What is the altitude above earth's surface?

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To determine the altitude of a satellite above Earth's surface with an orbital speed of 4.2 x 10^3 m/s, relevant equations include gravitational force and uniform circular motion. The gravitational force equation, Fg = G(m1*m2)/r^2, is essential, but the mass of the satellite and its radius need clarification. Participants emphasize the need to apply the equation for uniform circular motion, which connects velocity, mass, radius, and central force. The discussion highlights the importance of showing work for effective assistance. Understanding these principles is crucial for solving the altitude problem.
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Here's the question. I'm not sure how to apporoach it.

A satellite has an orbital speed of 4.2 x 10 exponent 3 m/s. What is the altitude above Earth's surface? (M of Earth = 5.98 x 10 exponent 24 kg, radius of Earth = 6.38 x 10 exponent 6 m)
 
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Thread moved to Homework Help.

What equations do you think apply? What do you know so far about forces in circular motion? What is the general equation for the gravitational attraction of two masses?

You must show us your work before we can offer much in the way of tutorial help (see the "Rules" link at the top of the page).
 
ok well, i think i should use the equation Fg = Gmm over r^2

but i don't know how to find the other mass. and the radius of the satellite.
 
oosta said:
ok well, i think i should use the equation Fg = Gmm over r^2

but i don't know how to find the other mass. and the radius of the satellite.

That's one of the two equations you need. What is the equation for uniform circular motion that relates the velocity (angular or orbital linear) to the mass, radius and central force?
 

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