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Escape Velocity & Orbital Speed Calculator

The Escape Velocity & Orbital Speed Calculator computes the velocities required to maintain orbit or break free from celestial gravitational capture.

Choose a celestial body or provide custom parameters.

Mass of the parent celestial body in kilograms.

Equatorial mean radius of the celestial body in kilometers.

Altitude above the surface (e.g., ISS orbits at ~400 km).

Calculated Result
10.85 km/skm/s

Escape Velocity

Circular Orbital Speed

7.67 km/s

Surface Gravity

9.82 m/s²

Orbital Period

92.4 min

Total Distance from Core

6,771 km

Calculation Breakdown

  1. Gravitational Parameter (GM)6.6743e-11 × 5.9720e+24 kg = 3.9859e+14 m³/s²
  2. Orbital Speed (v_orb = √(GM / r))√(3.9859e+14 / 6771000 m) = 7.67 km/s
  3. Escape Velocity (v_esc = √(2GM / r) = v_orb × √2)7.67 km/s × 1.4142 = 10.85 km/s

Escape Velocity by Celestial Body (km/s)

Interactive visualization based on your current inputs

Calculated Value
0.0154309463618MoonMarsEarthJupiterSun

What Is the Escape Velocity & Orbital Speed Calculator?

Escape velocity is the minimum speed an unpropelled object needs to break free from the gravitational capture of a massive body without further propulsion.

Circular orbital speed is the tangential velocity required to maintain a stable circular orbit at a specific radial distance.

How Does the Escape Velocity & Orbital Speed Calculator Work?

Total distance from center of mass is computed as r = (radiusKm + altitudeKm) · 1000 meters.

Orbital speed is v_orb = √(GM / r) using G = 6.6743 × 10⁻¹¹ m³/(kg·s²).

Escape velocity is calculated as v_esc = v_orb · √2.

Escape Velocity & Orbital Speed Calculator Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

v_esc = √(2 · G · M / r), v_orb = √(G · M / r)

Escape velocity equals the square root of 2GM/r, which is exactly √2 times the circular orbital velocity at the same radius.

How to Use the Escape Velocity & Orbital Speed Calculator

  1. Select a planet or celestial body from presets or configure custom mass and radius.
  2. Set orbital altitude in kilometers above the planet surface.
  3. Examine escape velocity, orbital speed, surface gravity, and orbital period.

Step-by-Step Example Calculation

Earth Low Earth Orbit (400 km ISS)

Input Values:

bodyPreset:earth
massKg:5.972e+24
radiusKm:6371
altitudeKm:400
Worked Steps: At 400 km altitude, circular orbital velocity is 7.67 km/s with an escape velocity of 10.85 km/s.

Understanding Your Result

Surface escape velocity from Earth is approximately 11.19 km/s (40,270 km/h).

The orbital speed for Low Earth Orbit (LEO) is approximately 7.67 km/s, giving a 92-minute orbit period.

Factors That Affect the Result

  • Celestial Mass: Directly increases gravitational potential and escape velocity.
  • Altitude: Increasing altitude reduces both required orbital speed and local escape velocity.

When Should You Use This Calculator?

  • Aerospace trajectory engineering and rocket delta-v budgeting.
  • Astrophysics coursework and satellite orbital mission planning.

Assumptions & Limitations

  • Neglects atmospheric drag and non-spherical gravitational perturbations (J2 effect).

Frequently Asked Questions

Calculation Accuracy & Reference Note

Calculations use universal gravitational constant G = 6.67430 × 10⁻¹¹ m³/(kg·s²).

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