[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 9th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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
348/14:31:55
256 -1
0 1
4 1
4
N/A 0
9 0
1 230
4
000/00:07:50
512 -0
4 0
3 213
2
Coasting Arc #1 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2012/340/15:24:58
435
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5830847
07 A = 6791342
43 meter
Y = -1466148
36 meter E =
0016931
Z = -3181943
51 I = 51
58999
XDOT = 3781
883278 Wp = 21
42223
YDOT = -4592
826726 meter/sec RA = 349
30386 deg
ZDOT = -4806
697133 TA = 195
22992
MA = 195
28095
Ha = 229
202 n
mi
Hp = 214
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19130075
70 X = -5798561
69
Y = -4810198
03 feet Y = -1531171
89 meter
Z = -10439447
22 Z = -3210191
29
XDOT = 12407
753538 XDOT = 3856
310119
YDOT = -15068
329155 feet/sec YDOT = -4550
119009 meter/sec
ZDOT = -15770
003718 ZDOT = -4788
144220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7079587
48 X = -2157858
26
Y = -18344550
12 feet Y = -5591418
88 meter
Z = -10556362
13 Z = -3217579
18
XDOT = 18185
840593 XDOT = 5543
044213
YDOT = 2025
480509 feet/sec YDOT = 617
366459 meter/sec
ZDOT = -15692
459222 ZDOT = -4783
061571
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
66792350
00016717 00000-0 10270-3 0 9005
2 25544 51
6466 349
6841 0016588 6
3421 353
7938 15
51937029 4654
Satellite: ISS
Catalog Number: 25544
Epoch time: 12340
66792350 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 349
6841 deg
Eccentricity:
0016588
Arg of perigee: 6
3421 deg
Mean anomaly: 353
7938 deg
Mean motion: 15
51937029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 323
Coasting Arc #2 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2012/341/15:24:58
435
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5253550
07 A = 6789018
32 meter
Y = 1747188
23 meter E =
0019741
Z = 3906022
49 I = 51
55323
XDOT = -4567
638652 Wp = 43
17791
YDOT = 4637
805935 meter/sec RA = 344
33182 deg
ZDOT = 4070
826476 TA = 4
21973
MA = 4
20311
Ha = 229
091 n
mi
Hp = 214
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17236056
67 X = 5214647
47
Y = 5732244
86 feet Y = 1805719
08 meter
Z = 12815034
41 Z = 3931449
75
XDOT = -14985
691116 XDOT = -4638
935398
YDOT = 15215
898738 feet/sec YDOT = 4586
328976 meter/sec
ZDOT = 13355
729909 ZDOT = 4048
463888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5521810
38 X = 1683047
80
Y = 17226232
12 feet Y = 5250555
55 meter
Z = 12920213
80 Z = 3938081
17
XDOT = -19924
914932 XDOT = -6073
114071
YDOT = -3555
631734 feet/sec YDOT = -1083
756552 meter/sec
ZDOT = 13262
389989 ZDOT = 4042
376469
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
69821237
00016717 00000-0 10270-3 0 9017
2 25544 51
6471 344
5658 0016428 9
7871 350
3597 15
51972671 4813
Satellite: ISS
Catalog Number: 25544
Epoch time: 12341
69821237 = yrday
fracday
Element set: 901
Inclination: 51
6471 deg
RA of node: 344
5658 deg
Eccentricity:
0016428
Arg of perigee: 9
7871 deg
Mean anomaly: 350
3597 deg
Mean motion: 15
51972671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 324
Coasting Arc #3 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2012/342/15:24:58
435
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4637969
59 A = 6786936
51 meter
Y = -2088156
05 meter E =
0023483
Z = -4515293
05 I = 51
51720
XDOT = 5185
047677 Wp = 33
21250
YDOT = -4644
038134 meter/sec RA = 339
35320 deg
ZDOT = -3166
857897 TA = 204
79154
MA = 204
90456
Ha = 229
389 n
mi
Hp = 214
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15216435
67 X = -4592340
17
Y = -6850905
68 feet Y = -2139765
47 meter
Z = -14813953
57 Z = -4537713
56
XDOT = 17011
311275 XDOT = 5251
976965
YDOT = -15236
345585 feet/sec YDOT = -4585
681374 meter/sec
ZDOT = -10389
953731 ZDOT = -3141
506460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3697094
28 X = -1126874
34
Y = -16188029
00 feet Y = -4934111
24 meter
Z = -14906617
81 Z = -4543537
11
XDOT = 21282
499623 XDOT = 6486
905885
YDOT = 4643
684853 feet/sec YDOT = 1415
395143 meter/sec
ZDOT = -10284
227420 ZDOT = -3134
632518
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
66410033
00016717 00000-0 10270-3 0 9024
2 25544 51
6472 339
7664 0016623 13
5428 346
6167 15
51966496 4960
Satellite: ISS
Catalog Number: 25544
Epoch time: 12342
66410033 = yrday
fracday
Element set: 902
Inclination: 51
6472 deg
RA of node: 339
7664 deg
Eccentricity:
0016623
Arg of perigee: 13
5428 deg
Mean anomaly: 346
6167 deg
Mean motion: 15
51966496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 318
Coasting Arc #4 (Orbit 511)
---------------------------------------
Vector Time (GMT): 2012/343/15:24:58
435
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3892678
47 A = 6784983
31 meter
Y = 2501786
09 meter E =
0015916
Z = 4949580
77 I = 51
48327
XDOT = -5716
335535 Wp = 38
14757
YDOT = 4645
782862 meter/sec RA = 334
37000 deg
ZDOT = 2156
040725 TA = 30
85878
MA = 30
76533
Ha = 229
294 n
mi
Hp = 214
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12771254
82 X = 3840369
37
Y = 8207959
62 feet Y = 2545023
80 meter
Z = 16238782
05 Z = 4968364
52
XDOT = -18754
381678 XDOT = -5778
334507
YDOT = 15242
069758 feet/sec YDOT = 4581
512488 meter/sec
ZDOT = 7073
624427 ZDOT = 2128
120207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1390555
21 X = 423841
23
Y = 15033893
61 feet Y = 4582330
77 meter
Z = 16316310
62 Z = 4973211
48
XDOT = -22508
721050 XDOT = -6860
658176
YDOT = -5438
425919 feet/sec YDOT = -1657
632220 meter/sec
ZDOT = 6957
252146 ZDOT = 2120
570454
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
69436727
00016717 00000-0 10270-3 0 9037
2 25544 51
6475 334
6479 0016507 16
8825 343
2872 15
52011864 5125
Satellite: ISS
Catalog Number: 25544
Epoch time: 12343
69436727 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 334
6479 deg
Eccentricity:
0016507
Arg of perigee: 16
8825 deg
Mean anomaly: 343
2872 deg
Mean motion: 15
52011864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 512
Checksum: 316
Coasting Arc #5 (Orbit 526)
---------------------------------------
Vector Time (GMT): 2012/344/15:24:58
435
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3177943
83 A = 6783953
61 meter
Y = -2962054
11 meter E =
0026634
Z = -5230540
94 I = 51
45237
XDOT = 6040
844934 Wp = 48
34959
YDOT = -4566
375147 meter/sec RA = 329
38158 deg
ZDOT = -1070
554566 TA = 211
26050
MA = 211
41915
Ha = 229
549 n
mi
Hp = 213
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10426324
89 X = -3119176
11
Y = -9718025
29 feet Y = -2997262
99 meter
Z = -17160567
39 Z = -5245836
92
XDOT = 19819
045058 XDOT = 6096
658724
YDOT = -14981
545758 feet/sec YDOT = -4498
510510 meter/sec
ZDOT = -3512
318130 ZDOT = -1041
072605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1007045
28 X = 306947
40
Y = -14140994
82 feet Y = -4310175
22 meter
Z = -17223572
94 Z = -5249745
03
XDOT = 23119
246803 XDOT = 7046
746426
YDOT = 5829
616971 feet/sec YDOT = 1776
867253 meter/sec
ZDOT = -3389
486319 ZDOT = -1033
115430
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
66023508
00016717 00000-0 10270-3 0 9045
2 25544 51
6475 329
8483 0016645 20
7064 339
4759 15
51991244 5273
Satellite: ISS
Catalog Number: 25544
Epoch time: 12344
66023508 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 329
8483 deg
Eccentricity:
0016645
Arg of perigee: 20
7064 deg
Mean anomaly: 339
4759 deg
Mean motion: 15
51991244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 527
Checksum: 322
Coasting Arc #6 (Orbit 542)
---------------------------------------
Vector Time (GMT): 2012/345/15:24:58
435
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2377166
72 A = 6783440
15 meter
Y = 3494858
28 meter E =
0017963
Z = 5297974
21 I = 51
42550
XDOT = -6274
750233 Wp = 30
35794
YDOT = 4414
302785 meter/sec RA = 324
39006 deg
ZDOT = -81
164556 TA = 60
50688
MA = 60
32783
Ha = 229
536 n
mi
Hp = 213
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7799103
40 X = 2312173
00
Y = 11466070
48 feet Y = 3521077
42 meter
Z = 17381805
14 Z = 5309364
98
XDOT = -20586
450895 XDOT = -6323
251249
YDOT = 14482
620686 feet/sec YDOT = 4343
863427 meter/sec
ZDOT = -266
287915 ZDOT = -111
764986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3795318
13 X = -1156812
97
Y = 13276489
94 feet Y = 4046674
13 meter
Z = 17428548
74 Z = 5312221
65
XDOT = -23379
204878 XDOT = -7125
981647
YDOT = -6100
630039 feet/sec YDOT = -1859
472036 meter/sec
ZDOT = -393
735664 ZDOT = -120
010630
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
69048051
00016717 00000-0 10270-3 0 9050
2 25544 51
6476 324
7292 0016626 24
1816 336
0113 15
52037079 5431
Satellite: ISS
Catalog Number: 25544
Epoch time: 12345
69048051 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 324
7292 deg
Eccentricity:
0016626
Arg of perigee: 24
1816 deg
Mean anomaly: 336
0113 deg
Mean motion: 15
52037079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 543
Checksum: 295
Coasting Arc #7 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2012/346/15:24:58
435
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1677728
02 A = 6784002
05 meter
Y = -4034798
39 meter E =
0025010
Z = -5205786
89 I = 51
40320
XDOT = 6313
857794 Wp = 59
81915
YDOT = -4151
368706 meter/sec RA = 319
39660 deg
ZDOT = 1199
358037 TA = 221
65593
MA = 221
84668
Ha = 229
697 n
mi
Hp = 213
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5504357
02 X = -1607196
45
Y = -13237527
51 feet Y = -4053164
86 meter
Z = -17079353
31 Z = -5213766
46
XDOT = 20714
756541 XDOT = 6353
983709
YDOT = -13619
976069 feet/sec YDOT = -4080
538975 meter/sec
ZDOT = 3934
901696 ZDOT = 1230
127949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6409309
87 X = 1953557
65
Y = -12780399
16 feet Y = -3895465
66 meter
Z = -17111882
85 Z = -5215701
89
XDOT = 22941
642268 XDOT = 6992
612563
YDOT = 6138
022134 feet/sec YDOT = 1870
869146 meter/sec
ZDOT = 4063
018998 ZDOT = 1238
408191
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
65632727
00016717 00000-0 10270-3 0 9067
2 25544 51
6479 319
9294 0016691 27
9481 332
2563 15
52020152 5580
Satellite: ISS
Catalog Number: 25544
Epoch time: 12346
65632727 = yrday
fracday
Element set: 906
Inclination: 51
6479 deg
RA of node: 319
9294 deg
Eccentricity:
0016691
Arg of perigee: 27
9481 deg
Mean anomaly: 332
2563 deg
Mean motion: 15
52020152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 558
Checksum: 321
Coasting Arc #8 (Orbit 573)
---------------------------------------
Vector Time (GMT): 2012/347/15:24:58
435
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 932959
27 A = 6785272
62 meter
Y = 4616273
36 meter E =
0022989
Z = 4878526
91 I = 51
38524
XDOT = -6272
794401 Wp = 39
16714
YDOT = 3750
294686 meter/sec RA = 314
40268 deg
ZDOT = -2325
577927 TA = 73
79392
MA = 73
54108
Ha = 229
764 n
mi
Hp = 213
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3060889
98 X = 857570
77
Y = 15145253
82 feet Y = 4626284
14 meter
Z = 16005665
72 Z = 4882876
71
XDOT = -20580
034124 XDOT = -6302
967528
YDOT = 12304
116424 feet/sec YDOT = 3679
979974 meter/sec
ZDOT = -7629
848841 ZDOT = -2356
123990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9238263
60 X = -2815822
74
Y = 12363041
09 feet Y = 3768254
92 meter
Z = 16023070
76 Z = 4883831
97
XDOT = -22000
954711 XDOT = -6705
890996
YDOT = -6286
876753 feet/sec YDOT = -1916
240034 meter/sec
ZDOT = -7756
987984 ZDOT = -2364
329938
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
68655159
00016717 00000-0 10270-3 0 9076
2 25544 51
6479 314
8099 0016713 31
7615 328
4542 15
52050517 5744
Satellite: ISS
Catalog Number: 25544
Epoch time: 12347
68655159 = yrday
fracday
Element set: 907
Inclination: 51
6479 deg
RA of node: 314
8099 deg
Eccentricity:
0016713
Arg of perigee: 31
7615 deg
Mean anomaly: 328
4542 deg
Mean motion: 15
52050517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 574
Checksum: 324
Coasting Arc #9 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2012/348/14:35:50
512
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1286944
40 A = 6786041
29 meter
Y = 4544779
80 meter E =
0023733
Z = 4864221
23 I = 51
36549
XDOT = -5946
090496 Wp = 44
22302
YDOT = 4233
261609 meter/sec RA = 309
58497 deg
ZDOT = -2358
394479 TA = 69
08253
MA = 68
82865
Ha = 230
447 n
mi
Hp = 213
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4222258
55 X = 1212398
70
Y = 14910694
89 feet Y = 4558753
74 meter
Z = 15958731
06 Z = 4870292
73
XDOT = -19508
170917 XDOT = -5981
529199
YDOT = 13888
653574 feet/sec YDOT = 4166
570886 meter/sec
ZDOT = -7737
514695 ZDOT = -2387
365923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10690462
61 X = -3258453
00
Y = 11184182
08 feet Y = 3408938
70 meter
Z = 15983287
11 Z = 4871705
91
XDOT = -21083
798128 XDOT = -6426
341669
YDOT = -8812
065214 feet/sec YDOT = -2685
917477 meter/sec
ZDOT = -7858
195531 ZDOT = -2395
177998
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 12348
65238663
00016717 00000-0 10270-3 0 9082
2 25544 51
6480 310
0099 0017150 38
7489 321
4889 15
51803285 5896
Satellite: ISS
Catalog Number: 25544
Epoch time: 12348
65238663 = yrday
fracday
Element set: 908
Inclination: 51
6480 deg
RA of node: 310
0099 deg
Eccentricity:
0017150
Arg of perigee: 38
7489 deg
Mean anomaly: 321
4889 deg
Mean motion: 15
51803285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 589
Checksum: 332
Coasting Arc #10 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2012/349/14:35:50
512
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -822265
56 A = 6787686
64 meter
Y = -5071794
67 meter E =
0022298
Z = -4447548
31 I = 51
35303
XDOT = 5790
739903 Wp = 64
61486
YDOT = -3788
295865 meter/sec RA = 304
59353 deg
ZDOT = 3271
666615 TA = 238
45678
MA = 238
67474
Ha = 230
488 n
mi
Hp = 213
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2697721
65 X = -743885
45
Y = -16639746
30 feet Y = -5080550
93 meter
Z = -14591693
92 Z = -4451353
11
XDOT = 18998
490494 XDOT = 5816
778069
YDOT = -12428
792208 feet/sec YDOT = -3723
395034 meter/sec
ZDOT = 10733
814353 ZDOT = 3299
860442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12764973
65 X = 3890763
97
Y = -10989703
32 feet Y = -3349661
57 meter
Z = -14606788
12 Z = -4452149
02
XDOT = 19740
648878 XDOT = 6016
949778
YDOT = 8603
754401 feet/sec YDOT = 2622
424341 meter/sec
ZDOT = 10851
213620 ZDOT = 3307
449911
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 12349
61836228
00016717 00000-0 10270-3 0 9091
2 25544 51
6486 305
2115 0017165 42
2492 317
9979 15
51817999 6042
Satellite: ISS
Catalog Number: 25544
Epoch time: 12349
61836228 = yrday
fracday
Element set: 909
Inclination: 51
6486 deg
RA of node: 305
2115 deg
Eccentricity:
0017165
Arg of perigee: 42
2492 deg
Mean anomaly: 317
9979 deg
Mean motion: 15
51817999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 604
Checksum: 337
Coasting Arc #11 (Orbit 619)
---------------------------------------
Vector Time (GMT): 2012/350/14:35:50
512
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 332052
78 A = 6789861
60 meter
Y = 5598332
10 meter E =
0027200
Z = 3818298
32 I = 51
34368
XDOT = -5615
956141 Wp = 60
24768
YDOT = 3180
924257 meter/sec RA = 299
60352 deg
ZDOT = -4139
908382 TA = 73
64125
MA = 73
34235
Ha = 230
563 n
mi
Hp = 212
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1089412
00 X = 250878
08
Y = 18367231
30 feet Y = 5601591
02 meter
Z = 12527225
44 Z = 3819714
86
XDOT = -18425
052955 XDOT = -5630
997921
YDOT = 10436
103204 feet/sec YDOT = 3118
039488 meter/sec
ZDOT = -13582
376580 ZDOT = -4167
226424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14890369
79 X = -4538584
71
Y = 10802329
07 feet Y = 3292549
90 meter
Z = 12532356
35 Z = 3819862
22
XDOT = -17920
053262 XDOT = -5462
032234
YDOT = -8677
009223 feet/sec YDOT = -2644
752411 meter/sec
ZDOT = -13696
064139 ZDOT = -4174
560349
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 12350
64872576
00016717 00000-0 10270-3 0 9104
2 25544 51
6485 300
0931 0017162 46
1729 314
0838 15
51826547 6202
Satellite: ISS
Catalog Number: 25544
Epoch time: 12350
64872576 = yrday
fracday
Element set: 910
Inclination: 51
6485 deg
RA of node: 300
0931 deg
Eccentricity:
0017162
Arg of perigee: 46
1729 deg
Mean anomaly: 314
0838 deg
Mean motion: 15
51826547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 620
Checksum: 300
Coasting Arc #12 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2012/351/14:35:50
512
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2895
75 A = 6791764
69 meter
Y = -6023169
51 meter E =
0021290
Z = -3138960
07 I = 51
33676
XDOT = 5395
579244 Wp = 54
87683
YDOT = -2500
768441 meter/sec RA = 294
61584 deg
ZDOT = 4828
886252 TA = 268
83308
MA = 269
07700
Ha = 230
545 n
mi
Hp = 212
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9500
48 X = 79705
03
Y = -19761054
83 feet Y = -6022739
76 meter
Z = -10298425
41 Z = -3138774
04
XDOT = 17702
031639 XDOT = 5399
684926
YDOT = -8204
620870 feet/sec YDOT = -2440
409178 meter/sec
ZDOT = 15842
802665 ZDOT = 4855
107244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16453567
60 X = 5015047
40
Y = -10945848
68 feet Y = -3336294
68 meter
Z = -10296866
22 Z = -3138484
82
XDOT = 15810
248450 XDOT = 4818
963727
YDOT = 8868
481110 feet/sec YDOT = 2703
113042 meter/sec
ZDOT = 15951
851024 ZDOT = 4862
124192
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 12351
61468066
00016717 00000-0 10270-3 0 9118
2 25544 51
6490 295
2949 0017150 49
5698 310
6946 15
51857988 6352
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
61468066 = yrday
fracday
Element set: 911
Inclination: 51
6490 deg
RA of node: 295
2949 deg
Eccentricity:
0017150
Arg of perigee: 49
5698 deg
Mean anomaly: 310
6946 deg
Mean motion: 15
51857988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 344
Coasting Arc #13 (Orbit 650)
---------------------------------------
Vector Time (GMT): 2012/352/14:35:50
512
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -353642
68 A = 6793802
64 meter
Y = 6390398
77 meter E =
0027567
Z = 2266441
75 I = 51
33121
XDOT = -5179
411675 Wp = 77
42110
YDOT = 1651
421343 meter/sec RA = 289
63004 deg
ZDOT = -5402
768046 TA = 77
26745
MA = 76
95946
Ha = 230
631 n
mi
Hp = 212
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1160245
01 X = -436084
94
Y = 20965875
23 feet Y = 6385983
00 meter
Z = 7435832
50 Z = 2264523
97
XDOT = -16992
820457 XDOT = -5171
248071
YDOT = 5418
049026 feet/sec YDOT = 1593
547938 meter/sec
ZDOT = -17725
616950 ZDOT = -5427
909236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17909447
91 X = -5458799
72
Y = 10967962
78 feet Y = 3343035
06 meter
Z = 7427056
34 Z = 2263766
77
XDOT = -13279
287811 XDOT = -4047
526925
YDOT = -9472
540746 feet/sec YDOT = -2887
230419 meter/sec
ZDOT = -17830
076481 ZDOT = -5434
607311
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 12352
64502257
00016717 00000-0 10270-3 0 9124
2 25544 51
6486 290
1761 0017144 53
5320 306
7409 15
51849544 6510
Satellite: ISS
Catalog Number: 25544
Epoch time: 12352
64502257 = yrday
fracday
Element set: 912
Inclination: 51
6486 deg
RA of node: 290
1761 deg
Eccentricity:
0017144
Arg of perigee: 53
5320 deg
Mean anomaly: 306
7409 deg
Mean motion: 15
51849544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 651
Checksum: 298
Coasting Arc #14 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2012/353/14:35:50
512
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 565196
47 A = 6795006
59 meter
Y = -6616349
22 meter E =
0025379
Z = -1406924
76 I = 51
32673
XDOT = 4982
172771 Wp = 50
23199
YDOT = -784
195630 meter/sec RA = 284
64595 deg
ZDOT = 5774
723841 TA = 294
37217
MA = 294
63686
Ha = 230
576 n
mi
Hp = 212
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1854319
12 X = 645974
35
Y = -21707182
48 feet Y = -6609577
11 meter
Z = -4615894
90 Z = -1403983
23
XDOT = 16345
711191 XDOT = 4962
519409
YDOT = -2572
820310 feet/sec YDOT = -728
592057 meter/sec
ZDOT = 18945
944360 ZDOT = 5798
879071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18715000
87 X = 5704332
26
Y = -11158369
91 feet Y = -3401071
15 meter
Z = -4602855
65 Z = -1402950
40
XDOT = 10757
314048 XDOT = 3278
829322
YDOT = 10301
671137 feet/sec YDOT = 3139
949362 meter/sec
ZDOT = 19046
204014 ZDOT = 5805
282983
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 12353
61095675
00016717 00000-0 10270-3 0 9134
2 25544 51
6490 285
3778 0017115 56
6528 303
6260 15
51890172 6661
Satellite: ISS
Catalog Number: 25544
Epoch time: 12353
61095675 = yrday
fracday
Element set: 913
Inclination: 51
6490 deg
RA of node: 285
3778 deg
Eccentricity:
0017115
Arg of perigee: 56
6528 deg
Mean anomaly: 303
6260 deg
Mean motion: 15
51890172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 319
Coasting Arc #15 (Orbit 681)
---------------------------------------
Vector Time (GMT): 2012/354/14:35:50
512
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -823304
26 A = 6795837
70 meter
Y = 6732776
47 meter E =
0024565
Z = 397850
89 I = 51
32231
XDOT = -4804
502999 Wp = 89
85935
YDOT = -216
269760 meter/sec RA = 279
66293 deg
ZDOT = -5961
982713 TA = 85
83916
MA = 85
55845
Ha = 230
651 n
mi
Hp = 212
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2701129
47 X = -900463
06
Y = 22089161
64 feet Y = 6723138
33 meter
Z = 1305285
09 Z = 393664
24
XDOT = -15762
805116 XDOT = -4772
765694
YDOT = -709
546456 feet/sec YDOT = -269
818983 meter/sec
ZDOT = -19560
310739 ZDOT = -5985
245600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19320628
01 X = -5888927
42
Y = 11044804
02 feet Y = 3366456
27 meter
Z = 1287077
70 Z = 392301
28
XDOT = -7983
413574 XDOT = -2433
344457
YDOT = -11550
453681 feet/sec YDOT = -3520
578282 meter/sec
ZDOT = -19656
744486 ZDOT = -5991
375719
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 12354
64127721
00016717 00000-0 10270-3 0 9147
2 25544 51
6488 280
2586 0017055 60
8049 299
4806 15
51868565 6824
Satellite: ISS
Catalog Number: 25544
Epoch time: 12354
64127721 = yrday
fracday
Element set: 914
Inclination: 51
6488 deg
RA of node: 280
2586 deg
Eccentricity:
0017055
Arg of perigee: 60
8049 deg
Mean anomaly: 299
4806 deg
Mean motion: 15
51868565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 682
Checksum: 335
Coasting Arc #16 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2012/355/14:35:50
512
Vector Time (MET): N/A
Weight (LBS) : 890855
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 974222
00 A = 6795652
10 meter
Y = -6691843
78 meter E =
0029888
Z = 530855
20 I = 51
31798
XDOT = 4690
000885 Wp = 58
04761
YDOT = 1173
778477 meter/sec RA = 274
67966 deg
ZDOT = 5957
925449 TA = 307
70614
MA = 307
97674
Ha = 230
586 n
mi
Hp = 212
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3196266
41 X = 1046400
43
Y = -21954868
04 feet Y = -6680545
87 meter
Z = 1741650
93 Z = 535762
92
XDOT = 15387
142012 XDOT = 4647
584654
YDOT = 3850
979256 feet/sec YDOT = 1225
987549 meter/sec
ZDOT = 19546
999504 ZDOT = 5980
606264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19312949
47 X = 5886587
00
Y = -10916413
87 feet Y = -3327322
95 meter
Z = 1762835
32 Z = 537312
20
XDOT = 5500
062299 XDOT = 1676
418989
YDOT = 13023
359991 feet/sec YDOT = 3969
520125 meter/sec
ZDOT = 19640
902167 ZDOT = 5986
546980
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 12355
67158504
00016717 00000-0 10270-3 0 9155
2 25544 51
6488 275
1399 0017076 63
8487 296
4419 15
51917587 6973
Satellite: ISS
Catalog Number: 25544
Epoch time: 12355
67158504 = yrday
fracday
Element set: 915
Inclination: 51
6488 deg
RA of node: 275
1399 deg
Eccentricity:
0017076
Arg of perigee: 63
8487 deg
Mean anomaly: 296
4419 deg
Mean motion: 15
51917587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 362
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