How Can You Calculate the Altitude of a Satellite Using Gravitational Equations?

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Homework Help Overview

The discussion revolves around calculating the altitude of a satellite using gravitational equations. The original poster presents a scenario involving a satellite's mass, gravitational potential energy, and free fall acceleration, seeking guidance on how to determine its height above the Earth.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss relevant gravitational equations, such as the gravitational force formula and its implications for calculating altitude. There are questions about the appropriateness of using standard gravitational acceleration in the context of the satellite's altitude.

Discussion Status

Some participants have provided formulas and engaged in clarifying the application of gravitational concepts. There is an ongoing exploration of how to apply these equations to the specific problem presented, with no clear consensus yet on the best approach.

Contextual Notes

The original poster has not provided their initial attempts or the relevant equations from their textbook, which is a requirement for further assistance in this forum.

chewtoy929
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how can I calculate the distance something is above the earth? as an example a 1750 kg satellite orbits the earth. it has a gravitational potential energy of 1.69*10^10 J. Its free fall accel is 6.44 m/s^2 how high is it.

How would I solve this? thanks.
 
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Welcome to the PF, chewtoy. On homework and coursework questions, you must show us the relevant equations and also your initial attempt at a solution, before we can offer much in the way of tutorial help.

You appear to be studying uniform circular motion and gravitational forces. Show us the relevant equations from your textbook for this subject matter, and tell us your thoughts on how you might use those equations to approach this question.
 
Use this formula :

F_g = GMm/r^2

or

mg = GMm/r^2
 
tnutty said:
Use this formula :

F_g = GMm/r^2

or

mg = GMm/r^2

dont you mean use a = GM/R^2? If a satellite is way above Earth's surface, using little g(9.81) for any calculation would be wrong. the point of that equation is the gravitational pull ISN'T 9.81.

the force one mass pulls on the other mass is equal to gravitational constant 6.67...something * mass of object 1 * mass of object 2 divided by the distance from the centers of the objects squared:
GMm/r^2 = F

you know by now that f = ma

substitute for f, use your given a, and solve for r.
 

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