Orbital Period & Kepler's Third Law
Orbital Period & Kepler's Third Law
- We use the to describe the timing of an orbit. Its unit is s.
- Linking speed to period gives an equation between the period and the radius.
Definition
1 markWhat is meant by orbital period?
Model answer: The time taken for an object to complete one full orbit.
From speed to period
- The distance travelled in one orbit is the circumference. Divide this distance by the period to find the speed.
- Substitute this speed into the circular-orbit equation. Rearranging gives the main period equation shown next.
Symbols
- = orbital period (time for one orbit) (s)
- = orbit radius from the centre (m)
- = gravitational constant (N m² kg⁻²)
- = mass of the planet (kg)
- The square of the period is proportional to the cube of the radius for circular orbits around the same central mass. This is (9702/42/M/J/23 Q1(b)).
The basic T² against r³ graph
- A common question asks you to show the same equation in a different arrangement (9702/42/M/J/23 Q1(b)).
- If data use orbit radius for objects around the same central mass, plot against . The graph is a straight line through the origin. Use its gradient to find the central mass.
- Change the orbit radius in the display. It shows how v and T change.
- The central mass does not change. Therefore, the value of T²/r³ stays constant.
Circular Orbit Explorer
Change the orbit radius measured from the Earth's centre. Watch the speed and period change together. The model uses an Earth mass of 6.0 × 10²⁴ kg.
Swipe left or right to see the whole diagram →
orbital speed v
5.77 km s⁻¹
orbital period T
3.6 h
Kepler ratio T²/r³
9.86e-14 s² m⁻³
The ratio T²/r³ stays constant. This is Kepler's third law for circular orbits around the same central mass.
