[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 18th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
There are no maneuvers
Coasting Arc #1 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2011/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4892054
74 A = 6770030
79 meter
Y = -4400379
96 meter E =
0025991
Z = 1551601
15 I = 51
47097
XDOT = 4308
379272 Wp = 74
00213
YDOT = -2739
142264 meter/sec RA = 211
14883 deg
ZDOT = 5742
816792 TA = 303
05861
MA = 303
30796
Ha = 215
714 n
mi
Hp = 200
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16050048
35 X = -4850022
53
Y = -14436942
14 feet Y = -4454850
84 meter
Z = 5090554
96 Z = 1527938
11
XDOT = 14135
102598 XDOT = 4310
791507
YDOT = -8986
687218 feet/sec YDOT = -2690
949670 meter/sec
ZDOT = 18841
262442 ZDOT = 5763
752550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4792389
70 X = 1460720
38
Y = 21072045
32 feet Y = 6422759
42 meter
Z = 4994497
67 Z = 1522322
89
XDOT = -15099
680866 XDOT = -4602
382728
YDOT = -1109
573160 feet/sec YDOT = -338
197899 meter/sec
ZDOT = 18926
471220 ZDOT = 5768
788428
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 11229
56107709
00016717 00000-0 10270-3 0 9007
2 25544 51
6357 211
8498 0012630 86
6127 273
6473 15
60451356 10496
Satellite: ISS
Catalog Number: 25544
Epoch time: 11229
56107709 = yrday
fracday
Element set: 900
Inclination: 51
6357 deg
RA of node: 211
8498 deg
Eccentricity:
0012630
Arg of perigee: 86
6127 deg
Mean anomaly: 273
6473 deg
Mean motion: 15
60451356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 307
Coasting Arc #2 (Orbit 1063)
---------------------------------------
Vector Time (GMT): 2011/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1576930
90 A = 6762447
17 meter
Y = 4788231
84 meter E =
0022135
Z = -4528157
28 I = 51
47173
XDOT = -6967
316589 Wp = 81
00412
YDOT = -647
601666 meter/sec RA = 206
11142 deg
ZDOT = -3120
828719 TA = 157
66654
MA = 157
57000
Ha = 215
809 n
mi
Hp = 200
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5173657
82 X = 1545267
50
Y = 15709422
05 feet Y = 4805688
89 meter
Z = -14856159
06 Z = -4520573
67
XDOT = -22858
650228 XDOT = -6944
396891
YDOT = -2124
677383 feet/sec YDOT = -725
386385 meter/sec
ZDOT = -10238
939368 ZDOT = -3154
619895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4500232
22 X = 1371670
78
Y = -15943998
46 feet Y = -4859730
73 meter
Z = -14825483
51 Z = -4518807
37
XDOT = 16475
866693 XDOT = 5021
844168
YDOT = 14269
193661 feet/sec YDOT = 4349
250228 meter/sec
ZDOT = -10376
309078 ZDOT = -3162
699007
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 11230
52172144
00016717 00000-0 10270-3 0 9011
2 25544 51
6358 207
0135 0012714 89
1312 271
1300 15
60407341 10643
Satellite: ISS
Catalog Number: 25544
Epoch time: 11230
52172144 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 207
0135 deg
Eccentricity:
0012714
Arg of perigee: 89
1312 deg
Mean anomaly: 271
1300 deg
Mean motion: 15
60407341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1064
Checksum: 248
Coasting Arc #3 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2011/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2568953
86 A = 6759377
94 meter
Y = -3447422
76 meter E =
0015676
Z = 5202539
11 I = 51
48953
XDOT = 6777
018848 Wp = 85
29738
YDOT = 3486
530593 meter/sec RA = 201
03758 deg
ZDOT = -1032
154266 TA = 14
60084
MA = 14
55561
Ha = 215
657 n
mi
Hp = 200
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8428326
30 X = 2582039
89
Y = -11310442
12 feet Y = -3418621
89 meter
Z = 17068697
88 Z = 5215050
83
XDOT = 22234
313805 XDOT = 6742
542076
YDOT = 11438
748664 feet/sec YDOT = 3562
122568 meter/sec
ZDOT = -3386
332894 ZDOT = -999
315578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13167578
98 X = -4013478
07
Y = 4882051
53 feet Y = 1488049
30 meter
Z = 17119686
61 Z = 5218080
48
XDOT = -11964
605106 XDOT = -3646
811636
YDOT = -20818
189217 feet/sec YDOT = -6345
384073 meter/sec
ZDOT = -3252
919136 ZDOT = -991
489753
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 11231
54639668
00016717 00000-0 10270-3 0 9024
2 25544 51
6357 201
8566 0012592 92
5221 267
7376 15
60429369 10809
Satellite: ISS
Catalog Number: 25544
Epoch time: 11231
54639668 = yrday
fracday
Element set: 902
Inclination: 51
6357 deg
RA of node: 201
8566 deg
Eccentricity:
0012592
Arg of perigee: 92
5221 deg
Mean anomaly: 267
7376 deg
Mean motion: 15
60429369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 317
Coasting Arc #4 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2011/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5793922
02 A = 6766225
04 meter
Y = 1095842
76 meter E =
0017405
Z = -3334686
43 I = 51
54137
XDOT = -3603
820569 Wp = 94
11510
YDOT = -4893
117160 meter/sec RA = 195
98028 deg
ZDOT = 4673
388094 TA = 226
93528
MA = 227
08112
Ha = 215
712 n
mi
Hp = 200
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19008930
52 X = -5789546
14
Y = 3595284
64 feet Y = 1031076
04 meter
Z = -10940572
29 Z = -3362822
49
XDOT = -11823
558297 XDOT = -3571
539254
YDOT = -16053
533989 feet/sec YDOT = -4933
236768 meter/sec
ZDOT = 15332
638103 ZDOT = 4655
959284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17930738
43 X = 5465289
07
Y = 7087782
93 feet Y = 2160356
24 meter
Z = -11055025
35 Z = -3369571
73
XDOT = 2006
180735 XDOT = 611
483888
YDOT = 18628
814615 feet/sec YDOT = 5678
062695 meter/sec
ZDOT = 15261
924095 ZDOT = 4651
834464
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 11232
50702042
00016717 00000-0 10270-3 0 9039
2 25544 51
6359 197
0220 0012636 95
7640 264
4957 15
60429984 10951
Satellite: ISS
Catalog Number: 25544
Epoch time: 11232
50702042 = yrday
fracday
Element set: 903
Inclination: 51
6359 deg
RA of node: 197
0220 deg
Eccentricity:
0012636
Arg of perigee: 95
7640 deg
Mean anomaly: 264
4957 deg
Mean motion: 15
60429984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 304
Coasting Arc #5 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2011/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6592525
26 A = 6770950
42 meter
Y = 1491750
90 meter E =
0022993
Z = -265072
17 I = 51
58739
XDOT = -1268
217680 Wp = 117
66929
YDOT = 4609
197954 meter/sec RA = 190
96812 deg
ZDOT = -6010
851453 TA = 65
19732
MA = 64
95832
Ha = 215
659 n
mi
Hp = 200
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21629019
88 X = 6576641
90
Y = 4894195
85 feet Y = 1565383
73 meter
Z = -869659
34 Z = -233084
47
XDOT = -4160
819159 XDOT = -1290
464945
YDOT = 15122
040531 feet/sec YDOT = 4594
891631 meter/sec
ZDOT = -19720
641251 ZDOT = -6017
066410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15935136
74 X = -4857029
68
Y = -15428815
49 feet Y = -4702702
96 meter
Z = -739615
54 Z = -225434
82
XDOT = 10189
569244 XDOT = 3105
780706
YDOT = -9652
957929 feet/sec YDOT = -2942
221577 meter/sec
ZDOT = -19746
069792 ZDOT = -6018
602073
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 11233
53167582
00016717 00000-0 10270-3 0 9048
2 25544 51
6365 191
8638 0012547 99
4923 260
7651 15
60465422 11115
Satellite: ISS
Catalog Number: 25544
Epoch time: 11233
53167582 = yrday
fracday
Element set: 904
Inclination: 51
6365 deg
RA of node: 191
8638 deg
Eccentricity:
0012547
Arg of perigee: 99
4923 deg
Mean anomaly: 260
7651 deg
Mean motion: 15
60465422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 307
Coasting Arc #6 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2011/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4541591
94 A = 6765168
11 meter
Y = -3398351
45 meter E =
0024300
Z = 3669780
18 I = 51
59843
XDOT = 5666
446531 Wp = 99
66185
YDOT = -2862
411373 meter/sec RA = 185
95546 deg
ZDOT = 4333
503461 TA = 304
21725
MA = 304
44728
Ha = 215
603 n
mi
Hp = 200
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14900236
04 X = -4521080
35
Y = -11149447
02 feet Y = -3449023
69 meter
Z = 12039961
21 Z = 3647767
07
XDOT = 18590
703842 XDOT = 5676
982231
YDOT = -9391
113430 feet/sec YDOT = -2798
986887 meter/sec
ZDOT = 14217
531039 ZDOT = 4361
056357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7289590
32 X = 2221867
13
Y = 17185296
24 feet Y = 5238078
29 meter
Z = 11950537
01 Z = 3642523
68
XDOT = -19460
551052 XDOT = -5931
575961
YDOT = -1775
340324 feet/sec YDOT = -541
123731 meter/sec
ZDOT = 14329
696009 ZDOT = 4367
691343
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 11234
55631956
00016717 00000-0 10270-3 0 9053
2 25544 51
6367 186
7074 0012483 103
9982 256
2562 15
60509302 11273
Satellite: ISS
Catalog Number: 25544
Epoch time: 11234
55631956 = yrday
fracday
Element set: 905
Inclination: 51
6367 deg
RA of node: 186
7074 deg
Eccentricity:
0012483
Arg of perigee: 103
9982 deg
Mean anomaly: 256
2562 deg
Mean motion: 15
60509302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 310
Coasting Arc #7 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2011/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 446967
26 A = 6759002
26 meter
Y = 4204115
01 meter E =
0026779
Z = -5296296
78 I = 51
60796
XDOT = -7641
703518 Wp = 95
98364
YDOT = 242
497462 meter/sec RA = 180
89784 deg
ZDOT = -457
126620 TA = 169
67674
MA = 169
62164
Ha = 215
529 n
mi
Hp = 200
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1466428
01 X = 425650
96
Y = 13793028
25 feet Y = 4208994
23 meter
Z = -17376301
76 Z = -5294177
10
XDOT = -25071
205768 XDOT = -7641
626609
YDOT = 795
595347 feet/sec YDOT = 157
043710 meter/sec
ZDOT = -1499
759251 ZDOT = -494
249401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5392226
46 X = 1643550
63
Y = -12791272
89 feet Y = -3898779
98 meter
Z = -17367818
92 Z = -5293711
21
XDOT = 21300
662114 XDOT = 6492
441812
YDOT = 11199
795787 feet/sec YDOT = 3413
697756 meter/sec
ZDOT = -1650
781282 ZDOT = -503
158135
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 11235
51691552
00016717 00000-0 10270-3 0 9069
2 25544 51
6368 181
8713 0012423 106
8734 253
3785 15
60485569 11421
Satellite: ISS
Catalog Number: 25544
Epoch time: 11235
51691552 = yrday
fracday
Element set: 906
Inclination: 51
6368 deg
RA of node: 181
8713 deg
Eccentricity:
0012423
Arg of perigee: 106
8734 deg
Mean anomaly: 253
3785 deg
Mean motion: 15
60485569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 314
Coasting Arc #8 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2011/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3836365
62 A = 6763127
64 meter
Y = -3620814
95 meter E =
0021296
Z = 4212866
89 I = 51
65306
XDOT = 6318
226335 Wp = 94
43299
YDOT = 2433
473734 meter/sec RA = 175
83651 deg
ZDOT = -3647
872734 TA = 32
84656
MA = 32
71438
Ha = 215
388 n
mi
Hp = 200
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12586501
37 X = 3856104
11
Y = -11879314
14 feet Y = -3577804
11 meter
Z = 13821741
77 Z = 4231551
53
XDOT = 20729
089025 XDOT = 6308
265613
YDOT = 7983
837710 feet/sec YDOT = 2504
072400 meter/sec
ZDOT = -11968
086396 ZDOT = -3617
203379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16645751
57 X = -5073625
08
Y = 4510714
54 feet Y = 1374865
79 meter
Z = 13897880
26 Z = 4236073
90
XDOT = -14179
989462 XDOT = -4322
060788
YDOT = -15694
673028 feet/sec YDOT = -4783
736339 meter/sec
ZDOT = -11843
388883 ZDOT = -3609
864932
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 11236
54153970
00016717 00000-0 10270-3 0 9071
2 25544 51
6372 176
7142 0012420 110
5281 249
7209 15
60515569 11582
Satellite: ISS
Catalog Number: 25544
Epoch time: 11236
54153970 = yrday
fracday
Element set: 907
Inclination: 51
6372 deg
RA of node: 176
7142 deg
Eccentricity:
0012420
Arg of perigee: 110
5281 deg
Mean anomaly: 249
7209 deg
Mean motion: 15
60515569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1158
Checksum: 297
Coasting Arc #9 (Orbit 1172)
---------------------------------------
Vector Time (GMT): 2011/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6419533
46 A = 6770290
73 meter
Y = 1878793
59 meter E =
0017364
Z = -1051969
21 I = 51
70712
XDOT = -2230
130173 Wp = 82
31165
YDOT = -4361
920715 meter/sec RA = 170
82003 deg
ZDOT = 5904
421341 TA = 266
27114
MA = 266
46971
Ha = 215
387 n
mi
Hp = 200
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21061461
47 X = -6434955
20
Y = 6164020
98 feet Y = 1806920
24 meter
Z = -3451342
55 Z = -1083192
15
XDOT = -7316
700042 XDOT = -2209
870655
YDOT = -14310
763501 feet/sec YDOT = -4386
746207 meter/sec
ZDOT = 19371
461094 ZDOT = 5893
636712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21517564
91 X = 6558553
78
Y = 4204897
72 feet Y = 1281652
83 meter
Z = -3578451
45 Z = -1090712
00
XDOT = 324
713163 XDOT = 98
972572
YDOT = 14556
187002 feet/sec YDOT = 4436
725798 meter/sec
ZDOT = 19327
721347 ZDOT = 5891
089466
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 11237
50211502
00016717 00000-0 10270-3 0 9085
2 25544 51
6371 171
8790 0012372 114
0105 246
2347 15
60521636 11730
Satellite: ISS
Catalog Number: 25544
Epoch time: 11237
50211502 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 171
8790 deg
Eccentricity:
0012372
Arg of perigee: 114
0105 deg
Mean anomaly: 246
2347 deg
Mean motion: 15
60521636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1173
Checksum: 269
Coasting Arc #10 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2011/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6166922
75 A = 6767663
48 meter
Y = 648358
92 meter E =
0017268
Z = -2711325
23 I = 51
72948
XDOT = -2783
583459 Wp = 120
10550
YDOT = 4923
773372 meter/sec RA = 165
82293 deg
ZDOT = -5186
929957 TA = 90
57744
MA = 90
37957
Ha = 215
381 n
mi
Hp = 200
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20232686
17 X = 6172385
18
Y = 2127161
80 feet Y = 717351
74 meter
Z = -8895424
00 Z = -2681353
70
XDOT = -9132
491664 XDOT = -2813
238541
YDOT = 16154
112112 feet/sec YDOT = 4892
479805 meter/sec
ZDOT = -17017
486735 ZDOT = -5200
524371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17224740
84 X = -5250101
01
Y = -10924715
90 feet Y = -3329853
41 meter
Z = -8773474
83 Z = -2674155
13
XDOT = 14473
747053 XDOT = 4411
598102
YDOT = -9197
732095 feet/sec YDOT = -2803
468743 meter/sec
ZDOT = -17072
969038 ZDOT = -5203
840963
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 11238
52671831
00016717 00000-0 10270-3 0 9094
2 25544 51
6385 166
7207 0012366 117
7191 242
5221 15
60550151 11890
Satellite: ISS
Catalog Number: 25544
Epoch time: 11238
52671831 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 166
7207 deg
Eccentricity:
0012366
Arg of perigee: 117
7191 deg
Mean anomaly: 242
5221 deg
Mean motion: 15
60550151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1189
Checksum: 298
Coasting Arc #11 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2011/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3274199
05 A = 6759781
31 meter
Y = -3071954
53 meter E =
0017940
Z = 5043249
73 I = 51
73273
XDOT = 6428
487150 Wp = 123
18638
YDOT = -3787
253270 meter/sec RA = 160
78934 deg
ZDOT = 1852
267554 TA = 308
86232
MA = 309
02226
Ha = 215
295 n
mi
Hp = 200
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10742122
85 X = -3264103
15
Y = -10078590
97 feet Y = -3108512
01 meter
Z = 16546094
91 Z = 5027368
65
XDOT = 21090
837105 XDOT = 6461
361395
YDOT = -12425
371621 feet/sec YDOT = -3715
182130 meter/sec
ZDOT = 6076
993286 ZDOT = 1883
576415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5467480
36 X = 1666488
01
Y = 13755340
33 feet Y = 4192627
73 meter
Z = 16481557
19 Z = 5023578
63
XDOT = -23345
717740 XDOT = -7115
774767
YDOT = 1788
552903 feet/sec YDOT = 545
150925 meter/sec
ZDOT = 6204
540070 ZDOT = 1891
143813
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 11239
55130965
00016717 00000-0 10270-3 0 9108
2 25544 51
6386 161
5637 0012295 122
2332 238
0018 15
60591374 12055
Satellite: ISS
Catalog Number: 25544
Epoch time: 11239
55130965 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 161
5637 deg
Eccentricity:
0012295
Arg of perigee: 122
2332 deg
Mean anomaly: 238
0018 deg
Mean motion: 15
60591374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 287
Coasting Arc #12 (Orbit 1219)
---------------------------------------
Vector Time (GMT): 2011/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -935075
01 A = 6760572
87 meter
Y = 4625397
80 meter E =
0023904
Z = -4863660
34 I = 51
76435
XDOT = -7172
622027 Wp = 116
71014
YDOT = 1121
456702 meter/sec RA = 155
72954 deg
ZDOT = 2444
288324 TA = 177
26519
MA = 177
25210
Ha = 215
175 n
mi
Hp = 200
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3067831
38 X = -963101
32
Y = 15175189
62 feet Y = 4614784
23 meter
Z = -15956890
88 Z = -4868271
18
XDOT = -23532
224499 XDOT = -7196
502955
YDOT = 3679
319887 feet/sec YDOT = 1041
114677 meter/sec
ZDOT = 8019
318648 ZDOT = 2409
386383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8981126
06 X = 2737447
22
Y = -12587032
98 feet Y = -3836527
65 meter
Z = -15975803
93 Z = -4869425
04
XDOT = 22073
070082 XDOT = 6727
871761
YDOT = 5746
565240 feet/sec YDOT = 1751
553085 meter/sec
ZDOT = 7877
220953 ZDOT = 2400
976947
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 11240
51185651
00016717 00000-0 10270-3 0 9119
2 25544 51
6394 156
7279 0012276 125
0653 235
1656 15
60574418 12201
Satellite: ISS
Catalog Number: 25544
Epoch time: 11240
51185651 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 156
7279 deg
Eccentricity:
0012276
Arg of perigee: 125
0653 deg
Mean anomaly: 235
1656 deg
Mean motion: 15
60574418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1220
Checksum: 294
Coasting Arc #13 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2011/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4549013
75 A = 6768600
19 meter
Y = -4501112
08 meter E =
0025870
Z = 2161394
85 I = 51
81851
XDOT = 4862
532250 Wp = 118
75730
YDOT = 2246
915529 meter/sec RA = 150
70599 deg
ZDOT = -5517
267458 TA = 37
22126
MA = 37
04222
Ha = 215
107 n
mi
Hp = 200
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14924585
80 X = 4588508
48
Y = -14767428
09 feet Y = -4450021
23 meter
Z = 7091190
44 Z = 2183589
86
XDOT = 15953
189796 XDOT = 4863
846848
YDOT = 7371
770108 feet/sec YDOT = 2301
298256 meter/sec
ZDOT = -18101
271188 ZDOT = -5493
642659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19528092
31 X = -5952162
54
Y = 7627730
73 feet Y = 2324932
33 meter
Z = 7181678
77 Z = 2188975
69
XDOT = -11247
510047 XDOT = -3428
241062
YDOT = -11728
512194 feet/sec YDOT = -3574
850517 meter/sec
ZDOT = -18005
174267 ZDOT = -5487
977116
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 11241
53642847
00016717 00000-0 10270-3 0 9128
2 25544 51
6394 151
5702 0012327 129
0950 231
1305 15
60579282 12364
Satellite: ISS
Catalog Number: 25544
Epoch time: 11241
53642847 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 151
5702 deg
Eccentricity:
0012327
Arg of perigee: 129
0950 deg
Mean anomaly: 231
1305 deg
Mean motion: 15
60579282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 286
Coasting Arc #14 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2011/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6039978
31 A = 6769545
61 meter
Y = 2597670
51 meter E =
0021487
Z = 1598455
36 I = 51
84767
XDOT = -627
912795 Wp = 95
14891
YDOT = -5042
805070 meter/sec RA = 145
71816 deg
ZDOT = 5754
292357 TA = 282
33333
MA = 282
57378
Ha = 215
031 n
mi
Hp = 200
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19816201
82 X = -6076341
99
Y = 8522541
05 feet Y = 2529924
60 meter
Z = 5244276
11 Z = 1569024
93
XDOT = -2060
081347 XDOT = -599
429493
YDOT = -16544
636057 feet/sec YDOT = -5049
667028 meter/sec
ZDOT = 18878
911933 ZDOT = 5751
311605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21597956
64 X = 6583057
18
Y = -294815
73 feet Y = -89859
84 meter
Z = 5124387
29 Z = 1561913
24
XDOT = -4332
199429 XDOT = -1320
454386
YDOT = 14544
566448 feet/sec YDOT = 4433
183853 meter/sec
ZDOT = 18866
937940 ZDOT = 5750
642684
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 11242
56098894
00016717 00000-0 10270-3 0 9130
2 25544 51
6395 146
4125 0012199 132
6065 227
6122 15
60599689 12529
Satellite: ISS
Catalog Number: 25544
Epoch time: 11242
56098894 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 146
4125 deg
Eccentricity:
0012199
Arg of perigee: 132
6065 deg
Mean anomaly: 227
6122 deg
Mean motion: 15
60599689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 323
Coasting Arc #15 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2011/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4922729
37 A = 6761539
81 meter
Y = 644142
89 meter E =
0018622
Z = -4602861
31 I = 51
84610
XDOT = -3615
829530 Wp = 106
80696
YDOT = 6041
891036 meter/sec RA = 140
70546 deg
ZDOT = -3036
952199 TA = 133
02968
MA = 132
87354
Ha = 214
904 n
mi
Hp = 200
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16150686
91 X = 4937520
30
Y = 2113329
69 feet Y = 699274
20 meter
Z = -15101251
02 Z = -4578910
96
XDOT = -11862
957774 XDOT = -3668
369522
YDOT = 19822
477151 feet/sec YDOT = 6001
162616 meter/sec
ZDOT = -9963
753933 ZDOT = -3054
645878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14340889
58 X = -4371103
14
Y = -7911031
92 feet Y = -2411282
53 meter
Z = -15003769
27 Z = -4573148
87
XDOT = 17662
391040 XDOT = 5383
496789
YDOT = -13080
276102 feet/sec YDOT = -3986
868156 meter/sec
ZDOT = -10035
983436 ZDOT = -3058
967751
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 11243
52150345
00016717 00000-0 10270-3 0 9148
2 25544 51
6399 141
5766 0012128 136
3342 223
8776 15
60641424 12675
Satellite: ISS
Catalog Number: 25544
Epoch time: 11243
52150345 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 141
5766 deg
Eccentricity:
0012128
Arg of perigee: 136
3342 deg
Mean anomaly: 223
8776 deg
Mean motion: 15
60641424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 297
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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