Velocity of a satellite in a eccentric orbit

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Homework Help Overview

The discussion revolves around the velocity of a satellite in an eccentric orbit around a planet. The satellite's closest and farthest points from the planet are specified as 100 km and 200 km, respectively. Participants explore the implications of these distances on the satellite's speed, particularly focusing on the relationship between distance and velocity in orbital mechanics.

Discussion Character

  • Exploratory, Assumption checking, Conceptual clarification

Approaches and Questions Raised

  • Participants discuss the application of conservation of angular momentum to determine the satellite's speed at different points in its orbit. Questions arise regarding the interpretation of the given distances as either radii or heights above the planet's surface, and the need for additional information about the planet's mass or radius is noted.

Discussion Status

The discussion is active, with participants providing insights and questioning assumptions. Some suggest that the speed at the closest point must be greater than the speed at the farthest point, while others clarify the meaning of the distances involved. There is a recognition of the need for more information to accurately assess the situation.

Contextual Notes

Participants note the potential confusion regarding whether the distances provided are radii or heights above the surface, which impacts the calculations. The original poster mentions their background as an engineer, indicating a desire for deeper understanding rather than a straightforward solution.

farolero
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Homework Statement


A satellite is orbiting an still planet, the farthest part of the orbit is at 200 km and the closest part at 100 km.

what would be the speed of the satellite at the closest part of the orbit at 100 km if the speed at the farthest part is 1 m/s?

Homework Equations



L=mvr

The Attempt at a Solution


I tried to apply conservation of momentum with which the result would be 0.5 m/s but I am not sure if this result is valid for its posible the planet acquires a rotation to keep conservation of momentum true, value I dot know how to obtain.

I was told to post this here though is not actually homework, I am already an engineer and finished already my studies but I still want to learn more
 
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farolero said:

Homework Statement


A satellite is orbiting an still planet, the farthest part of the orbit is at 200 km and the closest part at 100 km.
Are the given distances meant to be orbit radii or heights above the planet surface? It must be a very small planet if they are orbit radii!

If they are heights above the surface then you will need additional information to establish either the true orbit radii (so, the radius of the planet) or the mass of the planet
what would be the speed of the satellite at the closest part of the orbit at 100 km if the speed at the farthest part is 1 m/s?

Homework Equations



L=mvr

The Attempt at a Solution


I tried to apply conservation of momentum with which the result would be 0.5 m/s but I am not sure if this result is valid for its posible the planet acquires a rotation to keep conservation of momentum true, value I dot know how to obtain.

I was told to post this here though is not actually homework, I am already an engineer and finished already my studies but I still want to learn more
Conservation of angular momentum is a good approach, but as mentioned above you need a bit more information about the orbit to fix its size.
 
As it gets closer the speed increases so 0.5 m/s cannot be th right answer in any case.
But unless you specify what these distances mean, as suggested already, the only thing you can say is that the speed will be larger than 1 m/s.
 
The distances are to the center of the planet, I suppose the planet has such a mass as to make the farthest orbit data posible

My apologies I am a bit dislexic i meant 2 m/s where i said 0.5 m/s

Notice the radius halves which helps a lot in the calculations.
 
When the satellite is at 150 km from the planets center, what is the component of its velocity at right angles to a line drawn from the planet's center?
 
thanks i found the solution to keep angular momentum true it would be 2 m/s
 

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