Use our Orbit Apocentre Calculator to quickly determine the farthest point in an object's elliptical orbit from its primary body. Simply input the semi-major axis and orbital eccentricity to find the apocentre distance, crucial for satellite planning, space mission analysis, and understanding celestial mechanics.
Formula:
The apocentre distance (rapo) is calculated using the formula:
rapo = a(1 + e)
- a = Semi-major axis of the orbit (e.g., in kilometers or Astronomical Units)
- e = Orbital eccentricity (a dimensionless value)