A geosynchronous 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. a)How far will the GEO satellite travel in one day? b)What is the satellite's linear velocity in miles per hour?
radius earth + radius above earth = R C = 2pi R, is the lengthit travles in 24 hours
... distance above earth, not radius above earth .. :)
3966+22,3=3.982.3?
the , is not a decimal in this application
find diameter first ?
22300 +3960 ------ 26260
diameter? i spose if you like diameter beter than 2R
http://www.caddomillsisd.org/100820818134650763/lib/100820818134650763/chap06.pdf can you look page 355 number 12
a) 26260 than b) 26260/24?
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when we add the distance above the earth to the radius of the earth itself we get: 26260 as the overall Radius of our circle
the distance traveled is the circumference of the greater circle
and that distance divided by 24 is the speed
C = 2pi 26260 26260 26260 ------- 52520 pi = distance traveld in miles right?
3960 is radius of small circle or big circle?
small; since the earth itself is at the center of the whole thing
and the satellite is so much more farther up than that ... so add the 2 distances together
than a) = 2pi26260 ?
yes
b) 2pi26260/24 ?
yes, and simplify as wanted
can you show me in picture , where 22.300 miles
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