Solve Satellite Altitude Above Earth's Surface | 16.7 kN, -1.43e11 J

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Homework Help Overview

The problem involves determining the altitude of a communication satellite in orbit around the Earth, given the gravitational force it exerts and its gravitational potential energy. The context is rooted in gravitational physics and orbital mechanics.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • The original poster attempts to use gravitational force and potential energy equations to find two unknowns: the mass of the satellite and its height above the Earth's surface. They express uncertainty about their approach and seek alternative methods. Other participants suggest that the original poster is on the right track and encourage them to continue with their method.

Discussion Status

The discussion is ongoing, with participants providing encouragement and affirming the original poster's approach. Some participants clarify the equations related to gravitational potential energy and total energy, although there is no explicit consensus on the best method yet.

Contextual Notes

There is a mention of previous discussions on similar problems, indicating that this topic has been explored before, but specific details or constraints of the current problem are not fully resolved.

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When in orbit, a communication satellite attracts the Earth with a force of 16.7 kN and the earth-satellite gravitational potential energy (relative to zero at infinite separation) is - 1.43*10^11 J. Find the satellite's altitude above the Earth's surface. The radius of the Earth is 6.38*10^6.

OK, I must be making this harder than it needs to be. What I've been trying to do is to use the formulas for gravitational force to get an equation with two unknow variables (Mass of the satellite and height above Earth's surface) And I do the same for gravitational potential energy. Then, since both equations have the same two unknown variables, I solve for one of them and substitute. Is there another way of doing this? Am I doing it copmletely wrong? Please help me! :confused:
 
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You sound like you have the right idea. Give it a shot.
 
Total Energy of a satellite revolving around Earth is given by:

[itex]- \frac{GMm}{2r}[/itex]

BJ


Note:This post has been edited after Older Dan's remarks.
 
Last edited:
Dr.Brain said:
Potential Energy of a satellite revolving around Earth is given by:

[itex]- \frac{GMm}{2r}[/itex]

BJ
There is no 2 in the potential energy. Perhaps you meant the total energy

[itex]U = - \frac{GMm}{r}[/itex]

[itex]T = \frac{1}{2}mv^2 = \frac{r}{2} \left( \frac{mv^2}{r} \right) = \frac{r}{2} \left| F_c \right| = \frac{r}{2} \left( \frac{GMm}{r^2} \right) = \frac{GMm}{2r} = -\frac{1}{2} U[/itex]

[itex]E\ \ =\ \ T\ \ +\ \ U = \frac{GMm}{2r}\ \ -\ \ \frac{GMm}{r}\ \ =\ \ - \frac{GMm}{2r}[/itex]
 

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