Parabolic trajectory

unbound Kepler orbit with the eccentricity equal to 1 From Wikipedia, the free encyclopedia

Remove ads

In astronomy, a parabolic trajectory (also known as parabolic orbit or parabolic escape trajectory) refers to an object (such as an asteroid) which follows a path similar to a parabola around another object. This motion follows Kepler's Laws. A parabolic trajectory occurs when the eccentricity of its orbit is equal to 1.

Other types of motion in astronomy include circular orbit, elliptical orbit, and hyperbolic trajectory.


Remove ads
Loading related searches...

Wikiwand - on

Seamless Wikipedia browsing. On steroids.

Remove ads