[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 22nd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
032/21:57:47
723 3
1 4
9 4
9
N/A 0
2 -0
0 219
3
000/00:01:35
445 -3
8 -0
1 205
5
Coasting Arc #1 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2012/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -938504
38 A = 6766721
85 meter
Y = 4896182
49 meter E =
0012306
Z = -4563370
00 I = 51
81665
XDOT = -6857
427015 Wp = 311
19040
YDOT = 1566
539586 meter/sec RA = 146
89614 deg
ZDOT = 3093
614205 TA = 349
60566
MA = 349
63108
Ha = 216
672 n
mi
Hp = 205
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3079082
62 X = -971017
26
Y = 16063590
86 feet Y = 4885506
22 meter
Z = -14971686
35 Z = -4568007
62
XDOT = -22498
120129 XDOT = -6889
462549
YDOT = 5139
565572 feet/sec YDOT = 1489
676194 meter/sec
ZDOT = 10149
652902 ZDOT = 3060
224013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15543373
63 X = -4737620
28
Y = 5034324
75 feet Y = 1534462
18 meter
Z = -14991004
09 Z = -4569258
05
XDOT = -14909
989351 XDOT = -4544
564754
YDOT = -16243
286220 feet/sec YDOT = -4950
953640 meter/sec
ZDOT = 10012
773465 ZDOT = 3051
893352
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 12020
51058358
00016717 00000-0 10270-3 0 9007
2 25544 51
6400 147
8918 0022058 301
5297 58
3704 15
58842861 34833
Satellite: ISS
Catalog Number: 25544
Epoch time: 12020
51058358 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 147
8918 deg
Eccentricity:
0022058
Arg of perigee: 301
5297 deg
Mean anomaly: 58
3704 deg
Mean motion: 15
58842861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 304
Coasting Arc #2 (Orbit 3498)
---------------------------------------
Vector Time (GMT): 2012/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3855548
66 A = 6773609
93 meter
Y = -5152696
19 meter E =
0009416
Z = 2133556
09 I = 51
86540
XDOT = 5088
869203 Wp = 329
44695
YDOT = 1521
233884 meter/sec RA = 141
89242 deg
ZDOT = -5524
986894 TA = 186
96997
MA = 186
98307
Ha = 216
880 n
mi
Hp = 205
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12649437
86 X = 3902516
47
Y = -16905171
24 feet Y = -5109318
66 meter
Z = 6999855
95 Z = 2152399
39
XDOT = 16695
765102 XDOT = 5098
318810
YDOT = 4990
924817 feet/sec YDOT = 1578
194082 meter/sec
ZDOT = -18126
597421 ZDOT = -5500
242833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20919674
12 X = 6376316
67
Y = 2658720
16 feet Y = 810377
91 meter
Z = 7077394
84 Z = 2157189
95
XDOT = 4117
554440 XDOT = 1255
030593
YDOT = 15560
294108 feet/sec YDOT = 4742
777644 meter/sec
ZDOT = -18025
323439 ZDOT = -5494
118584
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 12021
53629407
00016717 00000-0 10270-3 0 9010
2 25544 51
6406 142
7415 0022028 305
4817 54
4283 15
58864297 34996
Satellite: ISS
Catalog Number: 25544
Epoch time: 12021
53629407 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 142
7415 deg
Eccentricity:
0022028
Arg of perigee: 305
4817 deg
Mean anomaly: 54
4283 deg
Mean motion: 15
58864297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3499
Checksum: 310
Coasting Arc #3 (Orbit 3514)
---------------------------------------
Vector Time (GMT): 2012/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5431484
00 A = 6774994
01 meter
Y = 3864709
97 meter E =
0022239
Z = 1131669
46 I = 51
89469
XDOT = -1977
743302 Wp = 345
93782
YDOT = -4497
020842 meter/sec RA = 136
91573 deg
ZDOT = 5910
543623 TA = 26
34288
MA = 26
22997
Ha = 217
187 n
mi
Hp = 205
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17819829
40 X = -5479793
54
Y = 12679494
65 feet Y = 3803701
58 meter
Z = 3712826
31 Z = 1105167
16
XDOT = -6488
659128 XDOT = -1956
021088
YDOT = -14754
005388 feet/sec YDOT = -4519
016161 meter/sec
ZDOT = 19391
547320 ZDOT = 5900
988509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19973905
24 X = -6088046
32
Y = -8952956
40 feet Y = -2728861
11 meter
Z = 3603979
01 Z = 1098492
80
XDOT = 8715
823929 XDOT = 2656
583134
YDOT = -11716
046700 feet/sec YDOT = -3571
051034 meter/sec
ZDOT = 19352
692973 ZDOT = 5898
700818
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 12022
56198426
00016717 00000-0 10270-3 0 9027
2 25544 51
6418 137
5910 0022065 309
8856 50
0359 15
58897754 35152
Satellite: ISS
Catalog Number: 25544
Epoch time: 12022
56198426 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 137
5910 deg
Eccentricity:
0022065
Arg of perigee: 309
8856 deg
Mean anomaly: 50
0359 deg
Mean motion: 15
58897754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3515
Checksum: 323
Coasting Arc #4 (Orbit 3529)
---------------------------------------
Vector Time (GMT): 2012/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5343052
76 A = 6768900
97 meter
Y = -1318000
36 meter E =
0019593
Z = -3946038
10 I = 51
89629
XDOT = -1440
508130 Wp = 330
27746
YDOT = 6354
409748 meter/sec RA = 131
92759 deg
ZDOT = -4047
712105 TA = 257
49928
MA = 257
71855
Ha = 217
390 n
mi
Hp = 205
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17529700
66 X = 5376562
24
Y = -4324148
17 feet Y = -1258063
50 meter
Z = -12946319
22 Z = -3920001
17
XDOT = -4726
076543 XDOT = -1491
795011
YDOT = 20847
801011 feet/sec YDOT = 6338
014547 meter/sec
ZDOT = -13279
895357 ZDOT = -4054
834084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12874755
09 X = 3924225
35
Y = 12766474
30 feet Y = 3891221
37 meter
Z = -12839535
02 Z = -3913490
27
XDOT = -19278
325993 XDOT = -5876
033763
YDOT = 5972
361139 feet/sec YDOT = 1820
375675 meter/sec
ZDOT = -13309
501272 ZDOT = -4056
735988
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 12023
52355050
00016717 00000-0 10270-3 0 9033
2 25544 51
6421 132
7639 0022100 313
2659 46
6651 15
58925324 35309
Satellite: ISS
Catalog Number: 25544
Epoch time: 12023
52355050 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 132
7639 deg
Eccentricity:
0022100
Arg of perigee: 313
2659 deg
Mean anomaly: 46
6651 deg
Mean motion: 15
58925324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3530
Checksum: 276
Coasting Arc #5 (Orbit 3545)
---------------------------------------
Vector Time (GMT): 2012/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3741726
48 A = 6763360
20 meter
Y = -1937735
52 meter E =
0019441
Z = 5299567
51 I = 51
89854
XDOT = 4183
791330 Wp = 320
69196
YDOT = -6395
857172 meter/sec RA = 126
90391 deg
ZDOT = 631
275704 TA = 123
39656
MA = 123
21042
Ha = 217
584 n
mi
Hp = 204
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12276005
50 X = -3745523
64
Y = -6357399
99 feet Y = -1979599
18 meter
Z = 17387032
50 Z = 5281381
58
XDOT = 13726
349507 XDOT = 4251
933624
YDOT = -20983
783374 feet/sec YDOT = -6348
690456 meter/sec
ZDOT = 2071
114514 ZDOT = 651
765158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1273980
08 X = -388309
13
Y = -13859132
68 feet Y = -4224263
64 meter
Z = 17312630
11 Z = 5276889
66
XDOT = 24054
706445 XDOT = 7331
874524
YDOT = 415
916422 feet/sec YDOT = 126
771325 meter/sec
ZDOT = 2155
510452 ZDOT = 656
999586
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 12024
54920045
00016717 00000-0 10270-3 0 9049
2 25544 51
6426 127
6131 0022177 317
4017 42
5417 15
58994437 35465
Satellite: ISS
Catalog Number: 25544
Epoch time: 12024
54920045 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 127
6131 deg
Eccentricity:
0022177
Arg of perigee: 317
4017 deg
Mean anomaly: 42
5417 deg
Mean motion: 15
58994437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3546
Checksum: 298
Coasting Arc #6 (Orbit 3560)
---------------------------------------
Vector Time (GMT): 2012/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1298218
80 A = 6766044
09 meter
Y = 4762202
03 meter E =
0014323
Z = -4617441
30 I = 51
92512
XDOT = -5521
881477 Wp = 343
62396
YDOT = 4413
540744 meter/sec RA = 121
87590 deg
ZDOT = 3010
546588 TA = 316
17016
MA = 316
28374
Ha = 217
799 n
mi
Hp = 204
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4259248
03 X = 1267300
34
Y = 15624022
41 feet Y = 4776546
66 meter
Z = -15149085
63 Z = -4611209
84
XDOT = -18116
409044 XDOT = -5585
448360
YDOT = 14480
120550 feet/sec YDOT = 4351
436228 meter/sec
ZDOT = 9877
121352 ZDOT = 2983
567842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10644968
77 X = -3244586
48
Y = 12235173
39 feet Y = 3729280
85 meter
Z = -15123863
17 Z = -4609753
49
XDOT = -21204
148751 XDOT = -6463
024539
YDOT = -6421
481502 feet/sec YDOT = -1957
267562 meter/sec
ZDOT = 9766
252752 ZDOT = 2976
753839
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 12025
51073107
00016717 00000-0 10270-3 0 9056
2 25544 51
6423 122
7860 0022114 321
3089 38
6481 15
59021755 35610
Satellite: ISS
Catalog Number: 25544
Epoch time: 12025
51073107 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 122
7860 deg
Eccentricity:
0022114
Arg of perigee: 321
3089 deg
Mean anomaly: 38
6481 deg
Mean motion: 15
59021755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3561
Checksum: 280
Coasting Arc #7 (Orbit 3576)
---------------------------------------
Vector Time (GMT): 2012/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1294163
99 A = 6773141
21 meter
Y = -6295665
88 meter E =
0013586
Z = 2162630
68 I = 51
96335
XDOT = 5253
880324 Wp = 2
39602
YDOT = -819
930267 meter/sec RA = 116
87797 deg
ZDOT = -5516
474228 TA = 153
71906
MA = 153
65007
Ha = 218
005 n
mi
Hp = 204
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4245944
84 X = 1353961
86
Y = -20655071
79 feet Y = -6280859
37 meter
Z = 7095245
02 Z = 2169062
85
XDOT = 17237
140169 XDOT = 5289
455654
YDOT = -2690
059932 feet/sec YDOT = -760
979292 meter/sec
ZDOT = -18098
668727 ZDOT = -5490
865269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19417070
71 X = 5918323
15
Y = -8201009
35 feet Y = -2499667
65 meter
Z = 7122032
77 Z = 2170795
59
XDOT = 11422
415114 XDOT = 3481
552127
YDOT = 11376
850199 feet/sec YDOT = 3467
663941 meter/sec
ZDOT = -17993
647720 ZDOT = -5484
463825
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 12026
53634355
00016717 00000-0 10270-3 0 9068
2 25544 51
6416 117
6356 0022148 325
3801 34
5912 15
59018209 35779
Satellite: ISS
Catalog Number: 25544
Epoch time: 12026
53634355 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 117
6356 deg
Eccentricity:
0022148
Arg of perigee: 325
3801 deg
Mean anomaly: 34
5912 deg
Mean motion: 15
59018209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3577
Checksum: 301
Coasting Arc #8 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2012/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3290231
44 A = 6774568
67 meter
Y = 5790341
60 meter E =
0026578
Z = 1141358
98 I = 51
98134
XDOT = -3679
364353 Wp =
45079
YDOT = -3252
419432 meter/sec RA = 111
90645 deg
ZDOT = 5918
501897 TA = 11
93027
MA = 11
86743
Ha = 218
305 n
mi
Hp = 204
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10794722
57 X = -3360280
02
Y = 18997183
73 feet Y = 5753156
57 meter
Z = 3744616
08 Z = 1125205
24
XDOT = -12071
405356 XDOT = -3671
471888
YDOT = -10670
667428 feet/sec YDOT = -3293
520106 meter/sec
ZDOT = 19417
657144 ZDOT = 5900
647286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21752113
11 X = -6630044
08
Y = 2181515
89 feet Y = 664926
04 meter
Z = 3678007
39 Z = 1121056
65
XDOT = 1799
680789 XDOT = 548
542704
YDOT = -14529
599386 feet/sec YDOT = -4428
621893 meter/sec
ZDOT = 19344
693447 ZDOT = 5896
262563
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 12027
56193535
00016717 00000-0 10270-3 0 9073
2 25544 51
6420 112
4843 0022286 329
5104 30
4754 15
59038942 35936
Satellite: ISS
Catalog Number: 25544
Epoch time: 12027
56193535 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 112
4843 deg
Eccentricity:
0022286
Arg of perigee: 329
5104 deg
Mean anomaly: 30
4754 deg
Mean motion: 15
59038942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 303
Coasting Arc #9 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2012/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4297504
43 A = 6768296
91 meter
Y = -3388979
26 meter E =
0022134
Z = -3995495
05 I = 51
96986
XDOT = 1316
412858 Wp = 350
68560
YDOT = 6407
930374 meter/sec RA = 106
92190 deg
ZDOT = -3994
918526 TA = 237
78025
MA = 237
99501
Ha = 218
444 n
mi
Hp = 204
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14099423
97 X = 4354490
18
Y = -11118698
35 feet Y = -3340603
36 meter
Z = -13108579
56 Z = -3974479
82
XDOT = 4318
939824 XDOT = 1264
066365
YDOT = 21023
393617 feet/sec YDOT = 6422
358556 meter/sec
ZDOT = -13106
688077 ZDOT = -3988
650816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17361337
29 X = 5291735
61
Y = 4822897
21 feet Y = 1470019
07 meter
Z = -13022200
18 Z = -3969166
61
XDOT = -13967
603711 XDOT = -4257
325611
YDOT = 14741
967068 feet/sec YDOT = 4493
351562 meter/sec
ZDOT = -13081
440941 ZDOT = -3987
223199
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 12028
52340895
00016717 00000-0 10270-3 0 9084
2 25544 51
6408 107
6561 0022262 332
9850 27
0145 15
59072733 36084
Satellite: ISS
Catalog Number: 25544
Epoch time: 12028
52340895 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 107
6561 deg
Eccentricity:
0022262
Arg of perigee: 332
9850 deg
Mean anomaly: 27
0145 deg
Mean motion: 15
59072733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 302
Coasting Arc #10 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2012/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4179265
86 A = 6762891
16 meter
Y = -320361
72 meter E =
0020506
Z = 5311317
65 I = 51
96083
XDOT = 1192
724299 Wp = 342
20951
YDOT = -7563
763016 meter/sec RA = 101
90019 deg
ZDOT = 501
814800 TA = 103
14213
MA = 102
91323
Ha = 218
646 n
mi
Hp = 203
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13711502
15 X = -4201173
73
Y = -1051055
51 feet Y = -367219
28 meter
Z = 17425582
83 Z = 5290962
02
XDOT = 3913
137464 XDOT = 1274
777494
YDOT = -24815
495458 feet/sec YDOT = -7549
966448 meter/sec
ZDOT = 1646
374015 ZDOT = 507
808302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7548898
96 X = -2300904
40
Y = -11620003
43 feet Y = -3541777
05 meter
Z = 17342162
23 Z = 5285891
05
XDOT = 21246
256070 XDOT = 6475
858850
YDOT = -11404
064383 feet/sec YDOT = -3475
958824 meter/sec
ZDOT = 1671
479594 ZDOT = 509
466980
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 12029
54896021
00016717 00000-0 10270-3 0 9095
2 25544 51
6413 102
5040 0022350 336
8285 23
1861 15
59135229 36249
Satellite: ISS
Catalog Number: 25544
Epoch time: 12029
54896021 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 102
5040 deg
Eccentricity:
0022350
Arg of perigee: 336
8285 deg
Mean anomaly: 23
1861 deg
Mean motion: 15
59135229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 288
Coasting Arc #11 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2012/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3103569
25 A = 6765980
55 meter
Y = 3930247
86 meter E =
0017852
Z = -4542007
71 I = 51
97582
XDOT = -3242
887489 Wp = 6
33312
YDOT = 6200
714130 meter/sec RA = 96
87459 deg
ZDOT = 3168
131325 TA = 295
14681
MA = 295
33189
Ha = 218
860 n
mi
Hp = 203
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10182313
81 X = 3081453
56
Y = 12894513
96 feet Y = 3964830
23 meter
Z = -14901600
10 Z = -4526984
60
XDOT = -10639
394650 XDOT = -3327
373983
YDOT = 20343
550295 feet/sec YDOT = 6163
977771 meter/sec
ZDOT = 10394
131643 ZDOT = 3152
172504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3740385
75 X = -1140069
58
Y = 16055551
33 feet Y = 4893732
05 meter
Z = -14840299
06 Z = -4523323
15
XDOT = -21424
788931 XDOT = -6530
275666
YDOT = 4499
056074 feet/sec YDOT = 1371
312291 meter/sec
ZDOT = 10328
259238 ZDOT = 3148
053416
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 12030
51039839
00016717 00000-0 10270-3 0 9102
2 25544 51
6404 97
6755 0022377 341
0938 18
9384 15
59161548 36399
Satellite: ISS
Catalog Number: 25544
Epoch time: 12030
51039839 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 97
6755 deg
Eccentricity:
0022377
Arg of perigee: 341
0938 deg
Mean anomaly: 18
9384 deg
Mean motion: 15
59161548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 325
Coasting Arc #12 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2012/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1323134
88 A = 6772981
10 meter
Y = -6356015
02 meter E =
0017913
Z = 1959723
37 I = 52
00287
XDOT = 4476
073521 Wp = 23
13334
YDOT = -2673
141654 meter/sec RA = 91
88005 deg
ZDOT = -5614
359228 TA = 135
35429
MA = 135
20990
Ha = 218
968 n
mi
Hp = 202
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4340993
69 X = -1261482
09
Y = -20853067
66 feet Y = -6370466
44 meter
Z = 6429538
60 Z = 1953445
38
XDOT = 14685
280581 XDOT = 4532
905434
YDOT = -8770
149784 feet/sec YDOT = -2622
769604 meter/sec
ZDOT = -18419
813739 ZDOT = -5592
476905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13354703
28 X = 4070513
56
Y = -16603337
15 feet Y = -5060697
16 meter
Z = 6404273
53 Z = 1952022
57
XDOT = 14951
502763 XDOT = 4557
218042
YDOT = 4913
364053 feet/sec YDOT = 1497
593363 meter/sec
ZDOT = -18329
905712 ZDOT = -5586
955261
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 12031
53591114
00016717 00000-0 10270-3 0 9115
2 25544 51
6410 92
5237 0022585 344
9700 15
0782 15
59206271 36556
Satellite: ISS
Catalog Number: 25544
Epoch time: 12031
53591114 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 92
5237 deg
Eccentricity:
0022585
Arg of perigee: 344
9700 deg
Mean anomaly: 15
0782 deg
Mean motion: 15
59206271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 285
Coasting Arc #13 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -734062
30 A = 6773929
75 meter
Y = 6567738
18 meter E =
0030102
Z = 1391493
69 I = 52
00520
XDOT = -4673
419769 Wp = 15
02165
YDOT = -1762
249901 meter/sec RA = 86
91066 deg
ZDOT = 5852
545747 TA =
13440
MA =
13360
Ha = 219
283 n
mi
Hp = 202
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2408340
88 X = -814208
99
Y = 21547697
44 feet Y = 6559081
28 meter
Z = 4565268
02 Z = 1387733
19
XDOT = -15332
742024 XDOT = -4681
796597
YDOT = -5781
659779 feet/sec YDOT = -1814
557940 meter/sec
ZDOT = 19201
265575 ZDOT = 5829
822371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18006868
65 X = -5488493
56
Y = 12083092
55 feet Y = 3682926
61 meter
Z = 4549351
45 Z = 1386642
32
XDOT = -4705
836020 XDOT = -1434
338819
YDOT = -14206
919343 feet/sec YDOT = -4330
269016 meter/sec
ZDOT = 19108
237457 ZDOT = 5824
190777
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 12032
56140663
00016717 00000-0 10270-3 0 9129
2 25544 51
6407 87
3720 0022623 349
3868 10
6807 15
59162041 36711
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
56140663 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 87
3720 deg
Eccentricity:
0022623
Arg of perigee: 349
3868 deg
Mean anomaly: 10
6807 deg
Mean motion: 15
59162041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 294
Coasting Arc #14 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2012/032/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 120621
79 A = 6776892
64 meter
Y = -6719272
30 meter E =
0010901
Z = -929127
45 I = 52
00727
XDOT = 4745
098122 Wp = 10
79070
YDOT = 907
216731 meter/sec RA = 84
82904 deg
ZDOT = -5945
631221 TA = 179
21689
MA = 179
21518
Ha = 219
276 n
mi
Hp = 205
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 395740
79 X = 200262
51
Y = -22044856
62 feet Y = -6717478
11 meter
Z = -3048318
42 Z = -928348
24
XDOT = 15567
907226 XDOT = 4763
482936
YDOT = 2976
432845 feet/sec YDOT = 960
382308 meter/sec
ZDOT = -19506
664110 ZDOT = -5922
535364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21759508
27 X = -6632298
12
Y = 3560718
72 feet Y = 1085307
07 meter
Z = -3044608
57 Z = -927996
69
XDOT = 362
861092 XDOT = 110
600061
YDOT = -14378
571165 feet/sec YDOT = -4382
588491 meter/sec
ZDOT = -19412
042403 ZDOT = -5916
790524
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 12032
94597781
00016717 00000-0 10270-3 0 9139
2 25544 51
6421 85
4411 0018934 347
2767 12
7908 15
58285469 36778
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
94597781 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 85
4411 deg
Eccentricity:
0018934
Arg of perigee: 347
2767 deg
Mean anomaly: 12
7908 deg
Mean motion: 15
58285469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3677
Checksum: 341
Coasting Arc #15 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2012/033/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1972188
17 A = 6771407
49 meter
Y = 5313827
20 meter E =
0019932
Z = 3681211
03 I = 51
98567
XDOT = -4304
654587 Wp = 26
40959
YDOT = -4624
958177 meter/sec RA = 79
85230 deg
ZDOT = 4378
293284 TA = 17
32671
MA = 17
25878
Ha = 219
526 n
mi
Hp = 205
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6470433
62 X = -2049344
08
Y = 17433816
26 feet Y = 5291341
44 meter
Z = 12077464
00 Z = 3671443
16
XDOT = -14122
882502 XDOT = -4273
885874
YDOT = -15173
747299 feet/sec YDOT = -4672
923599 meter/sec
ZDOT = 14364
479279 ZDOT = 4357
456357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18381617
32 X = 5602716
96
Y = 2982682
33 feet Y = 909121
58 meter
Z = 12036999
13 Z = 3668877
33
XDOT = -11860
552981 XDOT = -3615
096548
YDOT = 15578
688947 feet/sec YDOT = 4748
384391 meter/sec
ZDOT = 14279
406079 ZDOT = 4352
362973
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 12033
97204361
00016717 00000-0 10270-3 0 9143
2 25544 51
6423 80
2932 0019073 351
5141 8
5688 15
58321826 36934
Satellite: ISS
Catalog Number: 25544
Epoch time: 12033
97204361 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 80
2932 deg
Eccentricity:
0019073
Arg of perigee: 351
5141 deg
Mean anomaly: 8
5688 deg
Mean motion: 15
58321826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 301
Coasting Arc #16 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2012/034/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3537820
35 A = 6765571
76 meter
Y = -2513948
66 meter E =
0024641
Z = -5204566
92 I = 51
96060
XDOT = 2956
196468 Wp = 29
16764
YDOT = 6944
339209 meter/sec RA = 74
84451 deg
ZDOT = -1326
512919 TA = 228
03046
MA = 228
24065
Ha = 219
551 n
mi
Hp = 204
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11607022
13 X = 3590951
01
Y = -8247863
05 feet Y = -2474089
30 meter
Z = -17075350
78 Z = -5187251
72
XDOT = 9698
807310 XDOT = 2884
767542
YDOT = 22783
265123 feet/sec YDOT = 6976
997889 meter/sec
ZDOT = -4352
076507 ZDOT = -1312
325352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10561109
84 X = -3219026
28
Y = -9676754
11 feet Y = -2949474
65 meter
Z = -17004152
46 Z = -5182865
67
XDOT = 19472
361598 XDOT = 5935
175815
YDOT = -13599
649886 feet/sec YDOT = -4145
173285 meter/sec
ZDOT = -4294
453096 ZDOT = -1308
949304
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 12034
93396135
00016717 00000-0 10270-3 0 9152
2 25544 51
6426 75
4676 0019125 354
8506 5
2450 15
58385170 37087
Satellite: ISS
Catalog Number: 25544
Epoch time: 12034
93396135 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 75
4676 deg
Eccentricity:
0019125
Arg of perigee: 354
8506 deg
Mean anomaly: 5
2450 deg
Mean motion: 15
58385170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 313
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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