Satellite Distance Formula:
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The satellite distance calculation determines how far a satellite is from Earth's surface based on its orbital period. This is derived from Kepler's third law of planetary motion.
The calculator uses the following equation:
Where:
Explanation: The equation calculates the semi-major axis of the orbit and subtracts Earth's radius to get the distance from the surface.
Details: Knowing a satellite's distance is crucial for orbital mechanics, communication satellite placement, and understanding orbital characteristics.
Tips: Enter the orbital period in seconds. The result will be the distance from Earth's surface in meters.
Q1: What is geostationary orbit distance?
A: For a period of 86400 seconds (24 hours), the distance is about 35,786 km above Earth's equator.
Q2: How does altitude affect orbital period?
A: Higher orbits have longer periods. The International Space Station at ~400 km has a period of about 90 minutes.
Q3: What's the lowest possible orbit?
A: About 160 km, below which atmospheric drag would quickly de-orbit a satellite.
Q4: Does this work for other planets?
A: Yes, but you'd need to substitute that planet's mass and radius.
Q5: Why subtract Earth's radius?
A: The equation gives distance from Earth's center, so we subtract the radius to get altitude above surface.