Orbital Period Calculator
Calculate the orbital period of a satellite or celestial object based on the radius of orbit and the central body's mass.
Formula:
Orbital Period: T = 2π × √(r³ / (G × M))
Where:
T = orbital period (seconds)
G = gravitational constant = 6.67430 × 10⁻¹¹ N·m²/kg²
M = mass of central body (kg)
r = orbit radius from center of mass (m)