discreditedvalidity
New member
- Joined
- Mar 16, 2006
- Messages
- 5
Here is the word problem:
A satellite is in an elliptical orbit around the earth with the center of the earth at one focus. The heigh of the satellite over the earth varies between 140 and 440 mi. Assume th earth is a sphere with radius 3960 mi. Find an equation for the path of the satellite with the origin at the center of the earth.
Okay, so far I have done this, and I don't know if I'm doing it right:
2a = 140 + 2(3960) + 144
= 140 + 7920 + 440
= 8500
a= 4250
a - c = 3960 + 140 = 4100
c = a- 4100
c = 4250 - 4100
= 150
foci = (+150, 0) (-150, 0)
c^2 = a^2 - b^2
b^2 = a^2 - c^2
= 4250^2 - 150^2
=18040000
That's all I have.
1) Have I done right so far? If not, what am I doing wrong?
2) How on earth do I get the equation?
Thanks!
A satellite is in an elliptical orbit around the earth with the center of the earth at one focus. The heigh of the satellite over the earth varies between 140 and 440 mi. Assume th earth is a sphere with radius 3960 mi. Find an equation for the path of the satellite with the origin at the center of the earth.
Okay, so far I have done this, and I don't know if I'm doing it right:
2a = 140 + 2(3960) + 144
= 140 + 7920 + 440
= 8500
a= 4250
a - c = 3960 + 140 = 4100
c = a- 4100
c = 4250 - 4100
= 150
foci = (+150, 0) (-150, 0)
c^2 = a^2 - b^2
b^2 = a^2 - c^2
= 4250^2 - 150^2
=18040000
That's all I have.
1) Have I done right so far? If not, what am I doing wrong?
2) How on earth do I get the equation?
Thanks!