Need help with satellites and Kepler's Laws

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Homework Help Overview

The discussion revolves around a problem involving a satellite's orbit and the application of Kepler's Laws. The original poster presents a scenario where a satellite orbits a planet, and they seek to determine the planet's radius based on given parameters such as the satellite's mass, orbital period, and gravitational acceleration on the planet's surface.

Discussion Character

  • Exploratory, Assumption checking, Problem interpretation

Approaches and Questions Raised

  • Participants explore the relationship between gravitational force and centripetal force to derive the planet's mass. Questions are raised about how to find the period of a satellite given the planet's mass and orbital radius, and whether the known values can be used to determine the planet's mass.

Discussion Status

Some participants have offered suggestions regarding the use of formulas related to orbital mechanics, while others express confusion about the parameters involved. The discussion reflects a mix of interpretations and attempts to clarify the relationships between the variables without reaching a consensus.

Contextual Notes

There is a noted lack of clarity regarding the radius of the planet and how it relates to the satellite's orbital radius. The original poster expresses urgency due to a deadline, which may influence the discussion dynamics.

fiestytig
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Here's my problem:

A 23.0-kg satellite has a circular orbit with a period of 2.35 h and a radius of 8.90×106 m around a planet of unknown mass. If the magnitude of the gravitational acceleration on the surface of the planet is 8.90 m/s2, what is the radius of the planet?

I got to say, I have no idea where to start since I don't have the mass of the planet. Any help? Pretty please? Due tonight at 10 pm EST... thanks!
 
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The force acting on the satellite is also the centripetal force. F-mv^2/R and F-G(M*m)/r^2. that should help you find the mass of the planet. right?
 
First question: Do you know how to find the period of a satellite if you know the planet's mass and the Radius of its orbit?

Second question: If you do, can't you use this method to find the Planet's mass when you know the period and radius of the orbit?
 
I'm afraid I still don't follow, even with those suggestions... All I really know is T^2=4 Pi^2 r^3 /G M. But I don't really have the r either, do I?
 
fiestytig said:
I'm afraid I still don't follow, even with those suggestions... All I really know is T^2=4 Pi^2 r^3 /G M. But I don't really have the r either, do I?

Then what is this?

A 23.0-kg satellite has a circular orbit with a period of 2.35 h and a radius of 8.90×106 m around a planet of unknown mass.
 
So then how do I find the radius of the planet? (I got confused by the radiuses there for a minute.)
 
Aha! I figured it out! Thanks. Had to use a formula to find mass and then use g = G+M/R^2 to find R. :)
 

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