[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 1st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 2 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 353)
---------------------------------------
Vector Time (GMT): 2012/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -725829
88 A = 6785794
93 meter
Y = -4613317
29 meter E =
0019390
Z = -4934790
19 I = 51
78408
XDOT = 7183
424868 Wp = 17
59000
YDOT = 1330
885095 meter/sec RA = 24
75351 deg
ZDOT = -2285
081488 TA = 229
99428
MA = 230
16464
Ha = 228
103 n
mi
Hp = 216
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2381331
62 X = -650216
31
Y = -15135555
41 feet Y = -4621010
80 meter
Z = -16190256
52 Z = -4938133
00
XDOT = 23567
666891 XDOT = 7179
109355
YDOT = 4366
420915 feet/sec YDOT = 1411
190693 meter/sec
ZDOT = -7496
986509 ZDOT = -2250
194453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14823817
87 X = 4518299
69
Y = 3818551
90 feet Y = 1163894
62 meter
Z = -16203495
58 Z = -4938825
45
XDOT = -12973
148462 XDOT = -3954
215651
YDOT = 18945
035708 feet/sec YDOT = 5774
446884 meter/sec
ZDOT = -7352
517599 ZDOT = -2241
047364
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 12333
52001802
00016717 00000-0 10270-3 0 9007
2 25544 51
6481 25
1912 0016055 339
1193 20
9301 15
51809598 3541
Satellite: ISS
Catalog Number: 25544
Epoch time: 12333
52001802 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 25
1912 deg
Eccentricity:
0016055
Arg of perigee: 339
1193 deg
Mean anomaly: 20
9301 deg
Mean motion: 15
51809598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 354
Checksum: 272
Coasting Arc #2 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2012/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -85477
21 A = 6784439
19 meter
Y = 4337842
66 meter E =
0013254
Z = 5214666
24 I = 51
75176
XDOT = -7389
572215 Wp = 353
61316
YDOT = -1620
044726 meter/sec RA = 19
78745 deg
ZDOT = 1239
670715 TA = 84
57949
MA = 84
42830
Ha = 228
285 n
mi
Hp = 216
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -280437
05 X = -159309
59
Y = 14231767
27 feet Y = 4336473
52 meter
Z = 17108485
05 Z = 5214072
04
XDOT = -24244
003329 XDOT = -7376
929454
YDOT = -5315
107369 feet/sec YDOT = -1702
608961 meter/sec
ZDOT = 4067
161139 ZDOT = 1203
802503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13048970
09 X = -3977326
08
Y = -5696547
82 feet Y = -1736307
78 meter
Z = 17105432
70 Z = 5213735
89
XDOT = 13615
213327 XDOT = 4149
917022
YDOT = -19550
889479 feet/sec YDOT = -5959
111113 meter/sec
ZDOT = 3918
664136 ZDOT = 1194
408829
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 12334
55037387
00016717 00000-0 10270-3 0 9019
2 25544 51
6480 20
0726 0016117 343
2610 16
8007 15
51853874 3707
Satellite: ISS
Catalog Number: 25544
Epoch time: 12334
55037387 = yrday
fracday
Element set: 901
Inclination: 51
6480 deg
RA of node: 20
0726 deg
Eccentricity:
0016117
Arg of perigee: 343
2610 deg
Mean anomaly: 16
8007 deg
Mean motion: 15
51853874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 280
Coasting Arc #3 (Orbit 384)
---------------------------------------
Vector Time (GMT): 2012/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 871010
53 A = 6784012
57 meter
Y = -4119648
21 meter E =
0019551
Z = -5329072
43 I = 51
72151
XDOT = 7434
388053 Wp = 34
50553
YDOT = 1821
708073 meter/sec RA = 14
81849 deg
ZDOT = -177
765462 TA = 233
70922
MA = 233
88995
Ha = 228
455 n
mi
Hp = 216
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2857646
08 X = 942900
31
Y = -13515906
19 feet Y = -4109505
57 meter
Z = -17483833
42 Z = -5324666
81
XDOT = 24391
036918 XDOT = 7414
328340
YDOT = 5976
732522 feet/sec YDOT = 1904
731902 meter/sec
ZDOT = -583
220019 ZDOT = -141
697646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11550577
77 X = 3520616
11
Y = 7621552
69 feet Y = 2323049
26 meter
Z = -17465004
44 Z = -5323333
35
XDOT = -13782
935510 XDOT = -4201
038743
YDOT = 19778
031982 feet/sec YDOT = 6028
344148 meter/sec
ZDOT = -433
923289 ZDOT = -132
259819
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 12335
51632217
00016717 00000-0 10270-3 0 9020
2 25544 51
6484 15
2740 0016166 347
0021 13
0712 15
51846443 3857
Satellite: ISS
Catalog Number: 25544
Epoch time: 12335
51632217 = yrday
fracday
Element set: 902
Inclination: 51
6484 deg
RA of node: 15
2740 deg
Eccentricity:
0016166
Arg of perigee: 347
0021 deg
Mean anomaly: 13
0712 deg
Mean motion: 15
51846443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 385
Checksum: 271
Coasting Arc #4 (Orbit 400)
---------------------------------------
Vector Time (GMT): 2012/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1759605
43 A = 6784177
57 meter
Y = 3911024
94 meter E =
0017903
Z = 5258776
81 I = 51
69203
XDOT = -7332
919025 Wp = 1
25770
YDOT = -2020
885602 meter/sec RA = 9
84635 deg
ZDOT = -933
115050 TA = 97
77088
MA = 97
56757
Ha = 228
615 n
mi
Hp = 216
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5772983
68 X = -1828754
73
Y = 12831446
65 feet Y = 3890960
82 meter
Z = 17253204
75 Z = 5250061
04
XDOT = -24058
133283 XDOT = -7305
243152
YDOT = -6630
202105 feet/sec YDOT = -2102
732055 meter/sec
ZDOT = -3061
401084 ZDOT = -968
671324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10037489
90 X = -3059426
92
Y = -9924025
20 feet Y = -3024842
88 meter
Z = 17216531
54 Z = 5247598
81
XDOT = 13750
415984 XDOT = 4191
126792
YDOT = -19574
003078 feet/sec YDOT = -5966
156138 meter/sec
ZDOT = -3208
549395 ZDOT = -977
965856
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 12336
54665272
00016717 00000-0 10270-3 0 9032
2 25544 51
6476 10
1551 0016199 351
2566 8
8301 15
51897137 4010
Satellite: ISS
Catalog Number: 25544
Epoch time: 12336
54665272 = yrday
fracday
Element set: 903
Inclination: 51
6476 deg
RA of node: 10
1551 deg
Eccentricity:
0016199
Arg of perigee: 351
2566 deg
Mean anomaly: 8
8301 deg
Mean motion: 15
51897137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 401
Checksum: 296
Coasting Arc #5 (Orbit 415)
---------------------------------------
Vector Time (GMT): 2012/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2556410
51 A = 6785230
19 meter
Y = -3774513
04 meter E =
0016870
Z = -5031003
59 I = 51
66624
XDOT = 7073
330600 Wp = 39
50448
YDOT = 2174
019304 meter/sec RA = 4
87384 deg
ZDOT = 1979
480725 TA = 249
63956
MA = 249
82089
Ha = 228
789 n
mi
Hp = 215
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8387173
59 X = 2622867
54
Y = -12383572
96 feet Y = -3745553
66 meter
Z = -16505917
30 Z = -5018423
48
XDOT = 23206
465223 XDOT = 7038
878620
YDOT = 7132
609264 feet/sec YDOT = 2252
924912 meter/sec
ZDOT = 6494
359335 ZDOT = 2013
759359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8930531
11 X = 2722025
88
Y = 12069771
16 feet Y = 3678866
25 meter
Z = -16453239
94 Z = -5014947
53
XDOT = -13432
341521 XDOT = -4094
177696
YDOT = 18911
614407 feet/sec YDOT = 5764
260071 meter/sec
ZDOT = 6636
188843 ZDOT = 2022
710359
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 12337
51257712
00016717 00000-0 10270-3 0 9047
2 25544 51
6486 5
3563 0016290 354
7785 5
3194 15
51884118 4166
Satellite: ISS
Catalog Number: 25544
Epoch time: 12337
51257712 = yrday
fracday
Element set: 904
Inclination: 51
6486 deg
RA of node: 5
3563 deg
Eccentricity:
0016290
Arg of perigee: 354
7785 deg
Mean anomaly: 5
3194 deg
Mean motion: 15
51884118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 416
Checksum: 307
Coasting Arc #6 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2012/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3402591
62 A = 6786813
70 meter
Y = 3649654
26 meter E =
0021144
Z = 4603898
68 I = 51
64041
XDOT = -6637
342053 Wp = 20
37272
YDOT = -2367
074908 meter/sec RA = 359
90019 deg
ZDOT = -3005
440076 TA = 99
76707
MA = 99
52823
Ha = 228
885 n
mi
Hp = 215
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11163358
35 X = -3465514
73
Y = 11973931
31 feet Y = 3611252
22 meter
Z = 15104654
47 Z = 4587216
39
XDOT = -21776
056603 XDOT = -6595
779806
YDOT = -7765
993792 feet/sec YDOT = -2441
065220 meter/sec
ZDOT = -9860
367703 ZDOT = -3037
583339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7887983
62 X = -2404257
41
Y = -14417873
30 feet Y = -4394567
78 meter
Z = 15034986
91 Z = 4582664
01
XDOT = 13074
225076 XDOT = 3985
023803
YDOT = -17654
867952 feet/sec YDOT = -5381
203752 meter/sec
ZDOT = -9993
316064 ZDOT = -3045
962736
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 12338
54288241
00016717 00000-0 10270-3 0 9053
2 25544 51
6475
2369 0016322 358
9587 1
1528 15
51945606 4327
Satellite: ISS
Catalog Number: 25544
Epoch time: 12338
54288241 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node:
2369 deg
Eccentricity:
0016322
Arg of perigee: 358
9587 deg
Mean anomaly: 1
1528 deg
Mean motion: 15
51945606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 304
Coasting Arc #7 (Orbit 446)
---------------------------------------
Vector Time (GMT): 2012/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4094823
78 A = 6788849
15 meter
Y = -3586238
52 meter E =
0016028
Z = -4052885
61 I = 51
61779
XDOT = 6082
336465 Wp = 27
19254
YDOT = 2560
904367 meter/sec RA = 354
92860 deg
ZDOT = 3899
254780 TA = 283
17906
MA = 283
35784
Ha = 229
067 n
mi
Hp = 215
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13434461
22 X = 4154309
59
Y = -11765874
42 feet Y = -3540114
82 meter
Z = -13296868
80 Z = -4032848
77
XDOT = 19955
172129 XDOT = 6034
306067
YDOT = 8401
917214 feet/sec YDOT = 2628
652090 meter/sec
ZDOT = 12792
830643 ZDOT = 3928
686087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7271154
41 X = 2216247
87
Y = 16378833
08 feet Y = 4992268
32 meter
Z = -13213304
25 Z = -4027415
14
XDOT = -12682
716869 XDOT = -3865
692102
YDOT = 15995
510109 feet/sec YDOT = 4875
431481 meter/sec
ZDOT = 12914
506588 ZDOT = 3936
341608
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 12339
50878322
00016717 00000-0 10270-3 0 9066
2 25544 51
6486 355
4385 0016389 2
5769 357
5464 15
51932517 4479
Satellite: ISS
Catalog Number: 25544
Epoch time: 12339
50878322 = yrday
fracday
Element set: 906
Inclination: 51
6486 deg
RA of node: 355
4385 deg
Eccentricity:
0016389
Arg of perigee: 2
5769 deg
Mean anomaly: 357
5464 deg
Mean motion: 15
51932517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 339
Coasting Arc #8 (Orbit 462)
---------------------------------------
Vector Time (GMT): 2012/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4778323
60 A = 6791018
90 meter
Y = 3513349
33 meter E =
0021461
Z = 3312753
85 I = 51
59389
XDOT = -5353
700709 Wp = 41
97625
YDOT = -2827
744318 meter/sec RA = 349
95695 deg
ZDOT = -4689
967902 TA = 99
54026
MA = 99
29767
Ha = 229
115 n
mi
Hp = 214
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15676914
70 X = -4833348
16
Y = 11526736
64 feet Y = 3459607
33 meter
Z = 10868615
00 Z = 3289407
35
XDOT = -17564
634872 XDOT = -5298
899461
YDOT = -9277
376373 feet/sec YDOT = -2887
306144 meter/sec
ZDOT = -15387
033800 ZDOT = -4715
843071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6703488
18 X = -2043223
20
Y = -18324833
64 feet Y = -5585409
29 meter
Z = 10771342
64 Z = 3283105
24
XDOT = 12427
614973 XDOT = 3787
937044
YDOT = -13718
238016 feet/sec YDOT = -4181
318947 meter/sec
ZDOT = -15493
927066 ZDOT = -4722
548970
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 12340
53906357
00016717 00000-0 10270-3 0 9072
2 25544 51
6473 350
3187 0016455 6
4742 353
6619 15
51985781 4635
Satellite: ISS
Catalog Number: 25544
Epoch time: 12340
53906357 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 350
3187 deg
Eccentricity:
0016455
Arg of perigee: 6
4742 deg
Mean anomaly: 353
6619 deg
Mean motion: 15
51985781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 321
Coasting Arc #9 (Orbit 477)
---------------------------------------
Vector Time (GMT): 2012/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5265014
95 A = 6792948
67 meter
Y = -3468045
66 meter E =
0020898
Z = -2503044
54 I = 51
57124
XDOT = 4570
334588 Wp = 19
08535
YDOT = 3132
352390 meter/sec RA = 344
98799 deg
ZDOT = 5305
298273 TA = 312
81301
MA = 312
98850
Ha = 229
227 n
mi
Hp = 214
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17273671
09 X = 5315563
37
Y = -11378102
54 feet Y = -3408886
25 meter
Z = -8212088
37 Z = -2477344
47
XDOT = 14994
536049 XDOT = 4509
196160
YDOT = 10276
746687 feet/sec YDOT = 3183
118718 meter/sec
ZDOT = 17405
834230 ZDOT = 5327
352506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6461454
44 X = 1969451
31
Y = 19693571
91 feet Y = 6002600
72 meter
Z = -8105069
88 Z = -2470425
30
XDOT = -12372
052162 XDOT = -3771
001499
YDOT = 11216
712644 feet/sec YDOT = 3418
854014 meter/sec
ZDOT = 17496
842140 ZDOT = 5333
037484
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 12341
50494057
00016717 00000-0 10270-3 0 9080
2 25544 51
6479 345
5206 0016398 10
3337 349
8149 15
51995300 4788
Satellite: ISS
Catalog Number: 25544
Epoch time: 12341
50494057 = yrday
fracday
Element set: 908
Inclination: 51
6479 deg
RA of node: 345
5206 deg
Eccentricity:
0016398
Arg of perigee: 10
3337 deg
Mean anomaly: 349
8149 deg
Mean motion: 15
51995300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 478
Checksum: 322
Coasting Arc #10 (Orbit 493)
---------------------------------------
Vector Time (GMT): 2012/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5695687
82 A = 6794517
46 meter
Y = 3374463
20 meter E =
0018771
Z = 1542605
42 I = 51
54629
XDOT = -3653
784872 Wp = 59
02095
YDOT = -3517
388751 meter/sec RA = 340
01842 deg
ZDOT = -5734
937209 TA = 104
13398
MA = 103
92532
Ha = 229
317 n
mi
Hp = 214
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18686639
84 X = -5740492
17
Y = 11071073
50 feet Y = 3310519
90 meter
Z = 5061041
41 Z = 1514827
01
XDOT = -11987
483175 XDOT = -3586
321814
YDOT = -11539
989341 feet/sec YDOT = -3557
870287 meter/sec
ZDOT = -18815
410791 ZDOT = -5752
523548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6160696
17 X = -1877780
19
Y = -20855740
49 feet Y = -6356829
70 meter
Z = 4945424
97 Z = 1507365
53
XDOT = 12572
149227 XDOT = 3831
991084
YDOT = -8241
458991 feet/sec YDOT = -2511
996700 meter/sec
ZDOT = -18887
841105 ZDOT = -5757
013969
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 12342
53519598
00016717 00000-0 10270-3 0 9093
2 25544 51
6467 340
4004 0016553 13
8683 346
2920 15
52014744 4941
Satellite: ISS
Catalog Number: 25544
Epoch time: 12342
53519598 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 340
4004 deg
Eccentricity:
0016553
Arg of perigee: 13
8683 deg
Mean anomaly: 346
2920 deg
Mean motion: 15
52014744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 308
Coasting Arc #11 (Orbit 508)
---------------------------------------
Vector Time (GMT): 2012/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5916089
92 A = 6795244
04 meter
Y = -3260689
02 meter E =
0026721
Z = -579766
71 I = 51
52069
XDOT = 2753
238604 Wp = 26
69421
YDOT = 3956
318573 meter/sec RA = 335
05003 deg
ZDOT = 5974
097134 TA = 327
03467
MA = 327
20101
Ha = 229
286 n
mi
Hp = 214
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19409743
85 X = 5954928
35
Y = -10697798
64 feet Y = -3194314
43 meter
Z = -1902121
74 Z = -550931
99
XDOT = 9032
935052 XDOT = 2679
772379
YDOT = 12980
047812 feet/sec YDOT = 3986
696028 meter/sec
ZDOT = 19600
056215 ZDOT = 5987
294114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5994608
87 X = 1827156
78
Y = 21346843
72 feet Y = 6506517
97 meter
Z = -1782146
68 Z = -543198
31
XDOT = -13113
192378 XDOT = -3996
901037
YDOT = 5285
207647 feet/sec YDOT = 1610
931291 meter/sec
ZDOT = 19654
228349 ZDOT = 5990
608801
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 12343
50104871
00016717 00000-0 10270-3 0 9107
2 25544 51
6466 335
6020 0016354 17
7026 342
4692 15
52055925 5094
Satellite: ISS
Catalog Number: 25544
Epoch time: 12343
50104871 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 335
6020 deg
Eccentricity:
0016354
Arg of perigee: 17
7026 deg
Mean anomaly: 342
4692 deg
Mean motion: 15
52055925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 509
Checksum: 285
Coasting Arc #12 (Orbit 524)
---------------------------------------
Vector Time (GMT): 2012/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6057844
84 A = 6795273
85 meter
Y = 3055569
80 meter E =
0015127
Z = -469307
84 I = 51
49288
XDOT = -1790
962425 Wp = 60
81808
YDOT = -4445
624297 meter/sec RA = 330
07884 deg
ZDOT = -5965
551258 TA = 124
24096
MA = 124
09757
Ha = 229
492 n
mi
Hp = 213
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19874819
04 X = -6089282
80
Y = 10024835
29 feet Y = 2987651
43 meter
Z = -1539723
90 Z = -498813
27
XDOT = -5875
860976 XDOT = -1712
137640
YDOT = -14585
381553 feet/sec YDOT = -4465
210917 meter/sec
ZDOT = -19572
018562 ZDOT = -5974
060577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5609217
62 X = -1709689
53
Y = -21532520
69 feet Y = -6563112
31 meter
Z = -1662448
39 Z = -506714
27
XDOT = 13902
419861 XDOT = 4237
457574
YDOT = -2140
377300 feet/sec YDOT = -652
387001 meter/sec
ZDOT = -19606
690139 ZDOT = -5976
119155
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 12344
53127870
00016717 00000-0 10270-3 0 9116
2 25544 51
6459 330
4814 0016626 21
1199 339
0635 15
52043640 5250
Satellite: ISS
Catalog Number: 25544
Epoch time: 12344
53127870 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 330
4814 deg
Eccentricity:
0016626
Arg of perigee: 21
1199 deg
Mean anomaly: 339
0635 deg
Mean motion: 15
52043640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 525
Checksum: 290
Coasting Arc #13 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2012/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6006923
28 A = 6794321
16 meter
Y = -2781949
53 meter E =
0028692
Z = 1449531
03 I = 51
46393
XDOT = 901
827397 Wp = 41
18619
YDOT = 4979
700590 meter/sec RA = 325
10629 deg
ZDOT = 5775
925608 TA = 334
68368
MA = 334
82400
Ha = 229
348 n
mi
Hp = 213
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19707753
53 X = 6030543
55
Y = -9127131
02 feet Y = -2714644
41 meter
Z = 4755679
22 Z = 1478770
05
XDOT = 2958
751304 XDOT = 818
017691
YDOT = 16337
600362 feet/sec YDOT = 4989
316337 meter/sec
ZDOT = 18949
887166 ZDOT = 5780
103528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5134169
70 X = 1564894
93
Y = 21075321
47 feet Y = 6423757
98 meter
Z = 4877261
68 Z = 1486589
36
XDOT = -15043
087652 XDOT = -4585
133116
YDOT = -757
115680 feet/sec YDOT = -230
768859 meter/sec
ZDOT = 18966
529661 ZDOT = 5780
998241
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 12345
56149343
00016717 00000-0 10270-3 0 9120
2 25544 51
6456 325
3624 0016381 24
8750 335
3188 15
52096085 5411
Satellite: ISS
Catalog Number: 25544
Epoch time: 12345
56149343 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 325
3624 deg
Eccentricity:
0016381
Arg of perigee: 24
8750 deg
Mean anomaly: 335
3188 deg
Mean motion: 15
52096085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 305
Coasting Arc #14 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2012/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5886728
41 A = 6792703
52 meter
Y = 2387931
96 meter E =
0016308
Z = -2434557
59 I = 51
43414
XDOT = -34
753184 Wp = 46
62836
YDOT = -5496
417073 meter/sec RA = 320
12836 deg
ZDOT = -5318
709535 TA = 160
60923
MA = 160
54711
Ha = 229
636 n
mi
Hp = 213
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19313413
41 X = -5901166
53
Y = 7834422
46 feet Y = 2322022
42 meter
Z = -7987393
66 Z = -2463190
31
XDOT = -114
019634 XDOT = 52
548975
YDOT = -18032
864414 feet/sec YDOT = -5496
317012 meter/sec
ZDOT = -17449
834433 ZDOT = -5318
666887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4296828
64 X = -1309673
37
Y = -20347184
83 feet Y = -6201821
94 meter
Z = -8106411
24 Z = -2470834
15
XDOT = 16266
285092 XDOT = 4957
963696
YDOT = 3501
755872 feet/sec YDOT = 1067
335190 meter/sec
ZDOT = -17448
910100 ZDOT = -5318
427799
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 12346
52731095
00016717 00000-0 10270-3 0 9139
2 25544 51
6457 320
5615 0016691 28
2814 331
9240 15
52081077 5564
Satellite: ISS
Catalog Number: 25544
Epoch time: 12346
52731095 = yrday
fracday
Element set: 913
Inclination: 51
6457 deg
RA of node: 320
5615 deg
Eccentricity:
0016691
Arg of perigee: 28
2814 deg
Mean anomaly: 331
9240 deg
Mean motion: 15
52081077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 297
Coasting Arc #15 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2012/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5615458
36 A = 6790482
42 meter
Y = -1890342
30 meter E =
0025607
Z = 3283073
09 I = 51
40456
XDOT = -730
269279 Wp = 55
56384
YDOT = 6025
329895 meter/sec RA = 315
14716 deg
ZDOT = 4706
367432 TA = 342
76104
MA = 342
84784
Ha = 229
437 n
mi
Hp = 213
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18423419
82 X = 5620230
61
Y = -6201910
43 feet Y = -1827520
47 meter
Z = 10771237
16 Z = 3310364
38
XDOT = -2395
896586 XDOT = -820
454223
YDOT = 19768
142699 feet/sec YDOT = 6016
658713 meter/sec
ZDOT = 15440
838033 ZDOT = 4702
601489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3179900
09 X = 969233
55
Y = 19113312
15 feet Y = 5825737
54 meter
Z = 10884630
21 Z = 3317635
29
XDOT = -17721
048974 XDOT = -5401
375727
YDOT = -5857
788255 feet/sec YDOT = -1785
453860 meter/sec
ZDOT = 15424
407314 ZDOT = 4701
359349
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 12347
55749990
00016717 00000-0 10270-3 0 9147
2 25544 51
6459 315
4423 0016458 31
8063 328
4079 15
52127783 5727
Satellite: ISS
Catalog Number: 25544
Epoch time: 12347
55749990 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 315
4423 deg
Eccentricity:
0016458
Arg of perigee: 31
8063 deg
Mean anomaly: 328
4079 deg
Mean motion: 15
52127783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 328
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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