Satellite Orbit around the earth, speed?

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Homework Help Overview

The problem involves a satellite in a circular orbit around the Earth, with a given mass of the Earth and the period of the satellite's orbit. The original poster attempts to determine the speed of the satellite but is unsure how to calculate the radius of its orbit.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • Participants discuss the relationship between gravitational force and centripetal force to find the radius. There are questions about the meaning of angular velocity and constants involved in the calculations.

Discussion Status

Some participants have provided insights on using gravitational principles and Kepler's Third Law to find the radius. There is ongoing clarification about the terms used in the equations, and multiple interpretations of the problem are being explored.

Contextual Notes

Participants note the importance of unit consistency when applying the formulas. The original poster expresses uncertainty about the radius of the satellite's orbit compared to the Earth's radius.

neoncrazy101
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The question is...
A satellite is in a circular orbit about the Earth (M = 5.98 x 1024 kg). The period of the satellite is 6.72 x 104 s. What is the speed at which the satellite travels?

I know the speed is equal to (2piR)/6.72x10^4s But I can't figure out the radius. I know the Earth's radius is 6.38x10^6 but how can I go about figuring out the radius that the satellite travels?
 
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You need to use the fact that the gravitational force of attraction between the Earth and the satellite is equal to the centripetal force experienced by the satellite.

You know T, so you can get ω using ω =2π /T.
 
alright thanks but one question, I am not familiar with the w looking thing nor the 2n. What are they?
 
neoncrazy101 said:
alright thanks but one question, I am not familiar with the w looking thing nor the 2n. What are they?

ω = omega = angular velocity

n = constant pi = 3.1415...
 
neoncrazy101 said:
The question is...
A satellite is in a circular orbit about the Earth (M = 5.98 x 1024 kg). The period of the satellite is 6.72 x 104 s. What is the speed at which the satellite travels?

I know the speed is equal to (2piR)/6.72x10^4s But I can't figure out the radius. I know the Earth's radius is 6.38x10^6 but how can I go about figuring out the radius that the satellite travels?

You could apply Kepler's Third Law to get the radius. The square of the period divided by the cube of the orbital radius equals 2pi divided by GM (i.e., the universal gravitational constant times the mass of the body at the center of the orbit).

Just be careful with units.
 

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