[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 19th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
077/06:07:21
649 -1
4 6
4 6
5
N/A -6
3 -1
0 193
7
000/00:14:43
299 0
2 0
5 187
1
Coasting Arc #1 (Orbit 2627)
---------------------------------------
Vector Time (GMT): 2011/075/06:11:25
979
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3845801
32 A = 6723842
21 meter
Y = 2130908
45 meter E =
0010382
Z = 5080527
95 I = 51
28669
XDOT = -2066
611977 Wp = 60
09165
YDOT = 7274
008330 meter/sec RA = 276
83982 deg
ZDOT = -1479
182568 TA = 44
19239
MA = 44
10950
Ha = 193
610 n
mi
Hp = 183
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12617458
41 X = 3797007
52
Y = 6991169
45 feet Y = 2173642
10 meter
Z = 16668398
80 Z = 5099091
77
XDOT = -6780
223023 XDOT = -2140
612279
YDOT = 23864
856726 feet/sec YDOT = 7250
484350 meter/sec
ZDOT = -4852
961181 ZDOT = -1489
402257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7938836
37 X = -2419757
32
Y = 11939411
54 feet Y = 3639132
64 meter
Z = 16743283
88 Z = 5103352
93
XDOT = -22400
532633 XDOT = -6827
682346
YDOT = -7997
336974 feet/sec YDOT = -2437
588310 meter/sec
ZDOT = -4894
361434 ZDOT = -1491
801365
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 11075
30310204
00016717 00000-0 10270-3 0 9004
2 25544 51
6445 277
3705 0005738 65
0158 295
1600 15
72943313 26285
Satellite: ISS
Catalog Number: 25544
Epoch time: 11075
30310204 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 277
3705 deg
Eccentricity:
0005738
Arg of perigee: 65
0158 deg
Mean anomaly: 295
1600 deg
Mean motion: 15
72943313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2628
Checksum: 283
Coasting Arc #2 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2011/076/06:11:25
979
Vector Time (MET): N/A
Weight (LBS) : 906657
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 967131
71 A = 6734698
02 meter
Y = -6586261
45 meter E =
0019345
Z = 962066
66 I = 51
32070
XDOT = 4686
831982 Wp = 59
05309
YDOT = 1562
898271 meter/sec RA = 271
70976 deg
ZDOT = 5910
098293 TA = 311
50459
MA = 311
67044
Ha = 193
681 n
mi
Hp = 183
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3173004
29 X = 1036035
21
Y = -21608469
31 feet Y = -6575061
03 meter
Z = 3156386
69 Z = 966932
93
XDOT = 15376
745347 XDOT = 4640
297435
YDOT = 5127
618999 feet/sec YDOT = 1615
049688 meter/sec
ZDOT = 19390
086263 ZDOT = 5932
753247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21379432
77 X = 6516451
11
Y = 4448436
92 feet Y = 1355883
57 meter
Z = 3176152
19 Z = 968091
19
XDOT = -5712
863938 XDOT = -1741
280928
YDOT = 13365
294154 feet/sec YDOT = 4073
741658 meter/sec
ZDOT = 19481
501564 ZDOT = 5937
961677
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 11076
31960810
00016717 00000-0 10270-3 0 9011
2 25544 51
6442 272
1583 0005747 68
0754 292
1019 15
72974320 26445
Satellite: ISS
Catalog Number: 25544
Epoch time: 11076
31960810 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 272
1583 deg
Eccentricity:
0005747
Arg of perigee: 68
0754 deg
Mean anomaly: 292
1019 deg
Mean motion: 15
72974320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 300
Coasting Arc #3 (Orbit 2658)
---------------------------------------
Vector Time (GMT): 2011/077/06:11:24
000
Vector Time (MET): N/A
Weight (LBS) : 906161
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4223682
46 A = 6725928
86 meter
Y = -595554
39 meter E =
0016001
Z = -5214236
33 I = 51
28233
XDOT = 145
502988 Wp = 92
19283
YDOT = -7647
252741 meter/sec RA = 266
53939 deg
ZDOT = 756
985654 TA = 185
05083
MA = 185
06699
Ha = 193
644 n
mi
Hp = 186
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13857225
91 X = -4191379
57
Y = -1953918
59 feet Y = -642606
21 meter
Z = -17107074
56 Z = -5234676
07
XDOT = 477
372008 XDOT = 227
327973
YDOT = -25089
411879 feet/sec YDOT = -7645
168034 meter/sec
ZDOT = 2483
548733 ZDOT = 757
892210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2546019
04 X = 776026
60
Y = -13657562
87 feet Y = -4162825
16 meter
Z = -17189568
67 Z = -5239380
53
XDOT = 24050
094094 XDOT = 7330
468680
YDOT = 1358
542594 feet/sec YDOT = 414
083783 meter/sec
ZDOT = 2487
337193 ZDOT = 758
140376
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 11077
27255343
00016717 00000-0 10270-3 0 9026
2 25544 51
6442 267
2697 0001603 55
9284 304
2030 15
72024961 26597
Satellite: ISS
Catalog Number: 25544
Epoch time: 11077
27255343 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 267
2697 deg
Eccentricity:
0001603
Arg of perigee: 55
9284 deg
Mean anomaly: 304
2030 deg
Mean motion: 15
72024961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2659
Checksum: 297
Coasting Arc #4 (Orbit 2658)
---------------------------------------
Vector Time (GMT): 2011/077/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4086339
12 A = 6728016
67 meter
Y = -2091296
31 meter E =
0012615
Z = -4930203
80 I = 51
28669
XDOT = 1226
939146 Wp = 99
87290
YDOT = -7298
047053 meter/sec RA = 266
51648 deg
ZDOT = 2081
154023 TA = 190
41476
MA = 190
44092
Ha = 193
680 n
mi
Hp = 187
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13406624
41 X = -4038700
52
Y = -6861208
35 feet Y = -2136726
49 meter
Z = -16175209
31 Z = -4949938
90
XDOT = 4025
390899 XDOT = 1298
346415
YDOT = -23943
723927 feet/sec YDOT = -7283
927153 meter/sec
ZDOT = 6827
933146 ZDOT = 2087
288753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7239784
44 X = 2206686
30
Y = -13107900
30 feet Y = -3995288
01 meter
Z = -16254833
91 Z = -4954473
38
XDOT = 22863
829725 XDOT = 6968
895300
YDOT = 4139
872622 feet/sec YDOT = 1261
833175 meter/sec
ZDOT = 6852
818966 ZDOT = 2088
739221
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 11077
27255336
00016717 00000-0 10270-3 0 9039
2 25544 51
6443 267
2691 0001243 6
1742 353
9435 15
71731906 26592
Satellite: ISS
Catalog Number: 25544
Epoch time: 11077
27255336 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 267
2691 deg
Eccentricity:
0001243
Arg of perigee: 6
1742 deg
Mean anomaly: 353
9435 deg
Mean motion: 15
71731906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2659
Checksum: 305
Coasting Arc #5 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2011/078/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 75149
68 A = 6737978
98 meter
Y = 6635982
43 meter E =
0008590
Z = -1146602
36 I = 51
32384
XDOT = -4891
138839 Wp = 136
68630
YDOT = -952
240188 meter/sec RA = 261
40166 deg
ZDOT = -5863
817139 TA = 55
90993
MA = 55
82844
Ha = 193
643 n
mi
Hp = 187
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 246554
07 X = 6509
20
Y = 21771595
91 feet Y = 6636438
85 meter
Z = -3761818
77 Z = -1146404
93
XDOT = -16047
043434 XDOT = -4851
642163
YDOT = -3124
147598 feet/sec YDOT = -1006
715841 meter/sec
ZDOT = -19238
245208 ZDOT = -5887
481932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21773102
08 X = -6636441
51
Y = 20648
49 feet Y = 6293
66 meter
Z = -3761124
48 Z = -1146390
74
XDOT = 3307
961231 XDOT = 1008
266583
YDOT = -14307
290195 feet/sec YDOT = -4360
862052 meter/sec
ZDOT = -19333
752688 ZDOT = -5892
927819
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 11078
28983667
00016717 00000-0 10270-3 0 9047
2 25544 51
6446 262
0621 0001202 6
7422 353
3756 15
71762344 26755
Satellite: ISS
Catalog Number: 25544
Epoch time: 11078
28983667 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 262
0621 deg
Eccentricity:
0001202
Arg of perigee: 6
7422 deg
Mean anomaly: 353
3756 deg
Mean motion: 15
71762344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 306
Coasting Arc #6 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2011/079/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4206013
41 A = 6726256
86 meter
Y = -440395
91 meter E =
0003531
Z = 5228399
61 I = 51
29098
XDOT = 1427
482554 Wp = 48
06787
YDOT = 7549
260782 meter/sec RA = 256
24351 deg
ZDOT = -509
910803 TA = 46
81513
MA = 46
78563
Ha = 193
336 n
mi
Hp = 187
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13799256
58 X = 4185226
92
Y = -1444868
47 feet Y = -393477
24 meter
Z = 17153542
03 Z = 5248781
87
XDOT = 4683
341711 XDOT = 1345
436230
YDOT = 24767
915950 feet/sec YDOT = 7564
764943 meter/sec
ZDOT = -1672
935705 ZDOT = -503
176433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1523518
99 X = 464368
59
Y = 13687822
48 feet Y = 4172048
29 meter
Z = 17235821
33 Z = 5253478
34
XDOT = -23742
114941 XDOT = -7236
596634
YDOT = 4725
574994 feet/sec YDOT = 1440
355258 meter/sec
ZDOT = -1645
862295 ZDOT = -501
658828
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 11079
30708596
00016717 00000-0 10270-3 0 9058
2 25544 51
6445 256
8550 0001356 3
6665 356
4506 15
71868777 26913
Satellite: ISS
Catalog Number: 25544
Epoch time: 11079
30708596 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 256
8550 deg
Eccentricity:
0001356
Arg of perigee: 3
6665 deg
Mean anomaly: 356
4506 deg
Mean motion: 15
71868777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 335
Coasting Arc #7 (Orbit 2705)
---------------------------------------
Vector Time (GMT): 2011/080/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2366248
54 A = 6738185
67 meter
Y = -6297217
82 meter E =
0012937
Z = -248988
78 I = 51
34034
XDOT = 4429
200810 Wp = 39
47746
YDOT = -1894
616763 meter/sec RA = 251
10252 deg
ZDOT = 6005
138951 TA = 317
80760
MA = 317
90710
Ha = 193
490 n
mi
Hp = 186
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7763282
61 X = -2294446
44
Y = -20660163
45 feet Y = -6323277
21 meter
Z = -816892
31 Z = -260308
87
XDOT = 14531
498722 XDOT = 4420
885735
YDOT = -6215
934261 feet/sec YDOT = -1845
132559 meter/sec
ZDOT = 19701
899446 ZDOT = 6026
636000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20476345
80 X = 6241190
20
Y = -8231256
54 feet Y = -2508886
99 meter
Z = -862497
84 Z = -262889
34
XDOT = 5944
696412 XDOT = 1811
943466
YDOT = 12773
528700 feet/sec YDOT = 3893
371548 meter/sec
ZDOT = 19788
700532 ZDOT = 6031
595922
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 11080
26073029
00016717 00000-0 10270-3 0 9062
2 25544 51
6452 251
9730 0001476 8
1562 351
9623 15
71879789 27068
Satellite: ISS
Catalog Number: 25544
Epoch time: 11080
26073029 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 251
9730 deg
Eccentricity:
0001476
Arg of perigee: 8
1562 deg
Mean anomaly: 351
9623 deg
Mean motion: 15
71879789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2706
Checksum: 314
Coasting Arc #8 (Orbit 2721)
---------------------------------------
Vector Time (GMT): 2011/081/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3316576
98 A = 6726311
43 meter
Y = 2747533
85 meter E =
0015017
Z = -5179799
89 I = 51
31257
XDOT = -3837
790474 Wp = 76
30381
YDOT = -6579
483084 meter/sec RA = 245
97184 deg
ZDOT = -1031
676636 TA = 183
78925
MA = 183
80064
Ha = 193
431 n
mi
Hp = 186
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10881158
08 X = -3321891
38
Y = 9014218
66 feet Y = 2710415
71 meter
Z = -16994094
14 Z = -5195924
98
XDOT = -12591
176095 XDOT = -3758
920505
YDOT = -21586
230592 feet/sec YDOT = -6621
958688 meter/sec
ZDOT = -3384
765865 ZDOT = -1050
128484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9439450
58 X = -2877144
54
Y = -10408389
65 feet Y = -3172477
16 meter
Z = -17059225
43 Z = -5199651
91
XDOT = 20304
760527 XDOT = 6188
891009
YDOT = -12739
704570 feet/sec YDOT = -3883
061953 meter/sec
ZDOT = -3459
159338 ZDOT = -1054
351766
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 11081
27791729
00016717 00000-0 10270-3 0 9079
2 25544 51
6457 246
7657 0001580 9
7802 350
3391 15
71953365 27229
Satellite: ISS
Catalog Number: 25544
Epoch time: 11081
27791729 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 246
7657 deg
Eccentricity:
0001580
Arg of perigee: 9
7802 deg
Mean anomaly: 350
3391 deg
Mean motion: 15
71953365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2722
Checksum: 322
Coasting Arc #9 (Orbit 2737)
---------------------------------------
Vector Time (GMT): 2011/082/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4208078
39 A = 6736966
70 meter
Y = 5026325
50 meter E =
0013808
Z = 1528670
72 I = 51
36200
XDOT = -2918
172817 Wp = 111
54928
YDOT = 4203
547511 meter/sec RA = 240
80711 deg
ZDOT = -5751
736688 TA = 51
54813
MA = 51
42430
Ha = 193
450 n
mi
Hp = 186
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13806031
47 X = 4144134
30
Y = 16490569
23 feet Y = 5073025
35 meter
Z = 5015323
89 Z = 1548957
93
XDOT = -9574
057798 XDOT = -2937
019905
YDOT = 13791
166376 feet/sec YDOT = 4170
809004 meter/sec
ZDOT = -18870
527191 ZDOT = -5765
959202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15673319
02 X = -4777227
64
Y = 14699147
76 feet Y = 4480300
24 meter
Z = 5097153
94 Z = 1553612
52
XDOT = -13238
585838 XDOT = -4035
120963
YDOT = -7511
388130 feet/sec YDOT = -2289
471102 meter/sec
ZDOT = -18928
002100 ZDOT = -5769
255040
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 11082
29507252
00016717 00000-0 10270-3 0 9089
2 25544 51
6457 241
5584 0001520 14
9643 345
1564 15
71952184 27385
Satellite: ISS
Catalog Number: 25544
Epoch time: 11082
29507252 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 241
5584 deg
Eccentricity:
0001520
Arg of perigee: 14
9643 deg
Mean anomaly: 345
1564 deg
Mean motion: 15
71952184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2738
Checksum: 308
Coasting Arc #10 (Orbit 2753)
---------------------------------------
Vector Time (GMT): 2011/083/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1630855
26 A = 6727751
11 meter
Y = -4419410
55 meter E =
0006825
Z = 4798406
52 I = 51
34773
XDOT = 5579
066330 Wp = 106
44063
YDOT = 4714
286964 meter/sec RA = 235
70020 deg
ZDOT = 2440
980808 TA = 319
58873
MA = 319
63942
Ha = 193
322 n
mi
Hp = 186
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5350575
01 X = 1656843
02
Y = -14499378
45 feet Y = -4401027
83 meter
Z = 15742803
55 Z = 4806392
50
XDOT = 18304
023393 XDOT = 5514
077820
YDOT = 15466
820747 feet/sec YDOT = 4776
312197 meter/sec
ZDOT = 8008
467219 ZDOT = 2467
925768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14850187
88 X = 4526337
27
Y = 4161061
19 feet Y = 1268291
45 meter
Z = 15775106
40 Z = 4808252
43
XDOT = -13760
038861 XDOT = -4194
059845
YDOT = 18274
933892 feet/sec YDOT = 5570
199850 meter/sec
ZDOT = 8117
189820 ZDOT = 2474
119457
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 11083
31219163
00016717 00000-0 10270-3 0 9095
2 25544 51
6458 236
3507 0001753 13
9579 346
1631 15
72026670 27545
Satellite: ISS
Catalog Number: 25544
Epoch time: 11083
31219163 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 236
3507 deg
Eccentricity:
0001753
Arg of perigee: 13
9579 deg
Mean anomaly: 346
1631 deg
Mean motion: 15
72026670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2754
Checksum: 304
Coasting Arc #11 (Orbit 2768)
---------------------------------------
Vector Time (GMT): 2011/084/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5337703
30 A = 6734417
11 meter
Y = -3099150
11 meter E =
0006241
Z = -2691153
63 I = 51
38860
XDOT = 685
798518 Wp = 44
68241
YDOT = -5659
037563 meter/sec RA = 230
51778 deg
ZDOT = 5168
382203 TA = 284
55459
MA = 284
62381
Ha = 193
225 n
mi
Hp = 186
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17512149
93 X = -5289578
26
Y = -10167815
31 feet Y = -3158570
55 meter
Z = -8829244
19 Z = -2716967
01
XDOT = 2249
995137 XDOT = 723
921092
YDOT = -18566
396204 feet/sec YDOT = -5651
155217 meter/sec
ZDOT = 16956
634523 ZDOT = 5171
806581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8524794
18 X = 2598357
27
Y = -18317671
36 feet Y = -5583226
23 meter
Z = -8933432
53 Z = -2722910
23
XDOT = 17348
754367 XDOT = 5287
900331
YDOT = -184
179838 feet/sec YDOT = -56
138015 meter/sec
ZDOT = 16970
535899 ZDOT = 5172
619342
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 11084
26570941
00016717 00000-0 10270-3 0 9106
2 25544 51
6454 231
4682 0001877 9
3650 350
7546 15
72082789 27692
Satellite: ISS
Catalog Number: 25544
Epoch time: 11084
26570941 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 231
4682 deg
Eccentricity:
0001877
Arg of perigee: 9
3650 deg
Mean anomaly: 350
7546 deg
Mean motion: 15
72082789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2769
Checksum: 322
Coasting Arc #12 (Orbit 2784)
---------------------------------------
Vector Time (GMT): 2011/085/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 472185
15 A = 6729892
13 meter
Y = 5250312
81 meter E =
0009159
Z = -4193456
07 I = 51
39314
XDOT = -6364
696103 Wp = 59
88720
YDOT = -2327
622253 meter/sec RA = 225
42675 deg
ZDOT = -3632
304230 TA = 172
92471
MA = 172
91177
Ha = 193
205 n
mi
Hp = 186
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1549163
87 X = 433810
88
Y = 17225435
73 feet Y = 5255378
36 meter
Z = -13758057
98 Z = -4191255
63
XDOT = -20881
548894 XDOT = -6320
550265
YDOT = -7636
555947 feet/sec YDOT = -2398
549442 meter/sec
ZDOT = -11917
008627 ZDOT = -3663
116266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16945162
35 X = -5164885
48
Y = 3495662
58 feet Y = 1065477
96 meter
Z = -13749237
08 Z = -4190767
46
XDOT = 5582
698832 XDOT = 1701
606604
YDOT = -20281
549863 feet/sec YDOT = -6181
816398 meter/sec
ZDOT = -12041
405859 ZDOT = -3670
220506
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 11085
28276199
00016717 00000-0 10270-3 0 9118
2 25544 51
6445 226
2600 0001882 9
5388 350
5809 15
72131689 27852
Satellite: ISS
Catalog Number: 25544
Epoch time: 11085
28276199 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 226
2600 deg
Eccentricity:
0001882
Arg of perigee: 9
5388 deg
Mean anomaly: 350
5809 deg
Mean motion: 15
72131689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2785
Checksum: 324
Coasting Arc #13 (Orbit 2800)
---------------------------------------
Vector Time (GMT): 2011/086/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5590861
06 A = 6731405
42 meter
Y = 949720
56 meter E =
0012687
Z = 3618697
58 I = 51
42206
XDOT = 1801
011594 Wp = 76
27447
YDOT = 6083
360305 meter/sec RA = 220
23775 deg
ZDOT = -4363
360044 TA = 60
24622
MA = 60
12007
Ha = 193
028 n
mi
Hp = 186
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18342720
01 X = 5562246
85
Y = 3115881
09 feet Y = 1012081
13 meter
Z = 11872367
38 Z = 3645788
04
XDOT = 5908
830690 XDOT = 1754
048561
YDOT = 19958
531185 feet/sec YDOT = 6103
237517 meter/sec
ZDOT = -14315
485709 ZDOT = -4354
725215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -791689
98 X = -241307
11
Y = 18518307
65 feet Y = 5644380
17 meter
Z = 11981765
65 Z = 3652042
17
XDOT = -17694
306960 XDOT = -5393
224761
YDOT = 8516
604786 feet/sec YDOT = 2595
861139 meter/sec
ZDOT = -14280
681723 ZDOT = -4352
751789
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 11086
29977868
00016717 00000-0 10270-3 0 9122
2 25544 51
6448 221
0515 0002104 12
2911 347
8302 15
72238514 28015
Satellite: ISS
Catalog Number: 25544
Epoch time: 11086
29977868 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 221
0515 deg
Eccentricity:
0002104
Arg of perigee: 12
2911 deg
Mean anomaly: 347
8302 deg
Mean motion: 15
72238514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2801
Checksum: 291
Coasting Arc #14 (Orbit 2816)
---------------------------------------
Vector Time (GMT): 2011/087/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2645169
22 A = 6732239
46 meter
Y = -5169569
22 meter E =
0013267
Z = 3392809
93 I = 51
44753
XDOT = 6176
938113 Wp = 81
35930
YDOT = -133
315758 meter/sec RA = 215
15192 deg
ZDOT = 4599
329062 TA = 318
81158
MA = 318
91161
Ha = 193
171 n
mi
Hp = 186
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8678376
69 X = -2603646
91
Y = -16960528
95 feet Y = -5198916
73 meter
Z = 11131266
17 Z = 3380061
09
XDOT = 20265
544989 XDOT = 6155
627436
YDOT = -437
387657 feet/sec YDOT = -64
360352 meter/sec
ZDOT = 15089
662276 ZDOT = 4629
284390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15536170
88 X = 4735424
89
Y = -11078975
71 feet Y = -3376871
80 meter
Z = 11079825
92 Z = 3377130
94
XDOT = 2507
792991 XDOT = 764
375304
YDOT = 18772
454392 feet/sec YDOT = 5721
844099 meter/sec
ZDOT = 15210
654660 ZDOT = 4636
207540
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 11087
31676230
00016717 00000-0 10270-3 0 9136
2 25544 51
6436 215
8420 0002125 15
1147 345
0078 15
72239823 28175
Satellite: ISS
Catalog Number: 25544
Epoch time: 11087
31676230 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 215
8420 deg
Eccentricity:
0002125
Arg of perigee: 15
1147 deg
Mean anomaly: 345
0078 deg
Mean motion: 15
72239823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2817
Checksum: 285
Coasting Arc #15 (Orbit 2831)
---------------------------------------
Vector Time (GMT): 2011/088/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5012905
14 A = 6728654
90 meter
Y = 1115223
59 meter E =
0009349
Z = -4356363
99 I = 51
46129
XDOT = -4162
135571 Wp = 98
12845
YDOT = -5510
722714 meter/sec RA = 209
96596 deg
ZDOT = 3383
556369 TA = 206
07683
MA = 206
12395
Ha = 193
039 n
mi
Hp = 185
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16446539
18 X = -5003841
12
Y = 3658870
06 feet Y = 1059216
57 meter
Z = -14292532
77 Z = -4380694
37
XDOT = -13655
300430 XDOT = -4116
640726
YDOT = -18079
798929 feet/sec YDOT = -5557
011584 meter/sec
ZDOT = 11100
906721 ZDOT = 3363
447997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6227672
34 X = -1898194
53
Y = -15565114
21 feet Y = -4744246
81 meter
Z = -14390823
15 Z = -4386322
90
XDOT = 14517
257979 XDOT = 4424
860232
YDOT = -15982
051203 feet/sec YDOT = -4871
329207 meter/sec
ZDOT = 11019
731072 ZDOT = 3358
814031
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 11088
27015040
00016717 00000-0 10270-3 0 9149
2 25544 51
6428 210
9578 0002097 18
7668 341
3572 15
72308805 28323
Satellite: ISS
Catalog Number: 25544
Epoch time: 11088
27015040 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 210
9578 deg
Eccentricity:
0002097
Arg of perigee: 18
7668 deg
Mean anomaly: 341
3572 deg
Mean motion: 15
72308805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2832
Checksum: 306
Coasting Arc #16 (Orbit 2847)
---------------------------------------
Vector Time (GMT): 2011/089/06:14:43
299
Vector Time (MET): N/A
Weight (LBS) : 906017
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4523096
82 A = 6734177
37 meter
Y = 4306728
07 meter E =
0005014
Z = -2520274
20 I = 51
50679
XDOT = -5103
404016 Wp = 107
18712
YDOT = 2270
243615 meter/sec RA = 204
87847 deg
ZDOT = -5289
638759 TA = 101
37544
MA = 101
31910
Ha = 193
063 n
mi
Hp = 186
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14839556
51 X = 4486844
87
Y = 14129685
26 feet Y = 4357105
14 meter
Z = -8268616
15 Z = -2498389
79
XDOT = -16743
451495 XDOT = -5102
715265
YDOT = 7448
305823 feet/sec YDOT = 2213
177585 meter/sec
ZDOT = -17354
457870 ZDOT = -5314
429293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11273056
56 X = -3436027
64
Y = 17153199
52 feet Y = 5228295
21 meter
Z = -8180244
36 Z = -2493338
48
XDOT = -9022
503656 XDOT = -2750
059114
YDOT = -14237
582945 feet/sec YDOT = -4339
615282 meter/sec
ZDOT = -17454
622817 ZDOT = -5320
169034
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 11089
28706403
00016717 00000-0 10270-3 0 9152
2 25544 51
6424 205
7491 0002170 20
9862 339
1389 15
72349491 28482
Satellite: ISS
Catalog Number: 25544
Epoch time: 11089
28706403 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 205
7491 deg
Eccentricity:
0002170
Arg of perigee: 20
9862 deg
Mean anomaly: 339
1389 deg
Mean motion: 15
72349491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2848
Checksum: 318
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