L/m = 7.8e10
2E/m = 0.
Probe is near earth. I checked eccentricity and it is 1--so we know it is a parabola.
As such, how do I find when it is closest to earth? I only know how to do this with elliptical or hyperbolic orbits.
Physics Stack Exchange is a question and answer site for active researchers, academics and students of physics. It only takes a minute to sign up.
Sign up to join this communityL/m = 7.8e10
2E/m = 0.
Probe is near earth. I checked eccentricity and it is 1--so we know it is a parabola.
As such, how do I find when it is closest to earth? I only know how to do this with elliptical or hyperbolic orbits.