Define the average orbital speed of a planet and recall, rearrange and use the equation
v = \(\displaystyle\frac{2\pi\,\color{#1976d2}{r}}{\color{#388e3c}{T}}\)
in calculations (AO1 + AO2) as required by the Cambridge IGCSE Physics syllabus.
The formula is a direct consequence of Kepler’s 3rd law – the square of the orbital period is proportional to the cube of the semi‑major axis (\(T^{2}\propto r^{3}\)).
For a near‑circular orbit the distance travelled in one revolution is the circumference \(2\pi r\); dividing by the period \(T\) therefore gives the average orbital speed.
Approximation note: The relation \(v = 2\pi r/T\) assumes a near‑circular orbit. For highly elliptical orbits the average speed must be obtained from the full elliptical geometry or from the more general vis‑viva equation
\(v = \sqrt{GM\!\left(\dfrac{2}{r}-\dfrac{1}{a}\right)}\).
| Speed | \(v = \dfrac{2\pi r}{T}\) |
| Radius | \(r = \dfrac{v\,T}{2\pi}\) |
| Period | \(T = \dfrac{2\pi r}{v}\) |
Check that the units reduce to metres per second (m s⁻¹):
| Quantity | Symbol | Value | Unit |
|---|---|---|---|
| Average orbital radius | r | 1.496 × 1011 | m |
| Orbital period | T | 3.156 × 107 | s |
Calculation
\[
\begin{aligned}
v &= \frac{2\pi (1.496\times10^{11}\,\text{m})}{3.156\times10^{7}\,\text{s}}\\[4pt]
&\approx \frac{9.40\times10^{11}\,\text{m}}{3.156\times10^{7}\,\text{s}}\\[4pt]
&\approx 2.98\times10^{4}\,\text{m s}^{-1}
\end{aligned}
\]
Sanity‑check: 30 km s⁻¹ is the commonly quoted value for Earth’s orbital speed – our result (29.8 km s⁻¹) is consistent.
A newly discovered exoplanet orbits its star with a period of 200 days and a semi‑major axis of 1.2 AU**. Estimate its average orbital speed.
\[
v = \frac{2\pi (1.795\times10^{11}\,\text{m})}{1.73\times10^{7}\,\text{s}}
\approx 6.5\times10^{4}\,\text{m s}^{-1}
= 65\ \text{km s}^{-1}
\]
This type of “unfamiliar” data (AU and days) mirrors the style of Cambridge exam questions and tests the student’s ability to convert units before applying the equation.
| Planet | Average radius (×1011 m) | Period (×107 s) | Average speed (km s⁻¹) |
|---|---|---|---|
| Venus | 1.082 | 1.94 | 35.0 |
| Earth | 1.496 | 3.16 | 29.8 |
| Mars | 2.279 | 5.94 | 24.1 |
Because \(T^{2}\propto r^{3}\) (Kepler’s 3rd law), a smaller radius implies a much shorter period. Substituting the smaller \(r\) and the correspondingly smaller \(T\) into \(v = 2\pi r/T\) therefore yields a larger speed for inner planets.
Engineers calculate the required orbital speed for a satellite to achieve a specific altitude. By rearranging \(v = 2\pi r/T\) (or using the related vis‑viva form \(v=\sqrt{GM/r}\)), they determine the launch velocity and the precise launch timing so that the satellite’s period matches the desired ground‑track repeat cycle.
“A communications satellite orbits the Earth at an average altitude of 20 000 km. If the satellite must complete one revolution every 12 hours, what is its average orbital speed?”
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