[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 10th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 ET - UTC (sec) : 68 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
283/16:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
3
285/09:32:03
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
1
285/12:56:35
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
286/19:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
290/03:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
6
294/08:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2017/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4466685
62 A = 6783683
14 meter
Y = -3520311
95 meter E =
0012461
Z = 3684199
86 I = 51
58781
XDOT = 5722
382544 Wp = 72
02632
YDOT = -2723
191990 meter/sec RA = 187
33385 deg
ZDOT = 4327
432011 TA = 331
91148
MA = 331
97865
Ha = 221
818 n
mi
Hp = 214
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14654480
37 X = -4444885
03
Y = -11549579
87 feet Y = -3570139
34 meter
Z = 12087269
87 Z = 3662554
76
XDOT = 18774
220946 XDOT = 5731
387671
YDOT = -8934
356922 feet/sec YDOT = -2659
149769 meter/sec
ZDOT = 14197
611585 ZDOT = 4355
252263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17516143
05 X = 5338920
40
Y = 6605275
94 feet Y = 2013288
11 meter
Z = 11991819
94 Z = 3655106
72
XDOT = -14665
590917 XDOT = -4470
072111
YDOT = 12841
123551 feet/sec YDOT = 3913
974458 meter/sec
ZDOT = 14321
212628 ZDOT = 4365
105609
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 17282
55655178
00016717 00000-0 10270-3 0 9009
2 25544 51
6404 188
1895 0004867
2632 359
8522 15
54119428 39534
Satellite: ISS
Catalog Number: 25544
Epoch time: 17282
55655178 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 188
1895 deg
Eccentricity:
0004867
Arg of perigee:
2632 deg
Mean anomaly: 359
8522 deg
Mean motion: 15
54119428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 327
Coasting Arc #2 (Orbit 3967)
---------------------------------------
Vector Time (GMT): 2017/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2971967
89 A = 6779886
27 meter
Y = 3866669
89 meter E =
0013420
Z = -4722726
93 I = 51
60899
XDOT = -6881
250269 Wp = 51
18560
YDOT = 1910
042609 meter/sec RA = 182
34221 deg
ZDOT = -2763
565107 TA = 191
38301
MA = 191
41339
Ha = 221
756 n
mi
Hp = 214
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9750550
81 X = 2951450
02
Y = 12685924
84 feet Y = 3899789
51 meter
Z = -15494510
91 Z = -4708339
77
XDOT = -22576
280410 XDOT = -6888
673131
YDOT = 6266
543994 feet/sec YDOT = 1833
050134 meter/sec
ZDOT = -9066
814656 ZDOT = -2797
010876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13354542
01 X = -4070464
40
Y = -8922916
85 feet Y = -2719705
06 meter
Z = -15431252
73 Z = -4703445
83
XDOT = 18733
334850 XDOT = 5709
920462
YDOT = -12083
909889 feet/sec YDOT = -3683
175734 meter/sec
ZDOT = -9215
258282 ZDOT = -2808
810724
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 17283
52107926
00016717 00000-0 10270-3 0 9011
2 25544 51
6413 183
3816 0004941 2
6214 357
4964 15
54158908 39685
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
52107926 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 183
3816 deg
Eccentricity:
0004941
Arg of perigee: 2
6214 deg
Mean anomaly: 357
4964 deg
Mean motion: 15
54158908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3968
Checksum: 320
Coasting Arc #3 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2017/283/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2411066
41 A = 6778644
89 meter
Y = 3906694
26 meter E =
0012698
Z = -4997935
59 I = 51
60740
XDOT = -7157
012744 Wp = 83
91476
YDOT = -1792
578327 meter/sec RA = 181
29692 deg
ZDOT = 2057
258052 TA = 206
09377
MA = 206
15783
Ha = 221
719 n
mi
Hp = 214
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7910322
86 X = -2430294
92
Y = 12817238
39 feet Y = 3879624
32 meter
Z = -16397426
48 Z = -5009694
92
XDOT = -23481
012938 XDOT = -7146
429071
YDOT = -5881
162489 feet/sec YDOT = -1872
553653 meter/sec
ZDOT = 6749
534291 ZDOT = 2022
516629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12965070
37 X = -3951753
45
Y = -7552072
33 feet Y = -2301871
65 meter
Z = -16450032
12 Z = -5013969
79
XDOT = 4871
694076 XDOT = 1484
892354
YDOT = -22689
187469 feet/sec YDOT = -6915
664340 meter/sec
ZDOT = 6595
816226 ZDOT = 2010
404786
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 17283
71398324
00016717 00000-0 10270-3 0 9027
2 25544 51
6371 182
4162 0004742 3
2550 356
8632 15
54143834 39712
Satellite: ISS
Catalog Number: 25544
Epoch time: 17283
71398324 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 182
4162 deg
Eccentricity:
0004742
Arg of perigee: 3
2550 deg
Mean anomaly: 356
8632 deg
Mean motion: 15
54143834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3971
Checksum: 303
Coasting Arc #4 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2017/284/16:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4031771
11 A = 6781920
47 meter
Y = -3543555
06 meter E =
0012737
Z = 4141116
55 I = 51
65085
XDOT = 6158
976513 Wp = 55
45941
YDOT = 2588
068703 meter/sec RA = 176
30323 deg
ZDOT = -3766
420533 TA = 73
38217
MA = 73
24235
Ha = 221
721 n
mi
Hp = 214
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13227595
51 X = 4050980
63
Y = -11625836
82 feet Y = -3498361
46 meter
Z = 13586340
40 Z = 4160748
75
XDOT = 20206
615855 XDOT = 6147
873985
YDOT = 8491
039053 feet/sec YDOT = 2656
880344 meter/sec
ZDOT = -12357
022746 ZDOT = -3736
528767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12098106
16 X = 3687502
76
Y = 12703583
19 feet Y = 3872052
16 meter
Z = 13673800
19 Z = 4167774
30
XDOT = -6814
928938 XDOT = -2077
190340
YDOT = 19702
396521 feet/sec YDOT = 6005
290460 meter/sec
ZDOT = -12224
875876 ZDOT = -3726
142167
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 17284
74280554
00016717 00000-0 10270-3 0 9037
2 25544 51
6369 177
2870 0004735 5
7041 354
4164 15
54142822 39878
Satellite: ISS
Catalog Number: 25544
Epoch time: 17284
74280554 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 177
2870 deg
Eccentricity:
0004735
Arg of perigee: 5
7041 deg
Mean anomaly: 354
4164 deg
Mean motion: 15
54142822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3987
Checksum: 319
Coasting Arc #5 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2017/285/09:32:03
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3350409
29 A = 6779471
49 meter
Y = -3407853
73 meter E =
0007400
Z = 4801797
12 I = 51
66760
XDOT = 6628
175366 Wp = 80
92709
YDOT = -2881
317017 meter/sec RA = 172
88412 deg
ZDOT = 2577
619951 TA = 343
70509
MA = 343
72887
Ha = 221
923 n
mi
Hp = 214
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10992156
47 X = -3335377
81
Y = -11180622
47 feet Y = -3445236
03 meter
Z = 15753927
55 Z = 4785558
34
XDOT = 21745
982172 XDOT = 6647
381435
YDOT = -9453
139819 feet/sec YDOT = -2807
088731 meter/sec
ZDOT = 8456
758368 ZDOT = 2609
864738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7414178
61 X = 2259841
64
Y = 13896502
04 feet Y = 4235653
82 meter
Z = 15682386
38 Z = 4779991
37
XDOT = -22478
229564 XDOT = -6851
364371
YDOT = 2279
153737 feet/sec YDOT = 694
686059 meter/sec
ZDOT = 8600
046478 ZDOT = 2621
294167
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 17285
45011904
00016717 00000-0 10270-3 0 9048
2 25544 51
6391 173
7645 0004863 9
0360 351
0880 15
54179177 39980
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
45011904 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 173
7645 deg
Eccentricity:
0004863
Arg of perigee: 9
0360 deg
Mean anomaly: 351
0880 deg
Mean motion: 15
54179177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 322
Coasting Arc #6 (Orbit 3999)
---------------------------------------
Vector Time (GMT): 2017/285/12:56:35
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4774918
33 A = 6784121
11 meter
Y = -3388152
22 meter E =
0014132
Z = 3420858
73 I = 51
68957
XDOT = 5389
631262 Wp = 69
03550
YDOT = 2926
947684 meter/sec RA = 172
13234 deg
ZDOT = -4603
718124 TA = 70
95436
MA = 70
80133
Ha = 221
853 n
mi
Hp = 214
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15665742
54 X = 4795833
62
Y = -11115984
97 feet Y = -3334638
72 meter
Z = 11223289
79 Z = 3444105
03
XDOT = 17682
517263 XDOT = 5378
863646
YDOT = 9602
846733 feet/sec YDOT = 2987
157797 meter/sec
ZDOT = -15104
062087 ZDOT = -4577
562958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6531749
44 X = -1990877
23
Y = 17999544
30 feet Y = 5486261
10 meter
Z = 11326760
30 Z = 3452396
54
XDOT = -18777
174470 XDOT = -5723
282778
YDOT = 2659
555680 feet/sec YDOT = 810
632571 meter/sec
ZDOT = -14988
503974 ZDOT = -4568
496011
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 17285
57872088
00016717 00000-0 10270-3 0 9050
2 25544 51
6406 173
1243 0005075 9
4826 350
6422 15
54182315 40002
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
57872088 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 173
1243 deg
Eccentricity:
0005075
Arg of perigee: 9
4826 deg
Mean anomaly: 350
6422 deg
Mean motion: 15
54182315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4000
Checksum: 296
Coasting Arc #7 (Orbit 4014)
---------------------------------------
Vector Time (GMT): 2017/286/12:56:35
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5806228
81 A = 6787549
37 meter
Y = 2907850
07 meter E =
0011447
Z = -1958260
92 I = 51
73334
XDOT = -3725
470268 Wp = 28
20109
YDOT = -3682
370561 meter/sec RA = 167
15880 deg
ZDOT = 5601
183506 TA = 310
22299
MA = 310
32308
Ha = 221
917 n
mi
Hp = 214
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19049307
11 X = -5828801
28
Y = 9540190
50 feet Y = 2842794
52 meter
Z = -6424740
57 Z = -1986521
03
XDOT = -12222
671484 XDOT = -3711
224174
YDOT = -12081
268245 feet/sec YDOT = -3723
951316 meter/sec
ZDOT = 18376
586305 ZDOT = 5583
120997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9915500
91 X = 3022244
68
Y = -18813395
41 feet Y = -5734322
92 meter
Z = -6550391
03 Z = -1996559
19
XDOT = 15694
091649 XDOT = 4783
559135
YDOT = 1926
890992 feet/sec YDOT = 587
316374 meter/sec
ZDOT = 18296
983281 ZDOT = 5576
920504
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 17286
54323342
00016717 00000-0 10270-3 0 9063
2 25544 51
6409 168
3158 0005061 11
1778 348
9486 15
54157914 40150
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
54323342 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 168
3158 deg
Eccentricity:
0005061
Arg of perigee: 11
1778 deg
Mean anomaly: 348
9486 deg
Mean motion: 15
54157914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4015
Checksum: 317
Coasting Arc #8 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2017/286/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 269775
33 A = 6777692
84 meter
Y = -4316511
82 meter E =
0007905
Z = 5215601
04 I = 51
70843
XDOT = 7521
202564 Wp = 35
24556
YDOT = -953
429880 meter/sec RA = 165
77152 deg
ZDOT = -1170
909821 TA = 66
00974
MA = 65
92700
Ha = 221
920 n
mi
Hp = 213
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 885089
65 X = 292688
62
Y = -14161784
19 feet Y = -4313366
55 meter
Z = 17111551
97 Z = 5216967
47
XDOT = 24675
861430 XDOT = 7536
992832
YDOT = -3128
050787 feet/sec YDOT = -869
234448 meter/sec
ZDOT = -3841
567655 ZDOT = -1134
335437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10340062
77 X = 3151651
13
Y = -9705483
73 feet Y = -2958231
44 meter
Z = 17118160
34 Z = 5217615
27
XDOT = 19313
992071 XDOT = 5886
904783
YDOT = 14045
776431 feet/sec YDOT = 4281
152656 meter/sec
ZDOT = -3679
302520 ZDOT = -1121
451408
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 17286
86473810
00016717 00000-0 10270-3 0 9075
2 25544 51
6401 166
7074 0004549 16
5836 343
5465 15
54153312 40207
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
86473810 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 166
7074 deg
Eccentricity:
0004549
Arg of perigee: 16
5836 deg
Mean anomaly: 343
5465 deg
Mean motion: 15
54153312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 306
Coasting Arc #9 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2017/287/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1984996
00 A = 6780072
71 meter
Y = 4553024
40 meter E =
0011340
Z = -4624553
58 I = 51
74827
XDOT = -7051
115015 Wp = 86
71052
YDOT = -41
064329 meter/sec RA = 160
78234 deg
ZDOT = 2993
085747 TA = 213
09265
MA = 213
16365
Ha = 221
941 n
mi
Hp = 213
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6512454
08 X = -2013297
61
Y = 14937744
10 feet Y = 4530668
19 meter
Z = -15172419
89 Z = -4634265
28
XDOT = -23133
579446 XDOT = -7064
670829
YDOT = -134
725488 feet/sec YDOT = -119
990254 meter/sec
ZDOT = 9819
835129 ZDOT = 2958
800423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14842592
31 X = -4524022
14
Y = 6627181
91 feet Y = 2019965
05 meter
Z = -15216060
45 Z = -4637855
23
XDOT = -16473
048556 XDOT = -5020
985200
YDOT = -14748
848408 feet/sec YDOT = -4495
448995 meter/sec
ZDOT = 9667
826018 ZDOT = 2946
753370
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 17287
82924353
00016717 00000-0 10270-3 0 9086
2 25544 51
6402 161
9004 0004531 20
0018 340
1311 15
54179917 40359
Satellite: ISS
Catalog Number: 25544
Epoch time: 17287
82924353 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 161
9004 deg
Eccentricity:
0004531
Arg of perigee: 20
0018 deg
Mean anomaly: 340
1311 deg
Mean motion: 15
54179917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 279
Coasting Arc #10 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2017/288/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3516634
38 A = 6783942
94 meter
Y = -4611315
28 meter E =
0014710
Z = 3512302
96 I = 51
79125
XDOT = 6079
738773 Wp = 72
49657
YDOT = 1173
949106 meter/sec RA = 155
80286 deg
ZDOT = -4526
030998 TA = 66
25767
MA = 66
10345
Ha = 222
005 n
mi
Hp = 213
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11537514
38 X = 3550876
76
Y = -15128987
13 feet Y = -4571798
06 meter
Z = 11523303
66 Z = 3529469
47
XDOT = 19946
649519 XDOT = 6088
144958
YDOT = 3851
539063 feet/sec YDOT = 1241
983445 meter/sec
ZDOT = -14849
183064 ZDOT = -4496
476925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18622495
67 X = 5676136
68
Y = -3664607
28 feet Y = -1116972
30 meter
Z = 11600014
03 Z = 3535684
28
XDOT = 12131
626109 XDOT = 3697
719638
YDOT = 14854
429479 feet/sec YDOT = 4527
630105 meter/sec
ZDOT = -14718
282134 ZDOT = -4486
132395
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 17288
85804686
00016717 00000-0 10270-3 0 9097
2 25544 51
6399 156
7713 0004463 24
7547 335
3819 15
54158209 40513
Satellite: ISS
Catalog Number: 25544
Epoch time: 17288
85804686 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 156
7713 deg
Eccentricity:
0004463
Arg of perigee: 24
7547 deg
Mean anomaly: 335
3819 deg
Mean motion: 15
54158209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 344
Coasting Arc #11 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2017/289/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672730
56 A = 6787375
48 meter
Y = 4463911
75 meter E =
0011022
Z = -2062359
82 I = 51
83336
XDOT = -4713
754593 Wp = 35
02281
YDOT = -2375
540502 meter/sec RA = 150
83630 deg
ZDOT = 5561
768855 TA = 302
22777
MA = 302
33457
Ha = 222
082 n
mi
Hp = 213
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15330480
84 X = -4712281
86
Y = 14645379
77 feet Y = 4411436
72 meter
Z = -6766272
39 Z = -2085155
35
XDOT = -15465
074124 XDOT = -4713
857028
YDOT = -7793
768051 feet/sec YDOT = -2428
252882 meter/sec
ZDOT = 18247
273146 ZDOT = 5538
870615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21139153
20 X = -6443213
90
Y = 1122891
65 feet Y = 342257
38 meter
Z = -6867936
34 Z = -2093347
00
XDOT = -6642
772233 XDOT = -2024
716977
YDOT = -14532
552079 feet/sec YDOT = -4429
521874 meter/sec
ZDOT = 18146
031518 ZDOT = 5530
910407
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 17289
82254418
00016717 00000-0 10270-3 0 9109
2 25544 51
6412 151
9634 0004666 25
4866 334
6516 15
54159779 40660
Satellite: ISS
Catalog Number: 25544
Epoch time: 17289
82254418 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 151
9634 deg
Eccentricity:
0004666
Arg of perigee: 25
4866 deg
Mean anomaly: 334
6516 deg
Mean motion: 15
54159779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 333
Coasting Arc #12 (Orbit 4070)
---------------------------------------
Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2197994
93 A = 6777247
46 meter
Y = 3576795
19 meter E =
0017822
Z = -5335292
51 I = 51
80529
XDOT = -6561
766458 Wp = 75
35916
YDOT = 3943
570090 meter/sec RA = 149
31982 deg
ZDOT = -55
254370 TA = 194
08977
MA = 194
13955
Ha = 222
264 n
mi
Hp = 213
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7211269
46 X = 2183751
50
Y = 11734892
35 feet Y = 3601294
43 meter
Z = -17504240
53 Z = -5324650
18
XDOT = -21528
105177 XDOT = -6605
108423
YDOT = 12938
222079 feet/sec YDOT = 3869
949590 meter/sec
ZDOT = -181
280743 ZDOT = -87
235563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13482161
49 X = 4109362
82
Y = -3094417
10 feet Y = -943178
33 meter
Z = -17457504
02 Z = -5321047
22
XDOT = 4976
733079 XDOT = 1516
908243
YDOT = 23587
584896 feet/sec YDOT = 7189
495876 meter/sec
ZDOT = -323
618124 ZDOT = -98
638804
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 17290
14404216
00016717 00000-0 10270-3 0 9110
2 25544 51
6382 150
3637 0005008 27
9475 332
1946 15
54168445 40712
Satellite: ISS
Catalog Number: 25544
Epoch time: 17290
14404216 = yrday
fracday
Element set: 911
Inclination: 51
6382 deg
RA of node: 150
3637 deg
Eccentricity:
0005008
Arg of perigee: 27
9475 deg
Mean anomaly: 332
1946 deg
Mean motion: 15
54168445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4071
Checksum: 296
Coasting Arc #13 (Orbit 4086)
---------------------------------------
Vector Time (GMT): 2017/291/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -581560
47 A = 6778298
18 meter
Y = -4473162
58 meter E =
0010341
Z = 5055411
77 I = 51
83550
XDOT = 6785
674878 Wp = 43
71492
YDOT = -3035
961226 meter/sec RA = 144
33221 deg
ZDOT = -1896
088534 TA = 64
65970
MA = 64
55263
Ha = 222
280 n
mi
Hp = 213
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1908006
78 X = -556054
31
Y = -14675730
24 feet Y = -4479522
79 meter
Z = 16585996
61 Z = 5052649
14
XDOT = 22262
712855 XDOT = 6828
329915
YDOT = -9960
502711 feet/sec YDOT = -2959
840893 meter/sec
ZDOT = -6220
762907 ZDOT = -1863
021284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14576308
91 X = -4442858
96
Y = -2633595
11 feet Y = -802719
79 meter
Z = 16574324
32 Z = 5051854
05
XDOT = -2745
056595 XDOT = -836
693250
YDOT = -23229
671433 feet/sec YDOT = -7080
403853 meter/sec
ZDOT = -6073
710685 ZDOT = -1851
267017
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 17291
17283323
00016717 00000-0 10270-3 0 9129
2 25544 51
6369 145
2343 0005063 29
9944 330
1498 15
54193613 40870
Satellite: ISS
Catalog Number: 25544
Epoch time: 17291
17283323 = yrday
fracday
Element set: 912
Inclination: 51
6369 deg
RA of node: 145
2343 deg
Eccentricity:
0005063
Arg of perigee: 29
9944 deg
Mean anomaly: 330
1498 deg
Mean motion: 15
54193613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4087
Checksum: 313
Coasting Arc #14 (Orbit 4101)
---------------------------------------
Vector Time (GMT): 2017/292/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -916384
29 A = 6781466
20 meter
Y = 5198863
91 meter E =
0010701
Z = -4265074
63 I = 51
87147
XDOT = -6496
075245 Wp = 82
76151
YDOT = 1823
860444 meter/sec RA = 139
35348 deg
ZDOT = 3628
009073 TA = 224
21179
MA = 224
29734
Ha = 222
373 n
mi
Hp = 213
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3006510
13 X = -953733
17
Y = 17056640
13 feet Y = 5188406
98 meter
Z = -13993027
00 Z = -4269617
52
XDOT = -21312
582824 XDOT = -6533
610810
YDOT = 5983
794109 feet/sec YDOT = 1751
007413 meter/sec
ZDOT = 11902
916906 ZDOT = 3596
361100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15447022
95 X = 4708252
59
Y = 7795774
71 feet Y = 2376152
13 meter
Z = -14013859
53 Z = -4271424
39
XDOT = 6
259252 XDOT = 1
907820
YDOT = 21078
169190 feet/sec YDOT = 6424
625969 meter/sec
ZDOT = 11762
303136 ZDOT = 3585
149996
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 17292
13732197
00016717 00000-0 10270-3 0 9135
2 25544 51
6365 140
4263 0005133 33
5600 326
5877 15
54174911 41020
Satellite: ISS
Catalog Number: 25544
Epoch time: 17292
13732197 = yrday
fracday
Element set: 913
Inclination: 51
6365 deg
RA of node: 140
4263 deg
Eccentricity:
0005133
Arg of perigee: 33
5600 deg
Mean anomaly: 326
5877 deg
Mean motion: 15
54174911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4102
Checksum: 289
Coasting Arc #15 (Orbit 4117)
---------------------------------------
Vector Time (GMT): 2017/293/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2264977
72 A = 6785257
68 meter
Y = -5653708
96 meter E =
0016268
Z = 2980126
49 I = 51
90890
XDOT = 5804
845751 Wp = 81
27867
YDOT = -324
873854 meter/sec RA = 134
38515 deg
ZDOT = -5002
508743 TA = 64
77315
MA = 64
60460
Ha = 222
323 n
mi
Hp = 213
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7431029
26 X = 2313554
31
Y = -18548913
92 feet Y = -5628108
54 meter
Z = 9777317
89 Z = 2991247
85
XDOT = 19044
769524 XDOT = 5832
347486
YDOT = -1065
859101 feet/sec YDOT = -259
806811 meter/sec
ZDOT = -16412
430258 ZDOT = -4974
243074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15778619
90 X = -4809323
35
Y = -12220296
33 feet Y = -3724746
32 meter
Z = 9827403
52 Z = 2995392
59
XDOT = 3393
334140 XDOT = 1034
288246
YDOT = -17546
573065 feet/sec YDOT = -5348
195470 meter/sec
ZDOT = -16287
005232 ZDOT = -4964
279195
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 17293
16610412
00016717 00000-0 10270-3 0 9145
2 25544 51
6367 135
2962 0005139 36
0063 324
1435 15
54221309 41182
Satellite: ISS
Catalog Number: 25544
Epoch time: 17293
16610412 = yrday
fracday
Element set: 914
Inclination: 51
6367 deg
RA of node: 135
2962 deg
Eccentricity:
0005139
Arg of perigee: 36
0063 deg
Mean anomaly: 324
1435 deg
Mean motion: 15
54221309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4118
Checksum: 281
Coasting Arc #16 (Orbit 4132)
---------------------------------------
Vector Time (GMT): 2017/294/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3296899
46 A = 6788168
04 meter
Y = 5755859
43 meter E =
0013657
Z = -1416589
65 I = 51
94087
XDOT = -4808
751504 Wp = 39
19401
YDOT = -1331
134624 meter/sec RA = 129
42911 deg
ZDOT = 5823
837620 TA = 305
42423
MA = 305
55167
Ha = 222
406 n
mi
Hp = 213
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10816599
26 X = -3354136
70
Y = 18884053
24 feet Y = 5718671
10 meter
Z = -4647603
82 Z = -1432744
86
XDOT = -15776
743781 XDOT = -4821
799106
YDOT = -4367
239580 feet/sec YDOT = -1384
981863 meter/sec
ZDOT = 19107
078806 ZDOT = 5800
445988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15419151
47 X = 4699757
37
Y = 15335494
67 feet Y = 4674258
78 meter
Z = -4720050
74 Z = -1438671
47
XDOT = -7241
684473 XDOT = -2207
265427
YDOT = 13089
598103 feet/sec YDOT = 3989
709502 meter/sec
ZDOT = 19003
489411 ZDOT = 5792
263573
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 17294
13058298
00016717 00000-0 10270-3 0 9152
2 25544 51
6367 130
4879 0005189 40
9663 319
1878 15
54224785 41334
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
13058298 = yrday
fracday
Element set: 915
Inclination: 51
6367 deg
RA of node: 130
4879 deg
Eccentricity:
0005189
Arg of perigee: 40
9663 deg
Mean anomaly: 319
1878 deg
Mean motion: 15
54224785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4133
Checksum: 340
Coasting Arc #17 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3331006
02 A = 6777047
86 meter
Y = 2539216
15 meter E =
0018593
Z = -5343424
68 I = 51
91230
XDOT = -4702
289187 Wp = 77
17568
YDOT = 6040
544266 meter/sec RA = 128
23348 deg
ZDOT = -56
995120 TA = 192
25966
MA = 192
30497
Ha = 222
375 n
mi
Hp = 213
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10928497
45 X = 3328320
70
Y = 8330761
63 feet Y = 2576450
32 meter
Z = -17530920
86 Z = -5327249
96
XDOT = -15427
457962 XDOT = -4769
209817
YDOT = 19818
058615 feet/sec YDOT = 5987
585877 meter/sec
ZDOT = -186
991864 ZDOT = -80
000988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8102053
30 X = -2469505
85
Y = -11211112
76 feet Y = -3417147
17 meter
Z = -17459510
73 Z = -5321658
87
XDOT = 19758
768255 XDOT = 6022
472564
YDOT = -13808
109353 feet/sec YDOT = -4208
711731 meter/sec
ZDOT = -289
873505 ZDOT = -88
353444
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 17294
38777613
00016717 00000-0 10270-3 0 9169
2 25544 51
6403 129
2066 0005177 38
7575 321
3949 15
54236769 41376
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
38777613 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 129
2066 deg
Eccentricity:
0005177
Arg of perigee: 38
7575 deg
Mean anomaly: 321
3949 deg
Mean motion: 15
54236769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 339
Coasting Arc #18 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2137877
85 A = 6778110
53 meter
Y = -3965313
27 meter E =
0010590
Z = 5059531
90 I = 51
93539
XDOT = 5240
673970 Wp = 49
11178
YDOT = -5269
883243 meter/sec RA = 123
25278 deg
ZDOT = -1906
400600 TA = 59
33648
MA = 59
23214
Ha = 222
391 n
mi
Hp = 213
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7014034
94 X = -2117955
16
Y = -13009557
98 feet Y = -3989108
80 meter
Z = 16599514
11 Z = 5049195
08
XDOT = 17193
812238 XDOT = 5308
474321
YDOT = -17289
643187 feet/sec YDOT = -5210
899461 meter/sec
ZDOT = -6254
595145 ZDOT = -1880
777366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3227414
51 X = 983715
94
Y = 14475197
64 feet Y = 4412040
24 meter
Z = 16554201
96 Z = 5045720
76
XDOT = -20304
902258 XDOT = -6188
934208
YDOT = 11584
475305 feet/sec YDOT = 3530
948073 meter/sec
ZDOT = -6140
184722 ZDOT = -1871
528303
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 17295
41654683
00016717 00000-0 10270-3 0 9176
2 25544 51
6400 124
0775 0005081 41
4670 318
6867 15
54265951 41535
Satellite: ISS
Catalog Number: 25544
Epoch time: 17295
41654683 = yrday
fracday
Element set: 917
Inclination: 51
6400 deg
RA of node: 124
0775 deg
Eccentricity:
0005081
Arg of perigee: 41
4670 deg
Mean anomaly: 318
6867 deg
Mean motion: 15
54265951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4153
Checksum: 315
Coasting Arc #19 (Orbit 4167)
---------------------------------------
Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 993464
09 A = 6781336
50 meter
Y = 5188851
13 meter E =
0011270
Z = -4260695
34 I = 51
96334
XDOT = -5403
739102 Wp = 86
09510
YDOT = 4022
016412 meter/sec RA = 118
27925 deg
ZDOT = 3647
231432 TA = 221
05628
MA = 221
14116
Ha = 222
416 n
mi
Hp = 213
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3259396
61 X = 956064
04
Y = 17023789
78 feet Y = 5199751
43 meter
Z = -13978659
24 Z = -4255960
32
XDOT = -17728
802827 XDOT = -5466
029667
YDOT = 13195
591904 feet/sec YDOT = 3961
239974 meter/sec
ZDOT = 11965
982388 ZDOT = 3620
829596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1213838
48 X = 369977
97
Y = -17306825
71 feet Y = -5275120
48 meter
Z = -13958380
24 Z = -4254514
30
XDOT = 19374
753171 XDOT = 5905
424767
YDOT = -8173
089363 feet/sec YDOT = -2491
157638 meter/sec
ZDOT = 11848
270274 ZDOT = 3611
352780
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 17296
38101717
00016717 00000-0 10270-3 0 9189
2 25544 51
6403 119
2685 0005080 44
3717 315
7843 15
54240827 41680
Satellite: ISS
Catalog Number: 25544
Epoch time: 17296
38101717 = yrday
fracday
Element set: 918
Inclination: 51
6403 deg
RA of node: 119
2685 deg
Eccentricity:
0005080
Arg of perigee: 44
3717 deg
Mean anomaly: 315
7843 deg
Mean motion: 15
54240827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4168
Checksum: 313
Coasting Arc #20 (Orbit 4183)
---------------------------------------
Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 108485
25 A = 6785197
38 meter
Y = -6098097
09 meter E =
0017026
Z = 2961000
15 I = 51
99157
XDOT = 5293
410842 Wp = 83
94329
YDOT = -2358
817032 meter/sec RA = 113
31677 deg
ZDOT = -5025
379593 TA = 62
39484
MA = 62
22205
Ha = 222
452 n
mi
Hp = 212
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 355922
73 X = 162284
30
Y = -20006880
23 feet Y = -6096583
04 meter
Z = 9714567
42 Z = 2961658
01
XDOT = 17366
833471 XDOT = 5343
805767
YDOT = -7738
901025 feet/sec YDOT = -2299
340874 meter/sec
ZDOT = -16487
465857 ZDOT = -4999
542745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5178440
29 X = -1578388
60
Y = 19326458
71 feet Y = 5890704
62 meter
Z = 9718359
30 Z = 2962155
92
XDOT = -17428
106631 XDOT = -5312
086901
YDOT = 3606
824426 feet/sec YDOT = 1099
360085 meter/sec
ZDOT = -16372
479142 ZDOT = -4990
331642
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 17297
40977845
00016717 00000-0 10270-3 0 9197
2 25544 51
6407 114
1386 0005251 47
1137 313
0456 15
54270800 41846
Satellite: ISS
Catalog Number: 25544
Epoch time: 17297
40977845 = yrday
fracday
Element set: 919
Inclination: 51
6407 deg
RA of node: 114
1386 deg
Eccentricity:
0005251
Arg of perigee: 47
1137 deg
Mean anomaly: 313
0456 deg
Mean motion: 15
54270800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4184
Checksum: 307
- 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