A geocentric satellite has orbital elementsi = 28.5 , N = 152 , and w = 180 . Determine its position and velocity vectors in the perifocal frame if it is currently at apogee with an altitude of 2,337 km and inertial velocity of 6.592 km/s.
A geocentric satellite has orbital elementsi = 28.5 , N = 152 , and w = 180 . Determine its position and velocity vectors in the perifocal frame if it is currently at apogee with an altitude of 2,337 km and inertial velocity of 6.592 km/s.
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Transcribed Image Text:A geocentric satellite has orbital elementsi
= 28.5 , N = 152 , and w = 180 . Determine
its position and velocity vectors in the
perifocal frame if it is currently at apogee
with an altitude of 2,337 km and inertial
velocity of 6.592 km/s.
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