[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 28th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15876 77 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 322)
---------------------------------------
Vector Time (GMT): 2012/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2037492
35 A = 6789640
19 meter
Y = -5159380
20 meter E =
0015839
Z = -3926386
67 I = 51
84930
XDOT = 6452
973580 Wp = 354
32860
YDOT = 568
019470 meter/sec RA = 34
66963 deg
ZDOT = -4078
224570 TA = 232
95120
MA = 233
09616
Ha = 227
703 n
mi
Hp = 217
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6684686
19 X = -1960573
73
Y = -16927100
38 feet Y = -5181734
44 meter
Z = -12881846
02 Z = -3936098
35
XDOT = 21171
173164 XDOT = 6465
953790
YDOT = 1863
580938 feet/sec YDOT = 640
253429 meter/sec
ZDOT = -13380
001871 ZDOT = -4046
844070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18133811
97 X = 5527185
89
Y = 1164094
45 feet Y = 354815
99 meter
Z = -12921434
18 Z = -3938453
14
XDOT = -10581
675181 XDOT = -3225
294595
YDOT = 17154
100522 feet/sec YDOT = 5228
569839 meter/sec
ZDOT = -13249
966378 ZDOT = -4038
589752
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 12331
52365924
00016717 00000-0 10270-3 0 9003
2 25544 51
6483 35
1061 0015944 330
7745 29
2513 15
51774883 3236
Satellite: ISS
Catalog Number: 25544
Epoch time: 12331
52365924 = yrday
fracday
Element set: 900
Inclination: 51
6483 deg
RA of node: 35
1061 deg
Eccentricity:
0015944
Arg of perigee: 330
7745 deg
Mean anomaly: 29
2513 deg
Mean motion: 15
51774883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 293
Coasting Arc #2 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2012/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1392414
30 A = 6787388
91 meter
Y = 4874661
23 meter E =
0011183
Z = 4505873
82 I = 51
81713
XDOT = -6883
677711 Wp = 6
48886
YDOT = -1006
841024 meter/sec RA = 29
71279 deg
ZDOT = 3226
508192 TA = 51
19948
MA = 51
09967
Ha = 227
853 n
mi
Hp = 217
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4568288
38 X = 1315912
35
Y = 15992983
03 feet Y = 4889804
03 meter
Z = 14783050
60 Z = 4512452
74
XDOT = -22584
244460 XDOT = -6887
581363
YDOT = -3303
284198 feet/sec YDOT = -1083
840647 meter/sec
ZDOT = 10585
656799 ZDOT = 3193
057346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16432268
83 X = -5008555
54
Y = -2416050
84 feet Y = -736412
30 meter
Z = 14809678
91 Z = 4513990
13
XDOT = 12054
204673 XDOT = 3674
121584
YDOT = -18148
360625 feet/sec YDOT = -5531
620319 meter/sec
ZDOT = 10447
097546 ZDOT = 3184
275332
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 12332
55403686
00016717 00000-0 10270-3 0 9016
2 25544 51
6487 29
9876 0016021 334
7446 25
2921 15
51828425 3392
Satellite: ISS
Catalog Number: 25544
Epoch time: 12332
55403686 = yrday
fracday
Element set: 901
Inclination: 51
6487 deg
RA of node: 29
9876 deg
Eccentricity:
0016021
Arg of perigee: 334
7446 deg
Mean anomaly: 25
2921 deg
Mean motion: 15
51828425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 312
Coasting Arc #3 (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 = -714673
58 A = 6785719
50 meter
Y = -4611105
36 meter E =
0019318
Z = -4938282
82 I = 51
78413
XDOT = 7184
997142 Wp = 17
46695
YDOT = 1339
877815 meter/sec RA = 24
75174 deg
ZDOT = -2275
272933 TA = 230
21875
MA = 230
38903
Ha = 228
048 n
mi
Hp = 216
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2344729
58 X = -639068
60
Y = -15128298
44 feet Y = -4618674
17 meter
Z = -16201715
28 Z = -4941571
45
XDOT = 23572
825268 XDOT = 7180
533305
YDOT = 4395
924591 feet/sec YDOT = 1420
200165 meter/sec
ZDOT = -7464
806212 ZDOT = -2240
378619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14802799
96 X = 4511893
43
Y = 3849466
48 feet Y = 1173317
38 meter
Z = -16214730
01 Z = -4942249
71
XDOT = -12999
990635 XDOT = -3962
397146
YDOT = 18939
596676 feet/sec YDOT = 5772
789067 meter/sec
ZDOT = -7320
308337 ZDOT = -2231
229981
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
51999944
00016717 00000-0 10270-3 0 9021
2 25544 51
6483 25
1895 0016039 338
7619 21
2865 15
51830386 3541
Satellite: ISS
Catalog Number: 25544
Epoch time: 12333
51999944 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 25
1895 deg
Eccentricity:
0016039
Arg of perigee: 338
7619 deg
Mean anomaly: 21
2865 deg
Mean motion: 15
51830386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 354
Checksum: 326
Coasting Arc #4 (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 = -107615
35 A = 6784332
06 meter
Y = 4332908
92 meter E =
0013251
Z = 5218355
40 I = 51
75181
XDOT = -7389
234138 Wp = 353
13162
YDOT = -1636
476297 meter/sec RA = 19
78540 deg
ZDOT = 1219
574543 TA = 85
25637
MA = 85
10506
Ha = 228
213 n
mi
Hp = 216
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -353068
74 X = -181408
84
Y = 14215580
46 feet Y = 4331292
43 meter
Z = 17120588
59 Z = 5217653
74
XDOT = -24242
894154 XDOT = -7376
310037
YDOT = -5369
016721 feet/sec YDOT = -1719
035176 meter/sec
ZDOT = 4001
228815 ZDOT = 1183
708655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13006692
25 X = -3964439
80
Y = -5757870
99 feet Y = -1754999
08 meter
Z = 17117091
38 Z = 5217289
45
XDOT = 13660
150427 XDOT = 4163
613850
YDOT = -19532
344236 feet/sec YDOT = -5953
458523 meter/sec
ZDOT = 3852
743683 ZDOT = 1174
316275
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
55033775
00016717 00000-0 10270-3 0 9038
2 25544 51
6481 20
0709 0016095 342
9377 17
1231 15
51885252 3708
Satellite: ISS
Catalog Number: 25544
Epoch time: 12334
55033775 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 20
0709 deg
Eccentricity:
0016095
Arg of perigee: 342
9377 deg
Mean anomaly: 17
1231 deg
Mean motion: 15
51885252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 290
Coasting Arc #5 (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 = 908500
75 A = 6783887
51 meter
Y = -4110268
56 meter E =
0019420
Z = -5329758
30 I = 51
72160
XDOT = 7428
855934 Wp = 34
53424
YDOT = 1847
922528 meter/sec RA = 14
81605 deg
ZDOT = -143
446866 TA = 234
00808
MA = 234
18829
Ha = 228
368 n
mi
Hp = 216
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2980645
52 X = 980286
20
Y = -13485133
07 feet Y = -4099707
26 meter
Z = -17486083
67 Z = -5325170
81
XDOT = 24372
886923 XDOT = 7408
336783
YDOT = 6062
737952 feet/sec YDOT = 1930
881921 meter/sec
ZDOT = -470
626202 ZDOT = -107
407039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11477680
52 X = 3498397
02
Y = 7725305
57 feet Y = 2354673
14 meter
Z = -17466501
87 Z = -5323789
77
XDOT = -13848
878580 XDOT = -4221
138191
YDOT = 19734
873715 feet/sec YDOT = 6015
189508 meter/sec
ZDOT = -321
449103 ZDOT = -97
977687
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
51626304
00016717 00000-0 10270-3 0 9042
2 25544 51
6485 15
2721 0016140 346
7130 13
3595 15
51888235 3853
Satellite: ISS
Catalog Number: 25544
Epoch time: 12335
51626304 = yrday
fracday
Element set: 904
Inclination: 51
6485 deg
RA of node: 15
2721 deg
Eccentricity:
0016140
Arg of perigee: 346
7130 deg
Mean anomaly: 13
3595 deg
Mean motion: 15
51888235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 385
Checksum: 289
Coasting Arc #6 (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 = -1815629
87 A = 6784058
42 meter
Y = 3895363
82 meter E =
0017946
Z = 5251339
31 I = 51
69224
XDOT = -7315
574706 Wp = 1
25066
YDOT = -2058
752755 meter/sec RA = 9
84345 deg
ZDOT = -984
588947 TA = 98
27489
MA = 98
07134
Ha = 228
510 n
mi
Hp = 215
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5956790
92 X = -1884563
75
Y = 12780065
03 feet Y = 3874674
41 meter
Z = 17228803
50 Z = 5242351
89
XDOT = -24001
229349 XDOT = -7287
226632
YDOT = -6754
438174 feet/sec YDOT = -2140
401490 meter/sec
ZDOT = -3230
278698 ZDOT = -1020
059333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9926226
10 X = -3025513
71
Y = -10078910
36 feet Y = -3072051
88 meter
Z = 17191006
13 Z = 5239818
67
XDOT = 13835
956285 XDOT = 4217
199476
YDOT = -19485
072242 feet/sec YDOT = -5939
050019 meter/sec
ZDOT = -3377
065705 ZDOT = -1029
329627
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
54656209
00016717 00000-0 10270-3 0 9054
2 25544 51
6477 10
1530 0016165 350
9945 9
0914 15
51949848 4018
Satellite: ISS
Catalog Number: 25544
Epoch time: 12336
54656209 = yrday
fracday
Element set: 905
Inclination: 51
6477 deg
RA of node: 10
1530 deg
Eccentricity:
0016165
Arg of perigee: 350
9945 deg
Mean anomaly: 9
0914 deg
Mean motion: 15
51949848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 401
Checksum: 306
Coasting Arc #7 (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 = 2633105
57 A = 6785140
38 meter
Y = -3750505
41 meter E =
0016648
Z = -5008892
65 I = 51
66664
XDOT = 7037
611222 Wp = 39
13451
YDOT = 2225
875493 meter/sec RA = 4
87045 deg
ZDOT = 2049
231151 TA = 250
71506
MA = 250
89520
Ha = 228
670 n
mi
Hp = 215
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8638797
79 X = 2699181
03
Y = -12304807
77 feet Y = -3720690
52 meter
Z = -16433374
84 Z = -4995940
87
XDOT = 23089
275664 XDOT = 7002
243197
YDOT = 7302
741120 feet/sec YDOT = 2304
376538 meter/sec
ZDOT = 6723
199315 ZDOT = 2083
334040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8773998
14 X = 2674314
63
Y = 12281409
20 feet Y = 3743373
52 meter
Z = -16379159
78 Z = -4992367
90
XDOT = -13538
955518 XDOT = -4126
673642
YDOT = 18755
341717 feet/sec YDOT = 5716
628155 meter/sec
ZDOT = 6864
293029 ZDOT = 2092
236515
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
51245044
00016717 00000-0 10270-3 0 9064
2 25544 51
6487 5
3540 0016251 354
5613 5
5360 15
51947104 4169
Satellite: ISS
Catalog Number: 25544
Epoch time: 12337
51245044 = yrday
fracday
Element set: 906
Inclination: 51
6487 deg
RA of node: 5
3540 deg
Eccentricity:
0016251
Arg of perigee: 354
5613 deg
Mean anomaly: 5
5360 deg
Mean motion: 15
51947104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 416
Checksum: 277
Coasting Arc #8 (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 = -3499250
84 A = 6786773
42 meter
Y = 3614463
55 meter E =
0021118
Z = 4559038
81 I = 51
64108
XDOT = -6573
131869 Wp = 21
01271
YDOT = -2434
599147 meter/sec RA = 359
89640 deg
ZDOT = -3091
240378 TA = 100
07651
MA = 99
83818
Ha = 228
744 n
mi
Hp = 215
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11480481
77 X = -3561555
34
Y = 11858476
22 feet Y = 3574984
06 meter
Z = 14957476
42 Z = 4541888
45
XDOT = -21565
393272 XDOT = -6530
402524
YDOT = -7987
530009 feet/sec YDOT = -2507
864889 meter/sec
ZDOT = -10141
864757 ZDOT = -3123
068879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7680037
27 X = -2340875
36
Y = -14682603
11 feet Y = -4475257
43 meter
Z = 14885872
98 Z = 4537214
08
XDOT = 13199
576284 XDOT = 4023
230851
YDOT = -17399
346745 feet/sec YDOT = -5303
320888 meter/sec
ZDOT = -10273
498805 ZDOT = -3131
362436
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
54271030
00016717 00000-0 10270-3 0 9073
2 25544 51
6476
2343 0016274 358
7643 1
3466 15
52019489 4322
Satellite: ISS
Catalog Number: 25544
Epoch time: 12338
54271030 = yrday
fracday
Element set: 907
Inclination: 51
6476 deg
RA of node:
2343 deg
Eccentricity:
0016274
Arg of perigee: 358
7643 deg
Mean anomaly: 1
3466 deg
Mean motion: 15
52019489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 289
Coasting Arc #9 (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 = 4209593
04 A = 6788855
13 meter
Y = -3536624
86 meter E =
0016041
Z = -3977411
31 I = 51
61873
XDOT = 5981
657970 Wp = 25
84987
YDOT = 2647
197640 meter/sec RA = 354
92448 deg
ZDOT = 3997
191340 TA = 285
75739
MA = 285
93424
Ha = 228
908 n
mi
Hp = 215
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13811000
77 X = 4268148
89
Y = -11603099
94 feet Y = -3489222
94 meter
Z = -13049249
70 Z = -3956819
18
XDOT = 19624
862106 XDOT = 5932
194349
YDOT = 8685
031626 feet/sec YDOT = 2713
811494 meter/sec
ZDOT = 13114
144815 ZDOT = 4026
130077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7005265
80 X = 2135205
02
Y = 16689378
92 feet Y = 5086922
69 meter
Z = -12963389
63 Z = -3951241
16
XDOT = -12832
957942 XDOT = -3911
485581
YDOT = 15614
044267 feet/sec YDOT = 4759
160693 meter/sec
ZDOT = 13233
766721 ZDOT = 4033
652096
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
50856197
00016717 00000-0 10270-3 0 9084
2 25544 51
6487 355
4356 0016328 2
4479 357
6749 15
52018288 4476
Satellite: ISS
Catalog Number: 25544
Epoch time: 12339
50856197 = yrday
fracday
Element set: 908
Inclination: 51
6487 deg
RA of node: 355
4356 deg
Eccentricity:
0016328
Arg of perigee: 2
4479 deg
Mean anomaly: 357
6749 deg
Mean motion: 15
52018288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 447
Checksum: 344
Coasting Arc #10 (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 = -4904773
40 A = 6791057
36 meter
Y = 3444255
13 meter E =
0021188
Z = 3198737
56 I = 51
59502
XDOT = -5206
087625 Wp = 43
18269
YDOT = -2933
773582 meter/sec RA = 349
95269 deg
ZDOT = -4789
820250 TA = 99
88623
MA = 99
64698
Ha = 228
938 n
mi
Hp = 214
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16091776
25 X = -4958462
07
Y = 11300049
65 feet Y = 3389106
57 meter
Z = 10494545
80 Z = 3174780
01
XDOT = -17080
339976 XDOT = -5149
626644
YDOT = -9625
241410 feet/sec YDOT = -2991
675421 meter/sec
ZDOT = -15714
633367 ZDOT = -4814
974290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6371148
51 X = -1941926
07
Y = -18658229
47 feet Y = -5687028
34 meter
Z = 10394749
45 Z = 3168319
63
XDOT = 12602
504046 XDOT = 3841
243233
YDOT = -13178
708420 feet/sec YDOT = -4016
870326 meter/sec
ZDOT = -15818
522409 ZDOT = -4821
485630
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
53878294
00016717 00000-0 10270-3 0 9092
2 25544 51
6474 350
3154 0016387 6
3660 353
7697 15
52079657 4636
Satellite: ISS
Catalog Number: 25544
Epoch time: 12340
53878294 = yrday
fracday
Element set: 909
Inclination: 51
6474 deg
RA of node: 350
3154 deg
Eccentricity:
0016387
Arg of perigee: 6
3660 deg
Mean anomaly: 353
7697 deg
Mean motion: 15
52079657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 463
Checksum: 332
Coasting Arc #11 (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 = 5396944
72 A = 6792954
41 meter
Y = -3373569
66 meter E =
0021349
Z = -2344476
52 I = 51
57241
XDOT = 4368
906956 Wp = 18
71453
YDOT = 3261
545751 meter/sec RA = 344
98364 deg
ZDOT = 5397
363222 TA = 315
10308
MA = 315
27556
Ha = 229
018 n
mi
Hp = 214
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17706511
54 X = 5445656
58
Y = -11068141
93 feet Y = -3312945
21 meter
Z = -7691852
11 Z = -2318140
01
XDOT = 14333
684240 XDOT = 4305
891598
YDOT = 10700
609420 feet/sec YDOT = 3310
049092 meter/sec
ZDOT = 17707
884587 ZDOT = 5418
434367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6050043
74 X = 1844053
33
Y = 20027381
28 feet Y = 6104345
81 meter
Z = -7582207
82 Z = -2311056
94
XDOT = -12583
888490 XDOT = -3835
569212
YDOT = 10496
339533 feet/sec YDOT = 3199
284290 meter/sec
ZDOT = 17794
799249 ZDOT = 5423
854811
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
50459759
00016717 00000-0 10270-3 0 9103
2 25544 51
6480 345
5169 0016304 10
2652 349
8830 15
52104295 4787
Satellite: ISS
Catalog Number: 25544
Epoch time: 12341
50459759 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 345
5169 deg
Eccentricity:
0016304
Arg of perigee: 10
2652 deg
Mean anomaly: 349
8830 deg
Mean motion: 15
52104295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 478
Checksum: 304
Coasting Arc #12 (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 = -5821079
57 A = 6794430
01 meter
Y = 3246252
77 meter E =
0018120
Z = 1336323
15 I = 51
54719
XDOT = -3392
584262 Wp = 59
90263
YDOT = -3667
614982 meter/sec RA = 340
01402 deg
ZDOT = -5800
700368 TA = 105
55909
MA = 105
35899
Ha = 229
101 n
mi
Hp = 214
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19098030
07 X = -5863438
83
Y = 10650435
61 feet Y = 3180920
94 meter
Z = 4384262
30 Z = 1307941
52
XDOT = -11130
525793 XDOT = -3323
141290
YDOT = -12032
857551 feet/sec YDOT = -3705
164537 meter/sec
ZDOT = -19031
169186 ZDOT = -5817
012988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5653234
93 X = -1723106
01
Y = -21147791
36 feet Y = -6445846
81 meter
Z = 4266162
50 Z = 1300326
33
XDOT = 12819
007611 XDOT = 3907
233520
YDOT = -7325
758477 feet/sec YDOT = -2232
891184 meter/sec
ZDOT = -19098
298765 ZDOT = -5821
161463
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
53477952
00016717 00000-0 10270-3 0 9113
2 25544 51
6468 340
3962 0016457 13
8372 346
3228 15
52128480 4947
Satellite: ISS
Catalog Number: 25544
Epoch time: 12342
53477952 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 340
3962 deg
Eccentricity:
0016457
Arg of perigee: 13
8372 deg
Mean anomaly: 346
3228 deg
Mean motion: 15
52128480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 494
Checksum: 314
Coasting Arc #13 (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 = 6025743
09 A = 6794960
39 meter
Y = -3089101
90 meter E =
0027079
Z = -325158
85 I = 51
52107
XDOT = 2428
382001 Wp = 27
77408
YDOT = 4129
103676 meter/sec RA = 335
04538 deg
ZDOT = 5998
920016 TA = 328
71324
MA = 328
87410
Ha = 229
032 n
mi
Hp = 213
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19769498
34 X = 6061417
80
Y = -10134848
74 feet Y = -3021518
79 meter
Z = -1066794
11 Z = -295799
11
XDOT = 7967
132549 XDOT = 2352
887215
YDOT = 13546
928070 feet/sec YDOT = 4155
837038 meter/sec
ZDOT = 19681
496117 ZDOT = 6010
533915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5365641
08 X = 1635447
40
Y = 21563946
20 feet Y = 6572690
80 meter
Z = -944665
83 Z = -287934
15
XDOT = -13406
556106 XDOT = -4086
318301
YDOT = 4163
718449 feet/sec YDOT = 1269
101383 meter/sec
ZDOT = 19729
082230 ZDOT = 6013
424264
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
50055655
00016717 00000-0 10270-3 0 9124
2 25544 51
6467 335
5974 0016238 17
6300 342
5412 15
52184617 5099
Satellite: ISS
Catalog Number: 25544
Epoch time: 12343
50055655 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 335
5974 deg
Eccentricity:
0016238
Arg of perigee: 17
6300 deg
Mean anomaly: 342
5412 deg
Mean motion: 15
52184617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 509
Checksum: 297
Coasting Arc #14 (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 = -6136867
83 A = 6794713
33 meter
Y = 2829534
92 meter E =
0014560
Z = -765838
48 I = 51
49241
XDOT = -1405
542359 Wp = 58
57673
YDOT = -4631
887704 meter/sec RA = 330
07359 deg
ZDOT = -5926
597164 TA = 129
69693
MA = 129
56846
Ha = 229
235 n
mi
Hp = 213
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20134080
81 X = -6164331
84
Y = 9283251
05 feet Y = 2760755
11 meter
Z = -2512593
45 Z = -795718
16
XDOT = -4611
359447 XDOT = -1324
852616
YDOT = -15196
481970 feet/sec YDOT = -4647
153891 meter/sec
ZDOT = -19444
216417 ZDOT = -5933
229579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4830825
98 X = -1472435
76
Y = -21623674
25 feet Y = -6590895
91 meter
Z = -2636838
72 Z = -803708
44
XDOT = 14226
574626 XDOT = 4336
259946
YDOT = -832
982394 feet/sec YDOT = -253
893034 meter/sec
ZDOT = -19471
082324 ZDOT = -5934
785892
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
53069874
00016717 00000-0 10270-3 0 9137
2 25544 51
6460 330
4762 0016507 21
1468 339
0362 15
52179538 5254
Satellite: ISS
Catalog Number: 25544
Epoch time: 12344
53069874 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 330
4762 deg
Eccentricity:
0016507
Arg of perigee: 21
1468 deg
Mean anomaly: 339
0362 deg
Mean motion: 15
52179538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 525
Checksum: 305
Coasting Arc #15 (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 = 6045604
04 A = 6793428
57 meter
Y = -2488683
21 meter E =
0028272
Z = 1780126
96 I = 51
46248
XDOT = 455
294721 Wp = 43
21984
YDOT = 5175
221228 meter/sec RA = 325
09989 deg
ZDOT = 5655
900459 TA = 336
40561
MA = 336
53503
Ha = 229
062 n
mi
Hp = 213
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19834658
92 X = 6064336
09
Y = -8164971
16 feet Y = -2420972
88 meter
Z = 5840311
55 Z = 1809542
05
XDOT = 1493
749085 XDOT = 369
914914
YDOT = 16979
072271 feet/sec YDOT = 5179
834798 meter/sec
ZDOT = 18556
103868 ZDOT = 5657
905308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4166891
54 X = 1270068
54
Y = 21006529
81 feet Y = 6402790
29 meter
Z = 5962584
00 Z = 1817395
60
XDOT = -15393
502579 XDOT = -4691
939586
YDOT = -2245
817823 feet/sec YDOT = -684
525273 meter/sec
ZDOT = 18563
711775 ZDOT = 5658
219349
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
56081824
00016717 00000-0 10270-3 0 9141
2 25544 51
6457 325
3565 0016260 24
8347 335
3584 15
52242819 5412
Satellite: ISS
Catalog Number: 25544
Epoch time: 12345
56081824 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 325
3565 deg
Eccentricity:
0016260
Arg of perigee: 24
8347 deg
Mean anomaly: 335
3584 deg
Mean motion: 15
52242819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 307
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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