We wish to send a satellite from earth, which is 1.50x10 m from the center of the sun, to the surface of the sun whi has a radius of 7.0x10 m. Pretend that the satellite is impervious to the extreme heat of the sun. (a) What is the length of the semi-major axis of an ellipse that (1) intercepts both the center of the earth and a point c the sun opposite to the earth and that (2) has one of its foci at the center of the sun? (b) What is the orbital period of an object that is following the ellipse described in (a)? (c) When the satellite reaches the back of the sun, what amount of time has passed since the satellite began its journe in the above stated elliptical orbit?

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We wish to send a satellite from earth, which is 1.50x10" m from the center of the sun, to the surface of the sun which
has a radius of 7.0x10' m. Pretend that the satellite is impervious to the extreme heat of the sun.
(a) What is the length of the semi-major axis of an ellipse that (1) intercepts both the center of the earth and a point on
the sun opposite to the earth and that (2) has one of its foci at the center of the sun?
(b) What is the orbital period of an object that is following the ellipse described in (a)?
(c) When the satellite reaches the back of the sun, what amount of time has passed since the satellite began its journey
in the above stated elliptical orbit?
Transcribed Image Text:We wish to send a satellite from earth, which is 1.50x10" m from the center of the sun, to the surface of the sun which has a radius of 7.0x10' m. Pretend that the satellite is impervious to the extreme heat of the sun. (a) What is the length of the semi-major axis of an ellipse that (1) intercepts both the center of the earth and a point on the sun opposite to the earth and that (2) has one of its foci at the center of the sun? (b) What is the orbital period of an object that is following the ellipse described in (a)? (c) When the satellite reaches the back of the sun, what amount of time has passed since the satellite began its journey in the above stated elliptical orbit?
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