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Imagine you are in charge of a rescue mission. The spacecraft in distress is in a circular orbit at 240 km altitude. The Shuttle (rescue

Imagine you are in charge of a rescue mission. The spacecraft in distress is in a circular orbit at 240 km altitude. The Shuttle (rescue vehicle) is in a coplanar circular orbit at 120 km altitude. The Shuttle is 135 degrees behind the target spacecraft.
What is the TOF of the Shuttles transfer orbit to rendezvous with the target spacecraft?
What is the Shuttles angular velocity? The target spacecrafts?
What is the lead angle?
What is the final phase angle?
How long must the Shuttle wait before starting the rendezvous maneuver?

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