[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 23rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
358/11:30:02
461 -1
1 1
7 1
7
N/A -1
0 -0
2 230
6
000/00:04:04
922 -0
9 0
1 212
6
Coasting Arc #1 (Orbit 717)
---------------------------------------
Vector Time (GMT): 2012/356/22:12:50
344
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 616448
44 A = 6795418
79 meter
Y = 6746248
71 meter E =
0026080
Z = 488683
59 I = 51
31518
XDOT = -4741
096429 Wp = 95
82619
YDOT = 884
293831 meter/sec RA = 268
09035 deg
ZDOT = -5954
583663 TA = 78
88514
MA = 78
59201
Ha = 230
486 n
mi
Hp = 211
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2022468
65 X = 538590
74
Y = 22133361
92 feet Y = 6752706
87 meter
Z = 1603292
63 Z = 491489
57
XDOT = -15554
778311 XDOT = -4721
706350
YDOT = 2901
226479 feet/sec YDOT = 831
384700 meter/sec
ZDOT = -19536
035639 ZDOT = -5977
568582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20674883
69 X = 6301704
55
Y = 8154171
56 feet Y = 2485391
49 meter
Z = 1614096
34 Z = 491976
56
XDOT = -3754
990019 XDOT = -1144
520958
YDOT = 13582
484510 feet/sec YDOT = 4139
941279 meter/sec
ZDOT = -19631
458198 ZDOT = -5983
668459
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 12356
95883062
00016717 00000-0 10270-3 0 9005
2 25544 51
6477 268
7425 0016944 70
7987 289
4996 15
52000586 7183
Satellite: ISS
Catalog Number: 25544
Epoch time: 12356
95883062 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 268
7425 deg
Eccentricity:
0016944
Arg of perigee: 70
7987 deg
Mean anomaly: 289
4996 deg
Mean motion: 15
52000586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 718
Checksum: 352
Coasting Arc #2 (Orbit 733)
---------------------------------------
Vector Time (GMT): 2012/357/22:12:50
344
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -435374
52 A = 6795386
49 meter
Y = -6754511
06 meter E =
0029288
Z = 472637
97 I = 51
31816
XDOT = 4823
765940 Wp = 63
83792
YDOT = 125
556469 meter/sec RA = 263
10709 deg
ZDOT = 5962
589438 TA = 301
28166
MA = 301
56816
Ha = 230
494 n
mi
Hp = 211
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1428394
10 X = -362107
77
Y = -22160469
36 feet Y = -6758970
07 meter
Z = 1550649
52 Z = 470700
40
XDOT = 15826
003741 XDOT = 4793
038441
YDOT = 411
930673 feet/sec YDOT = 179
326590 meter/sec
ZDOT = 19562
301306 ZDOT = 5985
948509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20586775
68 X = -6274849
23
Y = -8326684
78 feet Y = -2537973
52 meter
Z = 1543442
15 Z = 470441
17
XDOT = 6584
443151 XDOT = 2006
938272
YDOT = -12467
099894 feet/sec YDOT = -3799
972048 meter/sec
ZDOT = 19659
155259 ZDOT = 5992
110523
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 12357
98906898
00016717 00000-0 10270-3 0 9013
2 25544 51
6486 263
6240 0017026 74
3275 285
9754 15
52017706 7347
Satellite: ISS
Catalog Number: 25544
Epoch time: 12357
98906898 = yrday
fracday
Element set: 901
Inclination: 51
6486 deg
RA of node: 263
6240 deg
Eccentricity:
0017026
Arg of perigee: 74
3275 deg
Mean anomaly: 285
9754 deg
Mean motion: 15
52017706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 734
Checksum: 334
Coasting Arc #3 (Orbit 741)
---------------------------------------
Vector Time (GMT): 2012/358/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2401278
45 A = 6789547
19 meter
Y = 4958879
17 meter E =
0022946
Z = -3991216
06 I = 51
29803
XDOT = -4073
928043 Wp = 75
80612
YDOT = -5132
993084 meter/sec RA = 260
35971 deg
ZDOT = -3940
073484 TA = 152
93349
MA = 152
81366
Ha = 230
622 n
mi
Hp = 212
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7878210
14 X = -2437162
74
Y = 16269288
63 feet Y = 4931826
26 meter
Z = -13094540
87 Z = -4002968
14
XDOT = -13365
905653 XDOT = -3997
087015
YDOT = -16840
528492 feet/sec YDOT = -5178
120331 meter/sec
ZDOT = -12926
750274 ZDOT = -3959
678269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15466141
19 X = -4714079
84
Y = -9287612
63 feet Y = -2830864
33 meter
Z = -13143883
60 Z = -4006255
72
XDOT = 17335
016855 XDOT = 5283
713137
YDOT = -10521
926076 feet/sec YDOT = -3207
083068 meter/sec
ZDOT = -13007
426455 ZDOT = -3964
663583
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 12358
50418469
00016717 00000-0 10270-3 0 9025
2 25544 51
6485 261
0677 0016063 77
2199 283
0747 15
51731238 7421
Satellite: ISS
Catalog Number: 25544
Epoch time: 12358
50418469 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 261
0677 deg
Eccentricity:
0016063
Arg of perigee: 77
2199 deg
Mean anomaly: 283
0747 deg
Mean motion: 15
51731238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 742
Checksum: 320
Coasting Arc #4 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2012/359/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2595840
32 A = 6787593
01 meter
Y = -4343054
82 meter E =
0023988
Z = 4504118
52 I = 51
29732
XDOT = 4080
876163 Wp = 92
15275
YDOT = 5701
507073 meter/sec RA = 255
36681 deg
ZDOT = 3130
362341 TA = 326
27811
MA = 326
43049
Ha = 230
533 n
mi
Hp = 212
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8516536
48 X = 2622332
32
Y = -14248867
52 feet Y = -4313878
82 meter
Z = 14777291
74 Z = 4516792
95
XDOT = 13388
701321 XDOT = 4001
610795
YDOT = 18705
731867 feet/sec YDOT = 5746
698485 meter/sec
ZDOT = 10270
217654 ZDOT = 3149
995098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13560919
95 X = 4133368
40
Y = 9491633
68 feet Y = 2893049
94 meter
Z = 14830384
70 Z = 4520301
26
XDOT = -18979
617656 XDOT = -5784
987462
YDOT = 10865
186406 feet/sec YDOT = 3311
708817 meter/sec
ZDOT = 10350
950434 ZDOT = 3154
969692
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 12359
53460943
00016717 00000-0 10270-3 0 9034
2 25544 51
6481 255
9500 0016019 81
1497 279
1468 15
51743778 7585
Satellite: ISS
Catalog Number: 25544
Epoch time: 12359
53460943 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 255
9500 deg
Eccentricity:
0016019
Arg of perigee: 81
1497 deg
Mean anomaly: 279
1468 deg
Mean motion: 15
51743778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 758
Checksum: 333
Coasting Arc #5 (Orbit 772)
---------------------------------------
Vector Time (GMT): 2012/360/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2902686
72 A = 6785795
24 meter
Y = 3660337
96 meter E =
0028214
Z = -4947579
42 I = 51
30096
XDOT = -4029
311379 Wp = 79
91774
YDOT = -6121
262422 meter/sec RA = 250
37086 deg
ZDOT = -2170
496217 TA = 168
77545
MA = 168
71239
Ha = 230
535 n
mi
Hp = 212
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9523250
40 X = -2919367
45
Y = 12008982
79 feet Y = 3627785
56 meter
Z = -16232215
96 Z = -4961720
66
XDOT = -13219
525521 XDOT = -3950
018893
YDOT = -20082
881962 feet/sec YDOT = -6165
877119 meter/sec
ZDOT = -7121
050580 ZDOT = -2189
878479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11426880
71 X = -3482913
24
Y = -10119899
58 feet Y = -3084545
39 meter
Z = -16291311
51 Z = -4965591
75
XDOT = 20092
580430 XDOT = 6124
218515
YDOT = -11126
086918 feet/sec YDOT = -3391
231293 meter/sec
ZDOT = -7200
705483 ZDOT = -2194
775031
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 12360
50061715
00016717 00000-0 10270-3 0 9048
2 25544 51
6488 251
1517 0015977 84
3746 275
9227 15
51783158 7732
Satellite: ISS
Catalog Number: 25544
Epoch time: 12360
50061715 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 251
1517 deg
Eccentricity:
0015977
Arg of perigee: 84
3746 deg
Mean anomaly: 275
9227 deg
Mean motion: 15
51783158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 773
Checksum: 324
Coasting Arc #6 (Orbit 788)
---------------------------------------
Vector Time (GMT): 2012/361/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3220642
03 A = 6784567
88 meter
Y = -2936451
79 meter E =
0019270
Z = 5183167
41 I = 51
30795
XDOT = 3991
097712 Wp = 95
32122
YDOT = 6455
005417 meter/sec RA = 245
37383 deg
ZDOT = 1171
542079 TA = 343
37545
MA = 343
43854
Ha = 230
367 n
mi
Hp = 212
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10566410
87 X = 3228060
13
Y = -9634028
20 feet Y = -2900395
68 meter
Z = 17005142
42 Z = 5198830
76
XDOT = 13094
152597 XDOT = 3912
928789
YDOT = 21177
839294 feet/sec YDOT = 6499
199165 meter/sec
ZDOT = 3843
641991 ZDOT = 1190
741459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9182532
41 X = 2798835
88
Y = 10859034
83 feet Y = 3309833
82 meter
Z = 17070467
70 Z = 5203078
55
XDOT = -20919
184356 XDOT = -6376
167392
YDOT = 11494
939181 feet/sec YDOT = 3503
657462 meter/sec
ZDOT = 3922
512226 ZDOT = 1195
581726
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 12361
53100925
00016717 00000-0 10270-3 0 9050
2 25544 51
6484 246
0338 0015878 88
3113 271
9857 15
51809159 7896
Satellite: ISS
Catalog Number: 25544
Epoch time: 12361
53100925 = yrday
fracday
Element set: 905
Inclination: 51
6484 deg
RA of node: 246
0338 deg
Eccentricity:
0015878
Arg of perigee: 88
3113 deg
Mean anomaly: 271
9857 deg
Mean motion: 15
51809159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 789
Checksum: 330
Coasting Arc #7 (Orbit 803)
---------------------------------------
Vector Time (GMT): 2012/362/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3636557
32 A = 6784080
26 meter
Y = 2207033
74 meter E =
0030664
Z = -5311383
43 I = 51
32007
XDOT = -3850
917528 Wp = 90
46640
YDOT = -6599
641545 meter/sec RA = 240
37564 deg
ZDOT = -106
505944 TA = 178
51517
MA = 178
50605
Ha = 230
417 n
mi
Hp = 212
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11930962
33 X = -3635165
25
Y = 7240924
36 feet Y = 2166375
90 meter
Z = -17425798
64 Z = -5329045
89
XDOT = -12634
243859 XDOT = -3776
315359
YDOT = -21652
367275 feet/sec YDOT = -6642
287777 meter/sec
ZDOT = -349
428950 ZDOT = -125
032969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6941494
71 X = -2115767
59
Y = -12001093
24 feet Y = -3657933
22 meter
Z = -17499334
80 Z = -5333797
25
XDOT = 21086
599169 XDOT = 6427
195427
YDOT = -11579
862476 feet/sec YDOT = -3529
542083 meter/sec
ZDOT = -425
508732 ZDOT = -129
695061
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 12362
49698781
00016717 00000-0 10270-3 0 9069
2 25544 51
6484 241
2353 0015825 91
4904 268
8061 15
51827963 8048
Satellite: ISS
Catalog Number: 25544
Epoch time: 12362
49698781 = yrday
fracday
Element set: 906
Inclination: 51
6484 deg
RA of node: 241
2353 deg
Eccentricity:
0015825
Arg of perigee: 91
4904 deg
Mean anomaly: 268
8061 deg
Mean motion: 15
51827963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 804
Checksum: 331
Coasting Arc #8 (Orbit 819)
---------------------------------------
Vector Time (GMT): 2012/363/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4057746
18 A = 6784195
94 meter
Y = -1470992
53 meter E =
0018613
Z = 5218028
11 I = 51
33659
XDOT = 3668
749930 Wp = 88
90801
YDOT = 6676
377363 meter/sec RA = 235
37842 deg
ZDOT = -967
514838 TA = 10
39684
MA = 10
35840
Ha = 230
167 n
mi
Hp = 212
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13312815
54 X = 4048545
82
Y = -4826090
98 feet Y = -1425668
32 meter
Z = 17119514
78 Z = 5237717
72
XDOT = 12036
581135 XDOT = 3598
520518
YDOT = 21904
125207 feet/sec YDOT = 6717
011056 meter/sec
ZDOT = -3174
261281 ZDOT = -949
862229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4721336
81 X = 1439063
46
Y = 13244676
91 feet Y = 4036977
52 meter
Z = 17201381
06 Z = 5242980
95
XDOT = -21031
756454 XDOT = -6410
479367
YDOT = 11539
801096 feet/sec YDOT = 3517
331374 meter/sec
ZDOT = -3101
800994 ZDOT = -945
428943
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 12363
52734793
00016717 00000-0 10270-3 0 9079
2 25544 51
6480 236
1170 0015689 95
2407 265
0535 15
51875337 8203
Satellite: ISS
Catalog Number: 25544
Epoch time: 12363
52734793 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 236
1170 deg
Eccentricity:
0015689
Arg of perigee: 95
2407 deg
Mean anomaly: 265
0535 deg
Mean motion: 15
51875337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 820
Checksum: 316
Coasting Arc #9 (Orbit 834)
---------------------------------------
Vector Time (GMT): 2012/364/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4538885
97 A = 6785254
93 meter
Y = 794236
50 meter E =
0028416
Z = -5006681
54 I = 51
35761
XDOT = -3355
980031 Wp = 101
62406
YDOT = -6567
661119 meter/sec RA = 230
38272 deg
ZDOT = 2004
660287 TA = 187
97507
MA = 188
02035
Ha = 230
273 n
mi
Hp = 212
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14891358
17 X = -4523108
97
Y = 2605762
79 feet Y = 743568
57 meter
Z = -16426120
55 Z = -5028692
53
XDOT = -11010
433171 XDOT = -3292
027685
YDOT = -21547
444616 feet/sec YDOT = -6604
832418 meter/sec
ZDOT = 6576
969444 ZDOT = 1988
511969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2743125
47 X = -836104
64
Y = -14765020
75 feet Y = -4500378
32 meter
Z = -16517548
52 Z = -5034548
79
XDOT = 20365
727410 XDOT = 6207
473714
YDOT = -11052
173257 feet/sec YDOT = -3368
702409 meter/sec
ZDOT = 6510
720407 ZDOT = 1984
467580
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 12364
49329790
00016717 00000-0 10270-3 0 9084
2 25544 51
6475 231
3181 0015651 98
6013 261
6912 15
51869249 8357
Satellite: ISS
Catalog Number: 25544
Epoch time: 12364
49329790 = yrday
fracday
Element set: 908
Inclination: 51
6475 deg
RA of node: 231
3181 deg
Eccentricity:
0015651
Arg of perigee: 98
6013 deg
Mean anomaly: 261
6912 deg
Mean motion: 15
51869249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 835
Checksum: 325
Coasting Arc #10 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2012/365/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4995370
93 A = 6786728
11 meter
Y = -136675
13 meter E =
0022863
Z = 4572315
47 I = 51
38323
XDOT = 2947
552012 Wp = 89
61920
YDOT = 6417
512545 meter/sec RA = 225
39029 deg
ZDOT = -3015
224544 TA = 30
61683
MA = 30
48359
Ha = 229
999 n
mi
Hp = 212
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16389012
23 X = 4974317
08
Y = -448409
21 feet Y = -80931
88 meter
Z = 15001035
02 Z = 4596531
22
XDOT = 9670
446235 XDOT = 2890
218006
YDOT = 21054
831186 feet/sec YDOT = 6450
153609 meter/sec
ZDOT = -9892
468975 ZDOT = -3001
044398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 880243
69 X = 268298
28
Y = 16278829
80 feet Y = 4961787
32 meter
Z = 15101546
80 Z = 4602951
47
XDOT = -19601
002216 XDOT = -5974
385476
YDOT = 10222
983408 feet/sec YDOT = 3115
965343 meter/sec
ZDOT = -9834
352902 ZDOT = -2997
510765
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 12365
52362710
00016717 00000-0 10270-3 0 9099
2 25544 51
6473 226
1992 0015531 102
0703 258
2190 15
51929315 8519
Satellite: ISS
Catalog Number: 25544
Epoch time: 12365
52362710 = yrday
fracday
Element set: 909
Inclination: 51
6473 deg
RA of node: 226
1992 deg
Eccentricity:
0015531
Arg of perigee: 102
0703 deg
Mean anomaly: 258
2190 deg
Mean motion: 15
51929315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 292
Coasting Arc #11 (Orbit 865)
---------------------------------------
Vector Time (GMT): 2012/366/11:32:04
922
Vector Time (MET): N/A
Weight (LBS) : 903144
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5457308
68 A = 6788789
84 meter
Y = -410466
58 meter E =
0022718
Z = -4040919
66 I = 51
41115
XDOT = -2410
243265 Wp = 106
97430
YDOT = -6126
675414 meter/sec RA = 220
40171 deg
ZDOT = 3889
111354 TA = 203
56715
MA = 203
67140
Ha = 230
113 n
mi
Hp = 212
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17904556
02 X = -5432683
62
Y = -1346675
13 feet Y = -471355
66 meter
Z = -13257610
43 Z = -4067370
78
XDOT = -7907
622260 XDOT = -2360
446453
YDOT = -20100
641123 feet/sec YDOT = -6153
350102 meter/sec
ZDOT = 12759
551687 ZDOT = 3877
523233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 566307
28 X = 172610
46
Y = -17864606
66 feet Y = -5445132
11 meter
Z = -13367349
01 Z = -4074367
98
XDOT = 18428
234712 XDOT = 5616
925940
YDOT = -8899
270346 feet/sec YDOT = -2712
497602 meter/sec
ZDOT = 12712
144634 ZDOT = 3874
661684
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 12366
48954849
00016717 00000-0 10270-3 0 9107
2 25544 51
6464 221
3998 0015503 105
8185 254
4677 15
51911430 8669
Satellite: ISS
Catalog Number: 25544
Epoch time: 12366
48954849 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 221
3998 deg
Eccentricity:
0015503
Arg of perigee: 105
8185 deg
Mean anomaly: 254
4677 deg
Mean motion: 15
51911430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 866
Checksum: 330
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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