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STS-54
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1993-01-17
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STS-54 element set GSFC-013 (Orbit 49)
STS-54
1 22313U 93 3 A 93 16.58718188 0.00059120 00000-0 19104-3 0 133
2 22313 28.4711 132.4570 0010406 269.4326 90.5092 15.89244921 494
Satellite: STS-54
Catalog number: 22313
Epoch time: 93016.58718188 (16 JAN 93 14:05:32.52 UTC)
Element set: GSFC-013
Inclination: 28.4711 deg
RA of node: 132.4570 deg Space Shuttle Flight STS-54
Eccentricity: 0.0010406 Keplerian Elements
Arg of perigee: 269.4326 deg
Mean anomaly: 90.5092 deg
Mean motion: 15.89244921 rev/day Semi-major Axis: 6682.5309 Km
Decay rate: 0.59E-03 rev/day*2 Apogee Alt: 311.10 Km
Epoch rev: 49 Perigee Alt: 297.19 Km
NOTE - This element set is based on NORAD element set # 013.
The spacecraft has been propagated to the next ascending
node, and the orbit number has been adjusted to bring it
into agreement with the NASA numbering convention.
R.A. Parise, Goddard Space Flight Center
G.L.CARMAN
STS-54
FLIGHT DAY 3 STATE VECTOR (ACTUAL)
ON ORBIT OPERATIONS
(Posted 01/15/93 by Bruce Williamson)
The following vector for the flight of STS-54 is provided by NASA
Johnson Space Center Flight Design and Dynamics Division for use in
ground track plotting programs. The vector is valid for flight
day three. The vector represents the trajectory of Endeavour after
the OMS-4 maneuver and during day 3.
Questions regarding these postings may be addressed to Roger Simpson,
Mail Code DM4, L. B. J. Space Center, Houston, Texas 77058,
Telephone (713) 483-1928.
Lift off Time : 1993/013/13:59:29.953
Lift off Date : 01/13/93
Vector Time (GMT) : 015/21:41:29.953
Vector Time (MET) : 002/07:42:00.000
Orbit Count : 38
Weight : 208114.0 LBS
Drag Coefficient : 2.00
Drag Area : 1208.5 SQ FT
M50 Elements Keplerian Elements
----------------------- --------------------------
X = -20680135.9 FT A = 3610.7809 NM
Y = 1639987.3 FT E = 0.0007676
Z = 7088501.4 FT I (M50) = 28.63417 DEG
Xdot = 1194.599724 FT/S Wp (M50) = 40.31458 DEG
Ydot = -23680.577422 FT/S RAAN (M50) = 136.72294 DEG
Zdot = 8966.082576 FT/S / N (True) = 2.11858 DEG
Anomalies \ M (Mean) = 2.11533 DEG
Ha = 164.02804 NM
Hp = 162.04195 NM
Mean of 1950 (M50) : Inertial, right-handed Cartesian system whose
Coordinate System origin is the center of the earth. The epoch
is the beginning of the Besselian year 1950.
X axis: Mean vernal equinox of epoch
Z axis: Earth's mean rotational axis of epoch
Y axis: Completes right-hand system
A: Semi-major axis
E: Eccentricity N: True anomaly
I: Inclination M: Mean anomaly
Wp: Argument of perigee Ha: Height of apogee
RAAN: Right ascension of ascending node Hp: Height of perigee
POSTED BY JBWMSON AT VMSPFHOU ON VMSPFHOU.VMBOARDS:PAONEWS