A satellite is in a circular orbit at an altitude of 250km above the earth's surface. The onboard rocket provides a Av = 200m/s, calculate the new velocity at perigee (V2) in the transfer orbit, Specific angular momentum of the transfer orbit (h₂), and eccentricity of the transfer orbit (e₂). Hohmann transfer ellipse B Apoapsis AUB Circle Circle AAVA A Periapsis

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