[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 26th 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
243/12:13:43
502 -5
9 6
7 6
7
N/A 2
6 0
1 215
1
000/00:17:27
005 2
0 -0
0 205
2
Coasting Arc #1 (Orbit 1158)
---------------------------------------
Vector Time (GMT): 2011/236/13:44:22
931
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6682066
45 A = 6770795
26 meter
Y = -908322
73 meter E =
0025231
Z = 481916
74 I = 51
68181
XDOT = 1083
999673 Wp = 120
81990
YDOT = 4673
102490 meter/sec RA = 175
49651 deg
ZDOT = -6002
761027 TA = 53
96739
MA = 53
73383
Ha = 215
536 n
mi
Hp = 200
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21922790
20 X = 6689385
84
Y = -2980061
47 feet Y = -833558
88 meter
Z = 1581091
65 Z = 514395
48
XDOT = 3556
429374 XDOT = 1060
823448
YDOT = 15331
701084 feet/sec YDOT = 4685
095005 meter/sec
ZDOT = -19694
097859 ZDOT = -5997
551211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22011262
06 X = -6709032
68
Y = 2135045
80 feet Y = 650761
96 meter
Z = 1713262
69 Z = 522202
47
XDOT = -2926
994781 XDOT = -892
148009
YDOT = -13855
658752 feet/sec YDOT = -4223
204788 meter/sec
ZDOT = -19673
056371 ZDOT = -5996
347582
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
60559806
00016717 00000-0 10270-3 0 9009
2 25544 51
6385 176
3969 0012516 111
0794 249
1702 15
60488507 11594
Satellite: ISS
Catalog Number: 25544
Epoch time: 11236
60559806 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 176
3969 deg
Eccentricity:
0012516
Arg of perigee: 111
0794 deg
Mean anomaly: 249
1702 deg
Mean motion: 15
60488507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1159
Checksum: 317
Coasting Arc #2 (Orbit 1174)
---------------------------------------
Vector Time (GMT): 2011/237/13:44:22
931
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5804347
79 A = 6766784
21 meter
Y = -1520409
01 meter E =
0024671
Z = 3112237
92 I = 51
69868
XDOT = 3823
923045 Wp = 99
41179
YDOT = -4544
031737 meter/sec RA = 170
49516 deg
ZDOT = 4874
969568 TA = 296
51302
MA = 296
76579
Ha = 215
514 n
mi
Hp = 200
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19043135
79 X = -5802033
29
Y = -4988218
52 feet Y = -1585303
87 meter
Z = 10210754
32 Z = 3084046
53
XDOT = 12545
679282 XDOT = 3850
769817
YDOT = -14908
240607 feet/sec YDOT = -4501
120256 meter/sec
ZDOT = 15993
994646 ZDOT = 4893
610981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18993922
60 X = 5789347
61
Y = 5392836
82 feet Y = 1643736
66 meter
Z = 10096091
52 Z = 3077288
69
XDOT = -12370
026374 XDOT = -3770
384039
YDOT = 13254
323019 feet/sec YDOT = 4039
917656 meter/sec
ZDOT = 16069
996967 ZDOT = 4898
135075
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
63021564
00016717 00000-0 10270-3 0 9019
2 25544 51
6386 171
2396 0012461 114
4010 245
8448 15
60515141 11753
Satellite: ISS
Catalog Number: 25544
Epoch time: 11237
63021564 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 171
2396 deg
Eccentricity:
0012461
Arg of perigee: 114
4010 deg
Mean anomaly: 245
8448 deg
Mean motion: 15
60515141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1175
Checksum: 276
Coasting Arc #3 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2011/238/13:44:22
931
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2403798
29 A = 6759275
81 meter
Y = 3617857
42 meter E =
0025027
Z = -5199557
07 I = 51
70472
XDOT = -6999
428550 Wp = 98
17957
YDOT = 2847
149122 meter/sec RA = 165
45221 deg
ZDOT = -1263
516404 TA = 159
73969
MA = 159
64021
Ha = 215
336 n
mi
Hp = 200
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7886477
33 X = 2388422
01
Y = 11869610
96 feet Y = 3644652
15 meter
Z = -17058914
26 Z = -5187917
04
XDOT = -22964
004430 XDOT = -7024
607912
YDOT = 9341
040425 feet/sec YDOT = 2768
736443 meter/sec
ZDOT = -4145
395026 ZDOT = -1297
580074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7940812
00 X = -2420359
50
Y = -11901160
68 feet Y = -3627473
78 meter
Z = -17011661
40 Z = -5185154
40
XDOT = 22108
532815 XDOT = 6738
680802
YDOT = -8668
499228 feet/sec YDOT = -2642
158565 meter/sec
ZDOT = -4284
111507 ZDOT = -1305
797187
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
59078408
00016717 00000-0 10270-3 0 9025
2 25544 51
6396 166
4040 0012408 117
9830 242
2583 15
60554780 11905
Satellite: ISS
Catalog Number: 25544
Epoch time: 11238
59078408 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 166
4040 deg
Eccentricity:
0012408
Arg of perigee: 117
9830 deg
Mean anomaly: 242
2583 deg
Mean motion: 15
60554780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 304
Coasting Arc #4 (Orbit 1205)
---------------------------------------
Vector Time (GMT): 2011/239/13:44:22
931
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1917938
17 A = 6761461
91 meter
Y = -4542219
62 meter E =
0018162
Z = 4609905
35 I = 51
74159
XDOT = 7091
529524 Wp = 99
51181
YDOT = -34
075380 meter/sec RA = 160
39307 deg
ZDOT = -2976
983223 TA = 20
05766
MA = 19
98637
Ha = 215
177 n
mi
Hp = 200
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6292448
08 X = 1946194
03
Y = -14902295
34 feet Y = -4520613
92 meter
Z = 15124361
39 Z = 4619291
27
XDOT = 23266
172978 XDOT = 7105
844828
YDOT = -111
795865 feet/sec YDOT = 45
306376 meter/sec
ZDOT = -9767
005325 ZDOT = -2942
498572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6004894
73 X = -1830291
91
Y = 14981761
74 feet Y = 4566440
98 meter
Z = 15162706
59 Z = 4621592
97
XDOT = -22228
618339 XDOT = -6775
282870
YDOT = 856
579044 feet/sec YDOT = 261
085293 meter/sec
ZDOT = -9626
651634 ZDOT = -2934
203418
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
61538001
00016717 00000-0 10270-3 0 9030
2 25544 51
6396 161
2466 0012267 121
6744 238
5610 15
60582356 12066
Satellite: ISS
Catalog Number: 25544
Epoch time: 11239
61538001 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 161
2466 deg
Eccentricity:
0012267
Arg of perigee: 121
6744 deg
Mean anomaly: 238
5610 deg
Mean motion: 15
60582356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1206
Checksum: 290
Coasting Arc #5 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2011/240/13:44:22
931
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5260835
21 A = 6769291
27 meter
Y = 3903035
41 meter E =
0014698
Z = -1722830
25 I = 51
79690
XDOT = -4118
452886 Wp = 95
24197
YDOT = -3050
978272 meter/sec RA = 155
37397 deg
ZDOT = 5704
650450 TA = 245
87248
MA = 246
02626
Ha = 215
141 n
mi
Hp = 200
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17259958
04 X = -5295719
69
Y = 12805234
28 feet Y = 3844010
38 meter
Z = -5652330
21 Z = -1748471
83
XDOT = -13511
984535 XDOT = -4111
741751
YDOT = -10009
771235 feet/sec YDOT = -3096
995460 meter/sec
ZDOT = 18716
044782 ZDOT = 5684
659905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16829205
57 X = 5129541
86
Y = -13321630
59 feet Y = -4060433
00 meter
Z = -5756823
07 Z = -1754679
67
XDOT = 12950
434906 XDOT = 3947
292559
YDOT = 8363
757745 feet/sec YDOT = 2549
273361 meter/sec
ZDOT = 18634
771975 ZDOT = 5679
878498
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
57592948
00016717 00000-0 10270-3 0 9048
2 25544 51
6405 156
4112 0012290 125
5873 234
6431 15
60588052 12217
Satellite: ISS
Catalog Number: 25544
Epoch time: 11240
57592948 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 156
4112 deg
Eccentricity:
0012290
Arg of perigee: 125
5873 deg
Mean anomaly: 234
6431 deg
Mean motion: 15
60588052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 289
Coasting Arc #6 (Orbit 1236)
---------------------------------------
Vector Time (GMT): 2011/241/13:44:22
931
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6218313
48 A = 6768876
58 meter
Y = -1630863
51 meter E =
0018696
Z = -2104917
30 I = 51
82220
XDOT = -476
290250 Wp = 133
68112
YDOT = 5288
073015 meter/sec RA = 150
38498 deg
ZDOT = -5547
407322 TA = 69
63765
MA = 69
43689
Ha = 215
177 n
mi
Hp = 200
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20401290
95 X = 6246313
10
Y = -5350602
07 feet Y = -1561170
14 meter
Z = -6905896
65 Z = -2074641
09
XDOT = -1562
632055 XDOT = -508
439254
YDOT = 17349
320914 feet/sec YDOT = 5282
566652 meter/sec
ZDOT = -18200
155256 ZDOT = -5549
799609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20165124
31 X = -6146329
89
Y = 6316414
27 feet Y = 1925243
07 meter
Z = -6782602
42 Z = -2067337
22
XDOT = 1087
416070 XDOT = 331
444418
YDOT = -15927
445410 feet/sec YDOT = -4854
685361 meter/sec
ZDOT = -18210
059131 ZDOT = -5550
426023
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
60050469
00016717 00000-0 10270-3 0 9051
2 25544 51
6406 151
2533 0012210 130
2372 229
9854 15
60556152 12376
Satellite: ISS
Catalog Number: 25544
Epoch time: 11241
60050469 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 151
2533 deg
Eccentricity:
0012210
Arg of perigee: 130
2372 deg
Mean anomaly: 229
9854 deg
Mean motion: 15
60556152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1237
Checksum: 271
Coasting Arc #7 (Orbit 1252)
---------------------------------------
Vector Time (GMT): 2011/242/13:44:22
931
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4513807
92 A = 6760810
70 meter
Y = -1473533
69 meter E =
0019464
Z = 4804391
64 I = 51
82113
XDOT = 4580
525611 Wp = 127
94194
YDOT = -5613
485139 meter/sec RA = 145
36500 deg
ZDOT = 2563
048079 TA = 296
85467
MA = 297
05352
Ha = 215
119 n
mi
Hp = 200
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14809081
09 X = -4520333
71
Y = -4834428
13 feet Y = -1524045
93 meter
Z = 15762439
76 Z = 4782448
08
XDOT = 15027
971164 XDOT = 4630
505573
YDOT = -18416
945995 feet/sec YDOT = -5561
983231 meter/sec
ZDOT = 8408
950391 ZDOT = 2585
421902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15185293
63 X = 4628477
50
Y = 3859283
23 feet Y = 1176309
53 meter
Z = 15673157
80 Z = 4777178
50
XDOT = -13472
676596 XDOT = -4106
471826
YDOT = 18239
645810 feet/sec YDOT = 5559
444043 meter/sec
ZDOT = 8500
209389 ZDOT = 2590
863822
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
62506842
00016717 00000-0 10270-3 0 9066
2 25544 51
6403 146
0957 0012185 132
9999 227
2180 15
60597820 12538
Satellite: ISS
Catalog Number: 25544
Epoch time: 11242
62506842 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 146
0957 deg
Eccentricity:
0012185
Arg of perigee: 132
9999 deg
Mean anomaly: 227
2180 deg
Mean motion: 15
60597820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1253
Checksum: 308
Coasting Arc #8 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2011/243/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2938587
11 A = 6770923
57 meter
Y = 5369390
38 meter E =
0008712
Z = -2907404
11 I = 51
86427
XDOT = -5749
036468 Wp = 123
38467
YDOT = -412
515383 meter/sec RA = 140
58716 deg
ZDOT = 5055
090572 TA = 203
55738
MA = 203
59730
Ha = 215
051 n
mi
Hp = 205
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9641033
84 X = -2984286
72
Y = 17616110
17 feet Y = 5336273
56 meter
Z = -9538727
39 Z = -2921791
10
XDOT = -18861
668201 XDOT = -5768
552927
YDOT = -1353
396927 feet/sec YDOT = -476
913353 meter/sec
ZDOT = 16584
942823 ZDOT = 5027
114553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14028675
58 X = 4275940
32
Y = -14330002
00 feet Y = -4367784
61 meter
Z = -9597473
39 Z = -2925309
89
XDOT = 16826
651340 XDOT = 5128
763328
YDOT = 5454
980711 feet/sec YDOT = 1662
678121 meter/sec
ZDOT = 16471
064640 ZDOT = 5020
380502
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
52155290
00016717 00000-0 10270-3 0 9074
2 25544 51
6398 141
5825 0007322 154
7312 205
4203 15
59218331 12677
Satellite: ISS
Catalog Number: 25544
Epoch time: 11243
52155290 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 141
5825 deg
Eccentricity:
0007322
Arg of perigee: 154
7312 deg
Mean anomaly: 205
4203 deg
Mean motion: 15
59218331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 285
Coasting Arc #9 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2011/244/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5026682
83 A = 6774625
12 meter
Y = -4511516
23 meter E =
0018531
Z = -373578
44 I = 51
89861
XDOT = 2929
195218 Wp = 146
35879
YDOT = 3750
017044 meter/sec RA = 135
60588 deg
ZDOT = -6030
547734 TA = 37
66545
MA = 37
53583
Ha = 215
081 n
mi
Hp = 205
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16491741
55 X = 5078572
66
Y = -14801562
43 feet Y = -4455014
68 meter
Z = -1225651
05 Z = -349032
57
XDOT = 9610
220530 XDOT = 2916
339326
YDOT = 12303
205525 feet/sec YDOT = 3782
700850 meter/sec
ZDOT = -19785
261595 ZDOT = -6016
349195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19742713
63 X = -6017579
12
Y = 10075930
50 feet Y = 3071143
62 meter
Z = -1125563
53 Z = -343071
76
XDOT = -5514
539144 XDOT = -1680
831531
YDOT = -12946
117531 feet/sec YDOT = -3945
976623 meter/sec
ZDOT = -19727
583480 ZDOT = -6012
967445
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 11244
54702645
00016717 00000-0 10270-3 0 9080
2 25544 51
6395 136
4305 0007432 159
5502 200
5952 15
59185012 12830
Satellite: ISS
Catalog Number: 25544
Epoch time: 11244
54702645 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 136
4305 deg
Eccentricity:
0007432
Arg of perigee: 159
5502 deg
Mean anomaly: 200
5952 deg
Mean motion: 15
59185012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 294
Coasting Arc #10 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2011/245/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5406615
80 A = 6769521
10 meter
Y = 2123480
09 meter E =
0016153
Z = 3470945
70 I = 51
90237
XDOT = 540
661922 Wp = 115
77501
YDOT = -6140
364943 meter/sec RA = 130
62060 deg
ZDOT = 4575
422591 TA = 284
90290
MA = 285
08172
Ha = 214
897 n
mi
Hp = 205
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17738240
81 X = -5446820
34
Y = 6966798
21 feet Y = 2062795
35 meter
Z = 11387617
14 Z = 3444582
67
XDOT = 1773
825205 XDOT = 587
057955
YDOT = -20145
554275 feet/sec YDOT = -6134
059339 meter/sec
ZDOT = 15011
228972 ZDOT = 4578
162056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18957653
55 X = 5778292
80
Y = -2494736
27 feet Y = -760395
62 meter
Z = 11280201
73 Z = 3438205
49
XDOT = -6646
176881 XDOT = -2025
754713
YDOT = 17771
216751 feet/sec YDOT = 5416
666866 meter/sec
ZDOT = 15022
603324 ZDOT = 4578
889493
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 11245
57248872
00016717 00000-0 10270-3 0 9092
2 25544 51
6392 131
2781 0007163 162
3374 197
8031 15
59222786 12991
Satellite: ISS
Catalog Number: 25544
Epoch time: 11245
57248872 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 131
2781 deg
Eccentricity:
0007163
Arg of perigee: 162
3374 deg
Mean anomaly: 197
8031 deg
Mean motion: 15
59222786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 327
Coasting Arc #11 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2011/246/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147277
24 A = 6762963
71 meter
Y = 1227138
34 meter E =
0016082
Z = -5211629
06 I = 51
89956
XDOT = -3555
977195 Wp = 106
54715
YDOT = 6672
644726 meter/sec RA = 125
59984 deg
ZDOT = -1266
286807 TA = 151
38068
MA = 151
29231
Ha = 214
655 n
mi
Hp = 205
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13606552
61 X = 4158563
98
Y = 4026044
41 feet Y = 1273578
73 meter
Z = -17098520
54 Z = -5191454
25
XDOT = -11666
591848 XDOT = -3624
176346
YDOT = 21891
879021 feet/sec YDOT = 6632
498269 meter/sec
ZDOT = -4154
484274 ZDOT = -1283
727483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12466274
92 X = -3799720
60
Y = -6981423
71 feet Y = -2127937
95 meter
Z = -17016416
33 Z = -5186603
70
XDOT = 15721
511763 XDOT = 4791
916785
YDOT = -17834
848975 feet/sec YDOT = -5436
061968 meter/sec
ZDOT = -4225
752648 ZDOT = -1288
009407
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 11246
53384925
00016717 00000-0 10270-3 0 9101
2 25544 51
6390 126
4476 0007091 167
1906 192
9431 15
59272766 13141
Satellite: ISS
Catalog Number: 25544
Epoch time: 11246
53384925 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 126
4476 deg
Eccentricity:
0007091
Arg of perigee: 167
1906 deg
Mean anomaly: 192
9431 deg
Mean motion: 15
59272766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 316
Coasting Arc #12 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2011/247/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1811891
17 A = 6764382
32 meter
Y = -4369854
07 meter E =
0007980
Z = 4827555
87 I = 51
92191
XDOT = 5259
774396 Wp = 115
26054
YDOT = -4989
254387 meter/sec RA = 120
56569 deg
ZDOT = -2542
169620 TA = 359
59722
MA = 359
59787
Ha = 214
515 n
mi
Hp = 205
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5944524
83 X = -1786343
21
Y = -14336791
56 feet Y = -4389972
86 meter
Z = 15838437
88 Z = 4818815
83
XDOT = 17256
477676 XDOT = 5327
523626
YDOT = -16368
944839 feet/sec YDOT = -4930
057587 meter/sec
ZDOT = -8340
451509 ZDOT = -2516
453179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2953530
32 X = 900236
04
Y = 15273453
83 feet Y = 4655348
73 meter
Z = 15803017
08 Z = 4816759
61
XDOT = -19196
463251 XDOT = -5851
081999
YDOT = 12233
017446 feet/sec YDOT = 3728
623717 meter/sec
ZDOT = -8235
530173 ZDOT = -2510
189597
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 11247
55929115
00016717 00000-0 10270-3 0 9111
2 25544 51
6394 121
2957 0007024 171
9769 188
1500 15
59309238 13305
Satellite: ISS
Catalog Number: 25544
Epoch time: 11247
55929115 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 121
2957 deg
Eccentricity:
0007024
Arg of perigee: 171
9769 deg
Mean anomaly: 188
1500 deg
Mean motion: 15
59309238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 310
Coasting Arc #13 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2011/248/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -807051
35 A = 6771698
37 meter
Y = 6240863
44 meter E =
0005762
Z = -2510902
70 I = 51
95995
XDOT = -5317
942727 Wp = 128
35121
YDOT = 1454
631002 meter/sec RA = 115
55972 deg
ZDOT = 5329
552406 TA = 203
57862
MA = 203
60504
Ha = 214
361 n
mi
Hp = 205
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2647806
25 X = -864580
52
Y = 20475273
76 feet Y = 6231516
83 meter
Z = -8237869
75 Z = -2514963
08
XDOT = -17447
318659 XDOT = -5359
703214
YDOT = 4772
411424 feet/sec YDOT = 1394
929045 meter/sec
ZDOT = 17485
408155 ZDOT = 5303
616640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6428352
71 X = 1959361
91
Y = -19612421
81 feet Y = -5977866
17 meter
Z = -8254659
52 Z = -2516020
22
XDOT = 16708
520500 XDOT = 5092
757048
YDOT = -1831
820840 feet/sec YDOT = -558
338992 meter/sec
ZDOT = 17379
719976 ZDOT = 5297
338649
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 11248
52063552
00016717 00000-0 10270-3 0 9124
2 25544 51
6388 116
4649 0006988 175
9071 184
2143 15
59277874 13456
Satellite: ISS
Catalog Number: 25544
Epoch time: 11248
52063552 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 116
4649 deg
Eccentricity:
0006988
Arg of perigee: 175
9071 deg
Mean anomaly: 184
2143 deg
Mean motion: 15
59277874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 334
Coasting Arc #14 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2011/249/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2973719
52 A = 6774150
43 meter
Y = -6015623
83 meter E =
0016411
Z = -855120
73 I = 51
97993
XDOT = 3941
338461 Wp = 156
82920
YDOT = 2789
929586 meter/sec RA = 110
58675 deg
ZDOT = -5973
854419 TA = 32
40429
MA = 32
30362
Ha = 214
380 n
mi
Hp = 206
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9756297
63 X = 3044920
35
Y = -19736298
67 feet Y = -5981971
79 meter
Z = -2805514
21 Z = -840501
58
XDOT = 12930
900461 XDOT = 3938
867515
YDOT = 9153
312291 feet/sec YDOT = 2833
990159 meter/sec
ZDOT = -19599
259905 ZDOT = -5954
713684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13030121
47 X = -3971581
02
Y = 17755413
25 feet Y = 5411849
96 meter
Z = -2745719
06 Z = -836895
17
XDOT = -9980
240592 XDOT = -3041
977332
YDOT = -10315
324786 feet/sec YDOT = -3144
110995 meter/sec
ZDOT = -19521
413669 ZDOT = -5950
126886
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 11249
54605949
00016717 00000-0 10270-3 0 9130
2 25544 51
6387 111
3131 0007168 179
8988 180
2170 15
59262614 13616
Satellite: ISS
Catalog Number: 25544
Epoch time: 11249
54605949 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 111
3131 deg
Eccentricity:
0007168
Arg of perigee: 179
8988 deg
Mean anomaly: 180
2170 deg
Mean motion: 15
59262614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 320
Coasting Arc #15 (Orbit 1376)
---------------------------------------
Vector Time (GMT): 2011/250/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157629
67 A = 6768118
44 meter
Y = 3702055
26 meter E =
0013746
Z = 3846816
07 I = 51
96898
XDOT = -1656
392655 Wp = 127
90234
YDOT = -6221
718029 meter/sec RA = 105
60122 deg
ZDOT = 4178
998943 TA = 278
29479
MA = 278
45063
Ha = 214
136 n
mi
Hp = 206
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13640517
29 X = -4217404
61
Y = 12145850
58 feet Y = 3655227
98 meter
Z = 12620787
63 Z = 3826473
35
XDOT = -5434
359103 XDOT = -1606
997573
YDOT = -20412
460726 feet/sec YDOT = -6239
964533 meter/sec
ZDOT = 13710
626452 ZDOT = 4171
072458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15438048
48 X = 4705517
18
Y = -9866141
47 feet Y = -3007199
92 meter
Z = 12537766
55 Z = 3821511
25
XDOT = 1556
750622 XDOT = 474
497589
YDOT = 19895
582493 feet/sec YDOT = 6064
173544 meter/sec
ZDOT = 13678
601783 ZDOT = 4169
237824
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 11250
57147236
00016717 00000-0 10270-3 0 9146
2 25544 51
6380 106
1598 0006897 184
0166 176
0936 15
59296892 13777
Satellite: ISS
Catalog Number: 25544
Epoch time: 11250
57147236 = yrday
fracday
Element set: 914
Inclination: 51
6380 deg
RA of node: 106
1598 deg
Eccentricity:
0006897
Arg of perigee: 184
0166 deg
Mean anomaly: 176
0936 deg
Mean motion: 15
59296892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1377
Checksum: 337
Coasting Arc #16 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2011/251/12:22:27
005
Vector Time (MET): N/A
Weight (LBS) : 885911
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213880
37 A = 6762386
91 meter
Y = 28366
06 meter E =
0014809
Z = -5300121
70 I = 51
95600
XDOT = -884
145486 Wp = 112
22561
YDOT = 7586
898968 meter/sec RA = 100
57868 deg
ZDOT = -669
279812 TA = 151
45147
MA = 151
37029
Ha = 213
988 n
mi
Hp = 206
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13825066
84 X = 4238996
58
Y = 93064
50 feet Y = 75628
44 meter
Z = -17388850
73 Z = -5279590
03
XDOT = -2900
739784 XDOT = -965
666779
YDOT = 24891
400813 feet/sec YDOT = 7576
556071 meter/sec
ZDOT = -2195
799907 ZDOT = -673
773273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13782673
33 X = -4200958
83
Y = -2020096
73 feet Y = -615725
48 meter
Z = -17305212
77 Z = -5274628
85
XDOT = 6158
870587 XDOT = 1877
223755
YDOT = -23246
674725 feet/sec YDOT = -7085
586456 meter/sec
ZDOT = -2214
430488 ZDOT = -674
958413
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 11251
53278676
00016717 00000-0 10270-3 0 9157
2 25544 51
6368 101
3285 0006974 187
5599 172
5452 15
59335061 13920
Satellite: ISS
Catalog Number: 25544
Epoch time: 11251
53278676 = yrday
fracday
Element set: 915
Inclination: 51
6368 deg
RA of node: 101
3285 deg
Eccentricity:
0006974
Arg of perigee: 187
5599 deg
Mean anomaly: 172
5452 deg
Mean motion: 15
59335061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 331
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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