[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 10th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 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 58)
---------------------------------------
Vector Time (GMT): 2012/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4422988
43 A = 6786674
57 meter
Y = 298097
90 meter E =
0002693
Z = -5137048
15 I = 51
93360
XDOT = -2401
894999 Wp = 297
56871
YDOT = 7088
604405 meter/sec RA = 118
68963 deg
ZDOT = -1654
805667 TA = 316
50573
MA = 316
52697
Ha = 225
156 n
mi
Hp = 219
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14511116
91 X = 4444281
44
Y = 978011
49 feet Y = 347677
33 meter
Z = -16853832
51 Z = -5115509
33
XDOT = -7880
232936 XDOT = -2472
943905
YDOT = 23256
576131 feet/sec YDOT = 7061
347576 meter/sec
ZDOT = -5429
152450 ZDOT = -1666
647125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10459193
24 X = -3187962
10
Y = 10253491
11 feet Y = 3125264
09 meter
Z = -16764602
21 Z = -5109850
75
XDOT = -11379
674708 XDOT = -3468
524851
YDOT = -20576
238668 feet/sec YDOT = -6271
637546 meter/sec
ZDOT = -5478
943406 ZDOT = -1669
981950
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 12314
51898175
00016717 00000-0 10270-3 0 9002
2 25544 51
6443 119
5230 0015572 263
8646 96
0731 15
51245987 598
Satellite: ISS
Catalog Number: 25544
Epoch time: 12314
51898175 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 119
5230 deg
Eccentricity:
0015572
Arg of perigee: 263
8646 deg
Mean anomaly: 96
0731 deg
Mean motion: 15
51245987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 59
Checksum: 314
Coasting Arc #2 (Orbit 74)
---------------------------------------
Vector Time (GMT): 2012/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4169634
23 A = 6786096
96 meter
Y = -827180
97 meter E =
0012902
Z = 5300931
70 I = 51
94445
XDOT = 2467
489370 Wp = 260
27483
YDOT = -7199
338532 meter/sec RA = 113
73969 deg
ZDOT = 817
046511 TA = 181
93143
MA = 181
93642
Ha = 224
987 n
mi
Hp = 220
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13679902
34 X = -4185825
98
Y = -2713848
33 feet Y = -873898
71 meter
Z = 17391508
19 Z = 5280636
02
XDOT = 8095
437565 XDOT = 2543
841364
YDOT = -23619
877072 feet/sec YDOT = -7171
318577 meter/sec
ZDOT = 2680
598788 ZDOT = 829
219552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11055549
93 X = 3369731
62
Y = -8671514
87 feet Y = -2643077
73 meter
Z = 17307481
15 Z = 5275320
25
XDOT = 11984
120984 XDOT = 3652
760076
YDOT = 20734
072602 feet/sec YDOT = 6319
745329 meter/sec
ZDOT = 2731
789508 ZDOT = 832
649442
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 12315
54973409
00016717 00000-0 10270-3 0 9011
2 25544 51
6437 114
4056 0015588 267
9888 91
9478 15
51210314 757
Satellite: ISS
Catalog Number: 25544
Epoch time: 12315
54973409 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 114
4056 deg
Eccentricity:
0015588
Arg of perigee: 267
9888 deg
Mean anomaly: 91
9478 deg
Mean motion: 15
51210314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 75
Checksum: 322
Coasting Arc #3 (Orbit 89)
---------------------------------------
Vector Time (GMT): 2012/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3944155
12 A = 6785660
78 meter
Y = 1389177
64 meter E =
0000706
Z = -5343498
53 I = 51
95601
XDOT = -2498
520056 Wp = 291
98759
YDOT = 7246
042315 meter/sec RA = 108
79179 deg
ZDOT = 39
831741 TA = 338
38900
MA = 338
39198
Ha = 224
983 n
mi
Hp = 219
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12940141
48 X = 3954286
15
Y = 4557669
43 feet Y = 1433340
12 meter
Z = -17531163
15 Z = -5324312
90
XDOT = -8197
244277 XDOT = -2579
554618
YDOT = 23773
104708 feet/sec YDOT = 7217
649214 meter/sec
ZDOT = 130
681565 ZDOT = 27
496630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11849156
20 X = -3611622
81
Y = 7112922
85 feet Y = 2168018
88 meter
Z = -17451794
17 Z = -5319306
86
XDOT = -12508
185086 XDOT = -3812
494814
YDOT = -20645
639287 feet/sec YDOT = -6292
790855 meter/sec
ZDOT = 78
796909 ZDOT = 24
017298
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 12316
51605264
00016717 00000-0 10270-3 0 9021
2 25544 51
6446 109
6099 0015517 271
2044 88
7329 15
51276773 901
Satellite: ISS
Catalog Number: 25544
Epoch time: 12316
51605264 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 109
6099 deg
Eccentricity:
0015517
Arg of perigee: 271
2044 deg
Mean anomaly: 88
7329 deg
Mean motion: 15
51276773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 90
Checksum: 306
Coasting Arc #4 (Orbit 105)
---------------------------------------
Vector Time (GMT): 2012/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3775414
46 A = 6786066
14 meter
Y = -1978893
76 meter E =
0012864
Z = 5291402
58 I = 51
96554
XDOT = 2496
262771 Wp = 284
03177
YDOT = -7179
259031 meter/sec RA = 103
84253 deg
ZDOT = -902
642304 TA = 174
58597
MA = 174
57205
Ha = 224
969 n
mi
Hp = 220
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12386530
39 X = -3778710
69
Y = -6492433
60 feet Y = -2021131
20 meter
Z = 17360244
68 Z = 5273053
23
XDOT = 8189
838486 XDOT = 2580
742185
YDOT = -23553
999444 feet/sec YDOT = -7150
871915 meter/sec
ZDOT = -2961
424883 ZDOT = -890
309947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12885694
10 X = 3927559
56
Y = -5671345
16 feet Y = -1728626
00 meter
Z = 17284405
00 Z = 5268286
64
XDOT = 12804
504394 XDOT = 3902
812939
YDOT = 20213
414842 feet/sec YDOT = 6161
048844 meter/sec
ZDOT = -2909
538438 ZDOT = -886
827316
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 12317
54678500
00016717 00000-0 10270-3 0 9039
2 25544 51
6444 104
4924 0015474 275
2652 84
6733 15
51231412 1063
Satellite: ISS
Catalog Number: 25544
Epoch time: 12317
54678500 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 104
4924 deg
Eccentricity:
0015474
Arg of perigee: 275
2652 deg
Mean anomaly: 84
6733 deg
Mean motion: 15
51231412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 106
Checksum: 286
Coasting Arc #5 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2012/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3646048
82 A = 6786591
20 meter
Y = 2566958
54 meter E =
0002509
Z = -5114216
49 I = 51
97569
XDOT = -2489
694626 Wp = 255
18890
YDOT = 7034
349505 meter/sec RA = 98
89633 deg
ZDOT = 1754
418841 TA = 31
70908
MA = 31
69397
Ha = 225
146 n
mi
Hp = 219
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11962102
42 X = 3641918
04
Y = 8421779
97 feet Y = 2607707
96 meter
Z = -16778925
50 Z = -5096513
57
XDOT = -8168
289455 XDOT = -2576
691985
YDOT = 23078
574491 feet/sec YDOT = 7006
021711 meter/sec
ZDOT = 5755
967327 ZDOT = 1742
112499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14048368
32 X = -4281942
66
Y = 4371404
62 feet Y = 1332404
13 meter
Z = -16705830
78 Z = -5091937
22
XDOT = -12888
410720 XDOT = -3928
387587
YDOT = -19603
360245 feet/sec YDOT = -5975
104203 meter/sec
ZDOT = 5704
182448 ZDOT = 1738
634810
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 12318
51308400
00016717 00000-0 10270-3 0 9047
2 25544 51
6457 99
6968 0015553 278
7640 81
1750 15
51300609 1216
Satellite: ISS
Catalog Number: 25544
Epoch time: 12318
51308400 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 99
6968 deg
Eccentricity:
0015553
Arg of perigee: 278
7640 deg
Mean anomaly: 81
1750 deg
Mean motion: 15
51300609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 121
Checksum: 297
Coasting Arc #6 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2012/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3576620
83 A = 6787858
10 meter
Y = -3152292
24 meter E =
0011151
Z = 4842102
48 I = 51
98373
XDOT = 2482
031449 Wp = 308
42396
YDOT = -6769
423214 meter/sec RA = 93
95013 deg
ZDOT = -2570
924298 TA = 166
82403
MA = 166
79488
Ha = 225
234 n
mi
Hp = 219
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11734320
32 X = -3564627
91
Y = -10342166
13 feet Y = -3192221
45 meter
Z = 15886162
98 Z = 4824755
89
XDOT = 8143
147798 XDOT = 2570
033399
YDOT = -22209
393746 feet/sec YDOT = -6741
175404 meter/sec
ZDOT = -8434
791005 ZDOT = -2558
652966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15368743
66 X = 4684393
07
Y = -3274842
75 feet Y = -998172
07 meter
Z = 15814612
59 Z = 4820293
92
XDOT = 12630
785287 XDOT = 3849
863355
YDOT = 18749
120148 feet/sec YDOT = 5714
731821 meter/sec
ZDOT = -8383
158925 ZDOT = -2555
186840
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 12319
54379574
00016717 00000-0 10270-3 0 9052
2 25544 51
6461 94
5799 0015487 282
6976 77
2444 15
51269565 1377
Satellite: ISS
Catalog Number: 25544
Epoch time: 12319
54379574 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 94
5799 deg
Eccentricity:
0015487
Arg of perigee: 282
6976 deg
Mean anomaly: 77
2444 deg
Mean motion: 15
51269565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 353
Coasting Arc #7 (Orbit 151)
---------------------------------------
Vector Time (GMT): 2012/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3543054
94 A = 6789211
04 meter
Y = 3697970
70 meter E =
0006557
Z = -4450772
45 I = 51
99108
XDOT = -2503
429897 Wp = 281
01710
YDOT = 6428
375541 meter/sec RA = 89
00707 deg
ZDOT = 3345
271277 TA = 22
62341
MA = 22
59452
Ha = 225
580 n
mi
Hp = 219
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11624195
98 X = 3523061
45
Y = 12132449
80 feet Y = 3737479
88 meter
Z = -14602271
82 Z = -4433608
37
XDOT = -8213
352682 XDOT = -2591
378211
YDOT = 21090
470934 feet/sec YDOT = 6399
888642 meter/sec
ZDOT = 10975
299464 ZDOT = 3332
896277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16692601
74 X = -5087905
01
Y = 2394983
77 feet Y = 729991
05 meter
Z = -14531542
00 Z = -4429214
00
XDOT = -12077
590082 XDOT = -3681
249457
YDOT = -17842
911609 feet/sec YDOT = -5438
519458 meter/sec
ZDOT = 10923
256795 ZDOT = 3329
408671
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 12320
51007591
00016717 00000-0 10270-3 0 9069
2 25544 51
6473 89
7842 0015656 286
5913 73
3519 15
51317144 1521
Satellite: ISS
Catalog Number: 25544
Epoch time: 12320
51007591 = yrday
fracday
Element set: 906
Inclination: 51
6473 deg
RA of node: 89
7842 deg
Eccentricity:
0015656
Arg of perigee: 286
5913 deg
Mean anomaly: 73
3519 deg
Mean motion: 15
51317144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 152
Checksum: 304
Coasting Arc #8 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2012/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3559427
20 A = 6790932
03 meter
Y = -4210474
81 meter E =
0008187
Z = 3973627
97 I = 51
99577
XDOT = 2554
439872 Wp = 332
95662
YDOT = -5978
206789 meter/sec RA = 84
06533 deg
ZDOT = -4042
544153 TA = 159
13917
MA = 159
10574
Ha = 225
682 n
mi
Hp = 219
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11677910
78 X = -3531383
55
Y = -13813893
73 feet Y = -4250122
04 meter
Z = 13036837
16 Z = 3956403
95
XDOT = 8380
708241 XDOT = 2640
737668
YDOT = -19613
539335 feet/sec YDOT = -5949
158634 meter/sec
ZDOT = -13262
940134 ZDOT = -4029
925411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18054184
55 X = 5502915
45
Y = -1757192
98 feet Y = -535592
42 meter
Z = 12965919
81 Z = 3952012
36
XDOT = 11134
525811 XDOT = 3393
803467
YDOT = 16835
138759 feet/sec YDOT = 5131
350294 meter/sec
ZDOT = -13209
922977 ZDOT = -4026
384523
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 12321
54076683
00016717 00000-0 10270-3 0 9072
2 25544 51
6478 84
6681 0015555 290
3950 69
5530 15
51315545 1683
Satellite: ISS
Catalog Number: 25544
Epoch time: 12321
54076683 = yrday
fracday
Element set: 907
Inclination: 51
6478 deg
RA of node: 84
6681 deg
Eccentricity:
0015555
Arg of perigee: 290
3950 deg
Mean anomaly: 69
5530 deg
Mean motion: 15
51315545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 168
Checksum: 319
Coasting Arc #9 (Orbit 182)
---------------------------------------
Vector Time (GMT): 2012/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3592723
40 A = 6792650
46 meter
Y = 4649313
07 meter E =
0011657
Z = -3393043
25 I = 51
99832
XDOT = -2664
050802 Wp = 305
05104
YDOT = 5469
558032 meter/sec RA = 79
12572 deg
ZDOT = 4669
035667 TA = 15
55691
MA = 15
52111
Ha = 226
120 n
mi
Hp = 219
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11787150
27 X = 3556949
62
Y = 15253651
79 feet Y = 4689289
33 meter
Z = -11132031
67 Z = -3375676
36
XDOT = -8740
324155 XDOT = -2747
695933
YDOT = 17944
744199 feet/sec YDOT = 5439
298971 meter/sec
ZDOT = 15318
358486 ZDOT = 4655
890845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19271331
93 X = -5873901
97
Y = 1346247
72 feet Y = 410336
31 meter
Z = -11060574
87 Z = -3371263
22
XDOT = -9882
016094 XDOT = -3012
038505
YDOT = -15929
348086 feet/sec YDOT = -4855
265297 meter/sec
ZDOT = 15263
207590 ZDOT = 4652
225673
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 12322
50702832
00016717 00000-0 10270-3 0 9082
2 25544 51
6485 79
8720 0015749 294
6056 65
3454 15
51335504 1833
Satellite: ISS
Catalog Number: 25544
Epoch time: 12322
50702832 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 79
8720 deg
Eccentricity:
0015749
Arg of perigee: 294
6056 deg
Mean anomaly: 65
3454 deg
Mean motion: 15
51335504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 183
Checksum: 309
Coasting Arc #10 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2012/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3654350
73 A = 6794264
20 meter
Y = -5030870
32 meter E =
0004735
Z = 2745544
73 I = 51
99732
XDOT = 2824
138105 Wp = 353
20255
YDOT = -4880
014080 meter/sec RA = 74
18808 deg
ZDOT = -5179
403958 TA = 155
96000
MA = 155
93789
Ha = 226
200 n
mi
Hp = 219
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11989339
68 X = -3611160
24
Y = -16505480
06 feet Y = -5071494
19 meter
Z = 9007692
67 Z = 2727896
57
XDOT = 9265
544965 XDOT = 2903
658149
YDOT = -16010
544882 feet/sec YDOT = -4847
987943 meter/sec
ZDOT = -16992
795137 ZDOT = -5165
491368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20399487
15 X = 6217763
68
Y = -1156838
54 feet Y = -352604
39 meter
Z = 8935116
90 Z = 2723423
63
XDOT = 8277
501101 XDOT = 2522
982336
YDOT = 15072
767166 feet/sec YDOT = 4594
179432 meter/sec
ZDOT = -16934
521832 ZDOT = -5161
642254
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 12323
53769842
00016717 00000-0 10270-3 0 9091
2 25544 51
6486 74
7562 0015608 298
2606 61
6970 15
51357436 1994
Satellite: ISS
Catalog Number: 25544
Epoch time: 12323
53769842 = yrday
fracday
Element set: 909
Inclination: 51
6486 deg
RA of node: 74
7562 deg
Eccentricity:
0015608
Arg of perigee: 298
2606 deg
Mean anomaly: 61
6970 deg
Mean motion: 15
51357436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 339
Coasting Arc #11 (Orbit 213)
---------------------------------------
Vector Time (GMT): 2012/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3701385
02 A = 6795701
17 meter
Y = 5315543
03 meter E =
0016347
Z = -2019481
58 I = 51
99345
XDOT = -3061
848259 Wp = 326
60764
YDOT = 4261
076262 meter/sec RA = 69
25107 deg
ZDOT = 5595
673539 TA = 11
19772
MA = 11
16139
Ha = 226
642 n
mi
Hp = 219
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12143651
63 X = 3651480
67
Y = 17439445
63 feet Y = 5356655
25 meter
Z = -6625595
74 Z = -2001621
34
XDOT = -10045
433922 XDOT = -3136
451687
YDOT = 13979
908996 feet/sec YDOT = 4226
419474 meter/sec
ZDOT = 18358
508987 ZDOT = 5580
618002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21243516
65 X = -6475023
88
Y = 1132705
72 feet Y = 345248
70 meter
Z = -6552177
94 Z = -1997103
84
XDOT = -6422
384232 XDOT = -1957
542714
YDOT = -14461
550635 feet/sec YDOT = -4407
880634 meter/sec
ZDOT = 18295
564104 ZDOT = 5576
487939
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 12324
50394095
00016717 00000-0 10270-3 0 9105
2 25544 51
6491 69
9594 0015798 302
6417 57
3210 15
51361229 2143
Satellite: ISS
Catalog Number: 25544
Epoch time: 12324
50394095 = yrday
fracday
Element set: 910
Inclination: 51
6491 deg
RA of node: 69
9594 deg
Eccentricity:
0015798
Arg of perigee: 302
6417 deg
Mean anomaly: 57
3210 deg
Mean motion: 15
51361229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 214
Checksum: 302
Coasting Arc #12 (Orbit 229)
---------------------------------------
Vector Time (GMT): 2012/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3748420
17 A = 6796642
84 meter
Y = -5530772
93 meter E =
0002270
Z = 1254903
22 I = 51
98492
XDOT = 3353
858924 Wp = 334
69635
YDOT = -3603
172766 meter/sec RA = 64
31582 deg
ZDOT = -5864
248847 TA = 191
75315
MA = 191
75845
Ha = 226
721 n
mi
Hp = 219
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12297966
42 X = -3692391
40
Y = -18145580
46 feet Y = -5572376
84 meter
Z = 4117136
56 Z = 1236829
42
XDOT = 11003
474160 XDOT = 3422
388552
YDOT = -11821
432960 feet/sec YDOT = -3565
284571 meter/sec
ZDOT = -19239
661572 ZDOT = -5847
789389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21898278
38 X = 6674595
25
Y = -1254405
14 feet Y = -382342
69 meter
Z = 4042864
53 Z = 1232265
11
XDOT = 4341
143261 XDOT = 1323
180466
YDOT = 14017
668687 feet/sec YDOT = 4272
585416 meter/sec
ZDOT = -19170
970060 ZDOT = -5843
311674
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 12325
53459046
00016717 00000-0 10270-3 0 9118
2 25544 51
6488 64
8436 0015654 306
1779 53
7924 15
51393627 2306
Satellite: ISS
Catalog Number: 25544
Epoch time: 12325
53459046 = yrday
fracday
Element set: 911
Inclination: 51
6488 deg
RA of node: 64
8436 deg
Eccentricity:
0015654
Arg of perigee: 306
1779 deg
Mean anomaly: 53
7924 deg
Mean motion: 15
51393627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 230
Checksum: 318
Coasting Arc #13 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2012/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3742437
36 A = 6797219
75 meter
Y = 5641358
93 meter E =
0019124
Z = -443941
98 I = 51
97351
XDOT = -3727
322385 Wp = 346
16055
YDOT = 2949
400406 meter/sec RA = 59
37956 deg
ZDOT = 6022
602021 TA = 9
07444
MA = 9
03992
Ha = 227
100 n
mi
Hp = 219
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12278337
79 X = 3681232
95
Y = 18508395
45 feet Y = 5682867
00 meter
Z = -1456502
55 Z = -425909
82
XDOT = -12228
747981 XDOT = -3789
282954
YDOT = 9676
510518 feet/sec YDOT = 2907
372691 meter/sec
ZDOT = 19759
192981 ZDOT = 6004
344156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22170157
84 X = -6757464
11
Y = 1418691
47 feet Y = 432417
16 meter
Z = -1382424
23 Z = -421362
91
XDOT = -2125
340906 XDOT = -647
803908
YDOT = -13914
265931 feet/sec YDOT = -4241
068256 meter/sec
ZDOT = 19683
120739 ZDOT = 5999
415201
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 12326
50081409
00016717 00000-0 10270-3 0 9121
2 25544 51
6495 60
0465 0015812 310
5674 49
4100 15
51394668 2453
Satellite: ISS
Catalog Number: 25544
Epoch time: 12326
50081409 = yrday
fracday
Element set: 912
Inclination: 51
6495 deg
RA of node: 60
0465 deg
Eccentricity:
0015812
Arg of perigee: 310
5674 deg
Mean anomaly: 49
4100 deg
Mean motion: 15
51394668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 245
Checksum: 288
Coasting Arc #14 (Orbit 260)
---------------------------------------
Vector Time (GMT): 2012/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3708897
68 A = 6797120
09 meter
Y = -5685941
42 meter E =
0004538
Z = -369345
51 I = 51
95656
XDOT = 4138
000438 Wp = 304
70589
YDOT = -2304
898446 meter/sec RA = 54
44388 deg
ZDOT = -6014
963488 TA = 239
24960
MA = 239
29430
Ha = 227
219 n
mi
Hp = 219
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12168299
48 X = -3643246
41
Y = -18654663
44 feet Y = -5727049
55 meter
Z = -1211763
50 Z = -387203
98
XDOT = 13576
116922 XDOT = 4192
686510
YDOT = -7562
002777 feet/sec YDOT = -2258
318962 meter/sec
ZDOT = -19734
132178 ZDOT = -5994
728145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22209497
36 X = 6769454
79
Y = -1618357
05 feet Y = -493275
23 meter
Z = -1285106
53 Z = -391700
47
XDOT = -124
734584 XDOT = -38
019101
YDOT = 14026
885890 feet/sec YDOT = 4275
394819 meter/sec
ZDOT = -19649
937782 ZDOT = -5989
301036
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 12327
53144352
00016717 00000-0 10270-3 0 9133
2 25544 51
6488 54
9308 0015721 314
1223 45
8635 15
51427095 2614
Satellite: ISS
Catalog Number: 25544
Epoch time: 12327
53144352 = yrday
fracday
Element set: 913
Inclination: 51
6488 deg
RA of node: 54
9308 deg
Eccentricity:
0015721
Arg of perigee: 314
1223 deg
Mean anomaly: 45
8635 deg
Mean motion: 15
51427095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 261
Checksum: 291
Coasting Arc #15 (Orbit 276)
---------------------------------------
Vector Time (GMT): 2012/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3584276
23 A = 6796547
33 meter
Y = 5634884
32 meter E =
0019036
Z = 1192033
32 I = 51
93710
XDOT = -4617
186765 Wp = 3
11876
YDOT = 1694
137506 meter/sec RA = 49
50548 deg
ZDOT = 5888
927241 TA = 9
77715
MA = 9
74016
Ha = 227
494 n
mi
Hp = 218
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11759436
45 X = 3515208
65
Y = 18487153
28 feet Y = 5674579
75 meter
Z = 3910870
49 Z = 1209278
15
XDOT = -15148
250542 XDOT = -4664
395389
YDOT = 5558
193916 feet/sec YDOT = 1642
241243 meter/sec
ZDOT = 19320
627432 ZDOT = 5866
382098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21831194
56 X = -6654148
10
Y = 1702757
03 feet Y = 519000
34 meter
Z = 3981664
55 Z = 1213611
36
XDOT = 2367
479650 XDOT = 721
607797
YDOT = -14499
729295 feet/sec YDOT = -4419
517489 meter/sec
ZDOT = 19226
931013 ZDOT = 5860
368573
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 12328
56206247
00016717 00000-0 10270-3 0 9140
2 25544 51
6497 49
8138 0015820 318
5093 41
4856 15
51437403 2779
Satellite: ISS
Catalog Number: 25544
Epoch time: 12328
56206247 = yrday
fracday
Element set: 914
Inclination: 51
6497 deg
RA of node: 49
8138 deg
Eccentricity:
0015820
Arg of perigee: 318
5093 deg
Mean anomaly: 41
4856 deg
Mean motion: 15
51437403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 277
Checksum: 313
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list