Semi Major Axis of Phasing Ellipse evaluator uses Semi Major Axis of Ellipse = ((Number of Period*Gravitational Parameter^0.5)/(2*pi))^(2/3) to evaluate the Semi Major Axis of Ellipse, Semi Major Axis of Phasing Ellipse refers to the longest radius of the ellipse used to describe the relative positions of two objects in space during orbital maneuvers, particularly in the context of orbital rendezvous and docking maneuvers. Semi Major Axis of Ellipse is denoted by a symbol.
How to evaluate Semi Major Axis of Phasing Ellipse using this online evaluator? To use this online evaluator for Semi Major Axis of Phasing Ellipse, enter Number of Period (n) & Gravitational Parameter (μ) and hit the calculate button.