Good morning,
I am simulating an orbit around the lunar / seline celestial body but I ran into a problem where changing inclination / declination massively increases the semi-major axis or apoapsis height even at a slightly small change in inclination / declination angle
I attached an image...
What is the equation for increasing Periapsis Height during Apoapsis Burn ???
Hi, I am stuck at a problem I can't figure out at all, and it has to do with a space-craft conducting a burn once it is at APOAPSIS.
figure 1
With the equation above, where the angle to the spacecraft is Θ = 0° ...