The surface value as baseline
The acceleration due to gravity at the Earth's surface follows from Newton's law of gravitation applied to a body of mass $m$ resting on a sphere of mass $M_E$ and radius $R$:
$$g = \frac{G M_E}{R^2} \approx 9.8~\text{m s}^{-2}.$$
This single number is the reference against which every variation is measured. Two facts drive everything below. First, $g$ depends on the distance from the centre of the Earth — so moving away weakens gravity. Second, the surface value uses the entire mass $M_E$, true only while all the Earth's mass stays below you; burrow inside and part of the mass ends up above you and stops pulling you down. These two ideas — distance and enclosed mass — split the problem cleanly into the height case and the depth case. For the surface derivation in full, see acceleration due to gravity.
Variation with height above the surface
Take a body at a height (altitude) $h$ above the surface. Its distance from the centre is now $R + h$, and the whole mass $M_E$ still lies below it. Newton's law gives the exact value:
$$g_h = \frac{G M_E}{(R+h)^2} = g\,\frac{R^2}{(R+h)^2} = \frac{g}{\left(1 + \dfrac{h}{R}\right)^2}.$$
This is the form to use whenever $h$ is comparable to $R$ — satellites, distant orbits, "height equal to half the radius" type problems. NIOS §5.3.1 notes the immediate consequence: at $h = R$, the distance from the centre doubles to $2R$, so $g$ falls to one-quarter of its surface value.
When the altitude is small compared with the radius ($h \ll R$) — aircraft, mountains, towers — the binomial expansion of $(1 + h/R)^{-2}$ keeping only the first-order term gives the working approximation NCERT §7.6 quotes:
$$g_h \approx g\left(1 - \frac{2h}{R}\right), \qquad h \ll R.$$
The factor of 2 is the signature of the inverse-square law: a fractional rise $h/R$ in distance produces twice that fractional drop in $g$. NIOS Example 5.2 illustrates the scale — at a typical cruising altitude of 10 km, with $R = 6400$ km, the value of $g$ falls only to about $9.77~\text{m s}^{-2}$, a change of roughly 0.3%.
Variation with depth below the surface
Now drop a body to a depth $d$ below the surface, so its distance from the centre is $r = R - d$. Two things change at once. The distance shrinks, which on its own would increase $g$. But the spherical shell of matter above the body — the outer shell of thickness $d$ — now contributes nothing: NIOS §5.3.2 states the standard shell result that the net gravitational force from a uniform spherical shell on a point inside it is exactly zero. Only the inner sphere of radius $r = R - d$ pulls the body.
Assuming the Earth has uniform density $\rho$, the mass of that inner sphere is $M' = \tfrac{4}{3}\pi\rho\,(R-d)^3$, and the acceleration at depth $d$ becomes
$$g_d = \frac{G M'}{(R-d)^2} = \frac{4}{3}\pi G \rho\,(R-d).$$
Since the surface value is $g = \tfrac{4}{3}\pi G \rho R$ (set $d = 0$), dividing one by the other removes the constants and leaves the clean linear law NCERT §7.6 gives:
$$g_d = g\left(1 - \frac{d}{R}\right), \qquad 0 \le d \le R.$$
The fall-off is linear in $d$ and the coefficient is just $d/R$ — no factor of 2. The single most important consequence: set $d = R$ (the body has reached the centre) and $g_d = 0$. At the centre of the Earth, matter surrounds you symmetrically in every direction and the pulls cancel exactly.
The g-versus-distance graph
The two laws meet at the surface and behave oppositely on either side of it. Plotting $g$ against distance $r$ from the centre makes the whole story visible in one curve: a straight line rising from zero at the centre to the peak at $r = R$, then an inverse-square tail decaying beyond the surface.
Read the graph from the centre outwards. At $r = 0$, $g = 0$. The line climbs steadily to its maximum at the surface. Beyond the surface, $g$ never increases again — the inverse-square tail only decays, passing through $g/4$ at $r = 2R$. The surface is the unique peak of the entire curve.
Height vs depth — the contrast
Place the three variations side by side. They share a starting point — the surface value $g$ — but differ in mechanism, in the fall-off coefficient, and in how fast they decay.
Above the surface
$g_h = \dfrac{gR^2}{(R+h)^2}$ $\approx g\!\left(1 - \dfrac{2h}{R}\right)$, $h\ll R$Mechanism: full mass below, distance grows. Inverse-square decay, never reaches zero.
Below the surface
$g_d = g\!\left(1 - \dfrac{d}{R}\right)$ $= \dfrac{4}{3}\pi G\rho\,(R-d)$Mechanism: overlying shell cancels, enclosed mass shrinks. Linear decay to exactly zero at the centre.
Along the surface
$g' = g - \omega^2 R\cos^2\!\lambda$ max at poles, min at equatorMechanism: rotation diverts part of gravity to centripetal force; flattened shape adds a smaller radius at the poles.
The decisive comparison: for the same small displacement $x$ from the surface, going up changes $g$ by $-2gx/R$ while going down changes it by only $-gx/R$. Height kills $g$ twice as fast as depth. That is the engine behind the NEET-favourite question "at what depth is $g$ the same as at height $h$" — the answer is $d = 2h$, because depth must travel twice as far to lose the same amount.
This whole topic rests on the surface formula $g = GM_E/R^2$ — revisit its derivation and the mass-of-the-Earth estimate in acceleration due to gravity.
Variation with latitude and shape
Even staying exactly on the surface, $g$ is not the same everywhere — it depends on latitude $\lambda$ (the angular distance north or south of the equator). NIOS §5.3.3 traces this to the Earth's daily rotation. Every point on the surface moves in a circle about the rotation axis, and circular motion needs centripetal force. Part of the gravitational pull is "spent" supplying that force, so the effective gravity an object actually experiences is reduced:
$$g' = g - \omega^2 R\cos^2\!\lambda,$$
where $\omega$ is the Earth's angular speed of rotation. The radius of a point's circular path is $R\cos\lambda$, and only the component of the centripetal term along the local vertical reduces $g$, which together produce the $\cos^2\lambda$ dependence.
- At the equator ($\lambda = 0$, $\cos^2\lambda = 1$): the reduction is largest, $g' = g - \omega^2 R$. This is the smallest effective $g$ on Earth.
- At the poles ($\lambda = 90^\circ$, $\cos^2\lambda = 0$): the rotation term vanishes, $g' = g$. The poles lie on the rotation axis, trace no circle, and need no centripetal force — so the effective $g$ is largest there.
NIOS confirms the magnitude is small: with $\omega = 7.27\times10^{-5}~\text{rad s}^{-1}$ and $R \approx 6.37\times10^6$ m, the maximum correction $\omega^2 R$ is only about $0.034~\text{m s}^{-2}$ — a fraction of a percent of $g$.
A second, independent effect reinforces the same trend. The Earth is not a perfect sphere; rotation has flattened it so the equatorial radius is larger than the polar radius. Because $g \propto 1/R^2$, the smaller polar radius gives a larger $g$ at the poles. Both the rotation effect and the shape effect therefore point the same way: $g$ is maximum at the poles and minimum at the equator.
Worked examples
Assuming the Earth to be a sphere of uniform mass density, how much would a body weigh half way down to the centre of the Earth if it weighed 250 N on the surface?
Set up. "Half way down to the centre" means depth $d = R/2$. Use the depth law $g_d = g(1 - d/R)$, and remember weight is proportional to $g$ since $W = mg$.
Compute the factor. $\dfrac{g_d}{g} = 1 - \dfrac{d}{R} = 1 - \dfrac{R/2}{R} = 1 - \dfrac{1}{2} = \dfrac{1}{2}.$
Scale the weight. $W_d = W\left(1 - \dfrac{d}{R}\right) = 250 \times \dfrac{1}{2} = \boxed{125~\text{N}}.$ The body weighs half as much half way to the centre — and would weigh nothing at the centre itself.
Compute the value of $g$ at an altitude of 10 km. Take $R = 6400$ km and the surface value $g = 9.8~\text{m s}^{-2}$.
Choose the formula. Here $h = 10$ km $\ll R = 6400$ km, so the small-height approximation $g_h = g(1 - 2h/R)$ is valid.
Substitute. $\dfrac{2h}{R} = \dfrac{2 \times 10}{6400} = 3.125\times10^{-3}.$ Then $g_h = 9.8\,(1 - 0.003125) = 9.8 \times 0.99688 \approx 9.77~\text{m s}^{-2}.$
Read it. Even at a typical aircraft cruising altitude, $g$ falls by only about 0.3%. (NIOS Example 5.2.) This is why aircraft and tower problems can safely use the linear approximation — the height is tiny next to $R$.
A body weighs 72 N on the surface of the Earth. What is the gravitational force on it at a height equal to half the radius of the Earth? (NEET 2020)
Spot the trap. Here $h = R/2$ is not small compared with $R$, so the $g(1-2h/R)$ approximation fails. Use the exact $g_h = g\,R^2/(R+h)^2$.
Compute the factor. $\dfrac{g_h}{g} = \dfrac{R^2}{(R + R/2)^2} = \dfrac{R^2}{(3R/2)^2} = \dfrac{1}{9/4} = \dfrac{4}{9}.$
Scale the weight. $W_h = 72 \times \dfrac{4}{9} = \boxed{32~\text{N}}.$ The linear approximation would have wrongly given $72(1 - 1) = 0$ N — a textbook demonstration of why the exact form is mandatory when $h \sim R$.
Variation of g in one breath
- Surface: $g = GM_E/R^2 \approx 9.8~\text{m s}^{-2}$ — the baseline and the maximum.
- Height (exact): $g_h = gR^2/(R+h)^2$. Small height: $g_h \approx g(1 - 2h/R)$. Inverse-square; note the factor 2.
- Depth: $g_d = g(1 - d/R)$, linear, valid for uniform density. $g = 0$ at the centre ($d = R$). No factor 2.
- Latitude: $g' = g - \omega^2 R\cos^2\lambda$. Maximum at the poles, minimum at the equator; the flattened shape adds the same trend.
- Contrast: height lowers $g$ twice as fast as depth, so "equal $g$" gives $d = 2h$.
- Graph: straight line up to the surface, inverse-square tail beyond it; peak at $r = R$, $g/4$ at $r = 2R$.