Orbits of planets and satellitesAQA A-Level Physics: Revision notes
Section 1
Circular orbits: speed and period
A satellite in a circular orbit has its centripetal force provided by the gravitational attraction of the planet: . The satellite mass cancels, giving
so orbital speed depends only on the orbital radius and the mass of the planet. Larger orbits are slower. The period is .
Worked example: at m, m s⁻¹.
Use r from the centre of the planet (r = R + h), not the height above the surface.
Section 2
Kepler's third law: T² ∝ r³
Using in :
Since is constant for a given planet, . Plotting against gives a straight line through the origin with gradient .
Section 3
Energy of an orbiting satellite
Kinetic energy: . Potential energy: . Total energy: .
The total is negative, showing the satellite is bound. Note and . Moving to a larger orbit increases the total energy (less negative) but decreases the speed and kinetic energy.
If a satellite loses energy to the atmosphere, r decreases and it speeds up, because E = −GMm/2r gets more negative and Ek increases.
Section 4
Escape velocity
The escape velocity is the minimum speed at the surface needed to escape the gravitational field (reach infinity). The kinetic energy must at least cancel the potential energy so the total energy is zero: , giving
For the Earth m s⁻¹. It is independent of the mass of the escaping body, and is times the orbital speed just above the surface.
Section 5
Synchronous, geostationary and low orbits
A synchronous orbit has a period equal to the Earth's rotation period. A geostationary orbit is a synchronous orbit that is in the equatorial plane, travels in the same direction as the Earth's rotation, and has radius about 4.2 × 10⁷ m (height about 3.6 × 10⁷ m). The satellite stays above a fixed point, which suits communications and broadcast television.
Low orbits (a few hundred km up, often polar) have short periods of about 90 minutes. They give higher-resolution images, and as the Earth rotates beneath them they cover the whole surface, which suits Earth observation and weather monitoring.
That's the notes covered.
Carry on to the next subtopic.
Exam questions on Orbits of planets and satellites
- An Earth-observation satellite is in a circular orbit 600 km above the Earth's surface. Take the Earth's mass as 5.97 × 10²⁴ kg and its radius as 6.37 × 10⁶ m.Calculate the orbital speed of the satellite. Use .2 marks
- A telecommunications company operates a satellite in a geostationary orbit to relay television signals. A weather-monitoring agency separately uses satellites in low polar orbits.Explain why a geostationary satellite must orbit in the plane of the equator.2 marks
- A student investigates the relationship between the orbital period and the orbital radius of satellites moving in circular orbits around the Earth, which has mass 5.97 × 10²⁴ kg.Derive the relationship between the orbital period T and orbital radius r for a satellite in a circular orbit, showing that .3 marks
Written by the Exaim team, led by Shaun Daswani (Head of Upper Secondary, Improve ME Institute; MSc Financial Mathematics, Imperial College London; BSc, UCL) and Jason Daswani (operational lead, Improve ME Institute; LSE).