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shade585
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[SOLVED] synchronous orbit
A orbiting satellite stays over a certain spot on the equator of (rotating) Mercury. What is the altitude of the orbit (called a "synchronous orbit")?
The answer needs to be in km.
I know the synchronous orbit is where the satellite has a period equal to the average roational period of the planet.
T^2 = ((4pi^2)/(GM))r^3
T would be the rotational period of Mercury.
G is the gravitational constant.
M would be mercury's mass.
I would be solving for r.
So far i have been plugging in numbers but nothing has been working. Should T be in years, days, hours, or seconds?
Homework Statement
A orbiting satellite stays over a certain spot on the equator of (rotating) Mercury. What is the altitude of the orbit (called a "synchronous orbit")?
The answer needs to be in km.
Homework Equations
I know the synchronous orbit is where the satellite has a period equal to the average roational period of the planet.
T^2 = ((4pi^2)/(GM))r^3
T would be the rotational period of Mercury.
G is the gravitational constant.
M would be mercury's mass.
I would be solving for r.
The Attempt at a Solution
So far i have been plugging in numbers but nothing has been working. Should T be in years, days, hours, or seconds?