Why is gravitational potential energy negative? What does the negative sign mean physically?
Define gravitational potential energy $U = -GMm/r$, calculate work done in gravitational fields, and understand why GPE is defined as zero at infinity.
Why GPE is always negative for bound objects
Gravitational Pe
Gpe Detailed
The gravitational potential energy of a mass $m$ at distance $r$ from a mass $M$ is defined as:
The negative sign is essential. Gravity is an attractive force, so work must be done against gravity to increase $r$ (to pull the masses apart). This means:
GPE is negative for all finite $r$ because gravity is always attractive. A bound system (planet orbiting a star, satellite orbiting Earth) has negative total energy. A positive total energy would mean the object is unbound — it would escape to infinity.
The choice of $U = 0$ at $r = \\infty$ is a convention, but a physically meaningful one. At infinite separation, there is no gravitational interaction — the masses do not influence each other. Setting $U = 0$ there means:
Find the gravitational potential energy of a 1000 kg satellite at $r = 8.0 \\times 10^6$ m from Earth's centre.
$m = 1000 \\text{ kg}$, $r = 8.0 \\times 10^6 \\text{ m}$, $G = 6.67 \\times 10^{-11} \\text{ N m}^2\\text{/kg}^2$, $M_E = 5.97 \\times 10^{24} \\text{ kg}$
Gravitational potential energy $U$
Use $U = -GMm/r$ with $r$ as the centre-to-centre distance.
$$U = -\\frac{(6.67 \\times 10^{-11} \\text{ N m}^2\\text{/kg}^2)(5.97 \\times 10^{24} \\text{ kg})(1000 \\text{ kg})}{8.0 \\times 10^6 \\text{ m}}$$
$$U = -\\frac{3.98 \\times 10^{17} \\text{ J m}}{8.0 \\times 10^6 \\text{ m}} = -4.97 \\times 10^{10} \\text{ J}$$
$U = -4.97 \\times 10^{10} \\text{ J}$
Calculating energy changes when moving between orbital radii
When an object moves from one point to another in a gravitational field, the work done by the gravitational force equals the change in gravitational potential energy:
Always write $r = R_{\\text{Earth}} + h$ explicitly. The most common error is using altitude $h$ instead of centre-to-centre distance $r$.
Calculate the energy required to move a satellite from $r_1 = 7.0 \\times 10^6$ m to $r_2 = 1.0 \\times 10^7$ m from Earth's centre. The satellite mass is 1000 kg.
$m = 1000 \\text{ kg}$, $r_1 = 7.0 \\times 10^6 \\text{ m}$, $r_2 = 1.0 \\times 10^7 \\text{ m}$, $G = 6.67 \\times 10^{-11} \\text{ N m}^2\\text{/kg}^2$, $M_E = 5.97 \\times 10^{24} \\text{ kg}$
Work done (energy required) $\\Delta U$
Use $\\Delta U = GMm(1/r_1 - 1/r_2)$
$$\\Delta U = (6.67 \\times 10^{-11})(5.97 \\times 10^{24})(1000)\\left(\\frac{1}{7.0 \\times 10^6} - \\frac{1}{1.0 \\times 10^7}\\right)$$
$$\\Delta U = 3.98 \\times 10^{17} \\times (1.429 \\times 10^{-7} - 1.000 \\times 10^{-7}) \\text{ J}$$
$$\\Delta U = 3.98 \\times 10^{17} \\times 4.29 \\times 10^{-8} \\text{ J} = 8.49 \\times 10^9 \\text{ J}$$
$\\Delta U = 8.49 \\times 10^9 \\text{ J}$ (approximately 8.5 GJ)
The near-surface approximation derived from the exact formula
For small heights above Earth's surface, the exact gravitational PE formula reduces to the familiar $mgh$. Here's the derivation:
Starting with the exact change in GPE when moving from Earth's surface ($R$) to height $h$ above the surface ($R + h$):
The $mgh$ formula is an approximation that is valid only when the height $h$ is much smaller than Earth's radius $R$. For large altitudes (satellites, spacecraft), the exact formula must be used.
In the exact formula, $g = GM/R^2$ is the gravitational field strength at Earth's surface. At altitude $h$, the field strength is $g' = GM/(R+h)^2$, which is less than $g$. The $mgh$ formula assumes $g$ is constant, which fails at large $h$.
For a 1 kg mass raised $h = 100 \\text{ m}$ above Earth's surface, compare the exact $\\Delta U$ with the $mgh$ approximation. $R_E = 6.37 \\times 10^6 \\text{ m}$.
$m = 1 \\text{ kg}$, $h = 100 \\text{ m}$, $R_E = 6.37 \\times 10^6 \\text{ m}$, $G = 6.67 \\times 10^{-11} \\text{ N m}^2\\text{/kg}^2$, $M_E = 5.97 \\times 10^{24} \\text{ kg}$
Exact $\\Delta U$ and approximate $mgh$
Exact: $\\Delta U = GMm(1/R - 1/(R+h))$. Approximate: $mgh$ with $g = 9.8 \\text{ m/s}^2$.
Exact calculation:
$$\\Delta U = (6.67 \\times 10^{-11})(5.97 \\times 10^{24})(1)\\left(\\frac{1}{6.37 \\times 10^6} - \\frac{1}{6.3701 \\times 10^6}\\right)$$
$$\\Delta U = 3.98 \\times 10^{14} \\times (1.5700 \\times 10^{-7} - 1.5698 \\times 10^{-7}) \\text{ J}$$
$$\\Delta U = 3.98 \\times 10^{14} \\times 2.46 \\times 10^{-11} \\text{ J} = 980.3 \\text{ J}$$
Approximate calculation:
$$mgh = 1 \\times 9.8 \\times 100 = 980 \\text{ J}$$
The difference is $0.3 \\text{ J}$ (about $0.03\\%$) — negligible for everyday heights.
"GPE can be positive" — With $U = -GMm/r$, GPE is always negative for finite $r$. Zero only at infinity. A positive GPE would imply an unbound object that escapes the gravitational field.
"The negative sign is just a convention with no physical meaning" — The negative sign encodes that gravity is attractive. Bound systems have negative total energy. The sign is essential for determining whether an object is bound or unbound.
Launching a satellite requires work against gravity. Consider a 1000 kg satellite moved from Earth's surface ($R_E = 6.37 \\times 10^6 \\text{ m}$) to geostationary orbit ($r = 4.22 \\times 10^7 \\text{ m}$):
$$\\Delta U = GMm\\left(\\frac{1}{R_E} - \\frac{1}{r}\\right)$$
$$\\Delta U = (6.67 \\times 10^{-11})(5.97 \\times 10^{24})(1000)\\left(\\frac{1}{6.37 \\times 10^6} - \\frac{1}{4.22 \\times 10^7}\\right)$$
$$\\Delta U = 3.98 \\times 10^{17} \\times (1.570 \\times 10^{-7} - 2.370 \\times 10^{-8}) \\text{ J} = 5.29 \\times 10^{10} \\text{ J}$$
This $5.29 \\times 10^{10} \\text{ J}$ (about 53 GJ) is the minimum energy needed, ignoring kinetic energy for orbit, air resistance, and other losses. In practice, rockets are only about 2% efficient due to carrying their own fuel — the vast majority of a rocket's launch mass is propellant.
1 Find the gravitational potential energy of a 500 kg satellite at $r = 6.5 \\times 10^6$ m from Earth's centre.
2 Calculate the energy required to move a 2000 kg satellite from Earth's surface to $r = 10^7$ m.
3 At what height above Earth's surface does the $mgh$ approximation deviate by 1% from the exact $\\Delta U$?
A student says: "If GPE is negative, that means energy has been taken away from the object." Explain why this statement is misleading. In your answer, discuss: (a) what the zero of GPE represents, (b) what a negative GPE tells us about the binding of the object to the central mass, and (c) what would happen if an object's total energy became positive.
Now that you have studied gravitational potential energy, revisit your earlier answer about why GPE is negative.
The negative sign arises because gravity is attractive. Work must be done against the field to separate the masses. Setting $U = 0$ at infinity means all finite separations have $U < 0$ — the object is bound. A bound object needs energy input to escape. If total energy were positive, the object would be unbound and could escape to infinity with kinetic energy remaining.
Has your understanding changed? Write a revised explanation:
1. Gravitational potential energy is defined as zero at:
2. The gravitational PE of a mass $m$ at distance $r$ from mass $M$ is:
3. Moving a satellite to a higher orbit:
4. Work done moving from $r_1$ to $r_2$ in a gravitational field:
5. The $mgh$ approximation is valid when:
Calculate the gravitational potential energy of a 1500 kg spacecraft at altitude 400 km above Earth. Calculate the energy required to move it to an altitude of 1000 km.
Show that for small heights $h$ above Earth's surface, $\\Delta U \\approx mgh$. Start from the exact expression and use the binomial approximation.
Evaluate the $mgh$ approximation by calculating the percentage error when using it to find the potential energy change of a 1 kg mass raised to: (a) 100 m, (b) 1000 km, (c) 36,000 km (geostationary altitude). Discuss the validity of the approximation in each case.
$r_1 = R_E + h_1 = 6.37 \\times 10^6 + 400 \\times 10^3 = 6.77 \\times 10^6 \\text{ m}$ (1 mark)
$r_2 = R_E + h_2 = 6.37 \\times 10^6 + 1000 \\times 10^3 = 7.37 \\times 10^6 \\text{ m}$
$U_1 = -\\dfrac{(6.67 \\times 10^{-11})(5.97 \\times 10^{24})(1500)}{6.77 \\times 10^6} = -8.83 \\times 10^{10} \\text{ J}$
$U_2 = -\\dfrac{(6.67 \\times 10^{-11})(5.97 \\times 10^{24})(1500)}{7.37 \\times 10^6} = -8.11 \\times 10^{10} \\text{ J}$
$\\Delta U = U_2 - U_1 = (-8.11 \\times 10^{10}) - (-8.83 \\times 10^{10}) = 7.2 \\times 10^9 \\text{ J}$ (2 marks)
$\\Delta U = GMm\\left(\\dfrac{1}{R} - \\dfrac{1}{R+h}\\right)$ (1 mark)
$\\Delta U = GMm\\left(\\dfrac{R+h-R}{R(R+h)}\\right) = \\dfrac{GMmh}{R(R+h)}$ (1 mark)
For $h \\ll R$: $R+h \\approx R$, so $\\Delta U \\approx \\dfrac{GMmh}{R^2} = mgh$ since $g = GM/R^2$ (1 mark)
(a) $h = 100 \\text{ m}$: Exact $\\Delta U = 980.3 \\text{ J}$, $mgh = 980 \\text{ J}$, error $= 0.03\\%$. The approximation is excellent for everyday heights. (1 mark)
(b) $h = 1000 \\text{ km}$: Exact $\\Delta U = 8.49 \\times 10^6 \\text{ J}$, $mgh = 9.8 \\times 10^6 \\text{ J}$, error $= 15.4\\%$. The approximation is poor at orbital altitudes. (1 mark)
(c) $h = 36{,}000 \\text{ km}$: Exact $\\Delta U = 5.29 \\times 10^7 \\text{ J}$, $mgh = 3.53 \\times 10^8 \\text{ J}$, error $= 567\\%$. The approximation is completely invalid for GEO. (1 mark)
The $mgh$ approximation is excellent for everyday heights ($h < 1 \\text{ km}$), acceptable for low Earth orbit only as an order-of-magnitude estimate, and completely invalid for geostationary altitude. The exact formula must be used for any significant altitude. (1 mark for discussion)
Tick this box when you have finished all sections of this lesson.