(a) Calculate the orbital inclination required to place a Venus-orbiting spacecraft in a 400 km-by-900 km sun-synchronous orbit. (b) Determine the periapsis and apoapsis for a Mars-orbiting spacecraft whose orbit satisfies all the following conditions: it is sun-synchronous, its argument of perigee is constant, and its period is 7 h.
(a) Calculate the orbital inclination required to place a Venus-orbiting spacecraft in a 400 km-by-900 km sun-synchronous orbit. (b) Determine the periapsis and apoapsis for a Mars-orbiting spacecraft whose orbit satisfies all the following conditions: it is sun-synchronous, its argument of perigee is constant, and its period is 7 h.
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
Transcribed Image Text:(a) Calculate the orbital inclination required to place a Venus-orbiting spacecraft in a
400 km-by-900 km sun-synchronous orbit.
(b) Determine the periapsis and apoapsis for a Mars-orbiting spacecraft whose orbit
satisfies all the following conditions: it is sun-synchronous, its argument of perigee is
constant, and its period is 7 h.
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