
500957 XDOT = -5787
695092
YDOT = -181
620873 feet/sec YDOT = -55
358042 meter/sec
ZDOT = -14948
921684 ZDOT = -4556
431329
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
41229093
00016717 00000-0 10270-3 0 9124
2 25544 51
6426 326
2979 0010585 284
4467 75
5511 15
55756795 11661
Satellite: ISS
Catalog Number: 25544
Epoch time: 12128
41229093 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 326
2979 deg
Eccentricity:
0010585
Arg of perigee: 284
4467 deg
Mean anomaly: 75
5511 deg
Mean motion: 15
55756795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1166
Checksum: 329
Coasting Arc #14 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2012/129/08:56:59
201
Vector Time (MET): N/A
Weight (LBS) : 926871
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4279445
06 A = 6783570
12 meter
Y = -5031347
05 meter E =
0011188
Z = -1512532
08 I = 51
44204
XDOT = 4592
115641 Wp = 332
25975
YDOT = 2174
808635 meter/sec RA = 320
90005 deg
ZDOT = 5750
785557 TA = 11
15455
MA = 11
12977
Ha = 217
458 n
mi
Hp = 214
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14040174
08 X = 4342736
18
Y = -16507044
14 feet Y = -4983137
64 meter
Z = -4962375
61 Z = -1491589
16
XDOT = 15065
996196 XDOT = 4539
518790
YDOT = 7135
198933 feet/sec YDOT = 2225
865917 meter/sec
ZDOT = 18867
406683 ZDOT = 5772
966590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14059061
56 X = 4285201
96
Y = -16516756
26 feet Y = -5034307
31 meter
Z = -4875829
87 Z = -1486152
94
XDOT = 13751
245554 XDOT = 4191
379645
YDOT = 6101
143516 feet/sec YDOT = 1859
628544 meter/sec
ZDOT = 18958
311303 ZDOT = 5778
493285
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
37580668
00016717 00000-0 10270-3 0 9139
2 25544 51
6429 321
4815 0010756 288
0551 71
9430 15
55788558 11813
Satellite: ISS
Catalog Number: 25544
Epoch time: 12129
37580668 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 321
4815 deg
Eccentricity:
0010756
Arg of perigee: 288
0551 deg
Mean anomaly: 71
9430 deg
Mean motion: 15
55788558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1181
Checksum: 326
Coasting Arc #15 (Orbit 1196)
---------------------------------------
Vector Time (GMT): 2012/130/08:56:59
201
Vector Time (MET): N/A
Weight (LBS) : 926871
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5231999
31 A = 6784290
28 meter
Y = 4250654
21 meter E =
0005370
Z = -736627
09 I = 51
42142
XDOT = -2528
140950 Wp = 219
59500
YDOT = -4144
041417 meter/sec RA = 315
90783 deg
ZDOT = -5936
554133 TA = 328
39234
MA = 328
42458
Ha = 217
695 n
mi
Hp = 214
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17165352
07 X = -5275563
74
Y = 13945715
93 feet Y = 4191903
25 meter
Z = -2416755
53 Z = -762149
56
XDOT = -8294
425689 XDOT = -2452
774859
YDOT = -13595
936407 feet/sec YDOT = -4171
890727 meter/sec
ZDOT = -19476
883639 ZDOT = -5948
653138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16898370
50 X = -5150623
33
Y = 14249821
47 feet Y = 4343345
58 meter
Z = -2522037
75 Z = -768717
11
XDOT = -7378
298973 XDOT = -2248
905527
YDOT = -12216
605118 feet/sec YDOT = -3723
621240 meter/sec
ZDOT = -19526
174291 ZDOT = -5951
577924
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 12130
40353710
00016717 00000-0 10270-3 0 9142
2 25544 51
6428 316
3454 0010790 291
0430 68
9569 15
55776275 11971
Satellite: ISS
Catalog Number: 25544
Epoch time: 12130
40353710 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 316
3454 deg
Eccentricity:
0010790
Arg of perigee: 291
0430 deg
Mean anomaly: 68
9569 deg
Mean motion: 15
55776275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1197
Checksum: 307
Coasting Arc #16 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2012/131/08:56:59
201
Vector Time (MET): N/A
Weight (LBS) : 926871
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5460549
42 A = 6780798
02 meter
Y = -2806655
69 meter E =
0007553
Z = 2866252
20 I = 51
38884
XDOT = 323
093344 Wp = 25
71407
YDOT = 5775
208743 meter/sec RA = 310
90734 deg
ZDOT = 5041
279839 TA = 7
06222
MA = 7
05159
Ha = 217
870 n
mi
Hp = 214
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17915188
37 X = 5477604
50
Y = -9208187
96 feet Y = -2745497
31 meter
Z = 9403714
58 Z = 2892820
64
XDOT = 1060
017532 XDOT = 234
000265
YDOT = 18947
535247 feet/sec YDOT = 5778
323230 meter/sec
ZDOT = 16539
632018 ZDOT = 5042
633466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17523756
26 X = 5341240
91
Y = -9828148
25 feet Y = -2995619
59 meter
Z = 9513149
66 Z = 2899608
02
XDOT = 906
514776 XDOT = 276
305704
YDOT = 17625
400793 feet/sec YDOT = 5372
222162 meter/sec
ZDOT = 16544
618794 ZDOT = 5042
799808
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 12131
43124445
00016717 00000-0 10270-3 0 9158
2 25544 51
6423 311
2075 0010953 296
3515 63
6513 15
55835264 12136
Satellite: ISS
Catalog Number: 25544
Epoch time: 12131
43124445 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 311
2075 deg
Eccentricity:
0010953
Arg of perigee: 296
3515 deg
Mean anomaly: 63
6513 deg
Mean motion: 15
55835264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1213
Checksum: 278
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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