[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 1st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -261576
71 A = 6776219
21 meter
Y = 6704491
06 meter E =
0029462
Z = 794365
02 I = 52
00679
XDOT = -4736
635768 Wp = 16
64649
YDOT = -898
152807 meter/sec RA = 86
92822 deg
ZDOT = 5993
768755 TA = 351
93328
MA = 351
98056
Ha = 219
644 n
mi
Hp = 204
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -858191
30 X = -340387
03
Y = 21996361
76 feet Y = 6701125
28 meter
Z = 2606184
44 Z = 792903
04
XDOT = -15540
143596 XDOT = -4755
356425
YDOT = -2946
695561 feet/sec YDOT = -951
225606 meter/sec
ZDOT = 19664
595654 ZDOT = 5970
713180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17338353
28 X = -5284730
08
Y = 13564357
11 feet Y = 4134416
05 meter
Z = 2599681
12 Z = 792382
80
XDOT = -6895
571746 XDOT = -2101
770268
YDOT = -12581
841004 feet/sec YDOT = -3834
945138 meter/sec
ZDOT = 19570
139895 ZDOT = 5964
978640
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 12032
56259614
00016717 00000-0 10270-3 0 9003
2 25544 51
6403 87
3897 0020393 353
7577 6
3321 15
58562903 36713
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
56259614 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 87
3897 deg
Eccentricity:
0020393
Arg of perigee: 353
7577 deg
Mean anomaly: 6
3321 deg
Mean motion: 15
58562903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 310
Coasting Arc #2 (Orbit 3685)
---------------------------------------
Vector Time (GMT): 2012/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2143040
50 A = 6770586
06 meter
Y = -5291763
53 meter E =
0021577
Z = -3662601
18 I = 51
98673
XDOT = 4133
101580 Wp = 12
03065
YDOT = 4722
901867 meter/sec RA = 81
95074 deg
ZDOT = -4389
461584 TA = 211
23217
MA = 211
36055
Ha = 219
608 n
mi
Hp = 203
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7030972
77 X = 2219846
62
Y = -17361428
91 feet Y = -5267369
16 meter
Z = -12016408
06 Z = -3652004
16
XDOT = 13560
044553 XDOT = 4101
304670
YDOT = 15495
084865 feet/sec YDOT = 4768
943117 meter/sec
ZDOT = -14401
120684 ZDOT = -4369
460523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17732203
53 X = 5404775
64
Y = -6121672
49 feet Y = -1865885
77 meter
Z = -11972549
38 Z = -3649233
05
XDOT = -3080
200924 XDOT = -938
845242
YDOT = 19185
723654 feet/sec YDOT = 5847
808570 meter/sec
ZDOT = -14319
481444 ZDOT = -4364
577944
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 12033
52434226
00016717 00000-0 10270-3 0 9015
2 25544 51
6409 82
5625 0020226 357
4696 2
6353 15
58642261 36869
Satellite: ISS
Catalog Number: 25544
Epoch time: 12033
52434226 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 82
5625 deg
Eccentricity:
0020226
Arg of perigee: 357
4696 deg
Mean anomaly: 2
6353 deg
Mean motion: 15
58642261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3686
Checksum: 298
Coasting Arc #3 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2012/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3668153
59 A = 6764616
64 meter
Y = 2244351
21 meter E =
0018394
Z = 5215463
95 I = 51
96126
XDOT = -2633
541635 Wp = 11
59977
YDOT = -7111
554690 meter/sec RA = 76
93926 deg
ZDOT = 1224
882422 TA = 66
81648
MA = 66
62282
Ha = 219
843 n
mi
Hp = 203
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12034624
64 X = -3718312
85
Y = 7363357
00 feet Y = 2203051
00 meter
Z = 17111102
20 Z = 5197522
79
XDOT = -8640
228461 XDOT = -2559
773173
YDOT = -23331
872342 feet/sec YDOT = -7140
592159 meter/sec
ZDOT = 4018
643116 ZDOT = 1212
267922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13614910
25 X = -4149824
64
Y = -4025366
05 feet Y = -1226931
57 meter
Z = 17037361
36 Z = 5192987
74
XDOT = 11138
254509 XDOT = 3394
939974
YDOT = -21114
934978 feet/sec YDOT = -6435
832181 meter/sec
ZDOT = 3967
480969 ZDOT = 1209
288199
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 12034
55018929
00016717 00000-0 10270-3 0 9028
2 25544 51
6404 77
4132 0020283 1
3284 358
7921 15
58672011 37022
Satellite: ISS
Catalog Number: 25544
Epoch time: 12034
55018929 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 77
4132 deg
Eccentricity:
0020283
Arg of perigee: 1
3284 deg
Mean anomaly: 358
7921 deg
Mean motion: 15
58672011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 284
Coasting Arc #4 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2012/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4470789
40 A = 6765980
64 meter
Y = 1310525
01 meter E =
0021377
Z = -4911623
13 I = 51
95872
XDOT = 435
147188 Wp = 38
10674
YDOT = 7285
548502 meter/sec RA = 71
91469 deg
ZDOT = 2361
852638 TA = 254
78763
MA = 255
02411
Ha = 219
987 n
mi
Hp = 203
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14667944
22 X = 4479661
61
Y = 4299622
73 feet Y = 1360569
91 meter
Z = -16114249
11 Z = -4889883
11
XDOT = 1427
648255 XDOT = 342
173286
YDOT = 23902
718184 feet/sec YDOT = 7289
894655 meter/sec
ZDOT = 7748
860362 ZDOT = 2363
740954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6990605
05 X = 2130736
42
Y = 13697755
06 feet Y = 4175075
74 meter
Z = -16025208
74 Z = -4884483
62
XDOT = -15459
655632 XDOT = -4712
103037
YDOT = 16879
442900 feet/sec YDOT = 5144
854196 meter/sec
ZDOT = 7756
021193 ZDOT = 2364
035260
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 12035
51190653
00016717 00000-0 10270-3 0 9031
2 25544 51
6413 72
5861 0020392 4
8787 355
2563 15
58671451 37171
Satellite: ISS
Catalog Number: 25544
Epoch time: 12035
51190653 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 72
5861 deg
Eccentricity:
0020392
Arg of perigee: 4
8787 deg
Mean anomaly: 355
2563 deg
Mean motion: 15
58671451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3717
Checksum: 306
Coasting Arc #5 (Orbit 3732)
---------------------------------------
Vector Time (GMT): 2012/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4275287
89 A = 6772707
65 meter
Y = -4453900
79 meter E =
0024157
Z = 2795384
90 I = 51
97031
XDOT = 2116
022232 Wp = 42
60645
YDOT = -5282
670080 meter/sec RA = 66
91247 deg
ZDOT = -5137
410648 TA = 105
81627
MA = 105
54980
Ha = 219
986 n
mi
Hp = 202
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14026535
08 X = -4238744
74
Y = -14612535
39 feet Y = -4501505
43 meter
Z = 9171210
29 Z = 2774704
92
XDOT = 6942
330156 XDOT = 2199
892588
YDOT = -17331
594750 feet/sec YDOT = -5258
538352 meter/sec
ZDOT = -16855
021811 ZDOT = -5126
927777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 638617
52 X = 194650
62
Y = -20283091
65 feet Y = -6182286
33 meter
Z = 9086767
08 Z = 2769646
60
XDOT = 15851
216475 XDOT = 4831
450782
YDOT = -7096
603671 feet/sec YDOT = -2163
044799 meter/sec
ZDOT = -16811
608716 ZDOT = -5124
178337
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 12036
53772020
00016717 00000-0 10270-3 0 9049
2 25544 51
6402 67
4361 0020444 9
0085 351
1433 15
58736116 37332
Satellite: ISS
Catalog Number: 25544
Epoch time: 12036
53772020 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 67
4361 deg
Eccentricity:
0020444
Arg of perigee: 9
0085 deg
Mean anomaly: 351
1433 deg
Mean motion: 15
58736116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3733
Checksum: 275
Coasting Arc #6 (Orbit 3748)
---------------------------------------
Vector Time (GMT): 2012/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2970714
93 A = 6775967
33 meter
Y = 6060896
87 meter E =
0031703
Z = 293406
00 I = 51
96863
XDOT = -4379
361131 Wp = 26
00717
YDOT = 1843
148909 meter/sec RA = 61
94004 deg
ZDOT = 6049
343436 TA = 337
15340
MA = 337
29415
Ha = 220
139 n
mi
Hp = 202
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9746440
07 X = 2901294
72
Y = 19884832
24 feet Y = 6093729
08 meter
Z = 962618
11 Z = 307668
59
XDOT = -14367
982713 XDOT = -4429
031630
YDOT = 6047
076472 feet/sec YDOT = 1793
898461 meter/sec
ZDOT = 19846
927284 ZDOT = 6027
948652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7085187
67 X = -2159565
20
Y = 20978196
80 feet Y = 6394154
39 meter
Z = 1020615
34 Z = 311083
55
XDOT = -13016
560793 XDOT = -3967
447730
YDOT = -5390
250046 feet/sec YDOT = -1642
948214 meter/sec
ZDOT = 19759
041351 ZDOT = 6022
555804
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 12037
56351807
00016717 00000-0 10270-3 0 9050
2 25544 51
6405 62
2868 0020511 12
8907 347
2768 15
58728861 37492
Satellite: ISS
Catalog Number: 25544
Epoch time: 12037
56351807 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 62
2868 deg
Eccentricity:
0020511
Arg of perigee: 12
8907 deg
Mean anomaly: 347
2768 deg
Mean motion: 15
58728861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3749
Checksum: 326
Coasting Arc #7 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2012/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -712385
66 A = 6771163
88 meter
Y = -5871912
48 meter E =
0021954
Z = -3325680
82 I = 51
93745
XDOT = 5695
317043 Wp = 28
31043
YDOT = 1983
585264 meter/sec RA = 56
96178 deg
ZDOT = -4716
173209 TA = 190
18632
MA = 190
23088
Ha = 220
157 n
mi
Hp = 202
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2337223
30 X = -630516
87
Y = -19264804
73 feet Y = -5879421
14 meter
Z = -10911026
30 Z = -3328942
46
XDOT = 18685
423370 XDOT = 5695
622354
YDOT = 6507
825669 feet/sec YDOT = 2047
275402 meter/sec
ZDOT = -15473
009217 ZDOT = -4688
505720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11688243
92 X = 3562576
75
Y = -15482203
81 feet Y = -4718975
72 meter
Z = -10923924
59 Z = -3329612
21
XDOT = 7929
281204 XDOT = 2416
844911
YDOT = 16837
736189 feet/sec YDOT = 5132
141991 meter/sec
ZDOT = -15359
709049 ZDOT = -4681
639318
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 12038
52518547
00016717 00000-0 10270-3 0 9064
2 25544 51
6401 57
4583 0020439 16
5499 343
6319 15
58768972 37640
Satellite: ISS
Catalog Number: 25544
Epoch time: 12038
52518547 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 57
4583 deg
Eccentricity:
0020439
Arg of perigee: 16
5499 deg
Mean anomaly: 343
6319 deg
Mean motion: 15
58768972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 338
Coasting Arc #8 (Orbit 3779)
---------------------------------------
Vector Time (GMT): 2012/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2006872
66 A = 6764673
83 meter
Y = 3935996
48 meter E =
0019799
Z = 5109003
24 I = 51
89731
XDOT = -5587
846085 Wp = 34
21119
YDOT = -5007
231086 meter/sec RA = 51
94840 deg
ZDOT = 1675
480335 TA = 39
78273
MA = 39
63772
Ha = 220
349 n
mi
Hp = 202
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6584227
89 X = -2075554
32
Y = 12913374
28 feet Y = 3913170
62 meter
Z = 16761821
66 Z = 5099087
20
XDOT = -18332
828364 XDOT = -5539
577807
YDOT = -16427
923510 feet/sec YDOT = -5069
447861 meter/sec
ZDOT = 5496
982727 ZDOT = 1648
453055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13679081
09 X = -4169383
92
Y = 4935820
35 feet Y = 1504438
04 meter
Z = 16720836
58 Z = 5096510
99
XDOT = -1959
109218 XDOT = -597
136490
YDOT = -23533
978926 feet/sec YDOT = -7173
156777 meter/sec
ZDOT = 5386
555674 ZDOT = 1641
822169
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 12039
55094755
00016717 00000-0 10270-3 0 9079
2 25544 51
6390 52
3074 0020489 20
5169 339
6804 15
58790928 37808
Satellite: ISS
Catalog Number: 25544
Epoch time: 12039
55094755 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 52
3074 deg
Eccentricity:
0020489
Arg of perigee: 20
5169 deg
Mean anomaly: 339
6804 deg
Mean motion: 15
58790928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 331
Coasting Arc #9 (Orbit 3794)
---------------------------------------
Vector Time (GMT): 2012/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4394335
46 A = 6765099
55 meter
Y = -1090684
73 meter E =
0025826
Z = -5039654
66 I = 51
87964
XDOT = 3815
043477 Wp = 52
83648
YDOT = 6347
985101 meter/sec RA = 46
91748 deg
ZDOT = 1974
833565 TA = 236
15718
MA = 236
40325
Ha = 220
391 n
mi
Hp = 201
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14417111
08 X = 4430686
04
Y = -3578361
96 feet Y = -1041341
64 meter
Z = -16534300
07 Z = -5018219
33
XDOT = 12516
546839 XDOT = 3734
182425
YDOT = 20826
722772 feet/sec YDOT = 6390
195280 meter/sec
ZDOT = 6479
112745 ZDOT = 1993
169606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13207603
11 X = 4025677
43
Y = 7008491
81 feet Y = 2136188
30 meter
Z = -16446309
85 Z = -5012835
24
XDOT = -4070
619703 XDOT = -1240
724885
YDOT = 22879
102663 feet/sec YDOT = 6973
550492 meter/sec
ZDOT = 6553
784770 ZDOT = 1997
593598
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 12040
51258256
00016717 00000-0 10270-3 0 9086
2 25544 51
6396 47
4800 0020498 23
7029 336
5066 15
58796458 37952
Satellite: ISS
Catalog Number: 25544
Epoch time: 12040
51258256 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 47
4800 deg
Eccentricity:
0020498
Arg of perigee: 23
7029 deg
Mean anomaly: 336
5066 deg
Mean motion: 15
58796458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3795
Checksum: 332
Coasting Arc #10 (Orbit 3810)
---------------------------------------
Vector Time (GMT): 2012/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5731144
46 A = 6771694
93 meter
Y = -1926894
42 meter E =
0028099
Z = 3050520
94 I = 51
88011
XDOT = -694
124630 Wp = 52
96178
YDOT = -5829
368276 meter/sec RA = 41
90401 deg
ZDOT = -4938
437543 TA = 92
10989
MA = 91
78810
Ha = 220
393 n
mi
Hp = 201
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18802967
39 X = -5723990
05
Y = -6321832
09 feet Y = -1990943
39 meter
Z = 10008270
80 Z = 3022697
36
XDOT = -2277
311777 XDOT = -604
898521
YDOT = -19125
224004 feet/sec YDOT = -5836
631878 meter/sec
ZDOT = -16202
222909 ZDOT = -4941
592351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10143952
57 X = -3091876
74
Y = -17113881
97 feet Y = -5216311
22 meter
Z = 9894336
67 Z = 3015793
82
XDOT = 9604
686950 XDOT = 2927
508582
YDOT = -15159
238616 feet/sec YDOT = -4620
535930 meter/sec
ZDOT = -16214
678885 ZDOT = -4942
234124
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 12041
53830806
00016717 00000-0 10270-3 0 9097
2 25544 51
6388 42
3285 0020610 27
4559 332
7680 15
58876477 38118
Satellite: ISS
Catalog Number: 25544
Epoch time: 12041
53830806 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 42
3285 deg
Eccentricity:
0020610
Arg of perigee: 27
4559 deg
Mean anomaly: 332
7680 deg
Mean motion: 15
58876477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 319
Coasting Arc #11 (Orbit 3826)
---------------------------------------
Vector Time (GMT): 2012/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5394908
10 A = 6775455
24 meter
Y = 4069655
12 meter E =
0032408
Z = 15860
16 I = 51
87011
XDOT = -2882
612130 Wp = 36
60434
YDOT = 3773
225904 meter/sec RA = 36
92357 deg
ZDOT = 6049
084487 TA = 323
56661
MA = 323
78673
Ha = 220
324 n
mi
Hp = 201
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17699829
71 X = 5348922
39
Y = 13351886
86 feet Y = 4129727
19 meter
Z = 52034
64 Z = 41956
01
XDOT = -9457
388877 XDOT = -2953
975512
YDOT = 12379
350080 feet/sec YDOT = 3740
592166 meter/sec
ZDOT = 19846
077712 ZDOT = 6034
907494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5039514
16 X = 1536043
92
Y = 21590221
72 feet Y = 6580699
58 meter
Z = 158698
94 Z = 48371
44
XDOT = -13710
658913 XDOT = -4179
008837
YDOT = 3005
109301 feet/sec YDOT = 915
957315 meter/sec
ZDOT = 19787
631862 ZDOT = 6031
270192
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 12042
56401456
00016717 00000-0 10270-3 0 9108
2 25544 51
6391 37
1792 0020401 31
8079 328
4303 15
58918930 38273
Satellite: ISS
Catalog Number: 25544
Epoch time: 12042
56401456 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 37
1792 deg
Eccentricity:
0020401
Arg of perigee: 31
8079 deg
Mean anomaly: 328
4303 deg
Mean motion: 15
58918930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3827
Checksum: 295
Coasting Arc #12 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2012/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3339217
48 A = 6771225
40 meter
Y = -4998755
66 meter E =
0022772
Z = -3149284
58 I = 51
83067
XDOT = 5853
369108 Wp = 45
23162
YDOT = -852
317052 meter/sec RA = 31
93889 deg
ZDOT = -4859
456402 TA = 170
94378
MA = 170
90264
Ha = 220
490 n
mi
Hp = 201
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10955437
94 X = -3267773
88
Y = -16400117
01 feet Y = -5035697
57 meter
Z = -10332298
50 Z = -3165332
35
XDOT = 19203
966891 XDOT = 5886
070727
YDOT = -2796
315786 feet/sec YDOT = -786
678495 meter/sec
ZDOT = -15943
098431 ZDOT = -4830
941848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1803415
40 X = 549681
01
Y = -19605557
40 feet Y = -5975773
90 meter
Z = -10397675
83 Z = -3169211
59
XDOT = 15356
667232 XDOT = 4680
712172
YDOT = 9795
606269 feet/sec YDOT = 2985
700791 meter/sec
ZDOT = -15826
109996 ZDOT = -4823
798327
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 12043
52560004
00016717 00000-0 10270-3 0 9111
2 25544 51
6388 32
3496 0020606 35
1387 325
1122 15
58899242 38427
Satellite: ISS
Catalog Number: 25544
Epoch time: 12043
52560004 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 32
3496 deg
Eccentricity:
0020606
Arg of perigee: 35
1387 deg
Mean anomaly: 325
1122 deg
Mean motion: 15
58899242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 292
Coasting Arc #13 (Orbit 3857)
---------------------------------------
Vector Time (GMT): 2012/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 57641
19 A = 6764472
02 meter
Y = 4484891
14 meter E =
0021579
Z = 5045251
66 I = 51
78188
XDOT = -7188
513089 Wp = 52
48117
YDOT = -2000
525455 meter/sec RA = 26
92008 deg
ZDOT = 1867
879735 TA = 19
55602
MA = 19
47337
Ha = 220
523 n
mi
Hp = 200
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 189111
53 X = -17022
49
Y = 14714209
77 feet Y = 4485118
42 meter
Z = 16552662
94 Z = 5045350
17
XDOT = -23584
360529 XDOT = -7174
682191
YDOT = -6563
403725 feet/sec YDOT = -2080
834442 meter/sec
ZDOT = 6128
214355 ZDOT = 1832
992286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8961207
26 X = -2731375
97
Y = 11672182
97 feet Y = 3557681
37 meter
Z = 16552682
31 Z = 5045257
57
XDOT = -13770
009970 XDOT = -4197
099039
YDOT = -19025
276163 feet/sec YDOT = -5798
904175 meter/sec
ZDOT = 5985
343171 ZDOT = 1824
332598
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 12044
55126988
00016717 00000-0 10270-3 0 9125
2 25544 51
6387 27
1993 0020547 38
4598 321
8017 15
58932673 38583
Satellite: ISS
Catalog Number: 25544
Epoch time: 12044
55126988 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 27
1993 deg
Eccentricity:
0020547
Arg of perigee: 38
4598 deg
Mean anomaly: 321
8017 deg
Mean motion: 15
58932673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 342
Coasting Arc #14 (Orbit 3872)
---------------------------------------
Vector Time (GMT): 2012/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3396535
22 A = 6764544
45 meter
Y = -2945581
33 meter E =
0029161
Z = -5073701
31 I = 51
75454
XDOT = 6230
862215 Wp = 65
03487
YDOT = 4060
150444 meter/sec RA = 21
87903 deg
ZDOT = 1834
274829 TA = 222
60459
MA = 222
83116
Ha = 220
588 n
mi
Hp = 200
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11143488
25 X = 3453867
48
Y = -9663980
73 feet Y = -2907278
68 meter
Z = -16646001
67 Z = -5057061
99
XDOT = 20442
461335 XDOT = 6176
087314
YDOT = 13320
703555 feet/sec YDOT = 4129
521546 meter/sec
ZDOT = 6017
962037 ZDOT = 1864
410631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14794470
98 X = 4509354
76
Y = -984160
01 feet Y = -299971
97 meter
Z = -16577523
43 Z = -5052829
14
XDOT = 8258
220674 XDOT = 2517
105661
YDOT = 21822
013214 feet/sec YDOT = 6651
349628 meter/sec
ZDOT = 6141
167876 ZDOT = 1871
827969
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 12045
51281794
00016717 00000-0 10270-3 0 9130
2 25544 51
6390 22
3710 0020590 42
1355 318
1379 15
58935555 38731
Satellite: ISS
Catalog Number: 25544
Epoch time: 12045
51281794 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 22
3710 deg
Eccentricity:
0020590
Arg of perigee: 42
1355 deg
Mean anomaly: 318
1379 deg
Mean motion: 15
58935555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3873
Checksum: 305
Coasting Arc #15 (Orbit 3888)
---------------------------------------
Vector Time (GMT): 2012/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5966211
69 A = 6771197
06 meter
Y = 750204
35 meter E =
0030656
Z = 3105018
45 I = 51
74868
XDOT = -3194
363949 Wp = 64
21832
YDOT = -4989
345853 meter/sec RA = 16
85533 deg
ZDOT = -4881
919221 TA = 80
03190
MA = 79
68605
Ha = 220
587 n
mi
Hp = 200
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19574185
34 X = -5989240
46
Y = 2461300
36 feet Y = 683357
73 meter
Z = 10187068
42 Z = 3075979
36
XDOT = -10480
196684 XDOT = -3114
619759
YDOT = -16369
244924 feet/sec YDOT = -5024
621317 meter/sec
ZDOT = -16016
795343 ZDOT = -4897
243382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17351115
60 X = -5288620
03
Y = -9516220
71 feet Y = -2900544
07 meter
Z = 10067940
46 Z = 3068708
25
XDOT = 490
817543 XDOT = 149
601187
YDOT = -18083
652271 feet/sec YDOT = -5511
897212 meter/sec
ZDOT = -16079
187306 ZDOT = -4900
936291
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 12046
53844913
00016717 00000-0 10270-3 0 9142
2 25544 51
6389 17
2195 0020596 45
6614 314
6225 15
59000095 38892
Satellite: ISS
Catalog Number: 25544
Epoch time: 12046
53844913 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 17
2195 deg
Eccentricity:
0020596
Arg of perigee: 45
6614 deg
Mean anomaly: 314
6225 deg
Mean motion: 15
59000095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3889
Checksum: 318
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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