Classical orbital elements

In summary, classical orbital elements are a set of six parameters that describe the orbit of a celestial object around another object. They are determined through observations and measurements, and are used to predict and track the motion of celestial objects. However, they have limitations such as assuming a two-body system and not accounting for non-gravitational forces.
  • #1
ExoP
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Hi!

Is there a way to calculate the classical orbital elements for a satellite or space shuttle around Earth using Matlab? I would like to get started with it since it is something that I've not tried before. so plese help

Best regards
 
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  • #2
You can program an algorithm to extract orbital elements in MATLAB.
 

What are classical orbital elements?

Classical orbital elements are a set of six parameters that describe the orbit of a celestial object around another object, such as a planet around a star. They include the semi-major axis, eccentricity, inclination, longitude of the ascending node, argument of periapsis, and true anomaly.

How are classical orbital elements determined?

Classical orbital elements are usually determined through observations and measurements of the celestial object's position and velocity. These measurements are then used to calculate the six parameters using mathematical equations and models.

What is the significance of classical orbital elements?

Classical orbital elements provide a standardized way of describing and predicting the motion of celestial objects in space. They are essential for understanding and studying the dynamics of the solar system, as well as for spacecraft and satellite missions.

Can classical orbital elements change over time?

Yes, the classical orbital elements of a celestial object can change over time due to various factors such as gravitational interactions with other objects, atmospheric drag, and tidal forces. These changes can be predicted and tracked using mathematical models and simulations.

What are some limitations of classical orbital elements?

One limitation of classical orbital elements is that they assume a two-body system and do not take into account the gravitational influence of other objects. They also do not account for any non-gravitational forces acting on the object, such as propulsion systems or solar radiation pressure.

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