A geosyncchronous equatorial orbiting (GEO) satellite orbits 22.300 miles above the equator of Earth. It completes one full revolution each 24 hours. Assume Earth's radius is 3960 miles.
Let me try......ok, I can assume that :)
Done, I have assumed that the Earth's radius is 3960 miles. Now what?
a) How far will the GEO satellite travel in one day ?
b) Whay is the satellite's linear velocity in miles per hour ?
Then it travels in a circle with radius 3960+22.3 miles in a day so 2πr with r=3988.3.
For part a. about 25,046.524 miles
For part b. just divide by 24 and you get 1043.60517 miles per hour.
a) 1 day = 3960+ 22.982.3 than ?
3960 + 22.982.3 represents the outer radius because satellite orbits above equator of the earth
The to solve for how far it will travel in one day (24 hours) you use the circumference formula: 2*pi*r...r = 3988.3
So 2*(pi)*(3988.3) = 25,046.524 miles
Then linear velocity in miles per hour is 25,046.525 miles/ 24 hours = 1043.6052 miles / hour
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radius small circle = 3960 big circle= 33.300?
no radius of big circle is 3960 + 33.300 = 3993
Think about it you start from center of inside circle
than small is ?
small is what you were given to start with: 3960
full revolution each 24 hours, for travel big circle ?
Good full revolution of 24 hours is 2*pi*r pi is constant = 3.14..or use your calculator for approximation r = 3993
Do you get it?
22.300+3960=26.260
26.260^2*3.14?
I don't know how u get 3993?
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