Coasting Arc #3 (begining on orbit 2220) ---------------------------------------
Vector Time (GMT): 2005/209/14:39:00
000
Vector Time (MET): N/A
Weight (LBS) : 402858
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3294532
06 A = 6736695
51 meter
Y = 5633827
51 meter E =
0013410
Z = 1650190
91 I = 51
88819
XDOT = -4969
131919 Wp = 75
37728
YDOT = 1210
361941 meter/sec RA = 48
24183 deg
ZDOT = 5753
037559 TA = 302
77568
MA = 302
90481
Ha = 193
570 n
mi
Hp = 186
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10808832
22 X = 3223272
79
Y = 18483686
04 feet Y = 5670270
14 meter
Z = 5414012
16 Z = 1666023
08
XDOT = -16302
926242 XDOT = -5010
243994
YDOT = 3971
003743 feet/sec YDOT = 1154
563979 meter/sec
ZDOT = 18874
795140 ZDOT = 5728
797984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5772155
47 X = -1759352
99
Y = -20603991
71 feet Y = -6280096
67 meter
Z = 5472364
96 Z = 1667976
84
XDOT = 15373
209701 XDOT = 4685
754317
YDOT = 713
418858 feet/sec YDOT = 217
450068 meter/sec
ZDOT = 18786
648154 ZDOT = 5726
170357
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 05209
67073619
00020000 00000-0 20000-3 0 9026
2 25544 51
6420 48
4666 0002876 173
6981 186
4218 15
71993341 22212
Satellite: ISS
Catalog Number: 25544
Epoch time: 05209
67073619 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 48
4666 deg
Eccentricity:
0002876
Arg of perigee: 173
6981 deg
Mean anomaly: 186
4218 deg
Mean motion: 15
71993341 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2221
Checksum: 300
INTERNATIONAL SPACE STATION ORBITAL DATA:
This data has been supplied courtesy of NASA JSC (Johnson Space Center)
David Cottle
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