x86
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Homework Statement
A satellite in orbit above Earths equator is traveling at an orbital speed of 7.45 km/s.
a) Determine the altitude of the satellite
b) Determine the satellites period
Homework Equations
v = sqrt(Gm/r)
The Attempt at a Solution
7.45 * 1000 = 7450 m/s
I plugged in the values to that equation and got a radius of 7.1 * 10^6 m.
Now, I'm not sure how to find the altitude, but shouldn't it be the value I found (7.1*10^6m) minus Earth's radius? This gives me the value of 700 km
For b, I'm not sure how to find the period, I tried T = 2pir / V where r was the radius I found and got 5988 seconds. Is this correct?