[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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 819)
---------------------------------------
Vector Time (GMT): 2012/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1829610
40 A = 6793723
89 meter
Y = 6073280
24 meter E =
0020456
Z = -2441638
79 I = 51
36708
XDOT = -5489
973559 Wp = 105
30981
YDOT = -466
347504 meter/sec RA = 235
31669 deg
ZDOT = -5316
474576 TA = 102
06982
MA = 101
84053
Ha = 230
510 n
mi
Hp = 212
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6002658
79 X = 1773422
52
Y = 19925460
10 feet Y = 6093426
20 meter
Z = -8010625
95 Z = -2432886
50
XDOT = -18011
724276 XDOT = -5458
524791
YDOT = -1530
011496 feet/sec YDOT = -527
563374 meter/sec
ZDOT = -17442
501890 ZDOT = -5343
067994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19104463
29 X = -5823040
41
Y = 8285197
06 feet Y = 2525328
07 meter
Z = -7975023
04 Z = -2430787
02
XDOT = 83
058313 XDOT = 25
316174
YDOT = -16568
845154 feet/sec YDOT = -5050
184003 meter/sec
ZDOT = -17552
785892 ZDOT = -5350
089140
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 12363
52744423
00016717 00000-0 10270-3 0 9003
2 25544 51
6477 236
1228 0015779 95
9055 264
3895 15
51757816 8201
Satellite: ISS
Catalog Number: 25544
Epoch time: 12363
52744423 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 236
1228 deg
Eccentricity:
0015779
Arg of perigee: 95
9055 deg
Mean anomaly: 264
3895 deg
Mean motion: 15
51757816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 820
Checksum: 328
Coasting Arc #2 (Orbit 835)
---------------------------------------
Vector Time (GMT): 2012/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1490763
58 A = 6791875
84 meter
Y = -5793700
19 meter E =
0028516
Z = 3192725
50 I = 51
37852
XDOT = 5897
583213 Wp = 93
26106
YDOT = 1135
331270 meter/sec RA = 230
33343 deg
ZDOT = 4775
409064 TA = 303
79770
MA = 304
06892
Ha = 230
497 n
mi
Hp = 212
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4890956
63 X = -1441375
73
Y = -19008202
72 feet Y = -5810095
03 meter
Z = 10474821
20 Z = 3185602
90
XDOT = 19349
026289 XDOT = 5861
251850
YDOT = 3724
840126 feet/sec YDOT = 1201
078100 meter/sec
ZDOT = 15667
352573 ZDOT = 4803
970725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18193413
52 X = 5545352
44
Y = -7405217
53 feet Y = -2257110
30 meter
Z = 10445935
30 Z = 3183921
08
XDOT = -1708
930785 XDOT = -520
882103
YDOT = 18248
023351 feet/sec YDOT = 5561
997517 meter/sec
ZDOT = 15785
740049 ZDOT = 4811
493567
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 12364
55782866
00016717 00000-0 10270-3 0 9011
2 25544 51
6470 231
0044 0015846 98
7560 261
5386 15
51781358 8360
Satellite: ISS
Catalog Number: 25544
Epoch time: 12364
55782866 = yrday
fracday
Element set: 901
Inclination: 51
6470 deg
RA of node: 231
0044 deg
Eccentricity:
0015846
Arg of perigee: 98
7560 deg
Mean anomaly: 261
5386 deg
Mean motion: 15
51781358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 836
Checksum: 325
Coasting Arc #3 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2012/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 980793
53 A = 6789621
45 meter
Y = 5460264
01 meter E =
0021625
Z = -3931753
41 I = 51
39053
XDOT = -6261
511915 Wp = 94
60321
YDOT = -1760
863409 meter/sec RA = 225
34801 deg
ZDOT = -4028
293575 TA = 133
12611
MA = 132
94505
Ha = 230
380 n
mi
Hp = 212
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3217826
56 X = 938762
07
Y = 17914251
99 feet Y = 5470997
19 meter
Z = -12899453
45 Z = -3927090
45
XDOT = -20543
018093 XDOT = -6221
787980
YDOT = -5777
110921 feet/sec YDOT = -1830
661092 meter/sec
ZDOT = -13216
186269 ZDOT = -4058
614890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17227004
38 X = -5250790
93
Y = 5915064
06 feet Y = 1802911
53 meter
Z = -12880724
69 Z = -3926044
89
XDOT = 3113
666421 XDOT = 949
045525
YDOT = -19835
470343 feet/sec YDOT = -6045
851361 meter/sec
ZDOT = -13341
820166 ZDOT = -4066
586787
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 12365
52380541
00016717 00000-0 10270-3 0 9024
2 25544 51
6462 226
2053 0015656 102
7930 257
4972 15
51793974 8512
Satellite: ISS
Catalog Number: 25544
Epoch time: 12365
52380541 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 226
2053 deg
Eccentricity:
0015656
Arg of perigee: 102
7930 deg
Mean anomaly: 257
4972 deg
Mean motion: 15
51793974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 310
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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