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Homework Help: Find the altitude of the satellite

  1. Sep 14, 2010 #1
    1. The problem statement, all variables and given/known data

    At the instant when theta is 120 degrees, the angle theta is increasing at the rate of 2.7 degrees per min. Find the altitude of the satellite and the rate at which the altitude is changing at this instant. Express the rate in units of mi/min.

    2. Relevant equations

    r = 4995/(1+0.12cos(theta))
    earth's radius = 3960 mi

    3. The attempt at a solution

    I think I found the altitude alright. I plugged in 120 degrees to the equation and subtracted the radius and got 1354 mi. But I've been working on the other part for the past half hour and I haven't gotten anywhere helpful. I tried to take the derivative of the equation but I get 0. And I'm just so stumped. Can anyone help me out?
  2. jcsd
  3. Sep 15, 2010 #2


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    Homework Helper

    I'm sorry but I don't quite understand this problem. Don't satellites orbit the Earth so the altitude above the surface is constant. Obviously if the satellite is higher but goes faster then the rate at which the angle changes will be equivalent to slower and lower altitude satellite. Obviously I'm not understanding it because I don't even know how the info of the radius of the Earth fits into this.
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