[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 21st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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
053/10:36:18
430 -1
3 1
9 1
9
N/A -0
6 -0
2 223
9
000/00:04:36
861 -1
3 -0
0 219
4
Coasting Arc #1 (Orbit 1658)
---------------------------------------
Vector Time (GMT): 2013/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 756964
14 A = 6782386
27 meter
Y = 4376373
22 meter E =
0011443
Z = 5134345
01 I = 51
44363
XDOT = -6889
444146 Wp = 319
60010
YDOT = 2981
341887 meter/sec RA = 327
31954 deg
ZDOT = -1518
860461 TA = 145
12787
MA = 145
05285
Ha = 223
400 n
mi
Hp = 218
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2483478
14 X = 683029
54
Y = 14358179
87 feet Y = 4384424
89 meter
Z = 16844963
94 Z = 5137842
44
XDOT = -22603
163208 XDOT = -6914
892029
YDOT = 9781
305405 feet/sec YDOT = 2904
157445 meter/sec
ZDOT = -4983
137996 ZDOT = -1552
390076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5172743
60 X = -1576652
25
Y = 13605030
56 feet Y = 4146813
32 meter
Z = 16858934
42 Z = 5138603
21
XDOT = -23434
993291 XDOT = -7142
985955
YDOT = -2534
943697 feet/sec YDOT = -772
650839 meter/sec
ZDOT = -5123
023917 ZDOT = -1561
497690
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 13051
54557909
00016717 00000-0 10270-3 0 9001
2 25544 51
6488 327
6770 0012809 297
9675 62
0180 15
52679839 16594
Satellite: ISS
Catalog Number: 25544
Epoch time: 13051
54557909 = yrday
fracday
Element set: 900
Inclination: 51
6488 deg
RA of node: 327
6770 deg
Eccentricity:
0012809
Arg of perigee: 297
9675 deg
Mean anomaly: 62
0180 deg
Mean motion: 15
52679839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1659
Checksum: 349
Coasting Arc #2 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2013/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 233981
99 A = 6784234
96 meter
Y = -4900423
21 meter E =
0003247
Z = -4683645
45 I = 51
42528
XDOT = 6729
628628 Wp = 344
89839
YDOT = -2363
521105 meter/sec RA = 322
32304 deg
ZDOT = 2811
741507 TA = 313
06404
MA = 313
09123
Ha = 223
623 n
mi
Hp = 218
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 767657
45 X = 311513
59
Y = -16077503
96 feet Y = -4897373
40 meter
Z = -15366290
85 Z = -4682320
25
XDOT = 22078
834081 XDOT = 6741
899468
YDOT = -7754
334334 feet/sec YDOT = -2288
197421 meter/sec
ZDOT = 9224
873712 ZDOT = 2844
462676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8606615
20 X = 2623296
31
Y = -13608481
34 feet Y = -4147865
11 meter
Z = -15360134
65 Z = -4681769
04
XDOT = 22010
611041 XDOT = 6708
834245
YDOT = 3363
978182 feet/sec YDOT = 1025
340550 meter/sec
ZDOT = 9361
310866 ZDOT = 2853
327552
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 13052
51101714
00016717 00000-0 10270-3 0 9019
2 25544 51
6495 322
8748 0012774 301
6269 58
3636 15
52686763 16742
Satellite: ISS
Catalog Number: 25544
Epoch time: 13052
51101714 = yrday
fracday
Element set: 901
Inclination: 51
6495 deg
RA of node: 322
8748 deg
Eccentricity:
0012774
Arg of perigee: 301
6269 deg
Mean anomaly: 58
3636 deg
Mean motion: 15
52686763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 315
Coasting Arc #3 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2013/053/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4768066
85 A = 6794462
07 meter
Y = 4818509
57 meter E =
0002531
Z = 435242
77 I = 51
43277
XDOT = -3671
351155 Wp = 188
11918
YDOT = -3094
268101 meter/sec RA = 317
63307 deg
ZDOT = -5970
022328 TA = 347
18020
MA = 347
18663
Ha = 223
854 n
mi
Hp = 219
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15643263
95 X = -4823708
32
Y = 15808758
43 feet Y = 4764878
97 meter
Z = 1427961
84 Z = 411945
01
XDOT = -12045
115338 XDOT = -3607
477428
YDOT = -10151
798230 feet/sec YDOT = -3134
966687 meter/sec
ZDOT = -19586
687427 ZDOT = -5987
701683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22207790
19 X = -6768934
45
Y = -1308312
01 feet Y = -398773
50 meter
Z = 1330413
29 Z = 405509
97
XDOT = -349
243315 XDOT = -106
449362
YDOT = -14039
719855 feet/sec YDOT = -4279
306612 meter/sec
ZDOT = -19659
835038 ZDOT = -5992
317720
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 13053
47644902
00016717 00000-0 10270-3 0 9027
2 25544 51
6485 318
0730 0011648 300
0737 59
9259 15
52338894 16894
Satellite: ISS
Catalog Number: 25544
Epoch time: 13053
47644902 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 318
0730 deg
Eccentricity:
0011648
Arg of perigee: 300
0737 deg
Mean anomaly: 59
9259 deg
Mean motion: 15
52338894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 325
Coasting Arc #4 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2013/054/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4966589
41 A = 6794250
69 meter
Y = -4568753
19 meter E =
0014603
Z = 697889
14 I = 51
40998
XDOT = 2804
758704 Wp = 2
91554
YDOT = 3955
533595 meter/sec RA = 312
65533 deg
ZDOT = 5943
521938 TA = 4
64689
MA = 4
63335
Ha = 224
041 n
mi
Hp = 219
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16294584
67 X = 5013918
97
Y = -14989347
74 feet Y = -4512948
97 meter
Z = 2289662
53 Z = 722131
14
XDOT = 9201
964252 XDOT = 2731
447282
YDOT = 12977
472424 feet/sec YDOT = 3986
488741 meter/sec
ZDOT = 19499
743892 ZDOT = 5956
968500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22044169
50 X = 6719062
86
Y = 1942635
24 feet Y = 592115
22 meter
Z = 2391097
86 Z = 728806
63
XDOT = -3338
308978 XDOT = -1017
516576
YDOT = 13846
181176 feet/sec YDOT = 4220
316022 meter/sec
ZDOT = 19555
176652 ZDOT = 5960
417844
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 13054
50645424
00016717 00000-0 10270-3 0 9033
2 25544 51
6482 312
9521 0011743 304
2922 55
7117 15
52361679 17053
Satellite: ISS
Catalog Number: 25544
Epoch time: 13054
50645424 = yrday
fracday
Element set: 903
Inclination: 51
6482 deg
RA of node: 312
9521 deg
Eccentricity:
0011743
Arg of perigee: 304
2922 deg
Mean anomaly: 55
7117 deg
Mean motion: 15
52361679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 290
Coasting Arc #5 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2013/055/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5043429
81 A = 6792971
64 meter
Y = 4179224
51 meter E =
0005016
Z = -1799906
31 I = 51
38664
XDOT = -1969
011569 Wp = 286
50845
YDOT = -4807
117856 meter/sec RA = 307
67524 deg
ZDOT = -5629
958622 TA = 273
31433
MA = 273
37171
Ha = 224
251 n
mi
Hp = 218
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16546685
71 X = -5081044
68
Y = 13711366
51 feet Y = 4122615
21 meter
Z = -5905204
43 Z = -1824498
07
XDOT = -6460
011709 XDOT = -1887
762815
YDOT = -15771
384042 feet/sec YDOT = -4828
682864 meter/sec
ZDOT = -18470
992854 ZDOT = -5639
325853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21301917
43 X = -6492824
43
Y = -2607229
36 feet Y = -794683
51 meter
Z = -6008035
27 Z = -1831249
15
XDOT = 6932
901292 XDOT = 2113
148314
YDOT = -13884
004378 feet/sec YDOT = -4231
844535 meter/sec
ZDOT = -18509
354122 ZDOT = -5641
651136
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 13055
47206850
00016717 00000-0 10270-3 0 9047
2 25544 51
6488 308
1519 0011743 307
3785 52
6297 15
52388384 17208
Satellite: ISS
Catalog Number: 25544
Epoch time: 13055
47206850 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 308
1519 deg
Eccentricity:
0011743
Arg of perigee: 307
3785 deg
Mean anomaly: 52
6297 deg
Mean motion: 15
52388384 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 319
Coasting Arc #6 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2013/056/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5002029
61 A = 6790852
41 meter
Y = -3601759
97 meter E =
0010820
Z = 2832696
42 I = 51
36138
XDOT = 1192
538667 Wp = 23
38318
YDOT = 5635
893445 meter/sec RA = 302
69006 deg
ZDOT = 5063
286807 TA = 8
93400
MA = 8
91476
Ha = 224
358 n
mi
Hp = 218
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16410858
31 X = 5028173
30
Y = -11816797
79 feet Y = -3545677
61 meter
Z = 9293623
42 Z = 2857059
26
XDOT = 3912
528435 XDOT = 1104
832696
YDOT = 18490
464060 feet/sec YDOT = 5648
739377 meter/sec
ZDOT = 16611
833356 ZDOT = 5068
866229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19878051
11 X = 6058829
98
Y = 3451606
44 feet Y = 1052049
64 meter
Z = 9395419
81 Z = 2863723
96
XDOT = -10321
827917 XDOT = -3146
093149
YDOT = 14191
998123 feet/sec YDOT = 4325
721028 meter/sec
ZDOT = 16634
342314 ZDOT = 5070
147537
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
50204209
00016717 00000-0 10270-3 0 9059
2 25544 51
6483 303
0306 0011771 311
7557 48
2588 15
52411341 17369
Satellite: ISS
Catalog Number: 25544
Epoch time: 13056
50204209 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 303
0306 deg
Eccentricity:
0011771
Arg of perigee: 311
7557 deg
Mean anomaly: 48
2588 deg
Mean motion: 15
52411341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 282
Coasting Arc #7 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2013/057/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4886406
46 A = 6788231
36 meter
Y = 2886826
62 meter E =
0010014
Z = -3730267
76 I = 51
33763
XDOT = -502
144933 Wp = 344
31612
YDOT = -6353
770490 meter/sec RA = 297
69985 deg
ZDOT = -4247
212924 TA = 240
38482
MA = 240
48462
Ha = 224
596 n
mi
Hp = 218
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16031517
27 X = -4900204
08
Y = 9471215
96 feet Y = 2832106
12 meter
Z = -12238411
29 Z = -3754038
97
XDOT = -1647
457130 XDOT = -410
426931
YDOT = -20845
703708 feet/sec YDOT = -6358
873525 meter/sec
ZDOT = -13934
425603 ZDOT = -4249
428646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18001570
15 X = -5486878
58
Y = -4496449
99 feet Y = -1370517
96 meter
Z = -12337649
62 Z = -3760515
60
XDOT = 13229
822941 XDOT = 4032
450033
YDOT = -14599
903056 feet/sec YDOT = -4450
050451 meter/sec
ZDOT = -13942
863078 ZDOT = -4249
784666
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
46762623
00016717 00000-0 10270-3 0 9065
2 25544 51
6486 298
2301 0011883 314
9299 45
0888 15
52452649 17515
Satellite: ISS
Catalog Number: 25544
Epoch time: 13057
46762623 = yrday
fracday
Element set: 906
Inclination: 51
6486 deg
RA of node: 298
2301 deg
Eccentricity:
0011883
Arg of perigee: 314
9299 deg
Mean anomaly: 45
0888 deg
Mean motion: 15
52452649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 334
Coasting Arc #8 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2013/058/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4705499
64 A = 6785627
31 meter
Y = -1988875
27 meter E =
0005626
Z = 4462669
90 I = 51
31524
XDOT = -112
193537 Wp = 5
51613
YDOT = 6955
583404 meter/sec RA = 292
70250 deg
ZDOT = 3223
347815 TA = 51
92175
MA = 51
87102
Ha = 224
680 n
mi
Hp = 218
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15437990
94 X = 4705711
77
Y = -6525181
32 feet Y = -1936253
62 meter
Z = 14641305
45 Z = 4485529
29
XDOT = -368
089031 XDOT = -205
621971
YDOT = 22820
155525 feet/sec YDOT = 6953
806832 meter/sec
ZDOT = 10575
288106 ZDOT = 3222
574927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15600092
35 X = 4754908
15
Y = 5894581
99 feet Y = 1796668
59 meter
Z = 14736634
71 Z = 4491726
26
XDOT = -15658
299796 XDOT = -4772
649778
YDOT = 15053
549489 feet/sec YDOT = 4588
321884 meter/sec
ZDOT = 10571
230128 ZDOT = 3222
110943
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
49756836
00016717 00000-0 10270-3 0 9079
2 25544 51
6481 293
1082 0011852 319
0600 40
9661 15
52463035 17679
Satellite: ISS
Catalog Number: 25544
Epoch time: 13058
49756836 = yrday
fracday
Element set: 907
Inclination: 51
6481 deg
RA of node: 293
1082 deg
Eccentricity:
0011852
Arg of perigee: 319
0600 deg
Mean anomaly: 40
9661 deg
Mean motion: 15
52463035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 312
Coasting Arc #9 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2013/059/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4507071
14 A = 6783437
54 meter
Y = 1006247
19 meter E =
0013723
Z = -4977086
14 I = 51
29744
XDOT = 627
659796 Wp = 20
81319
YDOT = -7354
061527 meter/sec RA = 287
70042 deg
ZDOT = -2044
349662 TA = 229
12585
MA = 229
24484
Ha = 224
886 n
mi
Hp = 217
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14786978
81 X = -4493811
09
Y = 3301335
92 feet Y = 955919
78 meter
Z = -16329022
78 Z = -4998948
83
XDOT = 2059
251298 XDOT = 719
778645
YDOT = -24127
498449 feet/sec YDOT = -7346
527840 meter/sec
ZDOT = -6707
183931 ZDOT = -2041
075871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13025270
61 X = -3970102
48
Y = -7544118
73 feet Y = -2299447
39 meter
Z = -16420083
57 Z = -5004841
47
XDOT = 17368
712736 XDOT = 5293
983642
YDOT = -15343
930151 feet/sec YDOT = -4676
829910 meter/sec
ZDOT = -6692
683930 ZDOT = -2039
930062
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
46312284
00016717 00000-0 10270-3 0 9083
2 25544 51
6481 288
3070 0012013 322
3824 37
6487 15
52516619 17820
Satellite: ISS
Catalog Number: 25544
Epoch time: 13059
46312284 = yrday
fracday
Element set: 908
Inclination: 51
6481 deg
RA of node: 288
3070 deg
Eccentricity:
0012013
Arg of perigee: 322
3824 deg
Mean anomaly: 37
6487 deg
Mean motion: 15
52516619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1782
Checksum: 307
Coasting Arc #10 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2013/060/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4291704
56 A = 6782191
84 meter
Y = 108842
99 meter E =
0009372
Z = 5253033
21 I = 51
28500
XDOT = -1090
024996 Wp = 334
75239
YDOT = 7549
656592 meter/sec RA = 282
69333 deg
ZDOT = 742
933498 TA = 108
16198
MA = 108
05991
Ha = 224
994 n
mi
Hp = 217
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14080395
55 X = 4264650
80
Y = 357096
42 feet Y = 156684
87 meter
Z = 17234360
94 Z = 5273816
10
XDOT = -3576
197495 XDOT = -1177
974803
YDOT = 24769
214540 feet/sec YDOT = 7536
975578 meter/sec
ZDOT = 2437
445858 ZDOT = 737
423779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10185353
06 X = 3104495
61
Y = 9573759
78 feet Y = 2918081
98 meter
Z = 17320795
61 Z = 5279378
50
XDOT = -18476
891275 XDOT = -5631
756461
YDOT = 15342
585130 feet/sec YDOT = 4676
419948 meter/sec
ZDOT = 2413
629371 ZDOT = 735
674232
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
49303299
00016717 00000-0 10270-3 0 9095
2 25544 51
6481 283
1849 0011994 326
0104 34
0279 15
52526381 17980
Satellite: ISS
Catalog Number: 25544
Epoch time: 13060
49303299 = yrday
fracday
Element set: 909
Inclination: 51
6481 deg
RA of node: 283
1849 deg
Eccentricity:
0011994
Arg of perigee: 326
0104 deg
Mean anomaly: 34
0279 deg
Mean motion: 15
52526381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 319
Coasting Arc #11 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2013/061/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4100213
11 A = 6782027
84 meter
Y = -1214186
94 meter E =
0012547
Z = -5270568
62 I = 51
27862
XDOT = 1482
560536 Wp = 42
28560
YDOT = -7493
156962 meter/sec RA = 277
68467 deg
ZDOT = 582
781745 TA = 233
25241
MA = 233
36768
Ha = 225
157 n
mi
Hp = 217
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13452142
74 X = -4060728
16
Y = -3983552
94 feet Y = -1259817
84 meter
Z = -17291891
79 Z = -5290390
99
XDOT = 4864
043752 XDOT = 1563
409438
YDOT = -24583
848299 feet/sec YDOT = -7476
125929 meter/sec
ZDOT = 1912
013598 ZDOT = 590
180973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7504188
51 X = -2287276
66
Y = -11732972
45 feet Y = -3576210
00 meter
Z = -17374201
33 Z = -5295656
57
XDOT = 18873
632084 XDOT = 5752
683059
YDOT = -14901
428313 feet/sec YDOT = -4541
955350 meter/sec
ZDOT = 1943
677062 ZDOT = 592
432769
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
45855864
00016717 00000-0 10270-3 0 9104
2 25544 51
6477 278
3829 0012138 329
3791 30
6651 15
52561976 18131
Satellite: ISS
Catalog Number: 25544
Epoch time: 13061
45855864 = yrday
fracday
Element set: 910
Inclination: 51
6477 deg
RA of node: 278
3829 deg
Eccentricity:
0012138
Arg of perigee: 329
3791 deg
Mean anomaly: 30
6651 deg
Mean motion: 15
52561976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1813
Checksum: 329
Coasting Arc #12 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2013/062/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3914240
19 A = 6783042
76 meter
Y = 2364591
50 meter E =
0014090
Z = 5014590
58 I = 51
27953
XDOT = -1870
296003 Wp = 356
44781
YDOT = 7179
667147 meter/sec RA = 272
67644 deg
ZDOT = -1912
092368 TA = 112
28200
MA = 112
13254
Ha = 225
309 n
mi
Hp = 217
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12841995
37 X = 3863148
48
Y = 7757846
14 feet Y = 2408077
72 meter
Z = 16452068
83 Z = 5033481
24
XDOT = -6136
141742 XDOT = -1941
153175
YDOT = 23555
338410 feet/sec YDOT = 7158
355989 meter/sec
ZDOT = -6273
268925 ZDOT = -1921
350722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4824757
99 X = 1470586
24
Y = 14115244
51 feet Y = 4302326
53 meter
Z = 16530371
24 Z = 5038457
15
XDOT = -18729
719222 XDOT = -5708
818419
YDOT = 13846
484569 feet/sec YDOT = 4220
408497 meter/sec
ZDOT = -6312
623963 ZDOT = -1924
087784
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
48843634
00016717 00000-0 10270-3 0 9111
2 25544 51
6480 273
2610 0012226 332
8107 27
2404 15
52599746 18296
Satellite: ISS
Catalog Number: 25544
Epoch time: 13062
48843634 = yrday
fracday
Element set: 911
Inclination: 51
6480 deg
RA of node: 273
2610 deg
Eccentricity:
0012226
Arg of perigee: 332
8107 deg
Mean anomaly: 27
2404 deg
Mean motion: 15
52599746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1829
Checksum: 301
Coasting Arc #13 (Orbit 1843)
---------------------------------------
Vector Time (GMT): 2013/063/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3759383
52 A = 6785053
96 meter
Y = -3394644
67 meter E =
0008896
Z = -4513970
96 I = 51
28499
XDOT = 2240
700650 Wp = 28
43507
YDOT = -6628
751797 meter/sec RA = 267
67078 deg
ZDOT = 3129
129004 TA = 273
06113
MA = 273
16292
Ha = 225
432 n
mi
Hp = 216
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12333935
44 X = -3699216
98
Y = -11137285
68 feet Y = -3436348
33 meter
Z = -14809616
01 Z = -4532087
23
XDOT = 7351
380085 XDOT = 2299
457872
YDOT = -21747
873349 feet/sec YDOT = -6603
366152 meter/sec
ZDOT = 10266
171272 ZDOT = 3140
157172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2561230
02 X = -780662
91
Y = -16351730
78 feet Y = -4984007
54 meter
Z = -14884583
42 Z = -4536821
02
XDOT = 18114
561428 XDOT = 5521
318323
YDOT = -12194
449747 feet/sec YDOT = -3716
868283 meter/sec
ZDOT = 10312
819641 ZDOT = 3143
347426
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
45393338
00016717 00000-0 10270-3 0 9121
2 25544 51
6471 268
4587 0012259 336
2799 23
7787 15
52601121 18449
Satellite: ISS
Catalog Number: 25544
Epoch time: 13063
45393338 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 268
4587 deg
Eccentricity:
0012259
Arg of perigee: 336
2799 deg
Mean anomaly: 23
7787 deg
Mean motion: 15
52601121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1844
Checksum: 324
Coasting Arc #14 (Orbit 1859)
---------------------------------------
Vector Time (GMT): 2013/064/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3595752
05 A = 6787575
38 meter
Y = 4367477
90 meter E =
0014855
Z = 3755568
60 I = 51
29637
XDOT = -2653
156451 Wp = 28
92882
YDOT = 5822
637538 meter/sec RA = 262
67026 deg
ZDOT = -4211
298504 TA = 105
94059
MA = 105
77686
Ha = 225
633 n
mi
Hp = 216
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11797086
77 X = 3528403
40
Y = 14328995
75 feet Y = 4407311
50 meter
Z = 12321419
29 Z = 3772872
42
XDOT = -8704
581533 XDOT = -2697
612114
YDOT = 19103
141528 feet/sec YDOT = 5792
719478 meter/sec
ZDOT = -13816
596141 ZDOT = -4224
295452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 473328
15 X = 144270
42
Y = 18506772
83 feet Y = 5640864
36 meter
Z = 12392903
97 Z = 3777357
13
XDOT = -17171
571136 XDOT = -5233
894882
YDOT = 9771
233217 feet/sec YDOT = 2978
271885 meter/sec
ZDOT = -13871
337172 ZDOT = -4227
983570
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
48377896
00016717 00000-0 10270-3 0 9137
2 25544 51
6473 263
3369 0012441 339
9477 20
1185 15
52659578 18609
Satellite: ISS
Catalog Number: 25544
Epoch time: 13064
48377896 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 263
3369 deg
Eccentricity:
0012441
Arg of perigee: 339
9477 deg
Mean anomaly: 20
1185 deg
Mean motion: 15
52659578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1860
Checksum: 340
Coasting Arc #15 (Orbit 1874)
---------------------------------------
Vector Time (GMT): 2013/065/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3431644
03 A = 6790250
61 meter
Y = -5125799
89 meter E =
0014046
Z = -2819706
59 I = 51
30846
XDOT = 3095
642179 Wp = 2
30722
YDOT = -4853
231262 meter/sec RA = 257
67410 deg
ZDOT = 5069
634999 TA = 325
50860
MA = 325
59967
Ha = 225
717 n
mi
Hp = 216
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11258674
64 X = -3360374
04
Y = -16816928
79 feet Y = -5163776
37 meter
Z = -9251005
86 Z = -2836203
53
XDOT = 10156
306361 XDOT = 3125
055437
YDOT = -15922
674743 feet/sec YDOT = -4818
449080 meter/sec
ZDOT = 16632
660759 ZDOT = 5084
744849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1115450
88 X = 339989
43
Y = -20175699
61 feet Y = -6149553
24 meter
Z = -9319059
64 Z = -2840449
38
XDOT = 16119
880498 XDOT = 4913
339576
YDOT = -6798
569849 feet/sec YDOT = -2072
204090 meter/sec
ZDOT = 16696
077482 ZDOT = 5088
964416
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
44924608
00016717 00000-0 10270-3 0 9144
2 25544 51
6458 258
5342 0012369 343
2219 16
8522 15
52635468 18755
Satellite: ISS
Catalog Number: 25544
Epoch time: 13065
44924608 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 258
5342 deg
Eccentricity:
0012369
Arg of perigee: 343
2219 deg
Mean anomaly: 16
8522 deg
Mean motion: 15
52635468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1875
Checksum: 323
Coasting Arc #16 (Orbit 1890)
---------------------------------------
Vector Time (GMT): 2013/066/10:38:36
861
Vector Time (MET): N/A
Weight (LBS) : 906332
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3213324
06 A = 6792243
95 meter
Y = 5740318
29 meter E =
0011604
Z = 1697908
55 I = 51
32312
XDOT = -3594
890603 Wp = 57
75255
YDOT = 3697
349200 meter/sec RA = 252
68422 deg
ZDOT = -5662
087282 TA = 103
57745
MA = 103
44817
Ha = 225
917 n
mi
Hp = 215
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10542401
76 X = 3140647
95
Y = 18833065
25 feet Y = 5775845
47 meter
Z = 5570566
12 Z = 1713341
33
XDOT = -11794
260509 XDOT = -3608
463604
YDOT = 12130
410761 feet/sec YDOT = 3657
072551 meter/sec
ZDOT = -18576
401845 ZDOT = -5679
583851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2510927
38 X = -765330
67
Y = 21419839
39 feet Y = 6528767
05 meter
Z = 5634138
15 Z = 1717285
31
XDOT = -15008
213434 XDOT = -4574
503455
YDOT = 3175
648853 feet/sec YDOT = 967
937770 meter/sec
ZDOT = -18649
615953 ZDOT = -5684
402942
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
47905951
00016717 00000-0 10270-3 0 9159
2 25544 51
6457 253
4121 0012515 347
3040 12
7795 15
52696974 18917
Satellite: ISS
Catalog Number: 25544
Epoch time: 13066
47905951 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 253
4121 deg
Eccentricity:
0012515
Arg of perigee: 347
3040 deg
Mean anomaly: 12
7795 deg
Mean motion: 15
52696974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1891
Checksum: 320
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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