Distance from Satellite to Earth Question

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Homework Help Overview

The problem involves a satellite in a circular orbit around Earth, specifically focusing on determining the distance from the Earth's center and the altitude of the satellite in terms of Earth's radius.

Discussion Character

  • Exploratory, Conceptual clarification, Assumption checking

Approaches and Questions Raised

  • Participants discuss the meaning of "in terms of Earth's radius" and explore how to relate the satellite's distance to Earth's radius. There are attempts to apply gravitational and centripetal force equations, with some questioning the need for the satellite's mass.

Discussion Status

Some participants have provided clarifications regarding the equations needed and the interpretation of the problem. There is an ongoing exploration of the relationship between the satellite's speed and its orbital radius, with no explicit consensus reached yet.

Contextual Notes

Participants note the absence of the satellite's mass as a constraint in their calculations, which raises questions about how to proceed with the problem.

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Homework Statement


A satellite in a circular orbit around Earth has a speed of 7.15x103 m/s. Determine, in terms of Earth's radius (radius of earth= 6.38 x106m):

a) the distance the satellite is from Earth's centre
b) the altitiude of the satellite


Homework Equations


FG = GMm / r2
Fc = mv2 / r
G = 6.67 x 10-11


The Attempt at a Solution


I'm seriously unsure on how to even start on this one, because I'm not sure what they mean by 'in terms of Earth's radius.' The answer key says 1.22 rearth for a. Do you have to do this through proportionality and ratios?

In terms of writing down the given/known:
v = 7.15 x 103 m/s
rearth = 6.38 x 106 m
Mearth = 5.98 x 1024 kg
G = 6.67 x 10-11 Nm2/kg2

I can't figure out the force of gravity because I don't have the mass of the satellite, so that cancels out finding Fc as well since I need the mass for that too.

Any help on how to start this would be appreciated, thank you.
 
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You won't need the mass of the satellite.

Fc = mv2/r = Fg = GMm/r2

v2 = GM/r
 
LowlyPion said:
You won't need the mass of the satellite.

Fc = mv2/r = Fg = GMm/r2

v2 = GM/r

Oh, I see. But I'm still confused by "in terms of Earth's radius," what exactly do they mean by that?
By the way, I used v2 = GM /r to find that r = 5.58 x 1010 Would that be the radius from the Earth's centre to the satellite?
Thanks for your help
 
In terms of Earth's radius means how many multiples of the Earth's radius is the satellite orbiting at.
 
Kurdt said:
In terms of Earth's radius means how many multiples of the Earth's radius is the satellite orbiting at.

Ah, I got it now. Thanks for the help Kurdt and LowlyPion.
 

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