Formula Used:
| From: | To: |
The circular orbital radius calculation determines the distance from the center of a celestial body to an object in a circular orbit, based on the orbital period. This calculation is fundamental in orbital mechanics and astronomy.
The calculator uses the following formula:
Where:
Explanation: This formula derives from Kepler's third law, relating the orbital period to the semi-major axis of the orbit for circular orbits around Earth.
Details: Accurate orbital radius calculation is crucial for satellite deployment, space mission planning, astronomical observations, and understanding celestial mechanics.
Tips: Enter the orbital period in seconds. The value must be positive and valid for Earth orbits.
Q1: What is Earth's gravitational parameter ([GM.Earth])?
A: Earth's gravitational parameter is 3.986004418E+14 m³/s², representing the product of Earth's mass and the gravitational constant.
Q2: Can this formula be used for other celestial bodies?
A: Yes, but you would need to use the appropriate gravitational parameter for the specific celestial body around which the orbit occurs.
Q3: What are typical orbital periods for Earth satellites?
A: Low Earth Orbit (LEO) satellites typically have periods of 90-120 minutes, while geostationary satellites have a period of 24 hours.
Q4: How accurate is this calculation?
A: This calculation provides excellent accuracy for circular orbits around Earth, assuming the gravitational parameter is precisely known.
Q5: What units does the calculator use?
A: The calculator uses seconds for time period and meters for orbital radius, following SI units convention.