[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 27th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1552 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
There are no maneuvers
Coasting Arc #1 (Orbit 3488)
---------------------------------------
Vector Time (GMT): 2016/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2201961
23 A = 6779256
94 meter
Y = 4034355
16 meter E =
0014504
Z = -4994630
87 I = 51
62795
XDOT = -7239
349054 Wp = 77
85474
YDOT = -1391
039570 meter/sec RA = 177
99218 deg
ZDOT = 2076
067256 TA = 212
32929
MA = 212
41826
Ha = 222
916 n
mi
Hp = 213
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7224282
26 X = -2222649
06
Y = 13236073
36 feet Y = 4009616
13 meter
Z = -16386584
23 Z = -5005377
31
XDOT = -23751
145190 XDOT = -7233
340666
YDOT = -4563
778116 feet/sec YDOT = -1471
961430 meter/sec
ZDOT = 6811
244278 ZDOT = 2040
914850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13758384
76 X = -4193555
67
Y = -6043349
86 feet Y = -1842013
04 meter
Z = -16434378
79 Z = -5009198
66
XDOT = 2216
874982 XDOT = 675
703495
YDOT = -23078
996305 feet/sec YDOT = -7034
478074 meter/sec
ZDOT = 6657
287432 ZDOT = 2029
141209
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 16361
51256258
00016717 00000-0 10270-3 0 9008
2 25544 51
6366 179
0985 0006727 16
0012 344
1352 15
53941821 34895
Satellite: ISS
Catalog Number: 25544
Epoch time: 16361
51256258 = yrday
fracday
Element set: 900
Inclination: 51
6366 deg
RA of node: 179
0985 deg
Eccentricity:
0006727
Arg of perigee: 16
0012 deg
Mean anomaly: 344
1352 deg
Mean motion: 15
53941821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3489
Checksum: 307
Coasting Arc #2 (Orbit 3504)
---------------------------------------
Vector Time (GMT): 2016/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3772868
75 A = 6782434
92 meter
Y = -3785614
13 meter E =
0015048
Z = 4171286
60 I = 51
67121
XDOT = 6335
834961 Wp = 53
49805
YDOT = 2189
544658 meter/sec RA = 173
00121 deg
ZDOT = -3725
472017 TA = 74
84588
MA = 74
67949
Ha = 222
954 n
mi
Hp = 213
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12378178
32 X = 3794657
84
Y = -12419993
85 feet Y = -3743301
96 meter
Z = 13685323
49 Z = 4189666
71
XDOT = 20786
860108 XDOT = 6328
976667
YDOT = 7183
545467 feet/sec YDOT = 2260
358249 meter/sec
ZDOT = -12222
677220 ZDOT = -3694
710698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13547902
63 X = 4129400
72
Y = 11031745
39 feet Y = 3362475
99 meter
Z = 13766573
75 Z = 4196051
68
XDOT = -4328
472018 XDOT = -1319
318271
YDOT = 20474
175455 feet/sec YDOT = 6240
528679 meter/sec
ZDOT = -12088
090851 ZDOT = -3684
450091
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 16362
54151821
00016717 00000-0 10270-3 0 9013
2 25544 51
6370 173
9698 0006739 18
9942 341
1461 15
53932088 35052
Satellite: ISS
Catalog Number: 25544
Epoch time: 16362
54151821 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 173
9698 deg
Eccentricity:
0006739
Arg of perigee: 18
9942 deg
Mean anomaly: 341
1461 deg
Mean motion: 15
53932088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3505
Checksum: 319
Coasting Arc #3 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2016/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5012757
87 A = 6785993
68 meter
Y = 3467513
46 meter E =
0010435
Z = -2979406
77 I = 51
71528
XDOT = -5006
725218 Wp = 43
13756
YDOT = -2964
852628 meter/sec RA = 168
02215 deg
ZDOT = 4990
837177 TA = 282
84299
MA = 282
95955
Ha = 223
051 n
mi
Hp = 213
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16446056
02 X = -5036687
39
Y = 11376356
49 feet Y = 3411323
94 meter
Z = -9774956
60 Z = -3003815
06
XDOT = -16426
263837 XDOT = -4997
442501
YDOT = -9727
206786 feet/sec YDOT = -3020
789814 meter/sec
ZDOT = 16374
137719 ZDOT = 4966
538190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13164623
99 X = -4012577
39
Y = -14982341
81 feet Y = -4566617
78 meter
Z = -9882617
63 Z = -3012221
85
XDOT = 6690
036123 XDOT = 2039
123010
YDOT = -16571
037324 feet/sec YDOT = -5050
852176 meter/sec
ZDOT = 16268
011549 ZDOT = 4958
489920
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 16363
50616217
00016717 00000-0 10270-3 0 9026
2 25544 51
6370 169
1621 0006747 24
7060 335
4415 15
53950947 35206
Satellite: ISS
Catalog Number: 25544
Epoch time: 16363
50616217 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 169
1621 deg
Eccentricity:
0006747
Arg of perigee: 24
7060 deg
Mean anomaly: 335
4415 deg
Mean motion: 15
53950947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 296
Coasting Arc #4 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2016/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5912658
10 A = 6788834
09 meter
Y = -2996747
50 meter E =
0015238
Z = 1450628
53 I = 51
75601
XDOT = 3336
673910 Wp = 92
34936
YDOT = 3754
909399 meter/sec RA = 163
05463 deg
ZDOT = -5791
149440 TA = 71
85545
MA = 71
68958
Ha = 223
108 n
mi
Hp = 213
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19398484
58 X = 5938682
62
Y = -9831848
76 feet Y = -2930482
82 meter
Z = 4759279
94 Z = 1479413
31
XDOT = 10947
092880 XDOT = 3322
568137
YDOT = 12319
256557 feet/sec YDOT = 3792
144054 meter/sec
ZDOT = -18999
834122 ZDOT = -5774
974776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12280019
53 X = 3742949
95
Y = 17914923
28 feet Y = 5460468
62 meter
Z = 4886086
77 Z = 1489279
25
XDOT = -9457
407364 XDOT = -2882
617765
YDOT = 11690
734436 feet/sec YDOT = 3563
335856 meter/sec
ZDOT = -18929
473032 ZDOT = -5769
703380
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 16364
53511149
00016717 00000-0 10270-3 0 9039
2 25544 51
6366 164
0339 0006790 26
4736 333
6762 15
53975919 35366
Satellite: ISS
Catalog Number: 25544
Epoch time: 16364
53511149 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 164
0339 deg
Eccentricity:
0006790
Arg of perigee: 26
4736 deg
Mean anomaly: 333
6762 deg
Mean motion: 15
53975919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 329
Coasting Arc #5 (Orbit 3551)
---------------------------------------
Vector Time (GMT): 2016/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6337768
20 A = 6789789
33 meter
Y = 2402205
18 meter E =
0018947
Z = 172479
28 I = 51
79196
XDOT = -1530
483382 Wp = 41
99310
YDOT = -4496
966821 meter/sec RA = 158
09400 deg
ZDOT = 6025
885310 TA = 319
86220
MA = 320
00201
Ha = 223
199 n
mi
Hp = 213
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20793202
75 X = -6364997
06
Y = 7881250
60 feet Y = 2331179
74 meter
Z = 565876
89 Z = 141626
54
XDOT = -5021
270937 XDOT = -1509
354106
YDOT = -14753
828153 feet/sec YDOT = -4513
964146 meter/sec
ZDOT = 19769
964927 ZDOT = 6018
501609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10868968
30 X = -3312861
54
Y = -19402890
89 feet Y = -5914001
14 meter
Z = 430071
51 Z = 131085
80
XDOT = 12413
797535 XDOT = 3783
725489
YDOT = -6481
165444 feet/sec YDOT = -1975
459227 meter/sec
ZDOT = 19738
298484 ZDOT = 6016
233378
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 16365
56405947
00016717 00000-0 10270-3 0 9042
2 25544 51
6389 158
9057 0006736 32
1781 327
9781 15
53969954 35521
Satellite: ISS
Catalog Number: 25544
Epoch time: 16365
56405947 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 158
9057 deg
Eccentricity:
0006736
Arg of perigee: 32
1781 deg
Mean anomaly: 327
9781 deg
Mean motion: 15
53969954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3552
Checksum: 357
Coasting Arc #6 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2016/366/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6340531
42 A = 6788381
24 meter
Y = -1597447
04 meter E =
0008610
Z = -1831223
25 I = 51
81673
XDOT = -328
732719 Wp = 91
32632
YDOT = 5154
369181 meter/sec RA = 153
13514 deg
ZDOT = -5657
745764 TA = 108
73912
MA = 108
64567
Ha = 223
324 n
mi
Hp = 213
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20802268
43 X = 6366818
38
Y = -5240967
99 feet Y = -1526395
83 meter
Z = -6007950
29 Z = -1800359
36
XDOT = -1078
519418 XDOT = -358
863365
YDOT = 16910
660043 feet/sec YDOT = 5150
525066 meter/sec
ZDOT = -18562
158019 ZDOT = -5659
415396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8604758
22 X = 2622730
31
Y = 19691949
88 feet Y = 6002106
32 meter
Z = -5872208
24 Z = -1789849
07
XDOT = -15399
620297 XDOT = -4693
804266
YDOT = 1214
596495 feet/sec YDOT = 370
209012 meter/sec
ZDOT = -18570
336029 ZDOT = -5660
238422
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 16366
52869382
00016717 00000-0 10270-3 0 9057
2 25544 51
6386 154
0980 0006931 35
4380 324
7232 15
53985305 35678
Satellite: ISS
Catalog Number: 25544
Epoch time: 16366
52869382 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 154
0980 deg
Eccentricity:
0006931
Arg of perigee: 35
4380 deg
Mean anomaly: 324
7232 deg
Mean motion: 15
53985305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3567
Checksum: 329
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