Eccentricity of orbit. Apogee and perigee positions and distances

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    Eccentricity Orbit
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Homework Help Overview

The discussion revolves around the eccentricity of a satellite's elliptical orbit around the Earth, focusing on the definitions and calculations related to apogee and perigee distances. Participants explore the relationship between these distances and the eccentricity formula.

Discussion Character

  • Exploratory, Conceptual clarification, Assumption checking

Approaches and Questions Raised

  • Participants express uncertainty about how to begin solving the problem and question the calculations related to the distances from the foci of the ellipse to its center. There are attempts to clarify the definitions of apogee and perigee in relation to the Earth's center.

Discussion Status

The discussion is ongoing, with participants seeking clarification on relevant equations and definitions. Some have suggested looking up information in textbooks or online resources, while others have indicated they may consult their teacher for further guidance.

Contextual Notes

One participant noted the absence of relevant equations in the original post, which may be crucial for progressing in the discussion. There is also a recognition that the center of the Earth is at one of the foci of the ellipse, which is a key assumption in understanding the problem.

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Homework Statement



A satellite is in an elliptical orbit about the Earth. The center of the Earth is a focus of the elliptical orbit. The perigee (C) is the point in the orbit where the satellite is closest to the Earth's center (F). The perigee distance (P) is the distance from the perigee to the Earth's center. The apogee (D) is the point furtheest from the Earth's center. The apogee distance (A) is the distance from the apogee to the Earth's center.

Show that the eccentricity of the orbit in terms of A and P is e=(A-p)/(A+P).

The Attempt at a Solution



Not sure where to begin, i know the distance from the center of the orbit to F is sqrt(a^2 - b^2), where a is the semi-major axis and b is the semi-minor axis.
 
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How is the distance from a focus of an ellipse to the centre calculated?
 


Kurdt said:
How is the distance from a focus of an ellipse to the centre calculated?

I mean the center of the elipse.

Let c equal the distance between the elipse center and a focus.
a = the semi major axis
b = semi minor

c=sqrt(A^2 - b^2)

Is that what you meant?
 


shad0w0f3vil said:
Not sure where to begin, i know the distance from the center of the orbit to F is sqrt(a^2 - b^2), where a is the semi-major axis and b is the semi-minor axis.
The center of the Earth is not at the center of the ellipse. It is at one of the two foci of the ellipse.
 


Sorry my bad, I did already understand that, just struggled to put it into words
 


It's a bit hard to help you here because you left out a very important part of the original post:

Homework Equations



What equations are relevant to solving this problem?
 


If you look up an ellipse in a textbook or even on the internet you'll probably find what you need to do this question.
 


yeh i will just ask my teacher, i can get an answer that isn't wrong, just not sure if its the answer the teacher is looking for.

Thanks for all your help you guys!
 

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