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What holds planets and satellites in their orbits?

Apply Newton's law of universal gravitation and the field model to orbital motion.

Newton's law of universal gravitation, gravitational fields, and how combining gravity with circular motion gives orbital speed, period and Kepler's third law.

Generated by Claude Opus 4.77 min answer

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What this dot point is asking

Newton's law of universal gravitation

Newton proposed that any two point masses attract each other along the line joining them with a force proportional to the product of their masses and inversely proportional to the square of their separation:

F=Gm1m2r2F = G\frac{m_1 m_2}{r^2}

Here G=6.67×1011 N m2kg2G = 6.67 \times 10^{-11}\ \text{N m}^2\,\text{kg}^{-2} is the universal gravitational constant and rr is the distance between the centres of the masses. The inverse-square dependence is crucial: doubling the separation reduces the force to a quarter.

The gravitational field

It is often more useful to describe gravity as a field. The gravitational field strength gg at a point is the force per unit mass placed there:

g=Fm=GMr2g = \frac{F}{m} = \frac{GM}{r^2}

where MM is the mass creating the field. Near Earth's surface this evaluates to about 9.8 N kg19.8\ \text{N kg}^{-1}, which is the same number as free-fall acceleration in m s2\text{m s}^{-2}. Field strength is a vector pointing toward the mass that creates it, and it falls off as the inverse square of distance from the centre.

Orbital motion

For a satellite in a stable circular orbit, gravity is the only force acting and it points toward the central body, so gravity provides exactly the centripetal force needed:

GMmr2=mv2r\frac{GMm}{r^2} = \frac{m v^2}{r}

The satellite mass mm cancels, leaving the orbital speed:

v=GMrv = \sqrt{\frac{GM}{r}}

A higher orbit means a slower speed. Substituting v=2πrTv = \frac{2\pi r}{T} and rearranging gives Kepler's third law:

T2=4π2GMr3T^2 = \frac{4\pi^2}{GM}\,r^3

so T2T^2 is proportional to r3r^3 for all satellites of the same central body.

A geostationary satellite is a special case: it has a period of exactly one day so it stays above the same point on the equator. Setting T=86400 sT = 86400\ \text{s} in Kepler's third law gives an orbital radius of about 4.2×107 m4.2 \times 10^7\ \text{m}.

When tackling orbital questions, decide first whether you need the field equation or the orbit equation. Use g=GMr2g = \frac{GM}{r^2} for field strength and weight, and use GMmr2=mv2r\frac{GMm}{r^2} = \frac{mv^2}{r} whenever the body is actually orbiting, since that is what links gravity to circular motion.

Exam-style practice questions

Practice questions written in the style of TASC exam questions on this dot point, with worked answer explainers. The year tag is the paper they imitate, not the source.

2024 TASC2 marksA neutron star (pulsar) has a diameter of about 30 km and a mass of 2.79 x 10^30 kg. Calculate the gravitational field strength at the surface of this object.
Show worked answer →

Use the field of a point/spherical mass: g = G M / r^2.

The radius is half the diameter: r = 30 / 2 = 15 km = 1.5 x 10^4 m.

g = (6.67 x 10^-11 x 2.79 x 10^30) / (1.5 x 10^4)^2
= (1.861 x 10^20) / (2.25 x 10^8)
= 8.27 x 10^11 N kg-1.

The surface gravity is about 8 x 10^11 N kg-1, around a hundred billion times Earth's. Markers want use of the radius (not diameter) and the inverse-square form g = GM/r^2.

2022 TASC5 marksThe asteroid 130 Elektra orbits the Sun with a period of 5.53 Earth years. One of its small moons orbits at 501 km from Elektra with a period of 1.19 Earth days, giving an acceleration of about 1.9 x 10^-3 m s-2. Calculate Elektra's gravitational field strength near this moon and hence the mass of Elektra.
Show worked answer →

For the orbiting moon, gravity supplies the centripetal acceleration, so the gravitational field strength at the moon equals its centripetal acceleration.

Field strength g = a = v^2 / r = 4 pi^2 r / T^2.
T = 1.19 days = 1.19 x 86400 = 1.028 x 10^5 s, r = 501 km = 5.01 x 10^5 m.
g = 4 pi^2 x 5.01 x 10^5 / (1.028 x 10^5)^2 = 1.978 x 10^7 / 1.057 x 10^10 = 1.87 x 10^-3 m s-2.

Mass of Elektra from g = G M / r^2:
M = g r^2 / G = 1.87 x 10^-3 x (5.01 x 10^5)^2 / 6.67 x 10^-11
= 1.87 x 10^-3 x 2.51 x 10^11 / 6.67 x 10^-11 = 7.04 x 10^18 kg.

Elektra has a mass of about 7 x 10^18 kg. Markers reward equating the moon's centripetal acceleration to the field strength, then solving M = g r^2 / G.

2023 TASC3 marksA Sun-like star HD137496 has a mass of 2.1 x 10^30 kg. Its exoplanet 'b' orbits every 1.62 Earth days. Calculate the orbital radius of 'b'.
Show worked answer →

Combine gravity as the centripetal force with the orbital period to get Kepler's third law form:
G M / r^2 = 4 pi^2 r / T^2, which rearranges to r^3 = G M T^2 / (4 pi^2).

Convert the period: T = 1.62 days = 1.62 x 86400 = 1.400 x 10^5 s.

r^3 = (6.67 x 10^-11 x 2.1 x 10^30 x (1.400 x 10^5)^2) / (4 pi^2)
= (1.401 x 10^20 x 1.959 x 10^10) / 39.48
= 2.745 x 10^30 / 39.48 = 6.95 x 10^28.

r = (6.95 x 10^28)^(1/3) = 4.11 x 10^9 m.

Planet 'b' orbits at about 4.1 x 10^9 m. Markers want r^3 = G M T^2 / 4 pi^2 with the period in seconds.