Estimate ground speed from altitude, inclination, latitude. Review orbital speed, period, and rotational effects instantly. Export clear results and explore trends with interactive plotting.
This curve shows approximate ground speed against altitude for the selected inclination and latitude.
These examples use the same approximate model shown in the formula section.
| Case | Altitude (km) | Inclination (°) | Latitude (°) | Ground Speed (km/s) | Ground Speed (km/h) | Period (min) |
|---|---|---|---|---|---|---|
| ISS-like LEO | 42 | 51.6 | 0 | 6.90492 | 24,857.72 | 92.97 |
| Sun-synchronous | 7 | 98 | 30 | 6.82986 | 24,587.48 | 98.77 |
| Navigation MEO | 20,2 | 55 | 20 | 0.7673 | 2,762.29 | 718.7 |
1. Orbital speed for a circular orbit
v_orbit = √(μ / (RE + h))
2. Surface-projected speed
v_projected = v_orbit × RE / (RE + h)
3. Local Earth rotation speed
v_rotation = ωE × RE × cos(φ)
4. Approximate ground speed
v_ground ≈ √(v_projected² + v_rotation² − 2v_projected v_rotation cos(i))
5. Direct mode
v = d / t
This page uses an approximate circular-orbit model. It is useful for planning, estimates, and comparisons, but it is not a full propagator.
Satellite ground speed is the apparent speed of the satellite’s subpoint moving across Earth’s surface. It differs from orbital speed because altitude and Earth rotation change the surface track.
Orbital speed is measured at the satellite’s altitude. Ground speed is projected onto Earth’s surface, so the smaller surface radius reduces the apparent track speed.
Earth’s surface rotates fastest at the equator and slows toward the poles. That changes the local rotational contribution used in the ground-speed estimate.
Inclination changes how the orbit aligns with Earth’s rotation. Prograde and retrograde tracks combine differently with the surface rotation term, which changes the estimated ground speed.
Use direct mode when you already know the surface distance and elapsed time. It is useful for checking measured data, image swaths, or mission reports.
Yes, for rough comparisons. A true geostationary satellite should show a very small apparent ground speed near the equator in an ideal circular case.
No. This is a simplified circular-orbit estimate. It does not model drag, J2 effects, eccentricity, station keeping, or detailed propagation physics.
Yes. After calculation, use the CSV button for tabular data or the PDF button for a shareable report snapshot of the result section.
Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.