[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 10th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11388 22 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 1407)
---------------------------------------
Vector Time (GMT): 2011/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4192375
65 A = 6757984
39 meter
Y = 419936
94 meter E =
0013664
Z = 5281385
94 I = 51
96203
XDOT = 170
722256 Wp = 161
53239
YDOT = -7645
389649 meter/sec RA = 95
56375 deg
ZDOT = 730
267962 TA = 281
45858
MA = 281
61201
Ha = 213
624 n
mi
Hp = 202
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13754513
28 X = -4222415
46
Y = 1377745
88 feet Y = 372887
62 meter
Z = 17327381
68 Z = 5260946
73
XDOT = 560
112387 XDOT = 252
654361
YDOT = -25083
299373 feet/sec YDOT = -7643
022372 meter/sec
ZDOT = 2395
892263 ZDOT = 731
296833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13825628
69 X = 4214051
62
Y = 1678113
62 feet Y = 511489
03 meter
Z = 17244097
58 Z = 5256000
94
XDOT = -5882
399242 XDOT = -1792
955289
YDOT = 23351
759308 feet/sec YDOT = 7117
616237 meter/sec
ZDOT = 2400
416500 ZDOT = 731
646949
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 11252
54927042
00016717 00000-0 10270-3 0 9001
2 25544 51
6381 96
1282 0011612 172
3349 187
7986 15
60864449 14080
Satellite: ISS
Catalog Number: 25544
Epoch time: 11252
54927042 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 96
1282 deg
Eccentricity:
0011612
Arg of perigee: 172
3349 deg
Mean anomaly: 187
7986 deg
Mean motion: 15
60864449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 315
Coasting Arc #2 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2011/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3332390
95 A = 6761837
84 meter
Y = 4025095
09 meter E =
0016925
Z = -4307984
11 I = 51
97591
XDOT = -2838
805522 Wp = 149
18949
YDOT = 6167
757790 meter/sec RA = 90
51856 deg
ZDOT = 3558
823536 TA = 156
95782
MA = 156
88182
Ha = 213
315 n
mi
Hp = 202
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10933041
16 X = 3308060
97
Y = 13205692
56 feet Y = 4062223
52 meter
Z = -14133806
13 Z = -4291855
04
XDOT = -9313
666412 XDOT = -2924
851475
YDOT = 20235
425820 feet/sec YDOT = 6135
531724 meter/sec
ZDOT = 11675
930235 ZDOT = 3544
823299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8133624
86 X = -2479128
86
Y = -15153017
83 feet Y = -4618639
83 meter
Z = -14068275
59 Z = -4288010
40
XDOT = 12161
130882 XDOT = 3706
712693
YDOT = -17339
043152 feet/sec YDOT = -5284
940353 meter/sec
ZDOT = 11618
621846 ZDOT = 3541
355939
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 11253
50961033
00016717 00000-0 10270-3 0 9017
2 25544 51
6367 91
2896 0011620 176
2971 183
8273 15
60914874 14235
Satellite: ISS
Catalog Number: 25544
Epoch time: 11253
50961033 = yrday
fracday
Element set: 901
Inclination: 51
6367 deg
RA of node: 91
2896 deg
Eccentricity:
0011620
Arg of perigee: 176
2971 deg
Mean anomaly: 183
8273 deg
Mean motion: 15
60914874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 306
Coasting Arc #3 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2011/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1295490
44 A = 6769122
78 meter
Y = -6554098
69 meter E =
0022093
Z = 997952
21 I = 52
00028
XDOT = 4522
373500 Wp = 149
61355
YDOT = -1805
916968 meter/sec RA = 85
52081 deg
ZDOT = -5951
272798 TA = 19
58085
MA = 19
49613
Ha = 213
059 n
mi
Hp = 202
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4250296
70 X = -1226952
75
Y = -21502948
47 feet Y = -6568202
35 meter
Z = 3274121
42 Z = 991825
92
XDOT = 14837
183398 XDOT = 4571
141380
YDOT = -5924
924435 feet/sec YDOT = -1755
072935 meter/sec
ZDOT = -19525
173221 ZDOT = -5929
184729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 230141
83 X = 70147
23
Y = 21921444
76 feet Y = 6681656
36 meter
Z = 3249458
51 Z = 990434
95
XDOT = -14192
545136 XDOT = -4325
887757
YDOT = 3048
749610 feet/sec YDOT = 929
258881 meter/sec
ZDOT = -19435
106635 ZDOT = -5923
820502
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 11254
53396023
00016717 00000-0 10270-3 0 9023
2 25544 51
6370 86
1304 0011396 180
4884 179
6263 15
60963949 14392
Satellite: ISS
Catalog Number: 25544
Epoch time: 11254
53396023 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 86
1304 deg
Eccentricity:
0011396
Arg of perigee: 180
4884 deg
Mean anomaly: 179
6263 deg
Mean motion: 15
60963949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 319
Coasting Arc #4 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2011/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1239215
11 A = 6766113
61 meter
Y = 6020704
75 meter E =
0015525
Z = 2829840
11 I = 51
98559
XDOT = -4618
521711 Wp = 127
08695
YDOT = -3370
112146 meter/sec RA = 80
53860 deg
ZDOT = 5119
293452 TA = 264
97149
MA = 265
14873
Ha = 212
984 n
mi
Hp = 202
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4065666
37 X = -1320194
46
Y = 19752968
32 feet Y = 6006394
61 meter
Z = 9284252
32 Z = 2823622
70
XDOT = -15152
630285 XDOT = -4605
361617
YDOT = -11056
798379 feet/sec YDOT = -3421
685149 meter/sec
ZDOT = 16795
582193 ZDOT = 5096
889172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7372641
76 X = 2247181
21
Y = -18783726
30 feet Y = -5725279
78 meter
Z = 9258645
76 Z = 2822035
23
XDOT = 11816
032339 XDOT = 3601
526657
YDOT = 12917
603205 feet/sec YDOT = 3937
285457 meter/sec
ZDOT = 16704
464973 ZDOT = 5091
520924
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 11255
55829741
00016717 00000-0 10270-3 0 9035
2 25544 51
6357 80
9694 0011666 184
4796 175
6258 15
60970959 14554
Satellite: ISS
Catalog Number: 25544
Epoch time: 11255
55829741 = yrday
fracday
Element set: 903
Inclination: 51
6357 deg
RA of node: 80
9694 deg
Eccentricity:
0011666
Arg of perigee: 184
4796 deg
Mean anomaly: 175
6258 deg
Mean motion: 15
60970959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 353
Coasting Arc #5 (Orbit 1469)
---------------------------------------
Vector Time (GMT): 2011/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3485663
60 A = 6758230
18 meter
Y = -2646478
09 meter E =
0014958
Z = -5158206
83 I = 51
95287
XDOT = 3007
032530 Wp = 125
87163
YDOT = 6893
870778 meter/sec RA = 75
51329 deg
ZDOT = -1516
573224 TA = 129
65777
MA = 129
52572
Ha = 212
915 n
mi
Hp = 202
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11435904
20 X = 3540055
54
Y = -8682670
90 feet Y = -2607195
71 meter
Z = -16923250
74 Z = -5141141
12
XDOT = 9865
592290 XDOT = 2937
087643
YDOT = 22617
686281 feet/sec YDOT = 6927
106007 meter/sec
ZDOT = -4975
633937 ZDOT = -1502
135757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12713493
65 X = -3875072
86
Y = 6847499
40 feet Y = 2087117
82 meter
Z = -16853602
75 Z = -5136978
12
XDOT = -5878
244393 XDOT = -1791
688891
YDOT = -22922
337449 feet/sec YDOT = -6986
728454 meter/sec
ZDOT = -4917
145185 ZDOT = -1498
745853
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 11256
51860238
00016717 00000-0 10270-3 0 9049
2 25544 51
6355 76
1315 0011585 187
0237 173
0758 15
60973840 14704
Satellite: ISS
Catalog Number: 25544
Epoch time: 11256
51860238 = yrday
fracday
Element set: 904
Inclination: 51
6355 deg
RA of node: 76
1315 deg
Eccentricity:
0011585
Arg of perigee: 187
0237 deg
Mean anomaly: 173
0758 deg
Mean motion: 15
60973840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1470
Checksum: 307
Coasting Arc #6 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2011/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4525927
93 A = 6760260
67 meter
Y = -1821434
93 meter E =
0009328
Z = 4671649
34 I = 51
95106
XDOT = -120
108056 Wp = 146
71219
YDOT = -7117
357277 meter/sec RA = 70
46456 deg
ZDOT = -2896
241869 TA = 331
85486
MA = 331
90525
Ha = 212
834 n
mi
Hp = 203
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14848844
90 X = -4527917
95
Y = -5975836
39 feet Y = -1872057
26 meter
Z = 15326933
54 Z = 4649657
73
XDOT = -394
055302 XDOT = -26
442014
YDOT = -23350
909703 feet/sec YDOT = -7118
176988 meter/sec
ZDOT = -9502
105870 ZDOT = -2896
597091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14009366
22 X = 4270054
82
Y = 7916561
59 feet Y = 2412967
97 meter
Z = 15237434
75 Z = 4644370
11
XDOT = -2206
878878 XDOT = -672
656682
YDOT = 22165
654758 feet/sec YDOT = 6756
091570 meter/sec
ZDOT = -9503
204587 ZDOT = -2896
576758
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 11257
54291281
00016717 00000-0 10270-3 0 9050
2 25544 51
6356 70
9712 0011592 191
3830 168
7066 15
60971198 14867
Satellite: ISS
Catalog Number: 25544
Epoch time: 11257
54291281 = yrday
fracday
Element set: 905
Inclination: 51
6356 deg
RA of node: 70
9712 deg
Eccentricity:
0011592
Arg of perigee: 191
3830 deg
Mean anomaly: 168
7066 deg
Mean motion: 15
60971198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 321
Coasting Arc #7 (Orbit 1500)
---------------------------------------
Vector Time (GMT): 2011/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3850953
33 A = 6768239
23 meter
Y = 5319263
32 meter E =
0005357
Z = -1653379
03 I = 51
96771
XDOT = -3099
299161 Wp = 158
52864
YDOT = 4028
843135 meter/sec RA = 65
45467 deg
ZDOT = 5743
921149 TA = 183
41377
MA = 183
41742
Ha = 212
517 n
mi
Hp = 203
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12634361
33 X = 3799217
92
Y = 17451651
31 feet Y = 5362037
61 meter
Z = -5424471
87 Z = -1634797
20
XDOT = -10168
304334 XDOT = -3172
023168
YDOT = 13217
989289 feet/sec YDOT = 3993
778803 meter/sec
ZDOT = 18844
885659 ZDOT = 5728
687665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10548340
75 X = -3215134
26
Y = -18807773
32 feet Y = -5732609
31 meter
Z = -5349045
23 Z = -1630388
99
XDOT = 10379
672966 XDOT = 3163
724320
YDOT = -11162
384556 feet/sec YDOT = -3402
294813 meter/sec
ZDOT = 18782
625636 ZDOT = 5724
944294
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 11258
50319090
00016717 00000-0 10270-3 0 9067
2 25544 51
6362 66
1328 0011611 194
4148 165
6679 15
61015620 15016
Satellite: ISS
Catalog Number: 25544
Epoch time: 11258
50319090 = yrday
fracday
Element set: 906
Inclination: 51
6362 deg
RA of node: 66
1328 deg
Eccentricity:
0011611
Arg of perigee: 194
4148 deg
Mean anomaly: 165
6679 deg
Mean motion: 15
61015620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1501
Checksum: 287
Coasting Arc #8 (Orbit 1516)
---------------------------------------
Vector Time (GMT): 2011/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1449019
99 A = 6767009
94 meter
Y = -6191688
87 meter E =
0015000
Z = -2287821
46 I = 51
95096
XDOT = 5348
190030 Wp = 177
78610
YDOT = 762
193052 meter/sec RA = 60
47346 deg
ZDOT = -5465
912364 TA = 27
67473
MA = 27
59498
Ha = 212
241 n
mi
Hp = 203
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4754002
60 X = -1368561
73
Y = -20313939
86 feet Y = -6207443
02 meter
Z = -7505975
91 Z = -2294664
89
XDOT = 17546
555216 XDOT = 5365
822117
YDOT = 2500
633373 feet/sec YDOT = 822
097922 meter/sec
ZDOT = -17932
783348 ZDOT = -5439
887944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2667078
47 X = 812925
52
Y = 20681610
24 feet Y = 6303754
80 meter
Z = -7533528
90 Z = -2296219
61
XDOT = -15810
491705 XDOT = -4819
037872
YDOT = -4435
922144 feet/sec YDOT = -1352
069069 meter/sec
ZDOT = -17826
810171 ZDOT = -5433
611740
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 11259
52747317
00016717 00000-0 10270-3 0 9078
2 25544 51
6367 60
9730 0011387 198
3968 161
6778 15
61055509 15176
Satellite: ISS
Catalog Number: 25544
Epoch time: 11259
52747317 = yrday
fracday
Element set: 907
Inclination: 51
6367 deg
RA of node: 60
9730 deg
Eccentricity:
0011387
Arg of perigee: 198
3968 deg
Mean anomaly: 161
6778 deg
Mean motion: 15
61055509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 338
Coasting Arc #9 (Orbit 1532)
---------------------------------------
Vector Time (GMT): 2011/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1808880
00 A = 6758785
50 meter
Y = 4226505
69 meter E =
0014074
Z = 4958201
71 I = 51
90749
XDOT = -5469
683308 Wp = 175
96035
YDOT = -4922
271184 meter/sec RA = 55
45299 deg
ZDOT = 2186
320172 TA = 252
74631
MA = 252
90038
Ha = 212
109 n
mi
Hp = 203
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5934645
67 X = -1880093
38
Y = 13866488
47 feet Y = 4205879
84 meter
Z = 16267065
98 Z = 4949240
85
XDOT = -17945
155209 XDOT = -5424
855802
YDOT = -16149
183676 feet/sec YDOT = -4983
185738 meter/sec
ZDOT = 7172
966444 ZDOT = 2159
857502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7152369
86 X = 2180042
33
Y = -13324293
77 feet Y = -4061244
74 meter
Z = 16230334
51 Z = 4947005
96
XDOT = 15627
737474 XDOT = 4763
334382
YDOT = 17051
631799 feet/sec YDOT = 5197
337372 meter/sec
ZDOT = 7065
435375 ZDOT = 2153
544702
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 11260
55174151
00016717 00000-0 10270-3 0 9084
2 25544 51
6367 55
8125 0011495 202
5832 157
4820 15
61062706 15331
Satellite: ISS
Catalog Number: 25544
Epoch time: 11260
55174151 = yrday
fracday
Element set: 908
Inclination: 51
6367 deg
RA of node: 55
8125 deg
Eccentricity:
0011495
Arg of perigee: 202
5832 deg
Mean anomaly: 157
4820 deg
Mean motion: 15
61062706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 289
Coasting Arc #10 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2011/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4624093
70 A = 6758997
52 meter
Y = -462778
60 meter E =
0015393
Z = -4918614
47 I = 51
89138
XDOT = 3125
596455 Wp = 154
11780
YDOT = 6614
693992 meter/sec RA = 50
39934 deg
ZDOT = 2305
283630 TA = 138
39545
MA = 138
27823
Ha = 211
969 n
mi
Hp = 204
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15170911
09 X = 4652818
78
Y = -1518302
49 feet Y = -410908
81 meter
Z = -16137186
58 Z = -4896080
70
XDOT = 10254
581546 XDOT = 3040
198633
YDOT = 21701
751942 feet/sec YDOT = 6649
168963 meter/sec
ZDOT = 7563
266501 ZDOT = 2320
260071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15334400
28 X = -4673925
21
Y = 522410
55 feet Y = 159230
74 meter
Z = -16045367
92 Z = -4890628
14
XDOT = -8736
976113 XDOT = -2663
030319
YDOT = -21202
184945 feet/sec YDOT = -6462
425971 meter/sec
ZDOT = 7623
905304 ZDOT = 2323
766337
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 11261
51197963
00016717 00000-0 10270-3 0 9098
2 25544 51
6379 50
9755 0011481 205
4934 154
5657 15
61077248 15488
Satellite: ISS
Catalog Number: 25544
Epoch time: 11261
51197963 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 50
9755 deg
Eccentricity:
0011481
Arg of perigee: 205
4934 deg
Mean anomaly: 154
5657 deg
Mean motion: 15
61077248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 330
Coasting Arc #11 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2011/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5541463
02 A = 6767244
49 meter
Y = -3206528
35 meter E =
0016516
Z = 2157556
50 I = 51
89846
XDOT = 893
784722 Wp = 152
83261
YDOT = -5266
110367 meter/sec RA = 45
37811 deg
ZDOT = -5528
587517 TA = 3
22464
MA = 3
21400
Ha = 211
810 n
mi
Hp = 204
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18180652
94 X = -5515676
19
Y = -10520106
14 feet Y = -3268352
10 meter
Z = 7078597
45 Z = 2130698
76
XDOT = 2932
364574 XDOT = 979
461948
YDOT = -17277
264985 feet/sec YDOT = -5255
636718 meter/sec
ZDOT = -18138
410490 ZDOT = -5524
037152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17698263
13 X = 5394430
60
Y = 11380449
78 feet Y = 3468761
09 meter
Z = 6969373
09 Z = 2124264
92
XDOT = -3035
789969 XDOT = -925
308783
YDOT = 15822
057311 feet/sec YDOT = 4822
563068 meter/sec
ZDOT = -18119
573257 ZDOT = -5522
845929
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 11262
53621848
00016717 00000-0 10270-3 0 9107
2 25544 51
6375 45
8149 0011468 209
7255 150
3251 15
61088370 15642
Satellite: ISS
Catalog Number: 25544
Epoch time: 11262
53621848 = yrday
fracday
Element set: 910
Inclination: 51
6375 deg
RA of node: 45
8149 deg
Eccentricity:
0011468
Arg of perigee: 209
7255 deg
Mean anomaly: 150
3251 deg
Mean motion: 15
61088370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 303
Coasting Arc #12 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2011/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938691
91 A = 6767566
36 meter
Y = 5202813
77 meter E =
0007583
Z = 1797323
88 I = 51
87975
XDOT = -4865
417753 Wp = 120
54118
YDOT = 1713
306017 meter/sec RA = 40
39181 deg
ZDOT = 5681
044487 TA = 259
18535
MA = 259
27071
Ha = 211
463 n
mi
Hp = 204
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922217
54 X = 3871489
21
Y = 17069598
98 feet Y = 5246482
95 meter
Z = 5896731
88 Z = 1816294
61
XDOT = -15962
656671 XDOT = -4911
812173
YDOT = 5621
082732 feet/sec YDOT = 1658
638765 meter/sec
ZDOT = 18638
597398 ZDOT = 5657
295512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12356241
26 X = -3766182
34
Y = -17457504
60 feet Y = -5321047
40 meter
Z = 5973708
85 Z = 1820786
46
XDOT = 14966
751865 XDOT = 4561
865969
YDOT = -4224
732086 feet/sec YDOT = -1287
698340 meter/sec
ZDOT = 18541
753091 ZDOT = 5651
526342
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 11263
56044067
00016717 00000-0 10270-3 0 9114
2 25544 51
6389 40
6548 0011482 213
4145 146
6288 15
61153874 15807
Satellite: ISS
Catalog Number: 25544
Epoch time: 11263
56044067 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 40
6548 deg
Eccentricity:
0011482
Arg of perigee: 213
4145 deg
Mean anomaly: 146
6288 deg
Mean motion: 15
61153874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 305
Coasting Arc #13 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2011/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -272902
64 A = 6759274
05 meter
Y = -4787477
97 meter E =
0006578
Z = -4764827
19 I = 51
82828
XDOT = 6829
902373 Wp = 143
89088
YDOT = 2267
990951 meter/sec RA = 35
37278 deg
ZDOT = -2677
012200 TA = 99
82053
MA = 99
74626
Ha = 211
227 n
mi
Hp = 204
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -895349
87 X = -196201
23
Y = -15706948
71 feet Y = -4790101
08 meter
Z = -15632635
14 Z = -4765966
43
XDOT = 22407
816185 XDOT = 6817
038047
YDOT = 7440
915195 feet/sec YDOT = 2344
295051 meter/sec
ZDOT = -8782
848426 ZDOT = -2643
863968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 588856
07 X = 179483
33
Y = 15717087
40 feet Y = 4790568
24 meter
Z = -15636994
04 Z = -4766155
78
XDOT = -21211
710858 XDOT = -6465
329469
YDOT = -7786
118245 feet/sec YDOT = -2373
208841 meter/sec
ZDOT = -8647
947397 ZDOT = -2635
894367
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 11264
52063688
00016717 00000-0 10270-3 0 9122
2 25544 51
6391 35
8177 0011298 217
7691 142
2674 15
61148855 15952
Satellite: ISS
Catalog Number: 25544
Epoch time: 11264
52063688 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 35
8177 deg
Eccentricity:
0011298
Arg of perigee: 217
7691 deg
Mean anomaly: 142
2674 deg
Mean motion: 15
61148855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 328
Coasting Arc #14 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2011/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3761963
92 A = 6758118
64 meter
Y = 2419566
70 meter E =
0005978
Z = 5067044
49 I = 51
79917
XDOT = -5603
145729 Wp = 207
44406
YDOT = -4928
243051 meter/sec RA = 30
31222 deg
ZDOT = -1812
728844 TA = 260
00314
MA = 260
07061
Ha = 211
089 n
mi
Hp = 204
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12342401
31 X = -3813355
05
Y = 7938210
97 feet Y = 2377211
07 meter
Z = 16624161
71 Z = 5048644
00
XDOT = -18383
024044 XDOT = -5538
814843
YDOT = -16168
776414 feet/sec YDOT = -4990
541264 meter/sec
ZDOT = -5947
273109 ZDOT = -1839
792247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12412988
13 X = 3783478
78
Y = -7984930
73 feet Y = -2433806
89 meter
Z = 16549061
10 Z = 5044153
82
XDOT = 17824
187079 XDOT = 5432
812222
YDOT = 15195
988144 feet/sec YDOT = 4631
737186 meter/sec
ZDOT = -6057
228120 ZDOT = -1846
243131
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 11265
54483126
00016717 00000-0 10270-3 0 9139
2 25544 51
6395 30
6570 0011171 221
2038 138
8276 15
61144278 16114
Satellite: ISS
Catalog Number: 25544
Epoch time: 11265
54483126 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 30
6570 deg
Eccentricity:
0011171
Arg of perigee: 221
2038 deg
Mean anomaly: 138
8276 deg
Mean motion: 15
61144278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1611
Checksum: 287
Coasting Arc #15 (Orbit 1625)
---------------------------------------
Vector Time (GMT): 2011/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6232350
12 A = 6766238
77 meter
Y = 739886
42 meter E =
0005838
Z = -2531771
63 I = 51
80061
XDOT = 1525
122950 Wp = 222
43131
YDOT = 5334
059001 meter/sec RA = 25
27823 deg
ZDOT = 5301
841764 TA = 109
14135
MA = 109
07814
Ha = 210
712 n
mi
Hp = 205
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20447342
91 X = 6235912
17
Y = 2427448
88 feet Y = 809600
09 meter
Z = -8306337
36 Z = -2501486
47
XDOT = 5003
684218 XDOT = 1439
607877
YDOT = 17500
193572 feet/sec YDOT = 5350
636124 meter/sec
ZDOT = 17394
493977 ZDOT = 5309
042640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20543296
25 X = -6261596
70
Y = -1998219
33 feet Y = -609057
25 meter
Z = -8183011
60 Z = -2494181
94
XDOT = -5409
055802 XDOT = -1648
680208
YDOT = -15896
801143 feet/sec YDOT = -4845
344989 meter/sec
ZDOT = 17423
511170 ZDOT = 5310
686205
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 11266
50499632
00016717 00000-0 10270-3 0 9146
2 25544 51
6401 25
8190 0011148 225
8609 134
1631 15
61183058 16263
Satellite: ISS
Catalog Number: 25544
Epoch time: 11266
50499632 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 25
8190 deg
Eccentricity:
0011148
Arg of perigee: 225
8609 deg
Mean anomaly: 134
1631 deg
Mean motion: 15
61183058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 293
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list