Calculate the true anomaly at given position


Voyager 1 is on an escape trajectory from the solar system with the orbital element a = - 480926000 km; e = 3.724716

a) What is the orbit would like around the sun?

b) What is the magnitude of the angular momentum?

c) What is the specific energy ?

d) What is the true anomaly of the asymptote

e) What is the distance from perigee to the sun?

f) The current distance is 125.6AU from the sun , assuming Voyager 1 was always on its hyperbolic trajectory, calculate the true anomaly at this position.

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Mechanical Engineering: Calculate the true anomaly at given position
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