Six original Cambridge-style questions on circular orbits, orbital speed and period, the geostationary condition and the field strength g = GM / r² of a point mass.
A satellite is in a circular orbit around the Earth. Explain why it is incorrect to say that the satellite stays in orbit because "gravity is balanced by the centripetal force".
A space station orbits the Earth (mass 6.0 × 10²⁴ kg) in a circular orbit of radius 6.8 × 10⁶ m. Calculate its orbital speed and the time it takes to complete one orbit, in minutes.
Io, a moon of Jupiter, moves in a circular orbit of radius 4.22 × 10⁸ m with a period of 1.77 days. Use these data to calculate the mass of Jupiter.
A satellite is placed in a circular orbit over the Earth's poles with a period of exactly 24 hours. Explain why this satellite is not geostationary, and explain why every geostationary satellite must orbit at the same height.
A satellite orbits the Earth (mass 6.0 × 10²⁴ kg) at a distance of 1.2 × 10⁷ m from the centre. Calculate the gravitational field strength at this distance, state the centripetal acceleration of the satellite, and hence calculate its orbital speed.
Mars has mass 6.42 × 10²³ kg and rotates once on its axis every 24.6 hours. A communications satellite is to be placed in orbit so that it remains above the same point on the Martian equator.
(a) State the condition on the period of the satellite's orbit. (b) Show that the radius of the orbit is about 2.0 × 10⁷ m. (c) Calculate the orbital speed of the satellite.
Mark this once you have attempted all six and checked your working. It records a Practiced badge on the topic and adds a one-time bonus. Revealing the solutions alone does not count.