[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 23rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10010 44 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 2836)
---------------------------------------
Vector Time (GMT): 2012/235/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -703405
75 A = 6791642
81 meter
Y = 4793865
63 meter E =
0013295
Z = -4760686
42 I = 51
80792
XDOT = -6956
852734 Wp = 33
37219
YDOT = 1677
439076 meter/sec RA = 148
96943 deg
ZDOT = 2731
465654 TA = 263
53470
MA = 263
68609
Ha = 230
963 n
mi
Hp = 219
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2307761
63 X = -733833
17
Y = 15727905
60 feet Y = 4785829
41 meter
Z = -15619049
92 Z = -4764177
59
XDOT = -22824
319995 XDOT = -6988
361969
YDOT = 5503
409042 feet/sec YDOT = 1599
467133 meter/sec
ZDOT = 8961
501488 ZDOT = 2697
593060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12530014
67 X = -3819148
47
Y = -9758501
04 feet Y = -2974391
12 meter
Z = -15633869
92 Z = -4765203
55
XDOT = 5923
745600 XDOT = 1805
557659
YDOT = -21662
855650 feet/sec YDOT = -6602
838402 meter/sec
ZDOT = 8821
381530 ZDOT = 2688
757090
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 12235
75984698
00016717 00000-0 10270-3 0 9006
2 25544 51
6429 149
9749 0015087 347
4287 12
6485 15
50044182 28374
Satellite: ISS
Catalog Number: 25544
Epoch time: 12235
75984698 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 149
9749 deg
Eccentricity:
0015087
Arg of perigee: 347
4287 deg
Mean anomaly: 12
6485 deg
Mean motion: 15
50044182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2837
Checksum: 344
Coasting Arc #2 (Orbit 2852)
---------------------------------------
Vector Time (GMT): 2012/236/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 730175
71 A = 6792402
03 meter
Y = -4972180
01 meter E =
0019131
Z = 4574257
88 I = 51
83575
XDOT = 6742
863052 Wp = 16
96768
YDOT = -1882
460758 meter/sec RA = 144
02570 deg
ZDOT = -3101
450885 TA = 104
14764
MA = 103
93499
Ha = 231
089 n
mi
Hp = 219
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2395589
60 X = 763500
72
Y = -16312926
53 feet Y = -4963828
34 meter
Z = 15007407
73 Z = 4577886
04
XDOT = 22122
254109 XDOT = 6778
478086
YDOT = -6176
052355 feet/sec YDOT = -1806
858772 meter/sec
ZDOT = -10175
363795 ZDOT = -3068
607902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13163842
92 X = 4012339
32
Y = 9904591
15 feet Y = 3018919
38 meter
Z = 15022816
71 Z = 4578954
53
XDOT = -4599
023473 XDOT = -1401
782355
YDOT = 21444
739870 feet/sec YDOT = 6536
356712 meter/sec
ZDOT = -10039
466234 ZDOT = -3060
029308
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 12236
79139215
00016717 00000-0 10270-3 0 9019
2 25544 51
6428 144
8638 0015102 350
8923 9
1951 15
50042494 28538
Satellite: ISS
Catalog Number: 25544
Epoch time: 12236
79139215 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 144
8638 deg
Eccentricity:
0015102
Arg of perigee: 350
8923 deg
Mean anomaly: 9
1951 deg
Mean motion: 15
50042494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2853
Checksum: 301
Coasting Arc #3 (Orbit 2867)
---------------------------------------
Vector Time (GMT): 2012/237/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -656472
78 A = 6792978
76 meter
Y = 5136441
23 meter E =
0013755
Z = -4395796
50 I = 51
86188
XDOT = -6523
220997 Wp = 31
30220
YDOT = 2088
754357 meter/sec RA = 139
08356 deg
ZDOT = 3431
125441 TA = 273
33050
MA = 273
48785
Ha = 231
199 n
mi
Hp = 218
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2153782
08 X = -692507
05
Y = 16851841
29 feet Y = 5128898
68 meter
Z = -14421904
52 Z = -4399073
10
XDOT = -21401
643690 XDOT = -6562
760614
YDOT = 6852
868625 feet/sec YDOT = 2015
586546 meter/sec
ZDOT = 11256
973231 ZDOT = 3399
340042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13920021
62 X = -4242822
59
Y = -9718690
99 feet Y = -2962257
01 meter
Z = -14435882
57 Z = -4400057
01
XDOT = 3293
916605 XDOT = 1003
985781
YDOT = -21164
112840 feet/sec YDOT = -6450
821594 meter/sec
ZDOT = 11125
412218 ZDOT = 3391
025644
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 12237
75845770
00016717 00000-0 10270-3 0 9027
2 25544 51
6428 140
0715 0014992 355
0226 5
0774 15
50069103 28681
Satellite: ISS
Catalog Number: 25544
Epoch time: 12237
75845770 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 140
0715 deg
Eccentricity:
0014992
Arg of perigee: 355
0226 deg
Mean anomaly: 5
0774 deg
Mean motion: 15
50069103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2868
Checksum: 302
Coasting Arc #4 (Orbit 2883)
---------------------------------------
Vector Time (GMT): 2012/238/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 635113
34 A = 6793868
14 meter
Y = -5338024
72 meter E =
0019999
Z = 4158157
02 I = 51
88682
XDOT = 6280
624339 Wp = 29
01956
YDOT = -2215
271635 meter/sec RA = 134
14354 deg
ZDOT = -3778
485638 TA = 99
93601
MA = 99
71022
Ha = 231
318 n
mi
Hp = 218
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2083705
20 X = 674557
82
Y = -17513204
48 feet Y = -5330702
00 meter
Z = 13642247
44 Z = 4161338
09
XDOT = 20605
722897 XDOT = 6323
284045
YDOT = -7267
951560 feet/sec YDOT = -2144
799213 meter/sec
ZDOT = -12396
606425 ZDOT = -3747
871321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14704328
67 X = 4481879
38
Y = 9719331
56 feet Y = 2962452
26 meter
Z = 13655855
38 Z = 4162304
72
XDOT = -2184
158259 XDOT = -665
731437
YDOT = 20657
365747 feet/sec YDOT = 6296
365080 meter/sec
ZDOT = -12269
857866 ZDOT = -3739
852678
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 12238
78998458
00016717 00000-0 10270-3 0 9034
2 25544 51
6426 134
9601 0015003 358
5479 1
5625 15
50066308 28845
Satellite: ISS
Catalog Number: 25544
Epoch time: 12238
78998458 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 134
9601 deg
Eccentricity:
0015003
Arg of perigee: 358
5479 deg
Mean anomaly: 1
5625 deg
Mean motion: 15
50066308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2884
Checksum: 323
Coasting Arc #5 (Orbit 2898)
---------------------------------------
Vector Time (GMT): 2012/239/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -511206
59 A = 6794512
15 meter
Y = 5510061
81 meter E =
0014816
Z = -3938304
71 I = 51
91083
XDOT = -6043
898973 Wp = 28
65109
YDOT = 2344
817669 meter/sec RA = 129
20573 deg
ZDOT = 4084
140948 TA = 283
89604
MA = 284
06081
Ha = 231
417 n
mi
Hp = 218
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1677186
99 X = -553652
11
Y = 18077630
60 feet Y = 5504107
88 meter
Z = -12920947
22 Z = -3940891
15
XDOT = -19829
064871 XDOT = -6089
509584
YDOT = 7692
971355 feet/sec YDOT = 2276
975972 meter/sec
ZDOT = 13399
412558 ZDOT = 4054
669582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15552879
09 X = -4740517
55
Y = -9350552
99 feet Y = -2850048
55 meter
Z = -12932117
86 Z = -3941709
52
XDOT = 1117
345564 XDOT = 340
566928
YDOT = -20135
385091 feet/sec YDOT = -6137
265376 meter/sec
ZDOT = 13277
361447 ZDOT = 4046
939769
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 12239
75703288
00016717 00000-0 10270-3 0 9048
2 25544 51
6437 130
1684 0014938 2
6152 357
5075 15
50095641 28998
Satellite: ISS
Catalog Number: 25544
Epoch time: 12239
75703288 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 130
1684 deg
Eccentricity:
0014938
Arg of perigee: 2
6152 deg
Mean anomaly: 357
5075 deg
Mean motion: 15
50095641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2899
Checksum: 320
Coasting Arc #6 (Orbit 2914)
---------------------------------------
Vector Time (GMT): 2012/240/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 435349
79 A = 6795465
31 meter
Y = -5716786
67 meter E =
0020667
Z = 3650714
52 I = 51
93184
XDOT = 5795
170923 Wp = 40
68473
YDOT = -2386
560479 meter/sec RA = 124
26926 deg
ZDOT = -4398
987378 TA = 96
29672
MA = 96
06128
Ha = 231
524 n
mi
Hp = 218
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1428312
97 X = 481509
68
Y = -18755861
77 feet Y = -5711660
19 meter
Z = 11977409
83 Z = 3652941
55
XDOT = 19013
027964 XDOT = 5842
796149
YDOT = -7829
922831 feet/sec YDOT = -2321
489016 meter/sec
ZDOT = -14432
373286 ZDOT = -4370
719484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16428927
83 X = 5007537
20
Y = 9147684
48 feet Y = 2788214
23 meter
Z = 11987116
99 Z = 3653673
26
XDOT = -299
909819 XDOT = -91
412513
YDOT = 19423
187440 feet/sec YDOT = 5920
187532 meter/sec
ZDOT = -14315
280207 ZDOT = -4363
297407
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 12240
78854169
00016717 00000-0 10270-3 0 9059
2 25544 51
6432 125
0568 0014941 6
1924 353
9409 15
50093140 29159
Satellite: ISS
Catalog Number: 25544
Epoch time: 12240
78854169 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 125
0568 deg
Eccentricity:
0014941
Arg of perigee: 6
1924 deg
Mean anomaly: 353
9409 deg
Mean motion: 15
50093140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2915
Checksum: 302
Coasting Arc #7 (Orbit 2929)
---------------------------------------
Vector Time (GMT): 2012/241/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -259335
46 A = 6796132
85 meter
Y = 5878660
42 meter E =
0016555
Z = -3391115
64 I = 51
95216
XDOT = -5564
144049 Wp = 26
87178
YDOT = 2436
539204 meter/sec RA = 119
33532 deg
ZDOT = 4672
611368 TA = 293
77870
MA = 293
95222
Ha = 231
624 n
mi
Hp = 218
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -850838
11 X = -308579
62
Y = 19286943
63 feet Y = 5875484
93 meter
Z = -11125707
47 Z = -3392495
24
XDOT = -18255
065779 XDOT = -5613
674452
YDOT = 7993
895025 feet/sec YDOT = 2374
040680 meter/sec
ZDOT = 15330
089790 ZDOT = 4645
461149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17301779
71 X = -5273582
46
Y = -8556873
71 feet Y = -2608135
11 meter
Z = -11131927
85 Z = -3393011
61
XDOT = -467
663859 XDOT = -142
543944
YDOT = -18752
368743 feet/sec YDOT = -5715
721993 meter/sec
ZDOT = 15217
602596 ZDOT = 4638
325271
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 12241
75557271
00016717 00000-0 10270-3 0 9062
2 25544 51
6448 120
2657 0014940 10
0439 350
1007 15
50121925 29309
Satellite: ISS
Catalog Number: 25544
Epoch time: 12241
75557271 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 120
2657 deg
Eccentricity:
0014940
Arg of perigee: 10
0439 deg
Mean anomaly: 350
1007 deg
Mean motion: 15
50121925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2930
Checksum: 275
Coasting Arc #8 (Orbit 2945)
---------------------------------------
Vector Time (GMT): 2012/242/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 128939
86 A = 6797062
03 meter
Y = -6070736
18 meter E =
0021053
Z = 3056360
83 I = 51
96843
XDOT = 5333
303330 Wp = 51
61015
YDOT = -2394
264648 meter/sec RA = 114
40184 deg
ZDOT = -4944
849398 TA = 93
58389
MA = 93
34310
Ha = 231
708 n
mi
Hp = 217
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 423031
04 X = 181967
68
Y = -19917113
45 feet Y = -6068997
64 meter
Z = 10027430
55 Z = 3057116
33
XDOT = 17497
714336 XDOT = 5383
700614
YDOT = -7855
198977 feet/sec YDOT = -2334
342805 meter/sec
ZDOT = -16223
259181 ZDOT = -4918
818410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18191093
80 X = 5544645
39
Y = 8116715
61 feet Y = 2473974
92 meter
Z = 10031089
70 Z = 3057476
14
XDOT = 946
089775 XDOT = 288
368163
YDOT = 17940
992268 feet/sec YDOT = 5468
414443 meter/sec
ZDOT = -16115
395626 ZDOT = -4911
972587
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 12242
78706338
00016717 00000-0 10270-3 0 9077
2 25544 51
6440 115
1539 0014928 13
6555 346
4997 15
50123485 29463
Satellite: ISS
Catalog Number: 25544
Epoch time: 12242
78706338 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 115
1539 deg
Eccentricity:
0014928
Arg of perigee: 13
6555 deg
Mean anomaly: 346
4997 deg
Mean motion: 15
50123485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2946
Checksum: 324
Coasting Arc #9 (Orbit 2960)
---------------------------------------
Vector Time (GMT): 2012/243/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 94945
68 A = 6797707
82 meter
Y = 6204084
71 meter E =
0018859
Z = -2759835
60 I = 51
98368
XDOT = -5131
149469 Wp = 26
98234
YDOT = 2368
677035 meter/sec RA = 109
47065 deg
ZDOT = 5178
386136 TA = 301
96364
MA = 302
14685
Ha = 231
820 n
mi
Hp = 217
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 311501
56 X = 38969
69
Y = 20354608
62 feet Y = 6204833
27 meter
Z = -9054578
75 Z = -2759510
79
XDOT = -16834
479886 XDOT = -5182
410154
YDOT = 7771
250114 feet/sec YDOT = 2311
011091 meter/sec
ZDOT = 16989
455826 ZDOT = 5153
334986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19006823
56 X = -5793279
82
Y = -7291238
00 feet Y = -2222369
34 meter
Z = -9053785
28 Z = -2759593
75
XDOT = -1386
390716 XDOT = -422
571890
YDOT = -17230
613327 feet/sec YDOT = -5251
890942 meter/sec
ZDOT = 16885
640584 ZDOT = 5146
743250
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 12243
75407700
00016717 00000-0 10270-3 0 9087
2 25544 51
6452 110
3629 0014992 17
2271 342
9386 15
50146219 29619
Satellite: ISS
Catalog Number: 25544
Epoch time: 12243
75407700 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 110
3629 deg
Eccentricity:
0014992
Arg of perigee: 17
2271 deg
Mean anomaly: 342
9386 deg
Mean motion: 15
50146219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2961
Checksum: 300
Coasting Arc #10 (Orbit 2976)
---------------------------------------
Vector Time (GMT): 2012/244/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -273150
05 A = 6798515
14 meter
Y = -6362118
32 meter E =
0021075
Z = 2382297
21 I = 51
99489
XDOT = 4941
447104 Wp = 61
50786
YDOT = -2250
679094 meter/sec RA = 104
53951 deg
ZDOT = -5398
018104 TA = 92
08921
MA = 91
84785
Ha = 231
871 n
mi
Hp = 217
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -896161
57 X = -213559
73
Y = -20873091
62 feet Y = -6364839
46 meter
Z = 7815935
73 Z = 2381115
59
XDOT = 16212
096798 XDOT = 4992
469408
YDOT = -7384
117763 feet/sec YDOT = -2195
135953 meter/sec
ZDOT = -17710
033150 ZDOT = -5373
888972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19820565
89 X = 6041308
48
Y = 6610726
76 feet Y = 2014949
52 meter
Z = 7811617
62 Z = 2380981
05
XDOT = 1517
380280 XDOT = 462
497509
YDOT = 16438
096944 feet/sec YDOT = 5010
331949 meter/sec
ZDOT = -17610
037045 ZDOT = -5367
539291
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 12244
78554924
00016717 00000-0 10270-3 0 9093
2 25544 51
6445 105
2509 0014957 20
9004 339
2755 15
50156076 29775
Satellite: ISS
Catalog Number: 25544
Epoch time: 12244
78554924 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 105
2509 deg
Eccentricity:
0014957
Arg of perigee: 20
9004 deg
Mean anomaly: 339
2755 deg
Mean motion: 15
50156076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2977
Checksum: 322
Coasting Arc #11 (Orbit 2991)
---------------------------------------
Vector Time (GMT): 2012/245/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 534506
96 A = 6799086
71 meter
Y = 6450109
21 meter E =
0021478
Z = -2053087
78 I = 52
00447
XDOT = -4789
457651 Wp = 29
30273
YDOT = 2160
505200 meter/sec RA = 99
60997 deg
ZDOT = 5583
455773 TA = 308
13508
MA = 308
32847
Ha = 232
005 n
mi
Hp = 217
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1753631
77 X = 472314
13
Y = 21161775
62 feet Y = 6455738
46 meter
Z = -6735852
28 Z = -2050642
89
XDOT = -15713
443737 XDOT = -4840
383825
YDOT = 7088
271652 feet/sec YDOT = 2106
662304 meter/sec
ZDOT = 18318
424451 ZDOT = 5560
065111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20494289
11 X = -6246659
32
Y = -5568514
50 feet Y = -1697283
22 meter
Z = -6726324
27 Z = -2050183
64
XDOT = -1640
632971 XDOT = -500
064930
YDOT = -15802
175189 feet/sec YDOT = -4816
502997 meter/sec
ZDOT = 18221
486840 ZDOT = 5553
909189
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 12245
75254543
00016717 00000-0 10270-3 0 9107
2 25544 51
6454 100
4595 0015084 24
2313 335
9544 15
50168328 29928
Satellite: ISS
Catalog Number: 25544
Epoch time: 12245
75254543 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 100
4595 deg
Eccentricity:
0015084
Arg of perigee: 24
2313 deg
Mean anomaly: 335
9544 deg
Mean motion: 15
50168328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2992
Checksum: 299
Coasting Arc #12 (Orbit 3007)
---------------------------------------
Vector Time (GMT): 2012/246/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -747346
15 A = 6799680
80 meter
Y = -6557280
33 meter E =
0020707
Z = 1638859
94 I = 52
01041
XDOT = 4660
910937 Wp = 70
08400
YDOT = -1982
463193 meter/sec RA = 94
68063 deg
ZDOT = -5740
888920 TA = 92
11009
MA = 91
87295
Ha = 232
020 n
mi
Hp = 216
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2451923
08 X = -681926
92
Y = -21513386
92 feet Y = -6565271
68 meter
Z = 5376837
09 Z = 1635388
95
XDOT = 15291
702548 XDOT = 4710
620645
YDOT = -6504
144333 feet/sec YDOT = -1930
064613 meter/sec
ZDOT = -18834
937403 ZDOT = -5718
125601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21144801
92 X = 6444935
63
Y = 4677905
80 feet Y = 1425825
69 meter
Z = 5363083
97 Z = 1634667
99
XDOT = 1457
680079 XDOT = 444
300888
YDOT = 15144
554213 feet/sec YDOT = 4616
060124 meter/sec
ZDOT = -18740
607049 ZDOT = -5712
137029
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 12246
78399908
00016717 00000-0 10270-3 0 9117
2 25544 51
6451 95
3474 0015018 28
0400 332
1557 15
50188203 30085
Satellite: ISS
Catalog Number: 25544
Epoch time: 12246
78399908 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 95
3474 deg
Eccentricity:
0015018
Arg of perigee: 28
0400 deg
Mean anomaly: 332
1557 deg
Mean motion: 15
50188203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3008
Checksum: 296
Coasting Arc #13 (Orbit 3022)
---------------------------------------
Vector Time (GMT): 2012/247/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1030219
15 A = 6800113
21 meter
Y = 6586659
86 meter E =
0024098
Z = -1282772
00 I = 52
01419
XDOT = -4576
218918 Wp = 33
67876
YDOT = 1845
023148 meter/sec RA = 89
75200 deg
ZDOT = 5870
454976 TA = 312
45053
MA = 312
65404
Ha = 232
174 n
mi
Hp = 216
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3379984
10 X = 962720
60
Y = 21609776
43 feet Y = 6597802
88 meter
Z = -4208569
55 Z = -1277931
82
XDOT = -15013
841596 XDOT = -4625
027536
YDOT = 6053
225551 feet/sec YDOT = 1793
576665 meter/sec
ZDOT = 19260
022887 ZDOT = 5848
105220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21599599
67 X = -6583557
98
Y = -3467990
91 feet Y = -1057043
63 meter
Z = -4189167
10 Z = -1276858
13
XDOT = -1313
095373 XDOT = -400
231470
YDOT = -14688
134382 feet/sec YDOT = -4476
943360 meter/sec
ZDOT = 19167
412024 ZDOT = 5842
227185
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 12247
75097789
00016717 00000-0 10270-3 0 9128
2 25544 51
6459 90
5558 0015197 31
2139 328
9911 15
50190361 30238
Satellite: ISS
Catalog Number: 25544
Epoch time: 12247
75097789 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 90
5558 deg
Eccentricity:
0015197
Arg of perigee: 31
2139 deg
Mean anomaly: 328
9911 deg
Mean motion: 15
50190361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3023
Checksum: 320
Coasting Arc #14 (Orbit 3038)
---------------------------------------
Vector Time (GMT): 2012/248/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1259093
72 A = 6800424
51 meter
Y = -6630842
50 meter E =
0019984
Z = 839734
06 I = 52
01428
XDOT = 4523
180536 Wp = 76
91227
YDOT = -1628
927770 meter/sec RA = 84
82383 deg
ZDOT = -5956
956736 TA = 94
07526
MA = 93
84681
Ha = 232
157 n
mi
Hp = 216
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4130884
92 X = -1188931
93
Y = -21754732
60 feet Y = -6644530
10 meter
Z = 2755033
00 Z = 833788
40
XDOT = 14839
831155 XDOT = 4569
996944
YDOT = -5344
251215 feet/sec YDOT = -1578
085475 meter/sec
ZDOT = -19543
821313 ZDOT = -5934
869465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22012776
41 X = 6709494
25
Y = 2429344
57 feet Y = 740464
22 meter
Z = 2731074
37 Z = 832431
47
XDOT = 889
936687 XDOT = 271
252702
YDOT = 14264
334598 feet/sec YDOT = 4347
769185 meter/sec
ZDOT = -19452
312563 ZDOT = -5929
064869
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 12248
78241293
00016717 00000-0 10270-3 0 9134
2 25544 51
6458 85
4440 0015101 35
1765 325
0379 15
50217647 30393
Satellite: ISS
Catalog Number: 25544
Epoch time: 12248
78241293 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 85
4440 deg
Eccentricity:
0015101
Arg of perigee: 35
1765 deg
Mean anomaly: 325
0379 deg
Mean motion: 15
50217647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3039
Checksum: 301
Coasting Arc #15 (Orbit 3053)
---------------------------------------
Vector Time (GMT): 2012/249/17:57:49
979
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1543179
25 A = 6800645
24 meter
Y = 6593807
32 meter E =
0026404
Z = -464040
72 I = 52
01214
XDOT = -4516
760577 Wp = 39
72730
YDOT = 1466
340437 meter/sec RA = 79
89542 deg
ZDOT = 6023
430287 TA = 315
29661
MA = 315
50915
Ha = 232
313 n
mi
Hp = 216
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5062924
04 X = 1471585
44
Y = 21633226
11 feet Y = 6610663
78 meter
Z = -1522443
31 Z = -456718
37
XDOT = -14818
768296 XDOT = -4562
082318
YDOT = 4810
828206 feet/sec YDOT = 1415
578215 meter/sec
ZDOT = 19761
910389 ZDOT = 6001
377846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22191116
26 X = -6763852
23
Y = -1128457
07 feet Y = -343953
72 meter
Z = -1492799
18 Z = -455005
19
XDOT = -560
948984 XDOT = -170
977250
YDOT = -14069
791253 feet/sec YDOT = -4288
472374 meter/sec
ZDOT = 19670
557279 ZDOT = 5995
585858
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 12249
74937422
00016717 00000-0 10270-3 0 9148
2 25544 51
6467 80
6523 0015301 38
2558 321
9675 15
50215677 30540
Satellite: ISS
Catalog Number: 25544
Epoch time: 12249
74937422 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 80
6523 deg
Eccentricity:
0015301
Arg of perigee: 38
2558 deg
Mean anomaly: 321
9675 deg
Mean motion: 15
50215677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3054
Checksum: 312
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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