- #1
Penguinluons
- 5
- 0
Hi. I have recently been trying my hands at calculating a few orbits but have encountered difficulties in trying to 'understand' the semi latus rectum.
P=h^2/GM
What does it have to do with the orbiting object's angular momentum? How come I get different values when I derive it from other equations? Please help me as I need to understand this to move on to elliptic orbits.
(Note: When I derived P from other equations, I got different values but they were all quite close to each other.)
P=h^2/GM
What does it have to do with the orbiting object's angular momentum? How come I get different values when I derive it from other equations? Please help me as I need to understand this to move on to elliptic orbits.
(Note: When I derived P from other equations, I got different values but they were all quite close to each other.)