Coasting Arc #4 (begining on orbit 2235) ---------------------------------------
Vector Time (GMT): 2005/210/14:39:00
000
Vector Time (MET): N/A
Weight (LBS) : 402858
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3748909
21 A = 6726275
12 meter
Y = -2083072
21 meter E =
0015219
Z = -5194773
43 I = 51
83461
XDOT = 4871
748969 Wp = 109
42348
YDOT = 5827
810792 meter/sec RA = 43
11275 deg
ZDOT = 1176
713595 TA = 171
81687
MA = 171
79202
Ha = 193
519 n
mi
Hp = 186
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12299570
90 X = 3797158
80
Y = -6834226
42 feet Y = -2040879
50 meter
Z = -17043219
91 Z = -5176444
44
XDOT = 15983
428377 XDOT = 4800
503377
YDOT = 19120
114147 feet/sec YDOT = 5881
890825 meter/sec
ZDOT = 3860
608908 ZDOT = 1200
207976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13651789
13 X = -4161065
33
Y = 3725267
12 feet Y = 1135461
42 meter
Z = -16976703
98 Z = -5174499
37
XDOT = -10741
515561 XDOT = -3274
013943
YDOT = -21344
711801 feet/sec YDOT = -6505
868157 meter/sec
ZDOT = 3946
893208 ZDOT = 1203
013050
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 05210
62429728
00020000 00000-0 20000-3 0 9030
2 25544 51
6428 43
5852 0002853 175
3557 184
7632 15
72005888 22364
Satellite: ISS
Catalog Number: 25544
Epoch time: 05210
62429728 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 43
5852 deg
Eccentricity:
0002853
Arg of perigee: 175
3557 deg
Mean anomaly: 184
7632 deg
Mean motion: 15
72005888 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2236
Checksum: 296
INTERNATIONAL SPACE STATION ORBITAL DATA:
This data has been supplied courtesy of NASA JSC (Johnson Space Center)
David Cottle
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