A satellite orbits Mars on a closed orbit with e=0.6 and r₁= 4500 km. Calculate the flight path angle(s) y and velocity vectors v components in the rotating frame (v, and v₁) when r= 10000 km.

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A satellite orbits Mars on a closed orbit with e=0.6 and rp= 4500 km. Calculate the flight
path angle(s) y and velocity vectors v components in the rotating frame (v, and v₁)
when r = 10000 km.
Transcribed Image Text:A satellite orbits Mars on a closed orbit with e=0.6 and rp= 4500 km. Calculate the flight path angle(s) y and velocity vectors v components in the rotating frame (v, and v₁) when r = 10000 km.
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