Calculating Geosynchronous Orbit for a Satellite Around Jupiter's Moon

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To determine the altitude for a satellite to achieve a geosynchronous orbit around one of Jupiter's moons, calculations must consider the moon's mass, radius, and rotational period. The satellite, with a mass of 183.0 kg, needs to be positioned at a specific height above the moon's surface, which has a radius of 3000.0 km and a mass of 4.80E+23 kg. The speed required for the satellite to maintain this orbit is linked to the gravitational force and centripetal acceleration. Additionally, the moon will exhibit uniform circular motion influenced by the satellite, necessitating the calculation of the moon's radius of motion. Understanding these relationships is crucial for solving the problem effectively.
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Homework Statement



1. One of Jupiter's moons has a mass of 4.80E+23 kg and a radius of 3000.0 km. How high above the surface of the moon should a satellite of mass 183.0 kg be so that it undergoes geosynchronous orbit about the moon? The rotational period of the moon is 0.2639 days.

2. How fast must the satellite be moving so that it maintains the geosynchronous orbit?

3. The moon will also travel in uniform circular motion in small circles due to the presence of the satellite. Using the fact that the period of motion for the moon is the same as the period of motion for the satellite, find the radius of motion for the moon.

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gonzalo12345 said:

Homework Statement



1. One of Jupiter's moons has a mass of 4.80E+23 kg and a radius of 3000.0 km. How high above the surface of the moon should a satellite of mass 183.0 kg be so that it undergoes geosynchronous orbit about the moon? The rotational period of the moon is 0.2639 days.

2. How fast must the satellite be moving so that it maintains the geosynchronous orbit?

3. The moon will also travel in uniform circular motion in small circles due to the presence of the satellite. Using the fact that the period of motion for the moon is the same as the period of motion for the satellite, find the radius of motion for the moon.

Homework Equations



i don't know

The Attempt at a Solution



I don't know how to star it

1. Work out the relationship between speed, v, of the satellite and the radius of orbit, r by analysing the force/acceleration. (If the satellite is moving in a circle of radius r, and speed v, what is the centripetal acceleration? What supplies that acceleration? What is the formula for calculating that central force/acceleration?)

2. How is the speed of the satellite related to the period of rotation and the radius, r? Substitute that expression for v into the relationship in 1.

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