[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 29th 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 3519)
---------------------------------------
Vector Time (GMT): 2016/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930840
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5013290
50 A = 6785992
32 meter
Y = 3467167
93 meter E =
0010469
Z = -2978828
83 I = 51
71535
XDOT = -5006
019584 Wp = 42
89441
YDOT = -2965
360539 meter/sec RA = 168
02202 deg
ZDOT = 4991
305916 TA = 283
09347
MA = 283
21029
Ha = 223
059 n
mi
Hp = 213
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16447803
48 X = -5037218
92
Y = 11375222
88 feet Y = 3410972
47 meter
Z = -9773060
48 Z = -3003239
71
XDOT = -16423
948767 XDOT = -4996
733517
YDOT = -9728
873159 feet/sec YDOT = -3021
289814 meter/sec
ZDOT = 16375
675577 ZDOT = 4967
010365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13163698
03 X = -4012295
16
Y = -14984219
02 feet Y = -4567189
96 meter
Z = -9880732
79 Z = -3011647
35
XDOT = 6691
816782 XDOT = 2039
665755
YDOT = -16569
004249 feet/sec YDOT = -5050
232495 meter/sec
ZDOT = 16269
564565 ZDOT = 4958
963279
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
50616079
00016717 00000-0 10270-3 0 9000
2 25544 51
6370 169
1620 0006791 24
4499 335
6975 15
53951907 35207
Satellite: ISS
Catalog Number: 25544
Epoch time: 16363
50616079 = yrday
fracday
Element set: 900
Inclination: 51
6370 deg
RA of node: 169
1620 deg
Eccentricity:
0006791
Arg of perigee: 24
4499 deg
Mean anomaly: 335
6975 deg
Mean motion: 15
53951907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 321
Coasting Arc #2 (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 = 5913342
92 A = 6788829
78 meter
Y = -2996025
33 meter E =
0015228
Z = 1449483
11 I = 51
75608
XDOT = 3335
166659 Wp = 92
15607
YDOT = 3755
635945 meter/sec RA = 163
05450 deg
ZDOT = -5791
493860 TA = 72
06163
MA = 71
89567
Ha = 223
116 n
mi
Hp = 213
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19400731
37 X = 5939364
87
Y = -9829479
42 feet Y = -2929753
00 meter
Z = 4755522
01 Z = 1478271
21
XDOT = 10942
147831 XDOT = 3321
054546
YDOT = 12321
640239 feet/sec YDOT = 3792
853709 meter/sec
ZDOT = -19000
964108 ZDOT = -5775
326533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12277967
94 X = 3742324
63
Y = 17917484
76 feet Y = 5461249
36 meter
Z = 4882343
29 Z = 1488138
23
XDOT = -9460
229478 XDOT = -2883
477945
YDOT = 11686
300604 feet/sec YDOT = 3561
984424 meter/sec
ZDOT = -18930
635334 ZDOT = -5770
057650
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
53510916
00016717 00000-0 10270-3 0 9018
2 25544 51
6367 164
0338 0006837 26
2261 333
9237 15
53977884 35362
Satellite: ISS
Catalog Number: 25544
Epoch time: 16364
53510916 = yrday
fracday
Element set: 901
Inclination: 51
6367 deg
RA of node: 164
0338 deg
Eccentricity:
0006837
Arg of perigee: 26
2261 deg
Mean anomaly: 333
9237 deg
Mean motion: 15
53977884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 324
Coasting Arc #3 (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 = -6338226
42 A = 6789780
79 meter
Y = 2400712
97 meter E =
0018990
Z = 174475
87 I = 51
79202
XDOT = -1527
812739 Wp = 41
88900
YDOT = -4498
003539 meter/sec RA = 158
09386 deg
ZDOT = 6025
853793 TA = 319
98780
MA = 320
12756
Ha = 223
206 n
mi
Hp = 213
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20794706
09 X = -6365448
25
Y = 7876354
89 feet Y = 2329682
44 meter
Z = 572427
38 Z = 143620
92
XDOT = -5012
508986 XDOT = -1506
671916
YDOT = -14757
229459 feet/sec YDOT = -4514
970934 meter/sec
ZDOT = 19769
861526 ZDOT = 6018
483093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10864355
50 X = -3311455
56
Y = -19405143
39 feet Y = -5914687
70 meter
Z = 436612
56 Z = 133079
51
XDOT = 12418
292543 XDOT = 3785
095567
YDOT = -6473
338452 feet/sec YDOT = -1973
073560 meter/sec
ZDOT = 19738
252314 ZDOT = 6016
219305
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
56405553
00016717 00000-0 10270-3 0 9023
2 25544 51
6389 158
9056 0006782 31
9109 328
2453 15
53972833 35522
Satellite: ISS
Catalog Number: 25544
Epoch time: 16365
56405553 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 158
9056 deg
Eccentricity:
0006782
Arg of perigee: 31
9109 deg
Mean anomaly: 328
2453 deg
Mean motion: 15
53972833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3552
Checksum: 329
Coasting Arc #4 (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 = 6340378
76 A = 6788365
32 meter
Y = -1594804
20 meter E =
0008606
Z = -1834157
42 I = 51
81677
XDOT = -332
913261 Wp = 90
89362
YDOT = 5155
396606 meter/sec RA = 153
13500 deg
ZDOT = -5656
509880 TA = 109
20525
MA = 109
11211
Ha = 223
329 n
mi
Hp = 213
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20801767
59 X = 6366650
43
Y = -5232297
25 feet Y = -1523754
78 meter
Z = -6017576
84 Z = -1803294
31
XDOT = -1092
235109 XDOT = -363
061089
YDOT = 16914
030858 feet/sec YDOT = 5151
505644 meter/sec
ZDOT = -18558
103280 ZDOT = -5658
199861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8596134
70 X = 2620101
86
Y = 19692946
52 feet Y = 6002410
10 meter
Z = -5881838
64 Z = -1792784
42
XDOT = -15405
137572 XDOT = -4695
485932
YDOT = 1202
227149 feet/sec YDOT = 366
438835 meter/sec
ZDOT = -18566
370784 ZDOT = -5659
029815
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
52868773
00016717 00000-0 10270-3 0 9038
2 25544 51
6386 154
0979 0006977 35
1737 324
9874 15
53989243 35678
Satellite: ISS
Catalog Number: 25544
Epoch time: 16366
52868773 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 154
0979 deg
Eccentricity:
0006977
Arg of perigee: 35
1737 deg
Mean anomaly: 324
9874 deg
Mean motion: 15
53989243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3567
Checksum: 370
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