Quick question on orbital eccentricity and mechanical energy

In summary, the conversation discusses the interpretation of a formula involving the specific orbital energy, gravitational parameter, and specific relative angular momentum in a two body problem. The question is whether the value of e is solely determined by the specific mechanical energy and angular momentum of a planet in orbit around the Sun. Further context is provided from a Wikipedia article on gravitational force.
  • #1
Contadoren11
11
0
Hi

I'm really at a loss: How should this formula be interpreted? Is e simply dependent on the specific mechanical energy of, say, a planet in orbit around the Sun as well as its angular momentum?

52dc105647c497f0c83b12338f0974bd.png
 
Astronomy news on Phys.org
  • #2
You need to provide some context. Where it's from and what the symbols mean.
 
  • #3
  • #4
Contadoren11 said:
Hi

I'm really at a loss: How should this formula be interpreted? Is e simply dependent on the specific mechanical energy of, say, a planet in orbit around the Sun as well as its angular momentum?

52dc105647c497f0c83b12338f0974bd.png

I'd say the answer to your question is "yes", but I think you're looking for more than that. Maybe you should elaborate.
 

Related to Quick question on orbital eccentricity and mechanical energy

1. What is orbital eccentricity?

Orbital eccentricity is a measure of how an orbit deviates from a perfect circle. It is defined as the ratio of the distance between the foci of an elliptical orbit to the length of the major axis of the ellipse.

2. How is orbital eccentricity related to mechanical energy?

The eccentricity of an orbit affects the mechanical energy of the orbiting body. An orbit with high eccentricity will have a higher total mechanical energy, as the body will experience greater variations in both kinetic and potential energy throughout its orbit.

3. What is the range of possible values for orbital eccentricity?

Orbital eccentricity can range from 0 to 1, with 0 representing a perfect circular orbit and 1 representing a parabolic orbit. An eccentricity of 1 or higher indicates that the orbiting body will not return to its starting point.

4. How is orbital eccentricity calculated?

Orbital eccentricity can be calculated using the equation e = (r_max - r_min) / (r_max + r_min), where r_max is the distance between the farthest point in the orbit and the center of the orbit, and r_min is the distance between the closest point and the center.

5. What factors can influence orbital eccentricity?

The primary factor that can influence orbital eccentricity is the gravitational pull of other objects. In a two-body system, the eccentricity will remain constant. However, in a multi-body system, the gravitational interactions between multiple objects can cause changes in eccentricity over time.

Similar threads

Replies
6
Views
808
  • Astronomy and Astrophysics
Replies
8
Views
1K
  • Astronomy and Astrophysics
Replies
30
Views
1K
  • Astronomy and Astrophysics
Replies
27
Views
2K
  • Introductory Physics Homework Help
Replies
5
Views
761
  • Astronomy and Astrophysics
Replies
7
Views
4K
  • Astronomy and Astrophysics
Replies
4
Views
2K
  • Astronomy and Astrophysics
Replies
2
Views
3K
  • Astronomy and Astrophysics
Replies
10
Views
1K
Replies
2
Views
810
Back
Top