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Orbital Velocity Calculator

Compute the speed, period, and angular speed of an object in a circular orbit from the central mass and orbital radius.

kg

Mass of the body being orbited (e.g. Earth ≈ 5.972e24 kg)

m

Distance from the center of the central mass
Orbital speed
7,672.32m/s

Speed needed to maintain a circular orbit

Orbital speed
7,672.318 m/s
Orbital speed
7.6723 km/s
Period
5,545.0579 s
Period
1.5403 h
Angular speed
0.0011 rad/s
Central massSatellitev = √(G·M / r) = 7.6723 km/s
Step by step
  1. 1

    G × M

    6.674 × 10⁻¹¹ × 5,972,000,000,000,000,000,000,000 = 398,571,280,000,000
  2. 2

    G × M ÷ r

    398,571,280,000,000 ÷ 6,771,000 = 58,864,463.1517
  3. 3

    Orbital speed v = √(G × M ÷ r)

    √58,864,463.1517 = 7,672.32
    The speed at which gravitational pull exactly provides the centripetal acceleration.
Results are estimates for general information only and are not professional advice — always verify important results independently before relying on them. Read the full disclaimer.
Quick answer

How does this calculator work?

Orbital velocity for a circular orbit is v = √(G·M/r), where G = 6.674×10⁻¹¹, M is the central mass in kg, and r is the orbital radius in meters. The period is T = 2π·√(r³/(G·M)) and angular speed is ω = v/r. The orbiting object's own mass does not affect the result.

Formula
v = √(G·M / r); T = 2π·√(r³ / (G·M)); ω = v / r
How this is calculated

For a circular orbit, gravity supplies exactly the centripetal force needed to keep the orbiting body on its path. Setting G·M·m/r² equal to m·v²/r and cancelling the orbiting mass m gives the orbital speed v = √(G·M / r), where G = 6.674×10⁻¹¹ N·m²/kg² is the gravitational constant, M is the central mass in kilograms, and r is the orbital radius in meters measured from the center of the central body.

The orbital period follows from the circumference 2πr divided by v, which simplifies to T = 2π·√(r³ / (G·M)) — a statement of Kepler's third law. The angular speed is ω = v / r in radians per second. Speed is reported in both m/s and km/s, and the period in both seconds and hours for convenience.

This model assumes a perfectly circular orbit, a point-mass (or spherically symmetric) central body, and that the orbiting mass is negligible compared with M. It ignores atmospheric drag, oblateness, and the gravity of other bodies. Both M and r must be positive; r is measured from the center, so for a surface-skimming orbit use the central body's radius plus altitude.

Frequently asked questions

No. The orbiting mass cancels out of the equation, so a small satellite and a large one at the same radius around the same body travel at the same speed.

Use Earth's radius (~6.371×10⁶ m) plus the altitude. For example, a 400 km orbit uses r ≈ 6.771×10⁶ m.

It is the same physical time, just different units. The calculator shows both so you can quickly relate short orbits (minutes to hours) to longer ones.

Also known as

orbital velocity
orbit speed
satellite speed
orbital period
v=sqrt(gm/r)
orbital speed
satellite velocity

APA

TG we-Calculate Editorial Team. (2026). Orbital Velocity Calculator [Online calculator]. TG we-Calculate. https://we-calculate.com/calculator/orbital-velocity-calculator

Chicago

TG we-Calculate Editorial Team. "Orbital Velocity Calculator." TG we-Calculate. 2026. https://we-calculate.com/calculator/orbital-velocity-calculator.

IEEE

TG we-Calculate Editorial Team, "Orbital Velocity Calculator," TG we-Calculate, 2026. [Online]. Available: https://we-calculate.com/calculator/orbital-velocity-calculator

BibTeX

@misc{wecalculate_orbital_velocity_calculator, title = {Orbital Velocity Calculator}, author = {{TG we-Calculate Editorial Team}}, howpublished = {\url{https://we-calculate.com/calculator/orbital-velocity-calculator}}, year = {2026}, note = {TG we-Calculate} }

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