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1.At a given time, a satellite has the following position and velocity vectors: (R vector = 7016I^ + 5036J^ + 766K^ km; V vector =

1.At a given time, a satellite has the following position and velocity vectors: (R vector = 7016I^ + 5036J^ + 766K^ km; V vector = 0.339I^ - 0.556J^ - 7.696K^ km/s) Based on this information, determine the size (semimajor axis) of this orbit.

Based on the position and velocity vectors given in problem 1, determine the right ascension of the ascending node for this orbit.

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