[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 26th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 123 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 362 ET - UTC (sec) : 67 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 1735)
---------------------------------------
Vector Time (GMT): 2013/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2841493
83 A = 6793819
25 meter
Y = -6067074
28 meter E =
0015504
Z = -1062774
47 I = 51
37065
XDOT = 4786
376257 Wp = 348
46991
YDOT = 1213
214331 meter/sec RA = 302
37883 deg
ZDOT = 5871
285779 TA = 359
96054
MA = 359
96066
Ha = 224
371 n
mi
Hp = 218
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9322486
31 X = 2914288
52
Y = -19905099
35 feet Y = -6034892
02 meter
Z = -3486792
87 Z = -1048793
48
XDOT = 15703
334176 XDOT = 4743
933558
YDOT = 3980
361978 feet/sec YDOT = 1266
501998 meter/sec
ZDOT = 19262
748619 ZDOT = 5894
433855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16953940
64 X = 5167561
11
Y = -14003321
07 feet Y = -4268212
26 meter
Z = -3427878
57 Z = -1044817
39
XDOT = 11366
989055 XDOT = 3464
658264
YDOT = 9023
282510 feet/sec YDOT = 2750
296509 meter/sec
ZDOT = 19358
892520 ZDOT = 5900
590440
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 13056
50202548
00016717 00000-0 10270-3 0 9008
2 25544 51
6486 303
0350 0011843 310
4496 49
5623 15
52427710 17360
Satellite: ISS
Catalog Number: 25544
Epoch time: 13056
50202548 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 303
0350 deg
Eccentricity:
0011843
Arg of perigee: 310
4496 deg
Mean anomaly: 49
5623 deg
Mean motion: 15
52427710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 282
Coasting Arc #2 (Orbit 1751)
---------------------------------------
Vector Time (GMT): 2013/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3185018
40 A = 6794356
60 meter
Y = 6000732
80 meter E =
0000387
Z = -83193
16 I = 51
35615
XDOT = -4190
951350 Wp = 206
29131
YDOT = -2307
512179 meter/sec RA = 297
39710 deg
ZDOT = -5981
792464 TA = 334
60699
MA = 334
60889
Ha = 224
603 n
mi
Hp = 218
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10449535
42 X = -3251479
03
Y = 19687443
57 feet Y = 5964744
31 meter
Z = -272943
45 Z = -98827
66
XDOT = -13749
840387 XDOT = -4135
779325
YDOT = -7570
578014 feet/sec YDOT = -2354
070338 meter/sec
ZDOT = -19625
303359 ZDOT = -6002
017075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17626787
88 X = -5372644
94
Y = 13639807
33 feet Y = 4157413
27 meter
Z = -338715
77 Z = -103240
57
XDOT = -8307
722114 XDOT = -2532
193700
YDOT = -11226
224633 feet/sec YDOT = -3421
753268 meter/sec
ZDOT = -19709
151145 ZDOT = -6007
349269
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 13057
53199143
00016717 00000-0 10270-3 0 9019
2 25544 51
6481 297
9144 0011770 313
6527 46
3648 15
52396821 17524
Satellite: ISS
Catalog Number: 25544
Epoch time: 13057
53199143 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 297
9144 deg
Eccentricity:
0011770
Arg of perigee: 313
6527 deg
Mean anomaly: 46
3648 deg
Mean motion: 15
52396821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1752
Checksum: 317
Coasting Arc #3 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2013/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3425134
53 A = 6793535
81 meter
Y = -5723229
34 meter E =
0016421
Z = 1230363
36 I = 51
34021
XDOT = 3630
158243 Wp = 12
75145
YDOT = 3425
068983 meter/sec RA = 292
41261 deg
ZDOT = 5827
294845 TA =
68183
MA =
67959
Ha = 224
724 n
mi
Hp = 218
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11237318
01 X = 3482901
64
Y = -18776999
14 feet Y = -5684604
17 meter
Z = 4036625
21 Z = 1247143
24
XDOT = 11909
967990 XDOT = 3563
281512
YDOT = 11237
102961 feet/sec YDOT = 3465
290552 meter/sec
ZDOT = 19118
421406 ZDOT = 5844
766707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17731002
32 X = 5404409
51
Y = -12801972
43 feet Y = -3902041
20 meter
Z = 4107117
52 Z = 1251849
42
XDOT = 5444
207868 XDOT = 1659
394558
YDOT = 13696
227757 feet/sec YDOT = 4174
610220 meter/sec
ZDOT = 19190
684101 ZDOT = 5849
320514
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 13058
56194423
00016717 00000-0 10270-3 0 9020
2 25544 51
6475 292
7922 0012004 317
9699 42
0531 15
52456721 17689
Satellite: ISS
Catalog Number: 25544
Epoch time: 13058
56194423 = yrday
fracday
Element set: 902
Inclination: 51
6475 deg
RA of node: 292
7922 deg
Eccentricity:
0012004
Arg of perigee: 317
9699 deg
Mean anomaly: 42
0531 deg
Mean motion: 15
52456721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 313
Coasting Arc #4 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2013/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602402
15 A = 6791913
09 meter
Y = 5271938
97 meter E =
0006347
Z = -2321402
89 I = 51
32331
XDOT = -3099
653239 Wp = 326
19651
YDOT = -4489
921396 meter/sec RA = 287
42616 deg
ZDOT = -5374
273639 TA = 239
75862
MA = 239
82147
Ha = 224
978 n
mi
Hp = 218
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11818904
68 X = -3649809
69
Y = 17296387
70 feet Y = 5231389
28 meter
Z = -7616151
22 Z = -2339018
72
XDOT = -10169
466006 XDOT = -3023
109048
YDOT = -14730
713240 feet/sec YDOT = -4524
156378 meter/sec
ZDOT = -17632
131361 ZDOT = -5389
144852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17462757
78 X = -5322648
57
Y = 11522690
25 feet Y = 3512115
99 meter
Z = -7690058
17 Z = -2343929
73
XDOT = -2865
050081 XDOT = -873
267265
YDOT = -16176
998524 feet/sec YDOT = -4930
749150 meter/sec
ZDOT = -17693
451123 ZDOT = -5392
963902
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 13059
52751691
00016717 00000-0 10270-3 0 9034
2 25544 51
6469 287
9913 0012013 320
8728 39
1554 15
52441527 17831
Satellite: ISS
Catalog Number: 25544
Epoch time: 13059
52751691 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 287
9913 deg
Eccentricity:
0012013
Arg of perigee: 320
8728 deg
Mean anomaly: 39
1554 deg
Mean motion: 15
52441527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 319
Coasting Arc #5 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2013/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3727422
92 A = 6789465
15 meter
Y = -4599137
71 meter E =
0011741
Z = 3308258
68 I = 51
30663
XDOT = 2624
251377 Wp = 28
60469
YDOT = 5486
990993 meter/sec RA = 282
43342 deg
ZDOT = 4674
485921 TA = 10
07874
MA = 10
05521
Ha = 225
104 n
mi
Hp = 217
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12229077
83 X = 3762503
88
Y = -15089034
50 feet Y = -4557258
80 meter
Z = 10853867
05 Z = 3326451
81
XDOT = 8609
748612 XDOT = 2539
992355
YDOT = 18001
938953 feet/sec YDOT = 5515
866443 meter/sec
ZDOT = 15336
239897 ZDOT = 4687
028941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16821459
71 X = 5127180
92
Y = -9623272
40 feet Y = -2933173
43 meter
Z = 10930089
58 Z = 3331491
30
XDOT = 672
558930 XDOT = 204
995962
YDOT = 18641
071289 feet/sec YDOT = 5681
798529 meter/sec
ZDOT = 15387
760504 ZDOT = 4690
189402
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 13060
55745047
00016717 00000-0 10270-3 0 9048
2 25544 51
6464 282
8684 0012158 325
5050 34
5312 15
52465003 17998
Satellite: ISS
Catalog Number: 25544
Epoch time: 13060
55745047 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 282
8684 deg
Eccentricity:
0012158
Arg of perigee: 325
5050 deg
Mean anomaly: 34
5312 deg
Mean motion: 15
52465003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 300
Coasting Arc #6 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2013/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3835185
99 A = 6786802
78 meter
Y = 3787484
77 meter E =
0012916
Z = -4133673
15 I = 51
29137
XDOT = -2195
170214 Wp = 3
69420
YDOT = -6313
093558 meter/sec RA = 277
43657 deg
ZDOT = -3735
720176 TA = 227
55265
MA = 227
66194
Ha = 225
301 n
mi
Hp = 217
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12582631
19 X = -3857173
21
Y = 12426131
13 feet Y = 3744473
97 meter
Z = -13561919
77 Z = -4152357
84
XDOT = -7202
002015 XDOT = -2106
265650
YDOT = -20712
249206 feet/sec YDOT = -6337
144598 meter/sec
ZDOT = -12256
299791 ZDOT = -3746
167525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16042225
22 X = -4889670
25
Y = 7297397
84 feet Y = 2224246
86 meter
Z = -13640088
16 Z = -4157498
87
XDOT = 1061
535307 XDOT = 323
555962
YDOT = -20728
517052 feet/sec YDOT = -6318
051997 meter/sec
ZDOT = -12299
010611 ZDOT = -3748
738434
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 13061
52300234
00016717 00000-0 10270-3 0 9052
2 25544 51
6455 278
0669 0012153 328
4129 31
6292 15
52488861 18142
Satellite: ISS
Catalog Number: 25544
Epoch time: 13061
52300234 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 278
0669 deg
Eccentricity:
0012153
Arg of perigee: 328
4129 deg
Mean anomaly: 31
6292 deg
Mean motion: 15
52488861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 298
Coasting Arc #7 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2013/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940351
68 A = 6784423
10 meter
Y = -2789460
95 meter E =
0007313
Z = 4762764
42 I = 51
28045
XDOT = 1797
214169 Wp = 7
49532
YDOT = 6982
841809 meter/sec RA = 272
43341 deg
ZDOT = 2609
508528 TA = 56
67989
MA = 56
60988
Ha = 225
433 n
mi
Hp = 217
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12927663
00 X = 3948115
05
Y = -9151774
78 feet Y = -2745353
69 meter
Z = 15625867
53 Z = 4781925
28
XDOT = 5896
371944 XDOT = 1706
320738
YDOT = 22909
585987 feet/sec YDOT = 7002
431373 meter/sec
ZDOT = 8561
379684 ZDOT = 2618
017887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15140935
26 X = 4614957
07
Y = -4373100
05 feet Y = -1332920
89 meter
Z = 15705899
01 Z = 4787158
02
XDOT = -2410
882654 XDOT = -734
837033
YDOT = 22446
842955 feet/sec YDOT = 6841
797733 meter/sec
ZDOT = 8595
956920 ZDOT = 2620
047669
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 13062
55291614
00016717 00000-0 10270-3 0 9068
2 25544 51
6456 272
9442 0012178 332
9439 27
1077 15
52476133 18304
Satellite: ISS
Catalog Number: 25544
Epoch time: 13062
55291614 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 272
9442 deg
Eccentricity:
0012178
Arg of perigee: 332
9439 deg
Mean anomaly: 27
1077 deg
Mean motion: 15
52476133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 306
Coasting Arc #8 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2013/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4061677
42 A = 6782641
45 meter
Y = 1737111
28 meter E =
0016159
Z = -5157118
25 I = 51
27334
XDOT = -1423
960661 Wp = 32
52028
YDOT = -7399
715971 meter/sec RA = 267
42677 deg
ZDOT = -1359
626956 TA = 224
25897
MA = 224
38831
Ha = 225
554 n
mi
Hp = 216
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13325713
33 X = -4055748
59
Y = 5699183
98 feet Y = 1691723
88 meter
Z = -16919679
28 Z = -5176835
07
XDOT = -4671
786947 XDOT = -1334
504977
YDOT = -24277
283370 feet/sec YDOT = -7415
139502 meter/sec
ZDOT = -4460
718359 ZDOT = -1366
326649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14343793
92 X = -4371988
39
Y = 1233597
70 feet Y = 376000
58 meter
Z = -17001902
64 Z = -5182179
93
XDOT = 3346
115147 XDOT = 1019
895897
YDOT = -23456
438277 feet/sec YDOT = -7149
522387 meter/sec
ZDOT = -4487
727599 ZDOT = -1367
859372
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 13063
51844775
00016717 00000-0 10270-3 0 9078
2 25544 51
6443 268
1422 0012167 335
9681 24
0902 15
52529656 18453
Satellite: ISS
Catalog Number: 25544
Epoch time: 13063
51844775 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 268
1422 deg
Eccentricity:
0012167
Arg of perigee: 335
9681 deg
Mean anomaly: 24
0902 deg
Mean motion: 15
52529656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 315
Coasting Arc #9 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2013/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4204896
82 A = 6782050
63 meter
Y = -571835
03 meter E =
0011487
Z = 5291912
31 I = 51
27387
XDOT = 1025
192737 Wp = 350
97303
YDOT = 7596
101849 meter/sec RA = 262
41773 deg
ZDOT = 17
365829 TA = 98
92560
MA = 98
79555
Ha = 225
677 n
mi
Hp = 216
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13795593
24 X = 4185272
30
Y = -1876099
19 feet Y = -524922
67 meter
Z = 17361917
04 Z = 5312291
45
XDOT = 3363
493233 XDOT = 940
090957
YDOT = 24921
593993 feet/sec YDOT = 7607
090369 meter/sec
ZDOT = 56
974506 ZDOT = 22
138945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13622037
30 X = 4151996
97
Y = 2307550
74 feet Y = 703341
47 meter
Z = 17446765
13 Z = 5317774
01
XDOT = -4081
071645 XDOT = -1243
910638
YDOT = 23792
538597 feet/sec YDOT = 7251
965764 meter/sec
ZDOT = 75
957288 ZDOT = 23
151781
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 13064
54833989
00016717 00000-0 10270-3 0 9088
2 25544 51
6445 263
0201 0012139 339
8285 20
2386 15
52514631 18615
Satellite: ISS
Catalog Number: 25544
Epoch time: 13064
54833989 = yrday
fracday
Element set: 908
Inclination: 51
6445 deg
RA of node: 263
0201 deg
Eccentricity:
0012139
Arg of perigee: 339
8285 deg
Mean anomaly: 20
2386 deg
Mean motion: 15
52514631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 307
Coasting Arc #10 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2013/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4366491
95 A = 6782462
09 meter
Y = -536761
33 meter E =
0013832
Z = -5169327
07 I = 51
27944
XDOT = -607
756215 Wp = 48
44525
YDOT = -7523
274859 meter/sec RA = 257
40838 deg
ZDOT = 1305
833246 TA = 234
11154
MA = 234
24003
Ha = 225
758 n
mi
Hp = 216
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14325761
00 X = -4335054
45
Y = -1761027
98 feet Y = -585414
73 meter
Z = -16959734
48 Z = -5190462
36
XDOT = -1993
950837 XDOT = -529
927468
YDOT = -24682
660297 feet/sec YDOT = -7529
635926 meter/sec
ZDOT = 4284
229810 ZDOT = 1303
070365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13141983
55 X = -4005676
59
Y = -5712141
41 feet Y = -1741060
70 meter
Z = -17047608
34 Z = -5196111
02
XDOT = 4626
101156 XDOT = 1410
035632
YDOT = -23287
752211 feet/sec YDOT = -7098
106874 meter/sec
ZDOT = 4273
588915 ZDOT = 1302
589901
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 13065
51385218
00016717 00000-0 10270-3 0 9094
2 25544 51
6432 258
2174 0012104 343
4930 16
5826 15
52565090 18764
Satellite: ISS
Catalog Number: 25544
Epoch time: 13065
51385218 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 258
2174 deg
Eccentricity:
0012104
Arg of perigee: 343
4930 deg
Mean anomaly: 16
5826 deg
Mean motion: 15
52565090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 302
Coasting Arc #11 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2013/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4535046
97 A = 6784164
55 meter
Y = 1665055
56 meter E =
0015824
Z = 4766155
86 I = 51
29270
XDOT = 101
912077 Wp = 13
70395
YDOT = 7207
967207 meter/sec RA = 252
40204 deg
ZDOT = -2598
188068 TA = 102
13906
MA = 101
96175
Ha = 225
923 n
mi
Hp = 216
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14878763
01 X = 4492938
65
Y = 5462780
72 feet Y = 1715534
24 meter
Z = 15636994
30 Z = 4788083
88
XDOT = 334
357208 XDOT = 33
924531
YDOT = 23648
186374 feet/sec YDOT = 7208
726512 meter/sec
ZDOT = -8524
239067 ZDOT = -2597
858688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12793531
50 X = 3899468
40
Y = 9202673
59 feet Y = 2804974
91 meter
Z = 15728048
29 Z = 4793909
12
XDOT = -5252
675676 XDOT = -1601
015546
YDOT = 21963
967153 feet/sec YDOT = 6694
617188 meter/sec
ZDOT = -8523
673497 ZDOT = -2598
015682
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 13066
54372160
00016717 00000-0 10270-3 0 9102
2 25544 51
6431 253
0954 0012141 346
8309 13
2524 15
52563490 18929
Satellite: ISS
Catalog Number: 25544
Epoch time: 13066
54372160 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 253
0954 deg
Eccentricity:
0012141
Arg of perigee: 346
8309 deg
Mean anomaly: 13
2524 deg
Mean motion: 15
52563490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 285
Coasting Arc #12 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2013/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4687288
20 A = 6786435
30 meter
Y = -2632518
62 meter E =
0010774
Z = -4140105
31 I = 51
31017
XDOT = 461
691168 Wp = 30
29610
YDOT = -6676
880518 meter/sec RA = 247
39941 deg
ZDOT = 3736
226912 TA = 278
28715
MA = 278
40930
Ha = 225
970 n
mi
Hp = 215
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15378242
14 X = -4637391
35
Y = -8636872
12 feet Y = -2684656
25 meter
Z = -13583022
68 Z = -4162753
81
XDOT = 1514
734804 XDOT = 518
169947
YDOT = -21905
775978 feet/sec YDOT = -6671
401440 meter/sec
ZDOT = 12257
962309 ZDOT = 3738
607556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12653468
58 X = -3856777
22
Y = -12182544
65 feet Y = -3713239
61 meter
Z = -13676978
29 Z = -4168742
98
XDOT = 5973
798810 XDOT = 1820
813877
YDOT = -19929
326239 feet/sec YDOT = -6074
458638 meter/sec
ZDOT = 12268
600589 ZDOT = 3739
469459
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 13067
50921413
00016717 00000-0 10270-3 0 9111
2 25544 51
6425 248
2924 0012059 350
9969 9
0964 15
52592461 19079
Satellite: ISS
Catalog Number: 25544
Epoch time: 13067
50921413 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 248
2924 deg
Eccentricity:
0012059
Arg of perigee: 350
9969 deg
Mean anomaly: 9
0964 deg
Mean motion: 15
52592461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 314
Coasting Arc #13 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2013/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4793806
69 A = 6789163
15 meter
Y = 3532138
71 meter E =
0016266
Z = 3264220
45 I = 51
33188
XDOT = -1149
045998 Wp = 44
63390
YDOT = 5933
573003 meter/sec RA = 242
40311 deg
ZDOT = -4707
391649 TA = 97
36567
MA = 97
18079
Ha = 226
167 n
mi
Hp = 215
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15727712
22 X = 4738096
88
Y = 11588381
58 feet Y = 3585434
97 meter
Z = 10709384
68 Z = 3287372
14
XDOT = -3769
835952 XDOT = -1192
444289
YDOT = 19467
103029 feet/sec YDOT = 5920
480436 meter/sec
ZDOT = -15444
198323 ZDOT = -4713
079615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12530698
07 X = 3819356
77
Y = 14918729
69 feet Y = 4547228
81 meter
Z = 10805348
21 Z = 3293470
13
XDOT = -7020
320957 XDOT = -2139
793828
YDOT = 17160
682705 feet/sec YDOT = 5230
576089 meter/sec
ZDOT = -15468
506760 ZDOT = -4714
800861
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 13068
53906045
00016717 00000-0 10270-3 0 9120
2 25544 51
6422 243
1697 0012148 354
1991 5
9018 15
52610800 19238
Satellite: ISS
Catalog Number: 25544
Epoch time: 13068
53906045 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 243
1697 deg
Eccentricity:
0012148
Arg of perigee: 354
1991 deg
Mean anomaly: 5
9018 deg
Mean motion: 15
52610800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 292
Coasting Arc #14 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2013/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4823060
14 A = 6791507
79 meter
Y = -4204570
55 meter E =
0016736
Z = -2250239
63 I = 51
35534
XDOT = 1904
756124 Wp = 13
46509
YDOT = -5076
297327 meter/sec RA = 237
41230 deg
ZDOT = 5426
601546 TA = 321
39832
MA = 321
51786
Ha = 226
207 n
mi
Hp = 215
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15823688
12 X = -4764754
40
Y = -13794522
79 feet Y = -4258179
34 meter
Z = -7382675
96 Z = -2273527
04
XDOT = 6249
199882 XDOT = 1935
018274
YDOT = -16654
518788 feet/sec YDOT = -5054
827204 meter/sec
ZDOT = 17803
810847 ZDOT = 5435
928715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12422288
59 X = -3786313
56
Y = -16879899
78 feet Y = -5144993
45 meter
Z = -7479144
24 Z = -2279643
16
XDOT = 8363
576341 XDOT = 2549
218069
YDOT = -14026
288059 feet/sec YDOT = -4275
212600 meter/sec
ZDOT = 17843
163719 ZDOT = 5438
596302
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 13069
50453234
00016717 00000-0 10270-3 0 9136
2 25544 51
6427 238
3669 0012061 358
6527 1
4590 15
52622013 19387
Satellite: ISS
Catalog Number: 25544
Epoch time: 13069
50453234 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 238
3669 deg
Eccentricity:
0012061
Arg of perigee: 358
6527 deg
Mean anomaly: 1
4590 deg
Mean motion: 15
52622013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 297
Coasting Arc #15 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2013/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4735905
65 A = 6793037
62 meter
Y = 4753053
76 meter E =
0012752
Z = 1070580
55 I = 51
37802
XDOT = -2762
359549 Wp = 67
96357
YDOT = 4085
789156 meter/sec RA = 232
42712 deg
ZDOT = -5858
898292 TA = 100
40160
MA = 100
25785
Ha = 226
391 n
mi
Hp = 215
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15537748
21 X = 4677203
48
Y = 15594008
41 feet Y = 4805685
58 meter
Z = 3512403
36 Z = 1093443
57
XDOT = -9062
859413 XDOT = -2779
381823
YDOT = 13404
820064 feet/sec YDOT = 4054
802675 meter/sec
ZDOT = -19222
107257 ZDOT = -5872
359359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12095289
59 X = 3686644
27
Y = 18374569
17 feet Y = 5600568
68 meter
Z = 3607058
71 Z = 1099431
49
XDOT = -10096
952408 XDOT = -3077
551094
YDOT = 10469
203207 feet/sec YDOT = 3191
013137 meter/sec
ZDOT = -19278
555097 ZDOT = -5876
103594
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 13070
53435515
00016717 00000-0 10270-3 0 9144
2 25544 51
6424 233
2439 0012271 1
8729 358
2467 15
52676329 19540
Satellite: ISS
Catalog Number: 25544
Epoch time: 13070
53435515 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 233
2439 deg
Eccentricity:
0012271
Arg of perigee: 1
8729 deg
Mean anomaly: 358
2467 deg
Mean motion: 15
52676329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 308
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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