[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 24th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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 2366)
---------------------------------------
Vector Time (GMT): 2012/205/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2615581
48 A = 6787364
56 meter
Y = 6167361
54 meter E =
0012751
Z = 1051285
41 I = 51
36013
XDOT = -4825
800543 Wp = 125
23026
YDOT = -1038
477159 meter/sec RA = 300
18883 deg
ZDOT = -5871
049883 TA = 43
32146
MA = 43
22128
Ha = 219
841 n
mi
Hp = 214
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8581304
08 X = -2689458
63
Y = 20234125
79 feet Y = 6137699
38 meter
Z = 3449099
11 Z = 1038399
98
XDOT = -15832
678948 XDOT = -4785
309568
YDOT = -3407
077292 feet/sec YDOT = -1092
215652 meter/sec
ZDOT = -19261
974681 ZDOT = -5894
394772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21498462
21 X = 6552731
28
Y = -4609004
88 feet Y = -1404824
69 meter
Z = 3395306
73 Z = 1034889
49
XDOT = 5919
730085 XDOT = 1804
333730
YDOT = 13245
590089 feet/sec YDOT = 4037
255859 meter/sec
ZDOT = -19358
122019 ZDOT = -5900
355591
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 12205
54611450
00016717 00000-0 10270-3 0 9003
2 25544 51
6427 300
6872 0000921 279
8848 80
2201 15
54648926 23672
Satellite: ISS
Catalog Number: 25544
Epoch time: 12205
54611450 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 300
6872 deg
Eccentricity:
0000921
Arg of perigee: 279
8848 deg
Mean anomaly: 80
2201 deg
Mean motion: 15
54648926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2367
Checksum: 299
Coasting Arc #2 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2012/206/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3446590
00 A = 6787468
25 meter
Y = -5781438
88 meter E =
0012959
Z = 822007
32 I = 51
34657
XDOT = 3772
609558 Wp = 50
02124
YDOT = 3097
968206 meter/sec RA = 295
19568 deg
ZDOT = 5916
999649 TA = 318
90890
MA = 319
00643
Ha = 219
821 n
mi
Hp = 214
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11307709
99 X = 3506990
00
Y = -18967975
34 feet Y = -5742559
29 meter
Z = 2696874
39 Z = 838897
04
XDOT = 12377
327947 XDOT = 3708
943877
YDOT = 10163
937685 feet/sec YDOT = 3139
799684 meter/sec
ZDOT = 19412
728506 ZDOT = 5935
172111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21977781
58 X = -6698827
83
Y = 2059524
75 feet Y = 627743
14 meter
Z = 2767128
40 Z = 843420
74
XDOT = 1135
976124 XDOT = 346
245522
YDOT = -14291
696461 feet/sec YDOT = -4356
109081 meter/sec
ZDOT = 19487
329762 ZDOT = 5939
738111
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 12206
57458898
00016717 00000-0 10270-3 0 9013
2 25544 51
6430 295
5555 0000988 296
0399 64
0652 15
54666187 23838
Satellite: ISS
Catalog Number: 25544
Epoch time: 12206
57458898 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 295
5555 deg
Eccentricity:
0000988
Arg of perigee: 296
0399 deg
Mean anomaly: 64
0652 deg
Mean motion: 15
54666187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2383
Checksum: 345
Coasting Arc #3 (Orbit 2397)
---------------------------------------
Vector Time (GMT): 2012/207/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4005959
33 A = 6784743
39 meter
Y = 4805688
51 meter E =
0004001
Z = -2623955
30 I = 51
32444
XDOT = -2595
723320 Wp = 127
86705
YDOT = -4998
425406 meter/sec RA = 290
19826 deg
ZDOT = -5199
443877 TA = 81
82978
MA = 81
78440
Ha = 219
790 n
mi
Hp = 214
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13142911
19 X = -4046653
29
Y = 15766694
59 feet Y = 4760663
98 meter
Z = -8608777
24 Z = -2643514
57
XDOT = -8516
152626 XDOT = -2514
379409
YDOT = -16399
033484 feet/sec YDOT = -5026
997333 meter/sec
ZDOT = -17058
542905 ZDOT = -5211
856361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20470904
49 X = 6239531
69
Y = 928978
43 feet Y = 283152
63 meter
Z = -8689930
20 Z = -2648690
73
XDOT = -7937
726484 XDOT = -2419
419032
YDOT = 15109
493618 feet/sec YDOT = 4605
373655 meter/sec
ZDOT = -17109
197034 ZDOT = -5214
883256
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 12207
53877486
00016717 00000-0 10270-3 0 9029
2 25544 51
6418 290
7450 0000996 297
4026 62
7026 15
54681525 23985
Satellite: ISS
Catalog Number: 25544
Epoch time: 12207
53877486 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 290
7450 deg
Eccentricity:
0000996
Arg of perigee: 297
4026 deg
Mean anomaly: 62
7026 deg
Mean motion: 15
54681525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2398
Checksum: 328
Coasting Arc #4 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2012/208/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4278542
46 A = 6780494
66 meter
Y = -3329572
14 meter E =
0009572
Z = 4065344
38 I = 51
30150
XDOT = 1412
173300 Wp = 100
66253
YDOT = 6497
971330 meter/sec RA = 285
18819 deg
ZDOT = 3826
265543 TA = 309
57491
MA = 309
65942
Ha = 219
649 n
mi
Hp = 214
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14037212
80 X = 4295707
99
Y = -10923793
10 feet Y = -3281631
11 meter
Z = 13337744
03 Z = 4086170
73
XDOT = 4633
114501 XDOT = 1320
819639
YDOT = 21318
803575 feet/sec YDOT = 6513
252086 meter/sec
ZDOT = 12553
364641 ZDOT = 3832
904327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17205834
06 X = -5244338
22
Y = -4245521
45 feet Y = -1294034
94 meter
Z = 13423965
01 Z = 4091624
53
XDOT = 13659
373463 XDOT = 4163
377032
YDOT = -15483
141229 feet/sec YDOT = -4719
261447 meter/sec
ZDOT = 12580
059917 ZDOT = 3834
402263
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 12208
56722931
00016717 00000-0 10270-3 0 9038
2 25544 51
6423 285
6129 0001075 303
9151 56
1900 15
54721886 24140
Satellite: ISS
Catalog Number: 25544
Epoch time: 12208
56722931 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 285
6129 deg
Eccentricity:
0001075
Arg of perigee: 303
9151 deg
Mean anomaly: 56
1900 deg
Mean motion: 15
54721886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2414
Checksum: 292
Coasting Arc #5 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2012/209/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4339958
24 A = 6776944
64 meter
Y = 1462593
13 meter E =
0012348
Z = -5006600
80 I = 51
28154
XDOT = -254
470185 Wp = 71
10630
YDOT = -7404
957512 meter/sec RA = 280
16552 deg
ZDOT = -1942
662247 TA = 179
92477
MA = 179
92458
Ha = 219
822 n
mi
Hp = 213
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14238708
13 X = -4331669
89
Y = 4798533
89 feet Y = 1414107
81 meter
Z = -16425855
66 Z = -5027663
76
XDOT = -834
875934 XDOT = -162
210547
YDOT = -24294
480025 feet/sec YDOT = -7407
287129 meter/sec
ZDOT = -6373
563802 ZDOT = -1943
675013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12636070
31 X = 3851474
23
Y = 7951771
48 feet Y = 2423699
95 meter
Z = -16512859
48 Z = -5033119
57
XDOT = -17779
221073 XDOT = -5419
106583
YDOT = 15010
284526 feet/sec YDOT = 4575
134724 meter/sec
ZDOT = -6376
972042 ZDOT = -1943
701079
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 12209
53139875
00016717 00000-0 10270-3 0 9046
2 25544 51
6414 280
8022 0001112 312
7597 47
3463 15
54699676 24296
Satellite: ISS
Catalog Number: 25544
Epoch time: 12209
53139875 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 280
8022 deg
Eccentricity:
0001112
Arg of perigee: 312
7597 deg
Mean anomaly: 47
3463 deg
Mean motion: 15
54699676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 316
Coasting Arc #6 (Orbit 2444)
---------------------------------------
Vector Time (GMT): 2012/210/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4199958
58 A = 6775531
53 meter
Y = 591301
47 meter E =
0002067
Z = 5282418
14 I = 51
27353
XDOT = -835
870989 Wp = 52
08554
YDOT = 7623
274921 meter/sec RA = 275
13423 deg
ZDOT = -187
446019 TA = 39
71689
MA = 39
70175
Ha = 219
608 n
mi
Hp = 213
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13779391
68 X = 4167373
79
Y = 1939965
45 feet Y = 638085
26 meter
Z = 17330768
17 Z = 5302742
10
XDOT = -2742
358887 XDOT = -920
143330
YDOT = 25010
744493 feet/sec YDOT = 7613
456520 meter/sec
ZDOT = -614
980378 ZDOT = -191
710487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7314327
58 X = -2229407
05
Y = -11714342
66 feet Y = -3570531
64 meter
Z = 17414517
35 Z = 5307944
89
XDOT = 20050
700000 XDOT = 6111
453360
YDOT = -13467
313684 feet/sec YDOT = -4104
837211 meter/sec
ZDOT = -633
349661 ZDOT = -193
044977
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 12210
55983447
00016717 00000-0 10270-3 0 9053
2 25544 51
6420 275
6704 0001187 317
9869 42
1193 15
54755857 24458
Satellite: ISS
Catalog Number: 25544
Epoch time: 12210
55983447 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 275
6704 deg
Eccentricity:
0001187
Arg of perigee: 317
9869 deg
Mean anomaly: 42
1193 deg
Mean motion: 15
54755857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2445
Checksum: 325
Coasting Arc #7 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2012/211/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3914555
30 A = 6777332
88 meter
Y = -2611141
95 meter E =
0011304
Z = -4888009
70 I = 51
27697
XDOT = 1852
887383 Wp = 102
21815
YDOT = -7069
873707 meter/sec RA = 270
10341 deg
ZDOT = 2294
959073 TA = 190
35147
MA = 190
37477
Ha = 219
862 n
mi
Hp = 213
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12843029
20 X = -3861321
50
Y = -8566738
68 feet Y = -2654618
73 meter
Z = -16036777
25 Z = -4906897
19
XDOT = 6079
026846 XDOT = 1920
658206
YDOT = -23195
123709 feet/sec YDOT = -7048
774903 meter/sec
ZDOT = 7529
393284 ZDOT = 2304
124008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1907322
45 X = 581351
88
Y = 15238068
50 feet Y = 4644563
28 meter
Z = -16114404
26 Z = -4911670
42
XDOT = -20343
444063 XDOT = -6200
681750
YDOT = 10542
023984 feet/sec YDOT = 3213
208910 meter/sec
ZDOT = 7567
908368 ZDOT = 2306
698471
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 12211
52398671
00016717 00000-0 10270-3 0 9061
2 25544 51
6413 270
8594 0001230 333
1537 26
9553 15
54740750 24608
Satellite: ISS
Catalog Number: 25544
Epoch time: 12211
52398671 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 270
8594 deg
Eccentricity:
0001230
Arg of perigee: 333
1537 deg
Mean anomaly: 26
9553 deg
Mean motion: 15
54740750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 293
Coasting Arc #8 (Orbit 2475)
---------------------------------------
Vector Time (GMT): 2012/212/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3460080
68 A = 6781102
86 meter
Y = 4390237
10 meter E =
0011029
Z = 3831946
97 I = 51
29109
XDOT = -2813
856428 Wp = 75
15482
YDOT = 5826
195504 meter/sec RA = 265
08174 deg
ZDOT = -4121
506317 TA = 58
41069
MA = 58
30308
Ha = 219
749 n
mi
Hp = 213
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11351970
74 X = 3392116
59
Y = 14403665
04 feet Y = 4428549
45 meter
Z = 12572004
49 Z = 3848590
97
XDOT = -9231
812428 XDOT = -2858
776032
YDOT = 19114
814646 feet/sec YDOT = 5794
478499 meter/sec
ZDOT = -13522
002354 ZDOT = -4135
284138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3150346
41 X = 960225
59
Y = -18019114
24 feet Y = -5492226
02 meter
Z = 12640211
34 Z = 3852736
42
XDOT = 19009
036323 XDOT = 5793
954271
YDOT = -6231
550387 feet/sec YDOT = -1899
376558 meter/sec
ZDOT = -13579
410544 ZDOT = -4139
004334
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 12212
55240429
00016717 00000-0 10270-3 0 9073
2 25544 51
6413 265
7277 0001330 335
7912 24
3178 15
54790667 24769
Satellite: ISS
Catalog Number: 25544
Epoch time: 12212
55240429 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 265
7277 deg
Eccentricity:
0001330
Arg of perigee: 335
7912 deg
Mean anomaly: 24
3178 deg
Mean motion: 15
54790667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2476
Checksum: 306
Coasting Arc #9 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2012/213/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2864025
46 A = 6785142
83 meter
Y = -5704541
69 meter E =
0006548
Z = -2294476
85 I = 51
30774
XDOT = 3683
774172 Wp = 35
48527
YDOT = -4014
023355 meter/sec RA = 260
07293 deg
ZDOT = 5394
503733 TA = 298
83172
MA = 298
89744
Ha = 219
874 n
mi
Hp = 213
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9396409
00 X = -2788877
45
Y = -18715687
97 feet Y = -5736148
62 meter
Z = -7527811
18 Z = -2308207
83
XDOT = 12085
873268 XDOT = 3702
181334
YDOT = -13169
367961 feet/sec YDOT = -3972
726675 meter/sec
ZDOT = 17698
503061 ZDOT = 5412
443284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7305488
44 X = -2226712
88
Y = 19604894
83 feet Y = 5975571
94 meter
Z = -7583887
98 Z = -2311569
06
XDOT = -16369
565117 XDOT = -4989
443448
YDOT = 758
940390 feet/sec YDOT = 231
325031 meter/sec
ZDOT = 17772
893229 ZDOT = 5417
177856
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 12213
51653928
00016717 00000-0 10270-3 0 9083
2 25544 51
6409 260
9165 0001242 345
9624 14
1494 15
54787462 24916
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
51653928 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 260
9165 deg
Eccentricity:
0001242
Arg of perigee: 345
9624 deg
Mean anomaly: 14
1494 deg
Mean motion: 15
54787462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 313
Coasting Arc #10 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2012/214/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2064668
80 A = 6787288
26 meter
Y = 6446593
05 meter E =
0011896
Z = 417964
45 I = 51
32119
XDOT = -4458
751638 Wp = 125
93085
YDOT = 1822
250754 meter/sec RA = 255
07443 deg
ZDOT = -5968
022550 TA = 49
54132
MA = 49
43766
Ha = 219
942 n
mi
Hp = 213
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6773847
76 X = 1990397
89
Y = 21150239
67 feet Y = 6469266
16 meter
Z = 1371274
43 Z = 427814
31
XDOT = -14628
450255 XDOT = -4449
806459
YDOT = 5978
512971 feet/sec YDOT = 1772
440647 meter/sec
ZDOT = -19580
126477 ZDOT = -5989
660572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10513778
84 X = 3204599
79
Y = -19559314
12 feet Y = -5961678
94 meter
Z = 1411286
87 Z = 430160
24
XDOT = 12952
118343 XDOT = 3947
805671
YDOT = 5517
062358 feet/sec YDOT = 1681
600607 meter/sec
ZDOT = -19669
559933 ZDOT = -5995
281867
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 12214
54493908
00016717 00000-0 10270-3 0 9098
2 25544 51
6408 255
7841 0001367 353
5679 6
5457 15
54803934 25076
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
54493908 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 255
7841 deg
Eccentricity:
0001367
Arg of perigee: 353
5679 deg
Mean anomaly: 6
5457 deg
Mean motion: 15
54803934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 328
Coasting Arc #11 (Orbit 2522)
---------------------------------------
Vector Time (GMT): 2012/215/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1099458
55 A = 6786537
92 meter
Y = -6522217
23 meter E =
0014722
Z = 1485080
76 I = 51
32624
XDOT = 5061
151200 Wp = 56
56302
YDOT = 463
149858 meter/sec RA = 250
07855 deg
ZDOT = 5747
736618 TA = 319
73336
MA = 319
84231
Ha = 220
075 n
mi
Hp = 213
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3607147
48 X = -1033658
07
Y = -21398350
48 feet Y = -6534144
21 meter
Z = 4872312
20 Z = 1479899
31
XDOT = 16604
826772 XDOT = 5027
675507
YDOT = 1519
520532 feet/sec YDOT = 519
559369 meter/sec
ZDOT = 18857
403603 ZDOT = 5772
241554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12562681
94 X = -3829105
45
Y = 17699769
50 feet Y = 5394889
74 meter
Z = 4851548
69 Z = 1478752
04
XDOT = -9291
032124 XDOT = -2831
906591
YDOT = -11821
073014 feet/sec YDOT = -3603
063055 meter/sec
ZDOT = 18958
451769 ZDOT = 5778
536099
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 12215
57333138
00016717 00000-0 10270-3 0 9102
2 25544 51
6399 250
6519 0001530 2
4878 357
6283 15
54771364 25230
Satellite: ISS
Catalog Number: 25544
Epoch time: 12215
57333138 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 250
6519 deg
Eccentricity:
0001530
Arg of perigee: 2
4878 deg
Mean anomaly: 357
6283 deg
Mean motion: 15
54771364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2523
Checksum: 306
Coasting Arc #12 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2012/216/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -74105
02 A = 6782892
28 meter
Y = 5968502
74 meter E =
0004659
Z = -3226453
51 I = 51
32643
XDOT = -5411
235510 Wp = 81
41270
YDOT = -2630
115291 meter/sec RA = 245
07590 deg
ZDOT = -4746
279864 TA = 136
10989
MA = 136
07286
Ha = 220
002 n
mi
Hp = 213
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -243126
71 X = -125167
52
Y = 19581701
89 feet Y = 5967388
61 meter
Z = -10585477
38 Z = -3226937
39
XDOT = -17753
397341 XDOT = -5358
367027
YDOT = -8628
987176 feet/sec YDOT = -2690
331383 meter/sec
ZDOT = -15571
784332 ZDOT = -4772
438432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13736833
76 X = 4186986
93
Y = -13955203
27 feet Y = -4253545
96 meter
Z = -10588021
12 Z = -3227228
84
XDOT = 5681
056691 XDOT = 1731
586079
YDOT = 17475
443891 feet/sec YDOT = 5326
515298 meter/sec
ZDOT = -15679
462658 ZDOT = -4779
100218
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 12216
53743724
00016717 00000-0 10270-3 0 9116
2 25544 51
6404 245
8400 0001423 3
0618 357
0544 15
54823180 25386
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
53743724 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 245
8400 deg
Eccentricity:
0001423
Arg of perigee: 3
0618 deg
Mean anomaly: 357
0544 deg
Mean motion: 15
54823180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 276
Coasting Arc #13 (Orbit 2553)
---------------------------------------
Vector Time (GMT): 2012/217/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1364249
02 A = 6778628
95 meter
Y = -4866375
13 meter E =
0008669
Z = 4511106
57 I = 51
32455
XDOT = 5434
297859 Wp = 102
92725
YDOT = 4425
625312 meter/sec RA = 240
06091 deg
ZDOT = 3123
737362 TA = 315
60754
MA = 315
67700
Ha = 220
029 n
mi
Hp = 213
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4475882
61 X = 1396650
94
Y = -15965797
68 feet Y = -4850938
10 meter
Z = 14800218
41 Z = 4517812
58
XDOT = 17829
061218 XDOT = 5369
231610
YDOT = 14519
768083 feet/sec YDOT = 4486
031190 meter/sec
ZDOT = 10248
482160 ZDOT = 3149
978382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14101367
51 X = -4298096
82
Y = 8675191
24 feet Y = 2644198
29 meter
Z = 14828323
46 Z = 4519672
99
XDOT = -2441
686842 XDOT = -744
226149
YDOT = -21709
900913 feet/sec YDOT = -6617
177798 meter/sec
ZDOT = 10356
349390 ZDOT = 3156
615294
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 12217
56580984
00016717 00000-0 10270-3 0 9128
2 25544 51
6390 240
7069 0001504 11
1618 348
9568 15
54822912 25540
Satellite: ISS
Catalog Number: 25544
Epoch time: 12217
56580984 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 240
7069 deg
Eccentricity:
0001504
Arg of perigee: 11
1618 deg
Mean anomaly: 348
9568 deg
Mean motion: 15
54822912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2554
Checksum: 312
Coasting Arc #14 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2012/218/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2727161
09 A = 6775705
88 meter
Y = 3380362
77 meter E =
0014754
Z = -5213565
47 I = 51
33181
XDOT = -5016
364982 Wp = 76
35017
YDOT = -5688
584097 meter/sec RA = 235
03577 deg
ZDOT = -1063
473328 TA = 183
40041
MA = 183
41045
Ha = 220
043 n
mi
Hp = 213
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8947378
91 X = -2739432
40
Y = 11090429
03 feet Y = 3349797
31 meter
Z = -17104873
58 Z = -5226843
50
XDOT = -16457
890360 XDOT = -4947
215205
YDOT = -18663
333651 feet/sec YDOT = -5744
293577 meter/sec
ZDOT = -3489
085721 ZDOT = -1087
674211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13993803
20 X = 4265311
22
Y = -2310679
00 feet Y = -704294
96 meter
Z = -17159957
47 Z = -5230355
04
XDOT = -466
180265 XDOT = -142
091745
YDOT = 23847
012662 feet/sec YDOT = 7268
569459 meter/sec
ZDOT = -3588
435480 ZDOT = -1093
755134
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 12218
52989954
00016717 00000-0 10270-3 0 9136
2 25544 51
6399 235
8955 0001475 8
5201 351
5977 15
54832368 25699
Satellite: ISS
Catalog Number: 25544
Epoch time: 12218
52989954 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 235
8955 deg
Eccentricity:
0001475
Arg of perigee: 8
5201 deg
Mean anomaly: 351
5977 deg
Mean motion: 15
54832368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 349
Coasting Arc #15 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2012/219/12:17:11
249
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4013002
12 A = 6775620
22 meter
Y = -1677850
20 meter E =
0005119
Z = 5192638
65 I = 51
34918
XDOT = 4140
943863 Wp = 44
81858
YDOT = 6356
951794 meter/sec RA = 230
00602 deg
ZDOT = -1141
905842 TA = 56
19248
MA = 56
14374
Ha = 219
927 n
mi
Hp = 213
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13166017
46 X = 4006241
58
Y = -5504757
87 feet Y = -1633012
08 meter
Z = 17036216
03 Z = 5212116
97
XDOT = 13585
773830 XDOT = 4075
098404
YDOT = 20856
141058 feet/sec YDOT = 6402
890233 meter/sec
ZDOT = -3746
410244 ZDOT = -1121
949557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13463113
15 X = -4103556
89
Y = -4431820
45 feet Y = -1350818
87 meter
Z = 17116734
01 Z = 5217180
53
XDOT = 3118
965864 XDOT = 950
660795
YDOT = -23682
189266 feet/sec YDOT = -7218
331288 meter/sec
ZDOT = -3664
621176 ZDOT = -1116
976535
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 12219
55825289
00016717 00000-0 10270-3 0 9141
2 25544 51
6388 230
7622 0001573 13
9750 346
1446 15
54863878 25859
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
55825289 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 230
7622 deg
Eccentricity:
0001573
Arg of perigee: 13
9750 deg
Mean anomaly: 346
1446 deg
Mean motion: 15
54863878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2585
Checksum: 334
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