Kepler's Third Law:
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The orbital period equation comes from Kepler's Third Law of Planetary Motion, which relates the orbital period of a satellite to the semi-major axis of its orbit and the standard gravitational parameter of the central body.
The calculator uses Kepler's Third Law:
Where:
Explanation: The equation shows that the square of the orbital period is proportional to the cube of the semi-major axis of the orbit.
Details: Calculating orbital period is essential for satellite mission planning, determining coverage patterns for communication satellites, and predicting when satellites will be visible from ground stations.
Tips: Enter the semi-major axis in meters and the standard gravitational parameter in m³/s². Common values for μ: Earth = 3.986×10¹⁴, Sun = 1.327×10²⁰.
Q1: What is the semi-major axis?
A: For circular orbits, it's equal to the orbital radius. For elliptical orbits, it's half the longest diameter of the ellipse.
Q2: How do I find the standard gravitational parameter?
A: It's the product of the gravitational constant (G) and the mass of the central body (M). Pre-calculated values are available for most celestial bodies.
Q3: Does this work for all orbits?
A: This works for idealized two-body systems. Perturbations from other bodies or non-spherical gravity fields may require more complex calculations.
Q4: Can I calculate for other units?
A: The calculator uses SI units. For other units, convert to meters and m³/s² before calculation.
Q5: What's the difference between sidereal and synodic period?
A: This calculator gives sidereal period (relative to fixed stars). Synodic period accounts for the motion of the central body and observer.