Hill Sphere Radius Calculator

Enter primary mass, secondary mass, orbital separation, and eccentricity to find the Hill sphere radius and stable moon orbit boundaries for any two-body system.

🌐 Hill Sphere Radius Calculator
System Preset
Primary Body Mass (M)
M⊕
Secondary Body Mass (m)
M⊕
Orbital Separation (a)
AU
Orbital Eccentricity (e)e = 0.0167
0 (circular)0.95 (highly elliptical)
Hill Sphere Radius rH
rH / a ratio
Max Stable Prograde Orbit (0.5 rH)
Max Stable Retrograde Orbit (0.7 rH)
Mass Parameter (m / 3M)1/3

🌐 What Is the Hill Sphere?

The Hill sphere (named after American astronomer George William Hill) is the region around a secondary body within which it can gravitationally dominate over the tidal forces of the primary. A satellite orbiting within the Hill sphere experiences a net gravitational pull toward the secondary body, allowing it to remain bound. A satellite beyond the Hill sphere is pulled more strongly toward the primary and will eventually drift into a solar orbit rather than a planetary orbit.

The Hill sphere radius is given by rH = a(1 − e)(m/3M)1/3, where a is the semi-major axis, e is the orbital eccentricity, m is the secondary body mass, and M is the primary mass. The eccentricity term (1 − e) reflects the fact that tidal forces are strongest at perihelion, where the secondary is closest to the primary, so the gravitational sphere of influence contracts at closest approach. For circular orbits (e = 0) the formula simplifies to rH = a(m/3M)1/3.

The Hill sphere governs which moons are stable around a planet. Prograde moons (orbiting in the same sense as the planet's orbit around its star) are typically stable only within about 0.5 rH. Retrograde moons (orbiting in the opposite direction) can remain stable out to about 0.7 rH because they are less vulnerable to resonant perturbations from the star's gravity. Jupiter's outermost known retrograde moon Neso orbits at about 47 million km, remarkably close to the 0.7 rH stability boundary of 35 million km. Beyond these limits, moons are gradually perturbed onto hyperbolic escape trajectories.

The Hill sphere is closely related to the Lagrange points. The L1 and L2 Lagrange point distances from the secondary body are approximately equal to rH (to first order), both being proportional to (m/3M)1/3. The key difference is that the Hill sphere formula uses m/3M (mass of secondary over three times the mass of the primary) while the Lagrange formula uses the mass ratio mu = m/(M+m). For small m/M, these are nearly identical. The Hill sphere formula also includes the eccentricity correction, which the standard Lagrange point formula omits. This calculator is therefore more appropriate when orbital eccentricity is significant.

📐 Formula

rH  =  a × (1 − e) × (m / 3M)1/3
rH = Hill sphere radius (metres)
a = semi-major axis of secondary's orbit around primary (metres)
e = orbital eccentricity (0 for circular, 0 to 1 for elliptical)
m = mass of secondary body (kg or any consistent unit)
M = mass of primary body (same units as m)
Stable prograde orbit limit ≈ 0.5 × rH (beyond this, prograde moons are lost)
Stable retrograde orbit limit ≈ 0.7 × rH (retrograde moons are more stable)
Example: Earth (1 M⊕) orbiting Sun (333,000 M⊕) at 1 AU with e = 0.0167: rH = 1 AU × 0.9833 × (1/999,000)1/3 ≈ 1,471,507 km

📖 How to Use This Calculator

Steps

1
Select a preset system or enter custom masses — Choose Sun-Earth, Sun-Mars, Sun-Jupiter, or Sun-Pluto from the dropdown to auto-fill realistic values, or select a preset and modify the inputs for a custom system.
2
Enter primary body mass in Earth masses — Input the mass of the larger body in Earth masses. The Sun is 333,000 M-Earth; Jupiter is 317.8 M-Earth; Mars is 0.107 M-Earth.
3
Enter secondary body mass and orbital separation — Input the secondary body mass in Earth masses and the orbital semi-major axis in AU. Earth is 1 M-Earth at 1 AU; Pluto is 0.00218 M-Earth at 39.48 AU.
4
Set the orbital eccentricity — Enter the orbital eccentricity from 0 (perfectly circular) to 0.95. Use the slider for quick exploration. Earth has e=0.0167, Mars e=0.0934, Pluto e=0.2488.
5
Read the Hill sphere radius and stable orbit limits — The calculator outputs the Hill sphere radius, the ratio r_H/a, and the approximate maximum stable prograde orbit (0.5 r_H) and retrograde orbit (0.7 r_H) boundaries.

💡 Example Calculations

Example 1 — Earth Orbiting the Sun (e = 0.0167)

Sun (333,000 M⊕) and Earth (1 M⊕) at 1 AU with eccentricity e = 0.0167

1
Mass parameter: (m/3M)1/3 = (1/999,000)1/3 = 0.010003
2
Eccentricity factor: (1 − 0.0167) = 0.9833
3
Hill sphere: rH = 1 AU × 0.9833 × 0.010003 = 0.009836 AU = 1,471,507 km
4
Max stable prograde moon orbit: 0.5 × 1,471,507 = 735,754 km. The Moon at 384,400 km is at 52% of this limit, safely inside. Max stable retrograde: 0.7 × 1,471,507 = 1,030,055 km.
Hill Sphere Radius = 1,471,507 km (0.9836% of orbital separation)
Try this example →

Example 2 — Jupiter Orbiting the Sun (e = 0.0489)

Sun (333,000 M⊕) and Jupiter (317.8 M⊕) at 5.203 AU with eccentricity e = 0.0489

1
Mass parameter: (317.8/3/333,000)1/3 = (3.178e-4)1/3 = 0.06826
2
Eccentricity factor: (1 − 0.0489) = 0.9511. Hill sphere: rH = 5.203 AU × 0.9511 × 0.06826 = 50,536,800 km (0.3378 AU)
3
Stable prograde orbit limit: 0.5 × 50,536,800 = 25,268,400 km. All Galilean moons (Io through Callisto, 422,000 to 1,883,000 km) are far inside this limit.
4
Stable retrograde orbit limit: 0.7 × 50,536,800 = 35,375,760 km. Jupiter's outermost retrograde moon Neso orbits at ~47 million km, slightly beyond this estimate, illustrating the approximation nature of the 0.7 r_H rule.
Hill Sphere Radius = 50,536,800 km (0.3378 AU) with 6.4927% of orbital separation
Try this example →

Example 3 — Pluto Orbiting the Sun (e = 0.2488)

Sun (333,000 M⊕) and Pluto (0.00218 M⊕) at 39.48 AU with eccentricity e = 0.2488

1
Mass parameter: (0.00218/3/333,000)1/3 = (2.182e-9)1/3 = 0.001297
2
Eccentricity factor: (1 − 0.2488) = 0.7512. Without eccentricity, rH would be 7,658,000 km. With it: rH = 39.48 AU × 0.7512 × 0.001297 = 5,754,770 km, a 25% reduction.
3
Stable prograde orbit limit: 0.5 × 5,754,770 = 2,877,385 km. Stable retrograde limit: 0.7 × 5,754,770 = 4,028,339 km.
4
Charon orbits Pluto at 19,600 km, only 0.34% of Pluto's Hill sphere radius, solidly bound. The high orbital eccentricity significantly constrains the size of Pluto's gravitational sphere of influence.
Hill Sphere Radius = 5,754,770 km (0.0385 AU), reduced by eccentricity from ~7.7 million km
Try this example →

❓ Frequently Asked Questions

What is the Hill sphere and what does it mean for moon stability?+
The Hill sphere is the region around a planet (or other secondary body) within which the planet's gravity dominates over the tidal forces from its host star. Moons orbiting within the Hill sphere experience a net gravitational pull toward the planet and remain bound. Beyond the Hill sphere, the star's tidal forces dominate and the moon will eventually escape into solar orbit. For long-term stability, prograde moons must be within about 0.5 Hill radii and retrograde moons within about 0.7 Hill radii.
Why does eccentricity reduce the Hill sphere radius?+
At perihelion (closest approach to the star), the gravitational tidal forces from the star are at their maximum, compressing the planet's sphere of gravitational influence. The Hill sphere formula accounts for this by including the factor (1-e), so a planet in an elliptical orbit has a smaller effective Hill sphere than one at the same average distance on a circular orbit. Pluto (e=0.2488) has a Hill sphere about 25% smaller than the circular-orbit estimate at the same semi-major axis.
How does Earth's Hill sphere compare to the Moon's orbit?+
Earth's Hill sphere radius with eccentricity e=0.0167 is about 1.47 million km. The Moon orbits at 384,400 km, which is 26% of Earth's Hill sphere radius, well within the prograde stability limit of 0.5 r_H = 735,000 km. Earth could theoretically support stable moons out to about 735,000 km in prograde orbits and 1,030,000 km in retrograde orbits. The Moon's position is very stable against solar perturbations.
Why can retrograde moons orbit farther out than prograde moons?+
Prograde moons move in the same direction as the planet's orbit around the star, making them susceptible to cumulative gravitational perturbations (especially mean-motion resonances with the star) that can build up and destabilize the orbit. Retrograde moons move in the opposite direction, which averages out many perturbation effects. Numerical simulations consistently show that retrograde orbits remain stable to about 0.6 to 0.75 Hill radii, while prograde orbits are limited to about 0.4 to 0.5 Hill radii.
What is Earth's Hill sphere and what objects does it contain?+
Earth's Hill sphere (accounting for eccentricity) has a radius of about 1.47 million km. It contains the Moon (384,400 km), all active satellites and space stations (300 to 36,000 km), and several L1 and L2 spacecraft such as SOHO and JWST at about 1.5 million km from Earth (just outside the Hill sphere). Earth's Hill sphere boundary roughly coincides with where the Sun's gravity begins to dominate, around the L1 and L2 Lagrange points.
Why does Jupiter have so many irregular moons?+
Jupiter has over 95 known moons, including more than 80 irregular moons in distant, eccentric, inclined, or retrograde orbits. Jupiter's large mass (317.8 M-Earth) and heliocentric distance (5.2 AU) give it an enormous Hill sphere of about 50 million km, providing a large capture zone. During the early solar system, Jupiter's gravity was strong enough to capture and retain many passing objects. The irregular moons likely represent captured Kuiper Belt objects or disrupted asteroids from the early solar system.
How is the Hill sphere used in spacecraft mission design?+
Mission designers use the Hill sphere to determine whether a spacecraft will remain bound to a planet during transit or escape into solar orbit. Spacecraft approaching a planet must enter its Hill sphere and perform an orbital insertion maneuver before reaching periapsis. For lunar missions, the spacecraft must stay within Earth's Hill sphere during transfer. L1 and L2 spacecraft (SOHO, JWST) orbit just at the Hill sphere boundary and require periodic station-keeping to remain near the equilibrium points.
What is the Hill sphere of the Sun itself?+
The Sun's Hill sphere is the region around the Sun dominated by its gravity against the galactic tidal field and nearest stars. It is estimated at roughly 1 to 2 light-years radius, comparable to the outer Oort Cloud (0.5 to 2 light-years). Beyond this, galactic tidal forces and passing stars can perturb objects into hyperbolic trajectories that leave the solar system. The Oort Cloud comets that fall toward the inner solar system are often perturbed from the outer edge of the Sun's Hill sphere by such gravitational events.
How does Pluto's Hill sphere compare to its moon Charon?+
Pluto's Hill sphere radius is about 5.75 million km (accounting for its high eccentricity e=0.2488). Charon orbits at only 19,600 km, about 0.34% of Pluto's Hill sphere radius, making it extremely well bound. Pluto also has four smaller moons (Styx, Nix, Kerberos, Hydra) orbiting between 42,700 and 64,700 km, all well within 2% of the Hill sphere. Despite Pluto's small mass (0.00218 Earth masses), its large heliocentric distance (39 AU) gives it a surprisingly large Hill sphere.
What happens to a moon that wanders beyond the Hill sphere?+
A moon that drifts beyond the Hill sphere boundary does not escape immediately. Instead, it enters a chaotic gravitational environment where the star's tidal forces begin to dominate. Over many orbital periods, perturbations build up and the moon's orbit becomes increasingly eccentric. Eventually it either escapes into a solar orbit, gets ejected from the system entirely, or (rarely) falls back to collide with the planet. The Hill sphere boundary is therefore a statistical stability boundary, not a hard wall. Objects just outside the Hill sphere can survive for millions of years before eventually escaping.

What is the Hill sphere and how does it differ from the Lagrange point?

The Hill sphere is the roughly spherical region around a secondary body within which it can hold satellites against perturbations from the primary. Its radius r_H = a(1-e)(m/(3M))^(1/3) includes eccentricity because the gravitational influence shrinks at perihelion. The L1 Lagrange point distance uses the slightly different formula r = a(mu/3)^(1/3) with mu = m/(M+m); for small m/M these are nearly identical, but the Hill sphere formula is the standard used for satellite stability analysis.

How far out can a moon orbit stably within the Hill sphere?

In general, prograde moons (orbiting in the same sense as the secondary's orbit around the primary) are stable only within about 0.5 times the Hill sphere radius. Retrograde moons can remain stable out to about 0.7 times r_H because retrograde orbits are less susceptible to resonant perturbations from the primary star. Objects beyond these limits are eventually ejected by tidal forces.

Why does orbital eccentricity shrink the Hill sphere?

At perihelion (closest approach to the primary star), the tidal forces from the primary are strongest. The Hill sphere formula accounts for this by multiplying by (1-e), so a body in a highly elliptical orbit has a smaller effective Hill sphere than one in a circular orbit. Pluto (e=0.2488) has a Hill sphere about 75% the size it would have at the same average distance but on a circular orbit.

What is Earth's Hill sphere radius and how does it compare to the Moon's orbit?

Earth's Hill sphere with eccentricity e=0.0167 has a radius of about 1.47 million km. The Moon orbits at 384,400 km, which is about 26% of Earth's Hill sphere radius, safely inside the stable prograde orbit limit of 0.5 r_H = 735,000 km. This means the Moon is well protected from solar perturbations. Earth could theoretically hold a moon at distances up to about 735,000 km on a prograde orbit.

Why does Jupiter have so many moons?

Jupiter's large mass (317.8 M-Earth) and relatively large heliocentric distance give it a Hill sphere of about 50 million km, one of the largest in the solar system after the Sun. This enormous gravitational sphere of influence allows Jupiter to capture and retain over 95 known moons, including numerous irregular satellites in distant, eccentric, and even retrograde orbits out near the Hill sphere boundary.

How is the Hill sphere different from the Roche limit?

The Roche limit defines how close a satellite can approach a primary before tidal forces tear it apart (roughly 2.44 times the primary's radius for fluid bodies). The Hill sphere defines how far away a satellite can orbit the secondary and still be gravitationally bound to it. Moons must orbit outside the Roche limit (to avoid being disrupted) and inside the Hill sphere (to avoid being captured by the primary). Planetary rings typically lie inside the Roche limit.

Can the Sun capture a body that is outside Earth's Hill sphere?

Yes. Objects beyond Earth's Hill sphere experience stronger gravitational influence from the Sun than from Earth and will eventually be pulled into solar orbit rather than remaining bound to Earth. The Hill sphere defines the boundary of Earth's gravitational dominance. Satellites in lunar-transfer trajectories that temporarily exceed the Hill sphere radius must be actively controlled to return to Earth capture.

What is the Hill sphere of a binary star system?

For a binary star system (two comparable-mass stars), neither star has a Hill sphere in the usual sense because neither mass is much larger than the other. Instead, circumbinary planets (orbiting both stars) can be stable outside about 2 to 4 times the binary separation, while circumstellar planets (orbiting one star) can be stable within about 0.2 to 0.5 times the binary separation. For a binary with a 10:1 mass ratio, the less massive star has a Hill sphere r_H = a(m/(3M))^(1/3) where M is the primary.

How does the Hill sphere relate to the Lagrange point calculator?

The Hill sphere radius and the L1/L2 Lagrange point distance from the secondary are both approximately a(mu/3)^(1/3) for small mass ratios mu = m/(M+m). The Hill sphere formula uses m/(3M) exactly, while the Lagrange formula uses m/(3(M+m)). For small m/M (such as Sun-Earth with m/M = 3e-6), the difference is negligible. The Hill sphere calculator adds the eccentricity correction (1-e), which is important for bodies in elliptical orbits.

What determines whether the Moon is stably bound to Earth?

The Moon orbits at 384,400 km, which is 26% of Earth's Hill sphere radius. The stable prograde orbit limit is 0.5 r_H = 735,000 km, so the Moon orbits well within this boundary. Over billions of years the Moon is gradually receding from Earth at 3.8 cm per year due to tidal energy transfer, but it will not escape Earth's Hill sphere within the Sun's remaining lifetime. The Moon's orbit is also nearly circular (e = 0.055), which helps with long-term stability.