[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 20th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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
116/12:16:22
012 4
1 6
6 6
6
N/A -2
3 -0
1 214
2
000/00:14:44
024 -4
7 -0
1 213
1
Coasting Arc #1 (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 = -3040612
82 A = 6765139
90 meter
Y = 2986522
13 meter E =
0004839
Z = 5257652
58 I = 51
92610
XDOT = -4404
931306 Wp = 284
80429
YDOT = -6205
267869 meter/sec RA = 60
41601 deg
ZDOT = 979
287749 TA = 155
87619
MA = 155
85352
Ha = 213
322 n
mi
Hp = 210
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9975763
84 X = -3099323
45
Y = 9798300
95 feet Y = 2952192
28 meter
Z = 17249516
35 Z = 5242738
44
XDOT = -14451
874362 XDOT = -4339
972558
YDOT = -20358
490384 feet/sec YDOT = -6254
163252 meter/sec
ZDOT = 3212
886314 ZDOT = 958
046892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4717263
20 X = -1437821
82
Y = 13243474
61 feet Y = 4036611
06 meter
Z = 17187966
37 Z = 5238892
15
XDOT = -21007
914560 XDOT = -6403
212358
YDOT = -11531
777844 feet/sec YDOT = -3514
885887 meter/sec
ZDOT = 3126
114426 ZDOT = 952
839677
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
54972502
00016717 00000-0 10270-3 0 9004
2 25544 51
6406 60
8231 0008267 292
1952 67
8325 15
58434731 8726
Satellite: ISS
Catalog Number: 25544
Epoch time: 12109
54972502 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 60
8231 deg
Eccentricity:
0008267
Arg of perigee: 292
1952 deg
Mean anomaly: 67
8325 deg
Mean motion: 15
58434731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 304
Coasting Arc #2 (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 = 4727794
29 A = 6766946
10 meter
Y = 171151
36 meter E =
0003601
Z = -4841489
59 I = 51
91640
XDOT = 2332
776228 Wp = 89
26331
YDOT = 6860
217366 meter/sec RA = 55
39073 deg
ZDOT = 2522
168214 TA = 205
41377
MA = 205
43148
Ha = 213
550 n
mi
Hp = 210
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15511136
12 X = 4749048
22
Y = 561520
21 feet Y = 224138
97 meter
Z = -15884152
19 Z = -4818470
27
XDOT = 7653
465315 XDOT = 2243
638226
YDOT = 22507
274824 feet/sec YDOT = 6885
805699 meter/sec
ZDOT = 8274
830097 ZDOT = 2533
283864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14138892
66 X = 4309534
48
Y = -6633127
96 feet Y = -2021777
40 meter
Z = -15789561
97 Z = -4812658
49
XDOT = 16563
989900 XDOT = 5048
704122
YDOT = 15515
308883 feet/sec YDOT = 4729
066148 meter/sec
ZDOT = 8319
918863 ZDOT = 2535
911269
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
51159041
00016717 00000-0 10270-3 0 9019
2 25544 51
6409 55
9962 0008241 296
0286 64
0020 15
58441454 8877
Satellite: ISS
Catalog Number: 25544
Epoch time: 12110
51159041 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 55
9962 deg
Eccentricity:
0008241
Arg of perigee: 296
0286 deg
Mean anomaly: 64
0020 deg
Mean motion: 15
58441454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 290
Coasting Arc #3 (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 = -5358933
82 A = 6773551
89 meter
Y = -3094750
86 meter E =
0006291
Z = 2751018
71 I = 51
92168
XDOT = 594
539364 Wp = 76
28169
YDOT = -5636
634257 meter/sec RA = 50
38946 deg
ZDOT = -5171
423875 TA = 72
65070
MA = 72
58189
Ha = 213
563 n
mi
Hp = 210
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17581803
86 X = -5337293
43
Y = -10153382
07 feet Y = -3154556
61 meter
Z = 9025651
93 Z = 2725037
59
XDOT = 1950
588463 XDOT = 682
647171
YDOT = -18492
894545 feet/sec YDOT = -5629
493416 meter/sec
ZDOT = -16966
613762 ZDOT = -5168
321238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20340475
86 X = -6199777
04
Y = -622222
26 feet Y = -189653
34 meter
Z = 8919151
77 Z = 2718557
46
XDOT = -6967
449980 XDOT = -2123
678754
YDOT = -15788
872025 feet/sec YDOT = -4812
448193 meter/sec
ZDOT = -16953
363915 ZDOT = -5167
385321
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
53755974
00016717 00000-0 10270-3 0 9020
2 25544 51
6418 50
8484 0008248 300
0699 59
9638 15
58482972 9038
Satellite: ISS
Catalog Number: 25544
Epoch time: 12111
53755974 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 50
8484 deg
Eccentricity:
0008248
Arg of perigee: 300
0699 deg
Mean anomaly: 59
9638 deg
Mean motion: 15
58482972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 903
Checksum: 332
Coasting Arc #4 (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 = 4580146
30 A = 6776604
95 meter
Y = 4973781
50 meter E =
0013248
Z = 292721
76 I = 51
91196
XDOT = -3666
010117 Wp = 11
05505
YDOT = 3018
792081 meter/sec RA = 45
41482 deg
ZDOT = 6035
060203 TA = 352
09519
MA = 352
11605
Ha = 213
724 n
mi
Hp = 210
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15026726
69 X = 4522766
05
Y = 16318180
76 feet Y = 5024678
71 meter
Z = 960373
23 Z = 314832
71
XDOT = -12027
592247 XDOT = -3728
811874
YDOT = 9904
173493 feet/sec YDOT = 2977
445596 meter/sec
ZDOT = 19800
066284 ZDOT = 6017
097904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21068184
64 X = 6421582
68
Y = 6930749
73 feet Y = 2112492
52 meter
Z = 1050789
87 Z = 320280
75
XDOT = -5276
045398 XDOT = -1608
138637
YDOT = 13032
796161 feet/sec YDOT = 3972
396270 meter/sec
ZDOT = 19725
975885 ZDOT = 6012
477450
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
56350861
00016717 00000-0 10270-3 0 9031
2 25544 51
6418 45
7000 0008290 303
6815 56
3549 15
58503001 9197
Satellite: ISS
Catalog Number: 25544
Epoch time: 12112
56350861 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 45
7000 deg
Eccentricity:
0008290
Arg of perigee: 303
6815 deg
Mean anomaly: 56
3549 deg
Mean motion: 15
58503001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 282
Coasting Arc #5 (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 = -2435670
24 A = 6771976
04 meter
Y = -5422915
03 meter E =
0004889
Z = -3246589
54 I = 51
87599
XDOT = 5993
654708 Wp = 335
74418
YDOT = 175
680309 meter/sec RA = 40
43523 deg
ZDOT = -4783
134753 TA = 241
79315
MA = 241
84253
Ha = 213
809 n
mi
Hp = 209
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7991044
09 X = -2359077
59
Y = -17791715
96 feet Y = -5449724
02 meter
Z = -10651540
50 Z = -3258235
96
XDOT = 19664
221483 XDOT = 6014
480565
YDOT = 576
378965 feet/sec YDOT = 242
821392 meter/sec
ZDOT = -15692
699321 ZDOT = -4753
966733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15789732
40 X = -4812710
44
Y = -11405048
61 feet Y = -3476258
82 meter
Z = -10698900
61 Z = -3261024
91
XDOT = 16543
966364 XDOT = 5042
600948
YDOT = -8274
530163 feet/sec YDOT = -2522
076794 meter/sec
ZDOT = -15572
849924 ZDOT = -4746
604657
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
52531645
00016717 00000-0 10270-3 0 9040
2 25544 51
6429 40
8738 0008280 307
5032 52
5370 15
58550165 9346
Satellite: ISS
Catalog Number: 25544
Epoch time: 12113
52531645 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 40
8738 deg
Eccentricity:
0008280
Arg of perigee: 307
5032 deg
Mean anomaly: 52
5370 deg
Mean motion: 15
58550165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 290
Coasting Arc #6 (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 = -613552
88 A = 6765457
70 meter
Y = 4446988
51 meter E =
0002937
Z = 5062573
89 I = 51
83057
XDOT = -6796
422451 Wp = 319
37455
YDOT = -3045
380772 meter/sec RA = 35
42214 deg
ZDOT = 1854
171108 TA = 112
74479
MA = 112
71374
Ha = 213
912 n
mi
Hp = 209
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2012968
77 X = -687827
68
Y = 14589857
30 feet Y = 4439712
12 meter
Z = 16609494
39 Z = 5059412
78
XDOT = -22297
973922 XDOT = -6770
870560
YDOT = -9991
406733 feet/sec YDOT = -3121
239689 meter/sec
ZDOT = 6083
238544 ZDOT = 1821
215898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5734313
13 X = 1747818
64
Y = 13582300
13 feet Y = 4139885
08 meter
Z = 16596085
67 Z = 5058486
91
XDOT = -23292
916378 XDOT = -7099
680912
YDOT = 2577
264415 feet/sec YDOT = 785
550194 meter/sec
ZDOT = 5948
097793 ZDOT = 1812
980207
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
55122421
00016717 00000-0 10270-3 0 9053
2 25544 51
6428 35
7256 0008316 310
1593 49
8833 15
58595218 9504
Satellite: ISS
Catalog Number: 25544
Epoch time: 12114
55122421 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 35
7256 deg
Eccentricity:
0008316
Arg of perigee: 310
1593 deg
Mean anomaly: 49
8833 deg
Mean motion: 15
58595218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 950
Checksum: 301
Coasting Arc #7 (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 = 3700049
95 A = 6765381
85 meter
Y = -2479621
88 meter E =
0007542
Z = -5097578
60 I = 51
80525
XDOT = 5651
871619 Wp = 67
84429
YDOT = 4890
599060 meter/sec RA = 30
38771 deg
ZDOT = 1728
255641 TA = 218
78667
MA = 218
84083
Ha = 214
129 n
mi
Hp = 209
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12139271
48 X = 3752265
86
Y = -8135242
40 feet Y = -2437953
65 meter
Z = -16724339
23 Z = -5079476
82
XDOT = 18542
885890 XDOT = 5588
368275
YDOT = 16045
272505 feet/sec YDOT = 4953
446704 meter/sec
ZDOT = 5670
130055 ZDOT = 1755
558399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6041548
55 X = 1841464
00
Y = -13399040
95 feet Y = -4084027
68 meter
Z = -16649714
61 Z = -5074833
01
XDOT = 23229
326270 XDOT = 7080
298647
YDOT = 3309
117970 feet/sec YDOT = 1008
619157 meter/sec
ZDOT = 5781
860618 ZDOT = 1762
311116
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
51299598
00016717 00000-0 10270-3 0 9061
2 25544 51
6433 30
8987 0008340 314
5041 45
5432 15
58600838 9659
Satellite: ISS
Catalog Number: 25544
Epoch time: 12115
51299598 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 30
8987 deg
Eccentricity:
0008340
Arg of perigee: 314
5041 deg
Mean anomaly: 45
5432 deg
Mean motion: 15
58600838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 314
Coasting Arc #8 (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 = -5906152
90 A = 6771734
09 meter
Y = 83570
78 meter E =
0009122
Z = 3311666
38 I = 51
79950
XDOT = -2728
811875 Wp = 51
20422
YDOT = -5401
329961 meter/sec RA = 25
36997 deg
ZDOT = -4716
052698 TA = 90
31101
MA = 90
20647
Ha = 214
199 n
mi
Hp = 209
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19377142
07 X = -5922735
99
Y = 274182
36 feet Y = 17431
76 meter
Z = 10865047
18 Z = 3282933
89
XDOT = -8952
794867 XDOT = -2645
300469
YDOT = -17720
898821 feet/sec YDOT = -5431
378211 meter/sec
ZDOT = -15472
613838 ZDOT = -4729
106554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16136823
55 X = -4918503
82
Y = 10849134
13 feet Y = 3306816
08 meter
Z = 10746965
87 Z = 3275675
20
XDOT = -16308
428653 XDOT = -4970
809053
YDOT = -8830
341436 feet/sec YDOT = -2691
488070 meter/sec
ZDOT = -15525
734248 ZDOT = -4732
243799
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
53886540
00016717 00000-0 10270-3 0 9074
2 25544 51
6430 25
7503 0008298 318
1574 41
8946 15
58619856 9813
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53886540 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 25
7503 deg
Eccentricity:
0008298
Arg of perigee: 318
1574 deg
Mean anomaly: 41
8946 deg
Mean motion: 15
58619856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 331
Coasting Arc #9 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:23:44
024
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2155162
10 A = 6772237
11 meter
Y = -4767810
86 meter E =
0004231
Z = -4302298
51 I = 51
78891
XDOT = 6799
523784 Wp =
88283
YDOT = 130
366815 meter/sec RA = 25
33657 deg
ZDOT = -3546
492476 TA = 233
04882
MA = 233
08757
Ha = 214
176 n
mi
Hp = 213
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7070741
79 X = -2080787
42
Y = -15642424
08 feet Y = -4791495
30 meter
Z = -14115152
58 Z = -4312587
75
XDOT = 22308
148896 XDOT = 6814
788925
YDOT = 427
712649 feet/sec YDOT = 206
488702 meter/sec
ZDOT = -11635
474003 ZDOT = -3513
423174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15280060
15 X = -4657362
33
Y = -7747142
60 feet Y = -2361329
06 meter
Z = -14156973
42 Z = -4315045
50
XDOT = 17082
290615 XDOT = 5206
682179
YDOT = -12653
682452 feet/sec YDOT = -3856
842411 meter/sec
ZDOT = -11499
591657 ZDOT = -3505
075537
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
53888389
00016717 00000-0 10270-3 0 9088
2 25544 51
6438 25
7505 0008036 278
9214 81
1030 15
57288127 9810
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53888389 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 25
7505 deg
Eccentricity:
0008036
Arg of perigee: 278
9214 deg
Mean anomaly: 81
1030 deg
Mean motion: 15
57288127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 322
Coasting Arc #10 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2012/117/12:23:44
024
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -773741
64 A = 6768184
52 meter
Y = 4159026
45 meter E =
0005336
Z = 5287733
78 I = 51
74729
XDOT = -7327
392545 Wp = 275
01392
YDOT = -2175
248035 meter/sec RA = 20
31790 deg
ZDOT = 639
734642 TA = 168
89508
MA = 168
88330
Ha = 214
446 n
mi
Hp = 213
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2538522
44 X = -845878
09
Y = 13645099
90 feet Y = 4149970
56 meter
Z = 17348207
95 Z = 5283799
80
XDOT = -24040
001789 XDOT = -7305
631607
YDOT = -7136
640536 feet/sec YDOT = -2257
065809 meter/sec
ZDOT = 2098
866935 ZDOT = 604
190949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6754466
81 X = 2058761
48
Y = 12148447
00 feet Y = 3702846
65 meter
Z = 17331635
24 Z = 5282682
42
XDOT = -22119
684267 XDOT = -6742
079764
YDOT = 9516
870247 feet/sec YDOT = 2900
742051 meter/sec
ZDOT = 1953
016544 ZDOT = 595
279443
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
56562827
00016717 00000-0 10270-3 0 9099
2 25544 51
6435 20
6072 0008123 282
1761 77
8483 15
57321840 9972
Satellite: ISS
Catalog Number: 25544
Epoch time: 12117
56562827 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 20
6072 deg
Eccentricity:
0008123
Arg of perigee: 282
1761 deg
Mean anomaly: 77
8483 deg
Mean motion: 15
57321840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 315
Coasting Arc #11 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2012/118/12:23:44
024
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3660212
01 A = 6770063
38 meter
Y = -2974766
33 meter E =
0003538
Z = -4860016
97 I = 51
72495
XDOT = 6255
147862 Wp = 110
84710
YDOT = 3707
616984 meter/sec RA = 15
29188 deg
ZDOT = 2441
732037 TA = 183
07386
MA = 183
07603
Ha = 214
735 n
mi
Hp = 212
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12008569
58 X = 3716813
46
Y = -9759732
04 feet Y = -2933519
03 meter
Z = -15944937
57 Z = -4842098
25
XDOT = 20522
138656 XDOT = 6201
362165
YDOT = 12164
097715 feet/sec YDOT = 3777
265149 meter/sec
ZDOT = 8010
931879 ZDOT = 2471
988898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2725791
68 X = 830821
30
Y = -15309481
66 feet Y = -4666330
01 meter
Z = -15871010
62 Z = -4837484
04
XDOT = 22313
638065 XDOT = 6801
196882
YDOT = -4459
733581 feet/sec YDOT = -1359
326796 meter/sec
ZDOT = 8134
904224 ZDOT = 2479
518808
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
52818521
00016717 00000-0 10270-3 0 9103
2 25544 51
6438 15
7854 0008186 286
2198 73
8056 15
57334634 10122
Satellite: ISS
Catalog Number: 25544
Epoch time: 12118
52818521 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 15
7854 deg
Eccentricity:
0008186
Arg of perigee: 286
2198 deg
Mean anomaly: 73
8056 deg
Mean motion: 15
57334634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
Checksum: 309
Coasting Arc #12 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2012/119/12:23:44
024
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5840480
09 A = 6775937
53 meter
Y = 1440245
24 meter E =
0005568
Z = 3116211
93 I = 51
71496
XDOT = -3739
148409 Wp = 73
56278
YDOT = -4591
068674 meter/sec RA = 10
28318 deg
ZDOT = -4877
355482 TA = 70
56307
MA = 70
50290
Ha = 214
821 n
mi
Hp = 212
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19161680
10 X = -5871289
07
Y = 4725214
06 feet Y = 1374761
11 meter
Z = 10223792
43 Z = 3087764
16
XDOT = -12267
547272 XDOT = -3663
839019
YDOT = -15062
561267 feet/sec YDOT = -4632
461042 meter/sec
ZDOT = -16001
822448 ZDOT = -4895
337295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11120673
74 X = -3389581
36
Y = 16377050
73 feet Y = 4991725
06 meter
Z = 10106749
64 Z = 3080537
29
XDOT = -17929
835798 XDOT = -5465
013951
YDOT = -2236
636759 feet/sec YDOT = -681
726884 meter/sec
ZDOT = -16075
263285 ZDOT = -4899
740249
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
55489487
00016717 00000-0 10270-3 0 9113
2 25544 51
6436 10
6424 0008124 290
2967 69
7313 15
57351784 10280
Satellite: ISS
Catalog Number: 25544
Epoch time: 12119
55489487 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 10
6424 deg
Eccentricity:
0008124
Arg of perigee: 290
2967 deg
Mean anomaly: 69
7313 deg
Mean motion: 15
57351784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1028
Checksum: 317
Coasting Arc #13 (Orbit 1042)
---------------------------------------
Vector Time (GMT): 2012/120/12:23:44
024
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6748240
44 A = 6779747
12 meter
Y = 208722
95 meter E =
0011625
Z = -525460
88 I = 51
69843
XDOT = 318
185465 Wp = 358
31786
YDOT = 4784
439609 meter/sec RA = 5
29574 deg
ZDOT = 5994
769678 TA = 356
00765
MA = 356
01691
Ha = 214
984 n
mi
Hp = 212
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22139896
46 X = 6747957
50
Y = 684786
59 feet Y = 284184
36 meter
Z = -1723953
03 Z = -492678
76
XDOT = 1043
915566 XDOT = 235
539857
YDOT = 15696
980346 feet/sec YDOT = 4787
535703 meter/sec
ZDOT = 19667
879522 ZDOT = 5996
114637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16667416
07 X = 5080228
42
Y = -14604363
79 feet Y = -4451410
08 meter
Z = -1589264
62 Z = -484407
86
XDOT = 10316
353223 XDOT = 3144
424462
YDOT = 9635
934172 feet/sec YDOT = 2937
032736 meter/sec
ZDOT = 19672
935141 ZDOT = 5996
310631
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
51741706
00016717 00000-0 10270-3 0 9127
2 25544 51
6440 5
8198 0008307 293
6143 66
4139 15
57396698 10435
Satellite: ISS
Catalog Number: 25544
Epoch time: 12120
51741706 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 5
8198 deg
Eccentricity:
0008307
Arg of perigee: 293
6143 deg
Mean anomaly: 66
4139 deg
Mean motion: 15
57396698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1043
Checksum: 306
Coasting Arc #14 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2012/121/12:23:44
024
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6148059
40 A = 6777721
48 meter
Y = -1788247
02 meter E =
0003464
Z = -2218752
38 I = 51
66108
XDOT = 3227
421246 Wp = 259
83972
YDOT = -4305
504852 meter/sec RA =
31226 deg
ZDOT = -5466
268052 TA = 304
83361
MA = 304
86618
Ha = 215
148 n
mi
Hp = 212
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20170798
54 X = -6116827
65
Y = -5866952
16 feet Y = -1856823
84 meter
Z = -7279371
32 Z = -2248543
66
XDOT = 10588
652381 XDOT = 3301
880465
YDOT = -14125
672085 feet/sec YDOT = -4268
997620 meter/sec
ZDOT = -17933
950303 ZDOT = -5450
408339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18556475
56 X = -5656013
75
Y = 9754223
36 feet Y = 2973087
28 meter
Z = -7401609
95 Z = -2256010
71
XDOT = -1401
164941 XDOT = -427
075074
YDOT = -16240
590800 feet/sec YDOT = -4950
132076 meter/sec
ZDOT = -17868
358351 ZDOT = -5446
275626
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
54409095
00016717 00000-0 10270-3 0 9134
2 25544 51
6438
6767 0008412 296
4877 63
5414 15
57381773 10598
Satellite: ISS
Catalog Number: 25544
Epoch time: 12121
54409095 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node:
6767 deg
Eccentricity:
0008412
Arg of perigee: 296
4877 deg
Mean anomaly: 63
5414 deg
Mean motion: 15
57381773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1059
Checksum: 316
Coasting Arc #15 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2012/122/12:23:44
024
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4137109
35 A = 6771628
07 meter
Y = 3122547
14 meter E =
0002220
Z = 4355297
59 I = 51
61040
XDOT = -6054
437138 Wp = 54
03403
YDOT = 3228
871886 meter/sec RA = 355
30529 deg
ZDOT = 3436
226833 TA = 1
12621
MA = 1
12571
Ha = 215
295 n
mi
Hp = 211
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13573193
39 X = 4080727
66
Y = 10244577
24 feet Y = 3168495
75 meter
Z = 14289034
09 Z = 4375258
61
XDOT = -19863
638904 XDOT = -6106
785622
YDOT = 10593
411701 feet/sec YDOT = 3160
874840 meter/sec
ZDOT = 11273
710083 ZDOT = 3406
687127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16781961
13 X = 5115141
75
Y = -2281866
25 feet Y = -695512
83 meter
Z = 14370744
72 Z = 4380202
99
XDOT = -6781
514968 XDOT = -2067
005762
YDOT = 20357
568846 feet/sec YDOT = 6204
986984 meter/sec
ZDOT = 11152
018404 ZDOT = 3399
135210
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
57074724
00016717 00000-0 10270-3 0 9146
2 25544 51
6436 355
5324 0008392 302
1120 57
9219 15
57411455 10759
Satellite: ISS
Catalog Number: 25544
Epoch time: 12122
57074724 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 355
5324 deg
Eccentricity:
0008392
Arg of perigee: 302
1120 deg
Mean anomaly: 57
9219 deg
Mean motion: 15
57411455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 289
Coasting Arc #16 (Orbit 1089)
---------------------------------------
Vector Time (GMT): 2012/123/12:23:44
024
Vector Time (MET): N/A
Weight (LBS) : 924708
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1217755
96 A = 6767663
03 meter
Y = -4050510
88 meter E =
0009676
Z = -5290241
67 I = 51
56647
XDOT = 7475
375191 Wp = 53
37672
YDOT = -1647
387890 meter/sec RA = 350
27171 deg
ZDOT = -454
341601 TA = 212
25575
MA = 212
31496
Ha = 215
393 n
mi
Hp = 211
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3995262
33 X = -1146672
67
Y = -13289077
68 feet Y = -4063731
33 meter
Z = -17356435
93 Z = -5295984
74
XDOT = 24525
509156 XDOT = 7495
448144
YDOT = -5404
815913 feet/sec YDOT = -1563
681402 meter/sec
ZDOT = -1490
622051 ZDOT = -417
977267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12256750
52 X = -3735857
56
Y = -6444218
45 feet Y = -1964197
78 meter
Z = -17379634
35 Z = -5297312
55
XDOT = 12702
529900 XDOT = 3871
731114
YDOT = -20498
342142 feet/sec YDOT = -6247
894685 meter/sec
ZDOT = -1341
052788 ZDOT = -408
752890
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
53321914
00016717 00000-0 10270-3 0 9150
2 25544 51
6427 350
7098 0008529 305
0276 55
0078 15
57481084 10904
Satellite: ISS
Catalog Number: 25544
Epoch time: 12123
53321914 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 350
7098 deg
Eccentricity:
0008529
Arg of perigee: 305
0276 deg
Mean anomaly: 55
0078 deg
Mean motion: 15
57481084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1090
Checksum: 298
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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