[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 6th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 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 3515)
---------------------------------------
Vector Time (GMT): 2012/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3068848
90 A = 6799722
17 meter
Y = 6018354
26 meter E =
0028521
Z = -658344
78 I = 51
34270
XDOT = -4033
124765 Wp = 135
60376
YDOT = -2687
561418 meter/sec RA = 292
54674 deg
ZDOT = -5944
747453 TA = 51
53114
MA = 51
27560
Ha = 232
918 n
mi
Hp = 214
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10068401
89 X = -3132721
16
Y = 19745256
74 feet Y = 5983679
30 meter
Z = -2159923
83 Z = -673408
88
XDOT = -13232
036631 XDOT = -3973
893443
YDOT = -8817
458722 feet/sec YDOT = -2732
331541 meter/sec
ZDOT = -19503
764611 ZDOT = -5964
196450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5070386
18 X = 1545453
71
Y = -21569965
73 feet Y = -6574525
55 meter
Z = -2222816
68 Z = -677514
52
XDOT = 13260
581591 XDOT = 4041
825269
YDOT = 5077
360813 feet/sec YDOT = 1547
579576 meter/sec
ZDOT = -19583
869380 ZDOT = -5969
163387
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 12279
53101165
00016717 00000-0 10270-3 0 9000
2 25544 51
6463 293
0811 0017977 133
6642 226
6002 15
50495144 35168
Satellite: ISS
Catalog Number: 25544
Epoch time: 12279
53101165 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 293
0811 deg
Eccentricity:
0017977
Arg of perigee: 133
6642 deg
Mean anomaly: 226
6002 deg
Mean motion: 15
50495144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 292
Coasting Arc #2 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2012/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2862551
10 A = 6799189
24 meter
Y = -6064684
40 meter E =
0024341
Z = 1122252
20 I = 51
33075
XDOT = 3961
083756 Wp = 103
63452
YDOT = 2971
128314 meter/sec RA = 287
57133 deg
ZDOT = 5839
564403 TA = 268
56943
MA = 268
84828
Ha = 232
779 n
mi
Hp = 214
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9391571
86 X = 2924703
19
Y = -19897258
52 feet Y = -6032325
98 meter
Z = 3681929
81 Z = 1136309
87
XDOT = 12995
681613 XDOT = 3899
197907
YDOT = 9747
796307 feet/sec YDOT = 3015
077949 meter/sec
ZDOT = 19158
675863 ZDOT = 5858
656931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3996397
53 X = -1218101
97
Y = 21626265
71 feet Y = 6591685
79 meter
Z = 3740663
57 Z = 1140154
26
XDOT = -13358
222289 XDOT = -4071
586154
YDOT = -5859
014921 feet/sec YDOT = -1785
827748 meter/sec
ZDOT = 19237
282342 ZDOT = 5863
523658
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 12280
56223778
00016717 00000-0 10270-3 0 9011
2 25544 51
6462 287
9692 0017882 137
4823 222
7716 15
50554427 35321
Satellite: ISS
Catalog Number: 25544
Epoch time: 12280
56223778 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 287
9692 deg
Eccentricity:
0017882
Arg of perigee: 137
4823 deg
Mean anomaly: 222
7716 deg
Mean motion: 15
50554427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 326
Coasting Arc #3 (Orbit 3546)
---------------------------------------
Vector Time (GMT): 2012/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2713439
80 A = 6798558
76 meter
Y = 5993587
02 meter E =
0025569
Z = -1675476
48 I = 51
31957
XDOT = -3915
019143 Wp = 140
92969
YDOT = -3342
302911 meter/sec RA = 282
59342 deg
ZDOT = -5682
751688 TA = 57
49944
MA = 57
25259
Ha = 232
675 n
mi
Hp = 214
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8902361
54 X = -2772120
48
Y = 19663999
42 feet Y = 5962915
44 meter
Z = -5496970
09 Z = -1688801
29
XDOT = -12844
550993 XDOT = -3849
748001
YDOT = -10965
560731 feet/sec YDOT = -3385
718485 meter/sec
ZDOT = -18644
198453 ZDOT = -5701
612145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3205492
78 X = 977034
20
Y = -21331534
26 feet Y = -6501851
64 meter
Z = -5552662
10 Z = -1692451
41
XDOT = 13670
992952 XDOT = 4166
918652
YDOT = 6871
119291 feet/sec YDOT = 2094
317160 meter/sec
ZDOT = -18721
813694 ZDOT = -5706
408814
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 12281
52899822
00016717 00000-0 10270-3 0 9028
2 25544 51
6454 283
1747 0017883 140
7877 219
4573 15
50543208 35473
Satellite: ISS
Catalog Number: 25544
Epoch time: 12281
52899822 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 283
1747 deg
Eccentricity:
0017883
Arg of perigee: 140
7877 deg
Mean anomaly: 219
4573 deg
Mean motion: 15
50543208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3547
Checksum: 335
Coasting Arc #4 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2012/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2516679
69 A = 6797621
58 meter
Y = -5943691
33 meter E =
0025343
Z = 2131249
94 I = 51
31116
XDOT = 3930
169497 Wp = 112
77983
YDOT = 3646
929729 meter/sec RA = 277
61573 deg
ZDOT = 5467
848406 TA = 270
90430
MA = 271
19467
Ha = 232
504 n
mi
Hp = 214
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8256823
13 X = 2572603
01
Y = -19500299
62 feet Y = -5915235
42 meter
Z = 6992289
81 Z = 2143612
19
XDOT = 12894
256880 XDOT = 3862
534848
YDOT = 11964
992550 feet/sec YDOT = 3690
501528 meter/sec
ZDOT = 17939
135191 ZDOT = 5486
776644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2258176
34 X = -688292
15
Y = 21038340
10 feet Y = 6412486
06 meter
Z = 7043991
46 Z = 2147008
60
XDOT = -14151
514309 XDOT = -4313
381561
YDOT = -7618
850580 feet/sec YDOT = -2322
225657 meter/sec
ZDOT = 18017
007347 ZDOT = 5491
583839
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 12282
56018906
00016717 00000-0 10270-3 0 9030
2 25544 51
6451 278
0627 0017797 144
9054 215
3273 15
50615279 35635
Satellite: ISS
Catalog Number: 25544
Epoch time: 12282
56018906 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 278
0627 deg
Eccentricity:
0017797
Arg of perigee: 144
9054 deg
Mean anomaly: 215
3273 deg
Mean motion: 15
50615279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 319
Coasting Arc #5 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2012/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2397012
31 A = 6796581
94 meter
Y = 5770830
57 meter E =
0022388
Z = -2658008
46 I = 51
30389
XDOT = -3970
218272 Wp = 142
85587
YDOT = -4017
125940 meter/sec RA = 272
63504 deg
ZDOT = -5181
645438 TA = 67
24458
MA = 67
00815
Ha = 232
391 n
mi
Hp = 215
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7864213
61 X = -2448452
68
Y = 18933171
16 feet Y = 5743737
86 meter
Z = -8720500
18 Z = -2669778
52
XDOT = -13025
650500 XDOT = -3899
831391
YDOT = -13179
547047 feet/sec YDOT = -4061
130242 meter/sec
ZDOT = -17000
149076 ZDOT = -5200
761452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1684324
99 X = 513382
26
Y = -20411096
34 feet Y = -6221302
16 meter
Z = -8769728
89 Z = -2673013
37
XDOT = 14828
736464 XDOT = 4519
798874
YDOT = 8505
026067 feet/sec YDOT = 2592
331945 meter/sec
ZDOT = -17078
769226 ZDOT = -5205
608860
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 12283
52691683
00016717 00000-0 10270-3 0 9047
2 25544 51
6445 273
2678 0017753 147
8929 212
3306 15
50599351 35788
Satellite: ISS
Catalog Number: 25544
Epoch time: 12283
52691683 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 273
2678 deg
Eccentricity:
0017753
Arg of perigee: 147
8929 deg
Mean anomaly: 212
3306 deg
Mean motion: 15
50599351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3578
Checksum: 339
Coasting Arc #6 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2012/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2242178
58 A = 6795356
26 meter
Y = -5624483
88 meter E =
0025639
Z = 3083576
94 I = 51
29968
XDOT = 4068
594648 Wp = 124
19277
YDOT = 4306
899092 meter/sec RA = 267
65496 deg
ZDOT = 4854
161018 TA = 271
36240
MA = 271
65610
Ha = 232
205 n
mi
Hp = 215
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7356228
93 X = 2289926
64
Y = -18453031
11 feet Y = -5599143
18 meter
Z = 10116722
25 Z = 3094585
93
XDOT = 13348
407639 XDOT = 3996
551011
YDOT = 14130
246364 feet/sec YDOT = 4351
994291 meter/sec
ZDOT = 15925
725126 ZDOT = 4873
750824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -997540
84 X = -304050
45
Y = 19816642
05 feet Y = 6040112
50 meter
Z = 10162782
12 Z = 3097615
99
XDOT = -15634
626781 XDOT = -4765
434243
YDOT = -9068
153906 feet/sec YDOT = -2763
973310 meter/sec
ZDOT = 16006
284871 ZDOT = 4878
715629
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 12284
55807176
00016717 00000-0 10270-3 0 9058
2 25544 51
6441 268
1554 0017690 152
2918 207
9179 15
50671790 35942
Satellite: ISS
Catalog Number: 25544
Epoch time: 12284
55807176 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 268
1554 deg
Eccentricity:
0017690
Arg of perigee: 152
2918 deg
Mean anomaly: 207
9179 deg
Mean motion: 15
50671790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3594
Checksum: 334
Coasting Arc #7 (Orbit 3608)
---------------------------------------
Vector Time (GMT): 2012/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2184951
48 A = 6794040
73 meter
Y = 5357321
55 meter E =
0019930
Z = -3557633
96 I = 51
29727
XDOT = -4183
177117 Wp = 140
58744
YDOT = -4635
598898 meter/sec RA = 262
67140 deg
ZDOT = -4440
287395 TA = 81
57137
MA = 81
34551
Ha = 232
079 n
mi
Hp = 215
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7168475
99 X = -2227413
43
Y = 17576514
28 feet Y = 5332650
25 meter
Z = -11672027
43 Z = -3568352
19
XDOT = -13724
334373 XDOT = -4109
459862
YDOT = -15208
657801 feet/sec YDOT = -4681
966113 meter/sec
ZDOT = -14567
872031 ZDOT = -4460
429693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 765863
46 X = 233435
18
Y = -18939006
77 feet Y = -5772609
26 meter
Z = -11716851
20 Z = -3571296
25
XDOT = 16578
151853 XDOT = 5053
020685
YDOT = 9675
936357 feet/sec YDOT = 2949
225402 meter/sec
ZDOT = -14650
693510 ZDOT = -4465
531382
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 12285
52476552
00016717 00000-0 10270-3 0 9067
2 25544 51
6439 263
3600 0017620 155
1178 205
0826 15
50658449 36092
Satellite: ISS
Catalog Number: 25544
Epoch time: 12285
52476552 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 263
3600 deg
Eccentricity:
0017620
Arg of perigee: 155
1178 deg
Mean anomaly: 205
0826 deg
Mean motion: 15
50658449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3609
Checksum: 313
Coasting Arc #8 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2012/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2102928
13 A = 6792685
73 meter
Y = -5126485
84 meter E =
0025063
Z = 3928616
59 I = 51
29818
XDOT = 4346
436032 Wp = 137
13164
YDOT = 4875
731653 meter/sec RA = 257
68911 deg
ZDOT = 4002
612005 TA = 270
69562
MA = 270
98279
Ha = 231
883 n
mi
Hp = 215
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6899370
50 X = 2141012
69
Y = -16819179
27 feet Y = -5102756
15 meter
Z = 12889162
03 Z = 3938925
79
XDOT = 14259
960734 XDOT = 4272
147515
YDOT = 15996
494925 feet/sec YDOT = 4923
921345 meter/sec
ZDOT = 13131
929150 ZDOT = 4023
545997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -448406
57 X = -136674
32
Y = 18143098
90 feet Y = 5530016
55 meter
Z = 12932265
70 Z = 3941754
58
XDOT = -17588
248882 XDOT = -5360
898259
YDOT = -9933
754941 feet/sec YDOT = -3027
808506 meter/sec
ZDOT = 13218
009528 ZDOT = 4028
849304
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 12286
55588373
00016717 00000-0 10270-3 0 9077
2 25544 51
6438 258
2472 0017581 159
6448 200
5407 15
50727046 36259
Satellite: ISS
Catalog Number: 25544
Epoch time: 12286
55588373 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 258
2472 deg
Eccentricity:
0017581
Arg of perigee: 159
6448 deg
Mean anomaly: 200
5407 deg
Mean motion: 15
50727046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3625
Checksum: 330
Coasting Arc #9 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2012/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2136450
43 A = 6791322
95 meter
Y = 4785539
38 meter E =
0019102
Z = -4322347
81 I = 51
30140
XDOT = -4508
619209 Wp = 135
87965
YDOT = -5126
997061 meter/sec RA = 252
70318 deg
ZDOT = -3470
629489 TA = 98
73382
MA = 98
51742
Ha = 231
743 n
mi
Hp = 215
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7009351
79 X = -2168807
19
Y = 15700588
53 feet Y = 4761466
78 meter
Z = -14180931
13 Z = -4332805
98
XDOT = -14792
057772 XDOT = -4434
093144
YDOT = -16820
856498 feet/sec YDOT = -5176
999007 meter/sec
ZDOT = -11386
579687 ZDOT = -3492
350834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 643728
82 X = 196208
54
Y = -17145970
10 feet Y = -5226091
69 meter
Z = -14224613
27 Z = -4335662
13
XDOT = 18638
120144 XDOT = 5680
899020
YDOT = 10158
680271 feet/sec YDOT = 3096
365747 meter/sec
ZDOT = -11475
899028 ZDOT = -3497
854024
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 12287
52254237
00016717 00000-0 10270-3 0 9085
2 25544 51
6442 253
4515 0017499 162
5491 197
6265 15
50717440 36400
Satellite: ISS
Catalog Number: 25544
Epoch time: 12287
52254237 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 253
4515 deg
Eccentricity:
0017499
Arg of perigee: 162
5491 deg
Mean anomaly: 197
6265 deg
Mean motion: 15
50717440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 319
Coasting Arc #10 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2012/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2151473
80 A = 6790037
92 meter
Y = -4493950
07 meter E =
0023552
Z = 4613078
72 I = 51
30820
XDOT = 4704
658508 Wp = 150
72446
YDOT = 5289
081679 meter/sec RA = 247
71942 deg
ZDOT = 2931
749510 TA = 269
78404
MA = 270
05393
Ha = 231
535 n
mi
Hp = 215
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7058641
08 X = 2179156
40
Y = -14743930
68 feet Y = -4469735
61 meter
Z = 15134772
70 Z = 4623598
49
XDOT = 15435
231324 XDOT = 4630
923140
YDOT = 17352
630181 feet/sec YDOT = 5341
280186 meter/sec
ZDOT = 9618
600753 ZDOT = 2954
425276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -756915
50 X = -230707
84
Y = 16288155
64 feet Y = 4964629
84 meter
Z = 15178679
62 Z = 4626461
55
XDOT = -19681
489998 XDOT = -5998
918151
YDOT = -10045
905460 feet/sec YDOT = -3061
991984 meter/sec
ZDOT = 9711
856908 ZDOT = 2960
173985
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 12288
55362312
00016717 00000-0 10270-3 0 9094
2 25544 51
6447 248
3386 0017482 167
0327 193
1277 15
50783506 36561
Satellite: ISS
Catalog Number: 25544
Epoch time: 12288
55362312 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 248
3386 deg
Eccentricity:
0017482
Arg of perigee: 167
0327 deg
Mean anomaly: 193
1277 deg
Mean motion: 15
50783506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3656
Checksum: 329
Coasting Arc #11 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2293910
74 A = 6788907
90 meter
Y = 4111064
68 meter E =
0019946
Z = -4899100
48 I = 51
31737
XDOT = -4874
432211 Wp = 133
37321
YDOT = -5437
672643 meter/sec RA = 242
73227 deg
ZDOT = -2299
994721 TA = 114
09793
MA = 113
88916
Ha = 231
384 n
mi
Hp = 216
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7525953
86 X = -2315911
69
Y = 13487745
00 feet Y = 4085289
23 meter
Z = -16073164
32 Z = -4910298
34
XDOT = -15992
231662 XDOT = -4802
091593
YDOT = -17840
133344 feet/sec YDOT = -5491
777341 meter/sec
ZDOT = -7545
914438 ZDOT = -2323
498835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1402766
94 X = 427563
36
Y = -15332608
70 feet Y = -4673379
13 meter
Z = -16119839
12 Z = -4913326
96
XDOT = 20639
049398 XDOT = 6290
782257
YDOT = 9856
685119 feet/sec YDOT = 3004
317624 meter/sec
ZDOT = -7642
586871 ZDOT = -2329
460478
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 12289
52024596
00016717 00000-0 10270-3 0 9103
2 25544 51
6452 243
5429 0017402 170
1334 190
0161 15
50775945 36710
Satellite: ISS
Catalog Number: 25544
Epoch time: 12289
52024596 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 243
5429 deg
Eccentricity:
0017402
Arg of perigee: 170
1334 deg
Mean anomaly: 190
0161 deg
Mean motion: 15
50775945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 297
Coasting Arc #12 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2012/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2418568
40 A = 6787922
73 meter
Y = -3791721
12 meter E =
0021154
Z = 5084214
53 I = 51
33019
XDOT = 5060
250196 Wp = 163
71479
YDOT = 5504
964213 meter/sec RA = 237
74823 deg
ZDOT = 1676
698469 TA = 269
88922
MA = 270
13162
Ha = 231
161 n
mi
Hp = 216
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7934935
70 X = 2436089
81
Y = -12440029
91 feet Y = -3764576
84 meter
Z = 16680493
85 Z = 5096006
98
XDOT = 16601
870722 XDOT = 4990
171196
YDOT = 18060
906209 feet/sec YDOT = 5561
159379 meter/sec
ZDOT = 5500
979230 ZDOT = 1701
110986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1943456
59 X = -592365
57
Y = 14570514
31 feet Y = 4441092
76 meter
Z = 16729599
91 Z = 5099182
05
XDOT = -21520
244447 XDOT = -6559
370507
YDOT = -9383
151888 feet/sec YDOT = -2859
984695 meter/sec
ZDOT = 5601
407206 ZDOT = 1707
308916
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 12290
55128867
00016717 00000-0 10270-3 0 9115
2 25544 51
6459 238
4302 0017396 174
4699 185
6647 15
50839600 36878
Satellite: ISS
Catalog Number: 25544
Epoch time: 12290
55128867 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 238
4302 deg
Eccentricity:
0017396
Arg of perigee: 174
4699 deg
Mean anomaly: 185
6647 deg
Mean motion: 15
50839600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 347
Coasting Arc #13 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2012/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2673277
15 A = 6787287
63 meter
Y = 3405931
57 meter E =
0021441
Z = -5237584
96 I = 51
34525
XDOT = -5189
368305 Wp = 136
18994
YDOT = -5541
647813 meter/sec RA = 232
76122 deg
ZDOT = -972
551282 TA = 124
54724
MA = 124
34469
Ha = 231
008 n
mi
Hp = 216
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8770594
31 X = -2685720
61
Y = 11174316
17 feet Y = 3375967
50 meter
Z = -17183677
69 Z = -5250602
35
XDOT = -17025
486564 XDOT = -5122
290192
YDOT = -18181
259229 feet/sec YDOT = -5599
303559 meter/sec
ZDOT = -3190
785047 ZDOT = -997
598480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2990087
26 X = 911378
60
Y = -13819713
50 feet Y = -4212248
67 meter
Z = -17237817
22 Z = -5254086
69
XDOT = 22182
236821 XDOT = 6761
145783
YDOT = 8836
330256 feet/sec YDOT = 2693
313462 meter/sec
ZDOT = -3293
842055 ZDOT = -1003
963058
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 12291
51787512
00016717 00000-0 10270-3 0 9121
2 25544 51
6461 233
6347 0017333 177
7384 182
3848 15
50834360 37028
Satellite: ISS
Catalog Number: 25544
Epoch time: 12291
51787512 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 233
6347 deg
Eccentricity:
0017333
Arg of perigee: 177
7384 deg
Mean anomaly: 182
3848 deg
Mean motion: 15
50834360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 313
Coasting Arc #14 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2012/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2904508
54 A = 6786819
78 meter
Y = -3096414
70 meter E =
0018083
Z = 5294125
31 I = 51
36376
XDOT = 5316
256982 Wp = 174
05336
YDOT = 5513
302501 meter/sec RA = 227
77807 deg
ZDOT = 290
217385 TA = 273
06465
MA = 273
27156
Ha = 230
765 n
mi
Hp = 216
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9529227
48 X = 2913199
15
Y = -10158840
89 feet Y = -3063885
95 meter
Z = 17369177
54 Z = 5308256
80
XDOT = 17441
787999 XDOT = 5252
801119
YDOT = 18088
262800 feet/sec YDOT = 5572
397411 meter/sec
ZDOT = 952
156776 ZDOT = 315
889847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3883643
54 X = -1183734
55
Y = 13299704
13 feet Y = 4053749
82 meter
Z = 17427901
08 Z = 5312024
25
XDOT = -22715
396807 XDOT = -6923
652947
YDOT = -8095
278428 feet/sec YDOT = -2467
440865 meter/sec
ZDOT = 1057
813300 ZDOT = 322
421494
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 12292
54887923
00016717 00000-0 10270-3 0 9133
2 25544 51
6464 228
5219 0017324 181
8834 178
2254 15
50892954 37183
Satellite: ISS
Catalog Number: 25544
Epoch time: 12292
54887923 = yrday
fracday
Element set: 913
Inclination: 51
6464 deg
RA of node: 228
5219 deg
Eccentricity:
0017324
Arg of perigee: 181
8834 deg
Mean anomaly: 178
2254 deg
Mean motion: 15
50892954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 340
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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