Sphere of Influence Calculator
Enter the masses of two bodies and their orbital distance to calculate the Hill sphere (gravitational sphere of influence) radius.
Input Parameters
Mass of the central / dominant body (e.g. the Sun)
Mass of the smaller body whose sphere is being calculated
Average distance between the two bodies (orbital semi-major axis)
Quick Presets
Enter the parameters and click Calculate
or choose a preset above
Hill Sphere Radius
—
kilometers
Result in Different Units
—
meters (m)
—
kilometers (km)
—
astronomical units (AU)
Practical Stable Orbit Limit
Objects typically remain in long-term stable orbits within ~1/3 of the Hill sphere radius (tidal truncation limit).
—
1/3 Hill radius (km)
—
1/3 Hill radius (AU)
Calculation Summary
Parent mass (M)
—
Orbiting mass (m)
—
Semi-major axis (a)
—
Mass ratio m / 3M
—
r = a × (m / 3M)1/3
Summary
Enter the masses of two bodies and their orbital distance to calculate the Hill sphere (gravitational sphere of influence) radius.
How it works
- Enter the mass of the parent body (e.g. the Sun) in kilograms.
- Enter the mass of the orbiting body (e.g. a planet) in kilograms.
- Enter the semi-major axis (average orbital distance) in meters or astronomical units.
- Click Calculate to compute the Hill sphere radius.
- The result is shown in meters, kilometers, and astronomical units for easy comparison.
Use cases
- Determine whether a moon can remain in stable orbit around a planet.
- Check the maximum distance at which an asteroid can hold a captured companion.
- Compare the Hill spheres of Solar System planets.
- Estimate stable satellite orbit limits for exoplanet systems.
- Educational exercises in orbital mechanics and celestial dynamics.
- Mission design for interplanetary probes near gravitational boundaries.
Frequently Asked Questions
Last updated: 2026-06-11 ·
Reviewed by Nham Vu