[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 8th 2011
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) : 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 1375)
---------------------------------------
Vector Time (GMT): 2011/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1629079
32 A = 6769788
71 meter
Y = 6568412
96 meter E =
0011457
Z = -249578
74 I = 51
99013
XDOT = -4639
413817 Wp = 104
09196
YDOT = -929
925780 meter/sec RA = 105
58097 deg
ZDOT = 6037
518683 TA = 253
22704
MA = 253
35277
Ha = 213
753 n
mi
Hp = 201
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5344748
42 X = -1701195
13
Y = 21549911
30 feet Y = 6549792
38 meter
Z = -818827
90 Z = -257668
02
XDOT = -15221
173941 XDOT = -4657
999095
YDOT = -3050
937598 feet/sec YDOT = -981
910302 meter/sec
ZDOT = 19808
132161 ZDOT = 6014
935657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10589973
80 X = 3227824
01
Y = -19513122
40 feet Y = -5947599
71 meter
Z = -852056
87 Z = -259706
93
XDOT = 12656
476680 XDOT = 3857
694092
YDOT = 6039
319941 feet/sec YDOT = 1840
784718 meter/sec
ZDOT = 19716
181395 ZDOT = 6009
492089
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
50050267
00016717 00000-0 10270-3 0 9001
2 25544 51
6382 106
4464 0011664 164
3480 195
8039 15
60861399 13766
Satellite: ISS
Catalog Number: 25544
Epoch time: 11250
50050267 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 106
4464 deg
Eccentricity:
0011664
Arg of perigee: 164
3480 deg
Mean anomaly: 195
8039 deg
Mean motion: 15
60861399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 301
Coasting Arc #2 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2011/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3601509
56 A = 6764781
92 meter
Y = -4562955
05 meter E =
0013400
Z = -3454714
95 I = 51
97945
XDOT = 2628
612722 Wp = 147
32609
YDOT = 5550
465491 meter/sec RA = 100
59526 deg
ZDOT = -4609
961732 TA = 73
10341
MA = 72
95653
Ha = 213
699 n
mi
Hp = 202
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11815976
24 X = 3669047
83
Y = -14970324
97 feet Y = -4522303
30 meter
Z = -11334366
65 Z = -3437054
87
XDOT = 8624
057488 XDOT = 2588
744936
YDOT = 18210
188620 feet/sec YDOT = 5579
637124 meter/sec
ZDOT = -15124
546365 ZDOT = -4597
289245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15068437
94 X = -4592859
89
Y = 11760108
70 feet Y = 3584481
13 meter
Z = -11262229
47 Z = -3432727
54
XDOT = -3335
859937 XDOT = -1016
770109
YDOT = -18648
401441 feet/sec YDOT = -5684
032759 meter/sec
ZDOT = -15073
161211 ZDOT = -4594
299537
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
52489230
00016717 00000-0 10270-3 0 9011
2 25544 51
6373 101
2870 0011624 168
6414 191
5006 15
60861105 13920
Satellite: ISS
Catalog Number: 25544
Epoch time: 11251
52489230 = yrday
fracday
Element set: 901
Inclination: 51
6373 deg
RA of node: 101
2870 deg
Eccentricity:
0011624
Arg of perigee: 168
6414 deg
Mean anomaly: 191
5006 deg
Mean motion: 15
60861105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 275
Coasting Arc #3 (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 = -4192410
45 A = 6757982
63 meter
Y = 419210
61 meter E =
0013671
Z = 5281356
37 I = 51
96108
XDOT = 171
143579 Wp = 161
26048
YDOT = -7645
498947 meter/sec RA = 95
56288 deg
ZDOT = 729
571754 TA = 281
73713
MA = 281
89048
Ha = 213
632 n
mi
Hp = 202
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13754627
45 X = -4222441
99
Y = 1375362
90 feet Y = 372160
95 meter
Z = 17327284
69 Z = 5260917
02
XDOT = 561
494683 XDOT = 253
080257
YDOT = -25083
657962 feet/sec YDOT = -7643
126933 meter/sec
ZDOT = 2393
608116 ZDOT = 730
602683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13825219
65 X = 4213926
95
Y = 1680463
98 feet Y = 512205
42 meter
Z = 17244000
02 Z = 5255971
21
XDOT = -5883
668517 XDOT = -1793
342164
YDOT = 23351
834627 feet/sec YDOT = 7117
639194 meter/sec
ZDOT = 2398
140743 ZDOT = 730
953298
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
54926935
00016717 00000-0 10270-3 0 9023
2 25544 51
6371 96
1272 0011608 172
0140 188
1203 15
60865028 14080
Satellite: ISS
Catalog Number: 25544
Epoch time: 11252
54926935 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 96
1272 deg
Eccentricity:
0011608
Arg of perigee: 172
0140 deg
Mean anomaly: 188
1203 deg
Mean motion: 15
60865028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 287
Coasting Arc #4 (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 = 3332117
57 A = 6761836
14 meter
Y = 4025980
50 meter E =
0016947
Z = -4307411
81 I = 51
97497
XDOT = -2839
405327 Wp = 148
99359
YDOT = 6166
984557 meter/sec RA = 90
51758 deg
ZDOT = 3559
615054 TA = 157
16345
MA = 157
08799
Ha = 213
321 n
mi
Hp = 202
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10932144
27 X = 3307774
94
Y = 13208597
45 feet Y = 4063105
81 meter
Z = -14131928
52 Z = -4291284
10
XDOT = -9315
634276 XDOT = -2925
446434
YDOT = 20232
888968 feet/sec YDOT = 6134
751811 meter/sec
ZDOT = 11678
527081 ZDOT = 3545
611915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8132150
36 X = -2478679
43
Y = -15155680
46 feet Y = -4619451
41 meter
Z = -14066403
55 Z = -4287439
80
XDOT = 12162
368822 XDOT = 3707
090017
YDOT = -17336
266531 feet/sec YDOT = -5284
094039 meter/sec
ZDOT = 11621
206904 ZDOT = 3542
143864
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
50960861
00016717 00000-0 10270-3 0 9037
2 25544 51
6358 91
2885 0011615 175
9801 184
1450 15
60916204 14235
Satellite: ISS
Catalog Number: 25544
Epoch time: 11253
50960861 = yrday
fracday
Element set: 903
Inclination: 51
6358 deg
RA of node: 91
2885 deg
Eccentricity:
0011615
Arg of perigee: 175
9801 deg
Mean anomaly: 184
1450 deg
Mean motion: 15
60916204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 296
Coasting Arc #5 (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 = -1294408
93 A = 6769118
08 meter
Y = -6554549
83 meter E =
0022121
Z = 996333
02 I = 51
99934
XDOT = 4522
884807 Wp = 149
47603
YDOT = -1803
770445 meter/sec RA = 85
51973 deg
ZDOT = -5951
544408 TA = 19
73596
MA = 19
65049
Ha = 213
064 n
mi
Hp = 202
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4246748
47 X = -1225858
42
Y = -21504428
57 feet Y = -6568641
32 meter
Z = 3268809
13 Z = 990212
02
XDOT = 14838
860914 XDOT = 4571
629965
YDOT = -5917
882038 feet/sec YDOT = -1752
920822 meter/sec
ZDOT = -19526
064332 ZDOT = -5929
453912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 226350
01 X = 68991
48
Y = 21922239
28 feet Y = 6681898
53 meter
Z = 3244167
77 Z = 988822
34
XDOT = -14192
842100 XDOT = -4325
978272
YDOT = 3041
794184 feet/sec YDOT = 927
138867 meter/sec
ZDOT = -19435
987951 ZDOT = -5924
089127
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
53395732
00016717 00000-0 10270-3 0 9041
2 25544 51
6361 86
1292 0011390 180
1696 179
9458 15
60966057 14392
Satellite: ISS
Catalog Number: 25544
Epoch time: 11254
53395732 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 86
1292 deg
Eccentricity:
0011390
Arg of perigee: 180
1696 deg
Mean anomaly: 179
9458 deg
Mean motion: 15
60966057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 327
Coasting Arc #6 (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 = -1240949
78 A = 6766100
43 meter
Y = 6019380
28 meter E =
0015577
Z = 2831807
11 I = 51
98463
XDOT = -4618
058558 Wp = 126
96358
YDOT = -3373
103794 meter/sec RA = 80
53739 deg
ZDOT = 5117
793342 TA = 265
12047
MA = 265
29834
Ha = 212
987 n
mi
Hp = 202
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4071357
55 X = -1321923
75
Y = 19748622
95 feet Y = 6005050
77 meter
Z = 9290705
74 Z = 2825581
29
XDOT = -15151
110754 XDOT = -4604
857758
YDOT = -11066
613498 feet/sec YDOT = -3424
671391 meter/sec
ZDOT = 16790
660572 ZDOT = 5095
391411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7377562
81 X = 2248681
14
Y = -18778482
69 feet Y = -5723681
52 meter
Z = 9265064
97 Z = 2823991
80
XDOT = 11813
243044 XDOT = 3600
676480
YDOT = 12926
661446 feet/sec YDOT = 3940
046409 meter/sec
ZDOT = 16699
553063 ZDOT = 5090
023774
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
55829276
00016717 00000-0 10270-3 0 9050
2 25544 51
6348 80
9681 0011658 184
1733 175
9327 15
60973889 14554
Satellite: ISS
Catalog Number: 25544
Epoch time: 11255
55829276 = yrday
fracday
Element set: 905
Inclination: 51
6348 deg
RA of node: 80
9681 deg
Eccentricity:
0011658
Arg of perigee: 184
1733 deg
Mean anomaly: 175
9327 deg
Mean motion: 15
60973889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 348
Coasting Arc #7 (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 = 3487490
56 A = 6758215
88 meter
Y = -2642484
56 meter E =
0015017
Z = -5159065
02 I = 51
95192
XDOT = 3004
538812 Wp = 125
73611
YDOT = 6895
777850 meter/sec RA = 75
51192 deg
ZDOT = -1512
598718 TA = 129
83203
MA = 129
69979
Ha = 212
917 n
mi
Hp = 202
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11441898
16 X = 3541841
87
Y = -8669568
76 feet Y = -2603181
97 meter
Z = -16926066
32 Z = -5141990
53
XDOT = 9857
410800 XDOT = 2934
553477
YDOT = 22623
943079 feet/sec YDOT = 6928
984967 meter/sec
ZDOT = -4962
594220 ZDOT = -1498
173464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12717463
46 X = -3876282
86
Y = 6833641
79 feet Y = 2082894
02 meter
Z = -16856382
77 Z = -5137825
47
XDOT = -5870
147058 XDOT = -1789
220823
YDOT = -22926
990527 feet/sec YDOT = -6988
146713 meter/sec
ZDOT = -4904
155315 ZDOT = -1494
786540
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
51859559
00016717 00000-0 10270-3 0 9065
2 25544 51
6346 76
1301 0011578 186
7194 173
3809 15
60977556 14707
Satellite: ISS
Catalog Number: 25544
Epoch time: 11256
51859559 = yrday
fracday
Element set: 906
Inclination: 51
6346 deg
RA of node: 76
1301 deg
Eccentricity:
0011578
Arg of perigee: 186
7194 deg
Mean anomaly: 173
3809 deg
Mean motion: 15
60977556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1470
Checksum: 336
Coasting Arc #8 (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 = -4526109
99 A = 6760257
15 meter
Y = -1827209
42 meter E =
0009375
Z = 4669140
21 I = 51
95015
XDOT = -115
389677 Wp = 146
33887
YDOT = -7115
460766 meter/sec RA = 70
46305 deg
ZDOT = -2901
244828 TA = 332
28252
MA = 332
33246
Ha = 212
835 n
mi
Hp = 203
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14849442
22 X = -4528023
24
Y = -5994781
58 feet Y = -1877833
36 meter
Z = 15318701
48 Z = 4647147
90
XDOT = -378
575056 XDOT = -21
720889
YDOT = -23344
687554 feet/sec YDOT = -7116
227699 meter/sec
ZDOT = -9518
519777 ZDOT = -2901
577122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14007379
36 X = 4269449
23
Y = 7935410
65 feet Y = 2418713
17 meter
Z = 15229200
13 Z = 4641860
20
XDOT = -2220
113097 XDOT = -676
690472
YDOT = 22157
553846 feet/sec YDOT = 6753
622412 meter/sec
ZDOT = -9519
525182 ZDOT = -2901
551275
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
54290321
00016717 00000-0 10270-3 0 9076
2 25544 51
6347 70
9697 0011584 191
0842 169
0061 15
60975818 14862
Satellite: ISS
Catalog Number: 25544
Epoch time: 11257
54290321 = yrday
fracday
Element set: 907
Inclination: 51
6347 deg
RA of node: 70
9697 deg
Eccentricity:
0011584
Arg of perigee: 191
0842 deg
Mean anomaly: 169
0061 deg
Mean motion: 15
60975818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 322
Coasting Arc #9 (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 = 3847708
90 A = 6768232
23 meter
Y = 5323577
61 meter E =
0005373
Z = -1647035
77 I = 51
96680
XDOT = -3104
738721 Wp = 157
78824
YDOT = 4021
403762 meter/sec RA = 65
45310 deg
ZDOT = 5746
190621 TA = 184
22558
MA = 184
23012
Ha = 212
517 n
mi
Hp = 203
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12623716
87 X = 3795894
67
Y = 17465805
82 feet Y = 5366315
18 meter
Z = -5403660
67 Z = -1628469
90
XDOT = -10186
150660 XDOT = -3177
390160
YDOT = 13193
581897 feet/sec YDOT = 3986
279007 meter/sec
ZDOT = 18852
331435 ZDOT = 5730
930889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10535995
84 X = -3211371
53
Y = -18820578
31 feet Y = -5736512
27 meter
Z = -5328299
24 Z = -1624065
61
XDOT = 10393
666042 XDOT = 3167
989410
YDOT = -11136
960300 feet/sec YDOT = -3394
545499 meter/sec
ZDOT = 18789
964863 ZDOT = 5727
181290
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
50317815
00016717 00000-0 10270-3 0 9082
2 25544 51
6353 66
1312 0011602 194
1195 165
9638 15
61021076 15018
Satellite: ISS
Catalog Number: 25544
Epoch time: 11258
50317815 = yrday
fracday
Element set: 908
Inclination: 51
6353 deg
RA of node: 66
1312 deg
Eccentricity:
0011602
Arg of perigee: 194
1195 deg
Mean anomaly: 165
9638 deg
Mean motion: 15
61021076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1501
Checksum: 284
Coasting Arc #10 (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 = -1441411
63 A = 6766976
43 meter
Y = -6190545
86 meter E =
0014984
Z = -2295711
37 I = 51
94997
XDOT = 5350
986536 Wp = 177
57351
YDOT = 773
550707 meter/sec RA = 60
47174 deg
ZDOT = -5461
549101 TA = 27
98181
MA = 27
90132
Ha = 212
240 n
mi
Hp = 203
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4729040
80 X = -1360928
39
Y = -20310189
84 feet Y = -6206214
79 meter
Z = -7531861
45 Z = -2302517
78
XDOT = 17555
730106 XDOT = 5368
470216
YDOT = 2537
896020 feet/sec YDOT = 833
486019 meter/sec
ZDOT = -17918
468180 ZDOT = -5435
511456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2642457
82 X = 805421
14
Y = 20675384
50 feet Y = 6301857
20 meter
Z = -7559263
69 Z = -2304063
57
XDOT = -15816
286919 XDOT = -4820
804253
YDOT = -4472
108704 feet/sec YDOT = -1363
098733 meter/sec
ZDOT = -17812
441732 ZDOT = -5429
232240
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
52745651
00016717 00000-0 10270-3 0 9099
2 25544 51
6358 60
9712 0011378 198
0993 161
9759 15
61061742 15179
Satellite: ISS
Catalog Number: 25544
Epoch time: 11259
52745651 = yrday
fracday
Element set: 909
Inclination: 51
6358 deg
RA of node: 60
9712 deg
Eccentricity:
0011378
Arg of perigee: 198
0993 deg
Mean anomaly: 161
9759 deg
Mean motion: 15
61061742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 332
Coasting Arc #11 (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 = -1818708
31 A = 6758749
13 meter
Y = 4217645
16 meter E =
0014078
Z = 4962049
99 I = 51
90649
XDOT = -5465
669915 Wp = 175
84075
YDOT = -4931
968221 meter/sec RA = 55
45099 deg
ZDOT = 2174
692375 TA = 252
98392
MA = 253
13823
Ha = 212
106 n
mi
Hp = 203
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5966890
78 X = -1889840
57
Y = 13837418
49 feet Y = 4196909
86 meter
Z = 16279691
56 Z = 4953041
58
XDOT = -17931
987911 XDOT = -5420
677787
YDOT = -16180
998101 feet/sec YDOT = -4992
836974 meter/sec
ZDOT = 7134
817504 ZDOT = 2148
249603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7182190
90 X = 2189131
79
Y = -13292665
33 feet Y = -4051604
39 meter
Z = 16242766
88 Z = 4950795
34
XDOT = 15614
076188 XDOT = 4759
170422
YDOT = 17080
064191 feet/sec YDOT = 5206
003565 meter/sec
ZDOT = 7027
368020 ZDOT = 2141
941772
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
55172035
00016717 00000-0 10270-3 0 9106
2 25544 51
6358 55
8106 0011482 202
2923 157
7735 15
61069649 15335
Satellite: ISS
Catalog Number: 25544
Epoch time: 11260
55172035 = yrday
fracday
Element set: 910
Inclination: 51
6358 deg
RA of node: 55
8106 deg
Eccentricity:
0011482
Arg of perigee: 202
2923 deg
Mean anomaly: 157
7735 deg
Mean motion: 15
61069649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 295
Coasting Arc #12 (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 = 4631148
63 A = 6758996
54 meter
Y = -448145
73 meter E =
0015418
Z = -4913374
48 I = 51
89052
XDOT = 3112
449572 Wp = 154
08977
YDOT = 6615
897674 meter/sec RA = 50
39716 deg
ZDOT = 2319
447268 TA = 138
56933
MA = 138
45232
Ha = 211
965 n
mi
Hp = 203
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15194057
18 X = 4659684
10
Y = -1470294
39 feet Y = -396198
11 meter
Z = -16119995
03 Z = -4890806
90
XDOT = 10211
448728 XDOT = 3026
970462
YDOT = 21705
701029 feet/sec YDOT = 6650
225174 meter/sec
ZDOT = 7609
735132 ZDOT = 2334
359645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15354269
68 X = -4679981
40
Y = 473004
07 feet Y = 144171
64 meter
Z = -16028039
45 Z = -4885346
42
XDOT = -8697
001630 XDOT = -2650
846097
YDOT = -21201
854262 feet/sec YDOT = -6462
325179 meter/sec
ZDOT = 7670
112890 ZDOT = 2337
850409
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
51195369
00016717 00000-0 10270-3 0 9119
2 25544 51
6370 50
9734 0011469 205
2107 154
8490 15
61085247 15488
Satellite: ISS
Catalog Number: 25544
Epoch time: 11261
51195369 = yrday
fracday
Element set: 911
Inclination: 51
6370 deg
RA of node: 50
9734 deg
Eccentricity:
0011469
Arg of perigee: 205
2107 deg
Mean anomaly: 154
8490 deg
Mean motion: 15
61085247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 301
Coasting Arc #13 (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 = -5539096
31 A = 6767245
56 meter
Y = -3220642
23 meter E =
0016593
Z = 2142406
02 I = 51
89762
XDOT = 913
203797 Wp = 152
80641
YDOT = -5254
901013 meter/sec RA = 45
37598 deg
ZDOT = -5536
152482 TA = 3
42890
MA = 3
41754
Ha = 211
803 n
mi
Hp = 204
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18172888
15 X = -5513078
23
Y = -10566411
52 feet Y = -3282438
23 meter
Z = 7028891
14 Z = 2115560
34
XDOT = 2996
075451 XDOT = 998
790984
YDOT = -17240
488888 feet/sec YDOT = -5244
210711 meter/sec
ZDOT = -18163
229928 ZDOT = -5531
507997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17687990
28 X = 5391299
44
Y = 11426318
18 feet Y = 3482741
78 meter
Z = 6919716
72 Z = 2109129
66
XDOT = -3094
470001 XDOT = -943
194456
YDOT = 15783
015294 feet/sec YDOT = 4810
663062 meter/sec
ZDOT = -18144
009933 ZDOT = -5530
294228
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
53618686
00016717 00000-0 10270-3 0 9125
2 25544 51
6366 45
8128 0011455 209
4504 150
6008 15
61097536 15646
Satellite: ISS
Catalog Number: 25544
Epoch time: 11262
53618686 = yrday
fracday
Element set: 912
Inclination: 51
6366 deg
RA of node: 45
8128 deg
Eccentricity:
0011455
Arg of perigee: 209
4504 deg
Mean anomaly: 150
6008 deg
Mean motion: 15
61097536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 305
Coasting Arc #14 (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 = 3923060
85 A = 6767508
87 meter
Y = 5208178
98 meter E =
0007687
Z = 1815694
63 I = 51
87872
XDOT = -4881
841059 Wp = 120
70703
YDOT = 1691
827757 meter/sec RA = 40
38954 deg
ZDOT = 5673
417324 TA = 259
23007
MA = 259
31661
Ha = 211
456 n
mi
Hp = 204
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12870934
54 X = 3855710
08
Y = 17087201
38 feet Y = 5251672
54 meter
Z = 5957003
37 Z = 1834589
06
XDOT = -16016
538907 XDOT = -4927
957032
YDOT = 5550
616002 feet/sec YDOT = 1636
978406 meter/sec
ZDOT = 18613
573898 ZDOT = 5649
589242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12304079
63 X = -3750283
47
Y = -17473515
85 feet Y = -5325927
63 meter
Z = 6033669
23 Z = 1839062
38
XDOT = 15017
125713 XDOT = 4577
219917
YDOT = -4156
451303 feet/sec YDOT = -1266
886357 meter/sec
ZDOT = 18516
408591 ZDOT = 5643
801339
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
56040276
00016717 00000-0 10270-3 0 9134
2 25544 51
6380 40
6525 0011469 213
1441 146
8998 15
61163914 15800
Satellite: ISS
Catalog Number: 25544
Epoch time: 11263
56040276 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 40
6525 deg
Eccentricity:
0011469
Arg of perigee: 213
1441 deg
Mean anomaly: 146
8998 deg
Mean motion: 15
61163914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 298
Coasting Arc #15 (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 = -246835
49 A = 6759201
46 meter
Y = -4778775
86 meter E =
0006666
Z = -4774992
95 I = 51
82721
XDOT = 6831
294866 Wp = 143
15680
YDOT = 2291
287148 meter/sec RA = 35
37005 deg
ZDOT = -2653
353650 TA = 100
80465
MA = 100
72961
Ha = 211
219 n
mi
Hp = 204
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -809827
72 X = -170183
94
Y = -15678398
48 feet Y = -4781107
75 meter
Z = -15665987
36 Z = -4776005
67
XDOT = 22412
384731 XDOT = 6818
055005
YDOT = 7517
346286 feet/sec YDOT = 2367
604720 meter/sec
ZDOT = -8705
228511 ZDOT = -2620
199566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 503527
79 X = 153475
27
Y = 15687383
57 feet Y = 4781514
51 meter
Z = -15669831
40 Z = -4776164
61
XDOT = -21216
944650 XDOT = -6466
924729
YDOT = -7856
379243 feet/sec YDOT = -2394
624393 meter/sec
ZDOT = -8570
305023 ZDOT = -2612
228971
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
52059250
00016717 00000-0 10270-3 0 9144
2 25544 51
6382 35
8152 0011282 217
4959 142
5411 15
61159870 15953
Satellite: ISS
Catalog Number: 25544
Epoch time: 11264
52059250 = yrday
fracday
Element set: 914
Inclination: 51
6382 deg
RA of node: 35
8152 deg
Eccentricity:
0011282
Arg of perigee: 217
4959 deg
Mean anomaly: 142
5411 deg
Mean motion: 15
61159870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 301
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