[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 29th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2472)
---------------------------------------
Vector Time (GMT): 2013/361/17:52:37
450
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2223717
29 A = 6789820
61 meter
Y = 3762242
23 meter E =
0012239
Z = -5206748
37 I = 51
35903
XDOT = -5688
491680 Wp = 61
66842
YDOT = -4984
379017 meter/sec RA = 228
32059 deg
ZDOT = -1168
515333 TA = 197
03803
MA = 197
07916
Ha = 227
021 n
mi
Hp = 222
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7295660
40 X = -2240329
22
Y = 12343314
40 feet Y = 3737282
61 meter
Z = -17082507
77 Z = -5217591
15
XDOT = -18663
030445 XDOT = -5626
656119
YDOT = -16352
949532 feet/sec YDOT = -5047
645550 meter/sec
ZDOT = -3833
711723 ZDOT = -1195
999658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6375228
14 X = -1943169
54
Y = 12781235
59 feet Y = 3895720
61 meter
Z = -17128707
65 Z = -5220830
09
XDOT = -18725
972372 XDOT = -5707
676379
YDOT = -14647
905884 feet/sec YDOT = -4464
681714 meter/sec
ZDOT = -3948
630362 ZDOT = -1203
542534
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 13361
76308038
00016717 00000-0 10270-3 0 9006
2 25544 51
6478 229
2258 0004796 318
7859 41
2929 15
50021494 24734
Satellite: ISS
Catalog Number: 25544
Epoch time: 13361
76308038 = yrday
fracday
Element set: 900
Inclination: 51
6478 deg
RA of node: 229
2258 deg
Eccentricity:
0004796
Arg of perigee: 318
7859 deg
Mean anomaly: 41
2929 deg
Mean motion: 15
50021494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2473
Checksum: 324
Coasting Arc #2 (Orbit 2488)
---------------------------------------
Vector Time (GMT): 2013/362/17:52:37
450
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2243089
51 A = 6789507
74 meter
Y = -3660734
49 meter E =
0002273
Z = 5259686
75 I = 51
37939
XDOT = 5951
816492 Wp = 354
39558
YDOT = 4762
248222 meter/sec RA = 223
34450 deg
ZDOT = 778
504479 TA = 88
14526
MA = 88
11923
Ha = 227
012 n
mi
Hp = 222
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7359217
54 X = 2258307
76
Y = -12010283
76 feet Y = -3635566
15 meter
Z = 17256190
13 Z = 5270620
19
XDOT = 19526
956994 XDOT = 5894
339848
YDOT = 15624
173957 feet/sec YDOT = 4828
483798 meter/sec
ZDOT = 2554
148554 ZDOT = 807
278684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6243955
11 X = 1903157
52
Y = -12562190
71 feet Y = -3828955
73 meter
Z = 17302759
49 Z = 5273881
09
XDOT = 19808
283492 XDOT = 6037
564808
YDOT = 13519
281153 feet/sec YDOT = 4120
676896 meter/sec
ZDOT = 2674
543911 ZDOT = 815
200984
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 13362
79464643
00016717 00000-0 10270-3 0 9016
2 25544 51
6478 224
1143 0004926 321
5526 38
5273 15
50035658 24894
Satellite: ISS
Catalog Number: 25544
Epoch time: 13362
79464643 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 224
1143 deg
Eccentricity:
0004926
Arg of perigee: 321
5526 deg
Mean anomaly: 38
5273 deg
Mean motion: 15
50035658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2489
Checksum: 314
Coasting Arc #3 (Orbit 2503)
---------------------------------------
Vector Time (GMT): 2013/363/17:52:37
450
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2282826
63 A = 6789294
67 meter
Y = 3590285
34 meter E =
0012971
Z = -5301579
63 I = 51
40216
XDOT = -6177
598231 Wp = 68
13122
YDOT = -4500
620727 meter/sec RA = 218
37234 deg
ZDOT = -383
859994 TA = 198
16582
MA = 198
21221
Ha = 227
206 n
mi
Hp = 221
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7489588
67 X = -2297050
70
Y = 11779151
39 feet Y = 3564678
31 meter
Z = -17393633
95 Z = -5312703
59
XDOT = -20267
710733 XDOT = -6124
947468
YDOT = -14765
816035 feet/sec YDOT = -4569
408143 meter/sec
ZDOT = -1259
383182 ZDOT = -413
742760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6178696
95 X = -1883266
83
Y = 12450546
04 feet Y = 3794926
43 meter
Z = -17440999
26 Z = -5316016
57
XDOT = -20713
883943 XDOT = -6313
591826
YDOT = -12237
102858 feet/sec YDOT = -3729
868951 meter/sec
ZDOT = -1384
501254 ZDOT = -421
995982
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 13363
76172941
00016717 00000-0 10270-3 0 9022
2 25544 51
6480 219
3248 0004887 326
2334 33
8505 15
50057063 25042
Satellite: ISS
Catalog Number: 25544
Epoch time: 13363
76172941 = yrday
fracday
Element set: 902
Inclination: 51
6480 deg
RA of node: 219
3248 deg
Eccentricity:
0004887
Arg of perigee: 326
2334 deg
Mean anomaly: 33
8505 deg
Mean motion: 15
50057063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2504
Checksum: 298
Coasting Arc #4 (Orbit 2519)
---------------------------------------
Vector Time (GMT): 2013/364/17:52:37
450
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2357680
88 A = 6789179
89 meter
Y = -3515964
37 meter E =
0004278
Z = 5307877
76 I = 51
42685
XDOT = 6385
168282 Wp = 358
41171
YDOT = 4235
383468 meter/sec RA = 213
39910 deg
ZDOT = -26
467715 TA = 91
86594
MA = 91
81694
Ha = 227
217 n
mi
Hp = 221
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7735173
50 X = 2371037
84
Y = -11535316
19 feet Y = -3489525
20 meter
Z = 17414297
12 Z = 5319363
16
XDOT = 20948
714837 XDOT = 6337
461294
YDOT = 13895
615053 feet/sec YDOT = 4306
519747 meter/sec
ZDOT = -86
836336 ZDOT = 4
435317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6235710
11 X = 1900644
44
Y = -12341292
55 feet Y = -3761625
97 meter
Z = 17463178
13 Z = 5322776
70
XDOT = 21520
572924 XDOT = 6559
470627
YDOT = 10914
675201 feet/sec YDOT = 3326
793001 meter/sec
ZDOT = 42
637277 ZDOT = 12
995842
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 13364
79327276
00016717 00000-0 10270-3 0 9030
2 25544 51
6481 214
2134 0005002 329
4369 30
6490 15
50072882 25206
Satellite: ISS
Catalog Number: 25544
Epoch time: 13364
79327276 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 214
2134 deg
Eccentricity:
0005002
Arg of perigee: 329
4369 deg
Mean anomaly: 30
6490 deg
Mean motion: 15
50072882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2520
Checksum: 290
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