[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 66 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 3155)
---------------------------------------
Vector Time (GMT): 2011/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4032091
44 A = 6763852
31 meter
Y = -1298682
42 meter E =
0022651
Z = 5285716
94 I = 51
29119
XDOT = 2314
135506 Wp = 219
91770
YDOT = 7307
810671 meter/sec RA = 252
50774 deg
ZDOT = 13
182565 TA = 229
85667
MA = 230
05531
Ha = 218
384 n
mi
Hp = 204
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13228646
44 X = 4020637
20
Y = -4260769
11 feet Y = -1253657
42 meter
Z = 17341591
01 Z = 5305276
67
XDOT = 7592
308092 XDOT = 2232
182083
YDOT = 23975
756796 feet/sec YDOT = 7333
230529 meter/sec
ZDOT = 43
249886 ZDOT = 24
225792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5998666
67 X = 1828393
60
Y = 12425174
15 feet Y = 3787193
08 meter
Z = 17421626
34 Z = 5310111
71
XDOT = -21819
915062 XDOT = -6650
710111
YDOT = 10333
102145 feet/sec YDOT = 3149
529534 meter/sec
ZDOT = 87
857523 ZDOT = 26
778973
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 11364
54809639
00016717 00000-0 10270-3 0 9006
2 25544 51
6433 253
1404 0024211 224
4487 135
4725 15
58778299 31567
Satellite: ISS
Catalog Number: 25544
Epoch time: 11364
54809639 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 253
1404 deg
Eccentricity:
0024211
Arg of perigee: 224
4487 deg
Mean anomaly: 135
4725 deg
Mean motion: 15
58778299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3156
Checksum: 317
Coasting Arc #2 (Orbit 3170)
---------------------------------------
Vector Time (GMT): 2011/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4689387
50 A = 6767831
00 meter
Y = -2313394
49 meter E =
0021550
Z = -4299805
00 I = 51
31489
XDOT = 167
983351 Wp = 207
58094
YDOT = -6839
970256 meter/sec RA = 247
43924 deg
ZDOT = 3471
070820 TA = 97
96323
MA = 97
71861
Ha = 218
087 n
mi
Hp = 204
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15385129
59 X = -4642282
70
Y = -7589876
95 feet Y = -2365570
51 meter
Z = -14106971
80 Z = -4322471
49
XDOT = 551
126481 XDOT = 227
595134
YDOT = -22440
847295 feet/sec YDOT = -6837
758632 meter/sec
ZDOT = 11388
027624 ZDOT = 3472
031320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5168421
94 X = 1575335
01
Y = -16278147
65 feet Y = -4961579
40 meter
Z = -14199451
46 Z = -4327992
80
XDOT = 21064
172960 XDOT = 6420
359918
YDOT = -3322
943893 feet/sec YDOT = -1012
833299 meter/sec
ZDOT = 11392
438135 ZDOT = 3472
415143
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 11365
50975071
00016717 00000-0 10270-3 0 9018
2 25544 51
6433 248
3119 0024179 228
2881 131
6206 15
58790914 31716
Satellite: ISS
Catalog Number: 25544
Epoch time: 11365
50975071 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 248
3119 deg
Eccentricity:
0024179
Arg of perigee: 228
2881 deg
Mean anomaly: 131
6206 deg
Mean motion: 15
58790914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3171
Checksum: 308
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
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