Quick answer: Escape velocity vₑ = √(2GM/R) = √(2gR) derived from energy conservation, with the Moon worked numerical, the three traps that cost marks, and why the Moon has no…
In one line: Escape velocity is the minimum launch speed at which an object leaves a planet’s gravitational pull forever — 11.2 km/s for Earth — derived purely from energy conservation, independent of the projectile’s mass.
JEE/NEET Physics · Gravitation series · Part 1 of 8 · All parts →
As a result, throw a ball at 40,320 km/h and it never comes back. That speed — 11.2 km/s — is Earth’s escape velocity. Most students can quote it; far fewer can answer the follow-ups examiners actually ask: 11.2 km/s from where? Does it depend on the ball’s mass? Why does a force as relentless as gravity have a speed limit at all? This card is Part 1 of the Gravitation series for JEE Main, JEE Advanced and NEET — eight parts, one chapter, exam-ready. By the end, you will not just recall the number; you will be able to derive it, apply it to any planet, and sidestep the three traps that cost candidates marks every year.
Notably, gravity weakens with height, so a projectile does not need speed to spare at infinity — it needs to arrive at infinity with exactly zero speed. That is the definition of escape velocity: the minimum launch speed for which the projectile just barely breaks free, arriving infinitely far away with nothing left in the tank. Any faster and it escapes with speed to spare; any slower and it turns back.
Meanwhile, apply energy conservation between the surface and infinity (where gravitational potential energy is conventionally defined as zero):
Walk through the derivation once so it sticks. At the surface, the total mechanical energy is the kinetic energy ½mv² plus the potential energy −GMm/R. At infinity, for the minimum case, both kinetic and potential energy are zero. Setting total energy equal:
½mv² − GMm/R = 0 ⟹ ½mv² = GMm/R ⟹ v² = 2GM/R ⟹ vₑ = √(2GM/R).
Indeed, the launched object’s mass m cancels from both sides: a coin and a truck escape at the same speed. And since g = GM/R² at the surface, you can substitute GM = gR² to get the second form, vₑ = √(2gR), which is often the faster route in problems. Finally, state the conditions in your solution — no air resistance, launch from the surface — because examiners award steps for them.
| Form. | When to use it. |
|---|---|
| vₑ = √(2GM/R). | Specifically, when planet mass M and radius R are given. |
| vₑ = √(2gR). | Similarly, when surface gravity g and R are given — faster, no G needed. |
| vₑ = √(2GM/(R+h)). | Overall, when launched from height h — the answer will not be 11.2 km/s. |
A quick comparison worth memorising: Earth’s vₑ ≈ 11.2 km/s, the Moon’s ≈ 2.4 km/s, Mars ≈ 5.0 km/s, Jupiter ≈ 59.5 km/s. Heavier and larger bodies demand dramatically higher escape speeds — a pattern examiners love to test through ratio problems rather than raw calculation.
Consequently, vₑ = √(2GM/R) = √(2 × 6.67×10⁻¹¹ × 7.4×10²² ÷ 1.7×10⁶) = √(5.8×10⁶)
Furthermore, sanity check: the Moon is far lighter than Earth. Meanwhile, a smaller vₑ than 11.2 km/s is plausible.
Answer: ≈ 2.4 km/s
Notice the problem-solving rhythm: write the formula, substitute with consistent SI units, take the square root, then sanity-check the order of magnitude against a known value. That last step takes two seconds and catches sign errors, unit slips and misplaced powers of ten before they cost you.
The black-hole connection deserves a pause. The radius at which vₑ = c is called the Schwarzschild radius, rs = 2GM/c². For Earth that works out to roughly 9 millimetres; for the Sun, about 3 km. The same energy-conservation argument you just learnt, pushed to its limit, predicts the most extreme objects in the universe — a satisfying reminder that exam-level physics and frontier physics share one toolbox.
Throw a ball up and gravity slows it. Throw harder, it goes higher before slowing. Now imagine being strong enough that gravity never gets time to finish the job — that’s escape velocity: the one throw speed where gravity’s braking never fully wins.
Earth’s escape speed is 11.2 km/s. At 10 km/s the ball rises, slows… and falls back. At 11.2 km/s the slowdown never reaches zero — speed stays positive forever. Notice something odd: the Moon needs only 2.4 km/s because it’s lighter, and the number does NOT care which direction you throw (as long as you don’t hit the ground).
Picture gravity’s pull as an uphill climb that gets shallower the higher you go — a hill that flattens toward horizontal but never quite levels off. Escape velocity is the launch speed whose ‘fuel’ exactly matches the total height of that infinite-but-shallow hill. Run out at the top and you slide back; arrive with anything left and you’re free.
Escape velocity is the minimum launch speed for which an object never returns. The “zero speed at infinity” condition comes straight from that definition of minimum: if the object still had speed left at infinity, a slightly slower launch would also have escaped, so the true minimum is the one that just barely makes it. Energy conservation between the surface and infinity then gives ½mvₑ² − GMm/R = 0, which rearranges to vₑ = √(2GM/R).
No, on both counts. The projectile’s mass m cancels out of the energy equation, so a coin and a truck need the same 11.2 km/s. Direction also does not matter in the idealised, airless treatment — the energy balance only cares about speed — though in practice launching vertically minimises atmospheric drag for real rockets.
The Moon calculation uses vₑ = √(2GM/R) = √(2 × 6.67×10⁻¹¹ × 7.4×10²² ÷ 1.7×10⁶) = √(5.8×10⁶) ≈ 2.4 km/s. The habit to carry into the exam is the sanity check: the Moon is far lighter than Earth, so a value much smaller than 11.2 km/s is plausible — and if your answer had come out larger, you would know to recheck the powers of ten. Remember also that 11.2 km/s is a surface value: from height h use R → (R+h), and from low orbit the requirement drops to ~10.9 km/s.
ISRO launches do not escape Earth at all — PSLV and GSLV reach only about 7.9 km/s, which is orbital velocity (covered in Part 2). Orbiting is far cheaper than escaping. The Moon’s low escape velocity of 2.4 km/s explains why it holds no atmosphere: gas molecules move fast enough to leak away over geological time. And the same formula predicts black holes: compress Earth’s mass to about 9 mm and the escape speed exceeds the speed of light, so nothing — not even light — can escape.
Use ratio reasoning wherever possible instead of recomputing constants. For the 4M/2R planet, scale Earth’s answer by √(4/2) = √2 to get ≈ 15.8 km/s. For the 0.5·vₑ projection, apply energy conservation with vₑ² = 2GM/R to find h = R/3. For the satellite at 2R, note that vₑ ∝ 1/√r, giving k = 1/√2 ≈ 0.707. Attempt each fully before opening the answer — the recap list below summarises the key facts: vₑ = √(2GM/R) = √(2gR) from the surface, no mass dependence, vₑ = √2 × orbital velocity, and the Moon’s 2.4 km/s as the atmosphere test case.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.
Quick answer: Orbital velocity vₒ = √(GM/r) = √(gR) from centripetal-force balance, the r = R+h trap, and why higher satellites move slower — with the √2 link to escape…
In one line: orbital velocity: JEE/NEET Physics · Gravitation series · Part 2 of 8 · All parts →✪ Key points — the 30-second versionFormula: vₒ = √(GM/r) = √(gR) — 7.9.
In fact, JEE/NEET Physics · Gravitation series · Part 2 of 9 · All parts →
Notably, the International Space Station has been falling for 25 years — and it has never hit the ground. not because gravity is missing up there (it’s still 89% as strong). it’s because the ISS moves sideways so fast that as it falls, the curved Earth keeps dropping away beneath it. Part 2 of the Gravitation series — and this one you can understand with a thrown ball.
Specifically, throw a ball sideways — it lands a few metres away. Meanwhile, throw harder — it lands farther. now imagine throwing extremely hard, from a very high mountain.
Similarly, here’s the key: the Earth is round, so its surface curves downward. Meanwhile, as the ball flies farther, the ground beneath it drops away. If the ball flies fast enough, its falling matches the Earth’s curving — the ball falls forever and never touches ground. That’s an orbit.
So an astronaut isn’t floating because there’s no gravity. Overall, the astronaut and the whole station are falling together — like being in a lift whose cable snapped. Indeed, everything falls together = everything floats together.
Earth
ISS — falls 24/7
gravity (89% of surface!)
7.7 km/s sideways
ground curves away
→ falls forever, never lands
| Letter | What it means (plain words) | Value / unit |
|---|---|---|
| vₒ | Consequently, orbit velocity — the sideways speed needed to keep falling around the planet forever | answer in m/s or km/s |
| G | Furthermore, gravity’s fixed strength number (same everywhere in the universe) | 6.67 × 10⁻¹¹ |
| M | Likewise, mass of the planet you’re orbiting — how much stuff it has | Earth: 6 × 10²⁴ kg |
| r | In short, distance from the planet’s CENTRE to the satellite — this is R + h, the #1 trap in this topic | Subsequently, earth’s surface orbit: 6.4 × 10⁶ m |
Feels wrong, right? In fact, higher = farther from Earth = fighting more gravity? No — it’s the opposite. As a result, farther from Earth, gravity is weaker. Meanwhile, the satellite needs less speed to keep circling. vₒ shrinks as r grows: doubling the orbit distance cuts the speed by √2.
Moreover, real numbers: ISS at 400 km flies at 7.7 km/s. TV satellites at 36,000 km crawl at 3.1 km/s. In other words, the Moon at 384,000 km strolls at 1 km/s. Indeed, low orbits are the fast lane; high orbits are the slow lane.
Therefore, from Part 1 : escape velocity 11.2 km/s, orbit velocity 7.9 km/s. Notably, the ratio is always √2, for any planet, at any height. Meanwhile, memorise the pair, and any question about either one hands you the other.
Meanwhile, shortcut form (when the question gives g instead of M): vₒ = √(gR).
Plug in: √(10 × 6.4×10⁶) = √(64×10⁶) = 8×10³.
As a result, common-sense check: the famous answer is 7.9 km/s (with g = 9.8) — ours says 8.
Answer: 8 km/s
In other words, step 1 — convert height to distance from centre: r = R + h = 2R. Meanwhile, this one line is the entire question!
Specifically, step 2 — apply ‘higher = slower’: v = 7.9/√2.
Similarly, common-sense check: higher orbit, slower speed — matches the rule.
Answer: ≈ 5.6 km/s
Overall, step 1 — speed: vₒ = √(GM/2R) ≈ 5.6 km/s.
Consequently, step 2 — time = distance ÷ speed: circle distance = 2πr = 2π × 1.28×10⁷ m.
Furthermore, common-sense check: about 4 hours — higher orbits are slower AND longer. Meanwhile, much more time than the ~90-minute ISS.
Answer: T ≈ 4 hours
Newton’s own thought experiment: fire a cannonball from a mountain. Faster and faster shots land farther away — until one shot is so fast the ground curves away beneath it as fast as it falls. It never lands. That’s an orbit: falling and missing.
The ISS falls toward Earth at the same rate as anything dropped — about 8 m of drop in the first second. But it moves 7.7 km sideways each second, and Earth’s surface curves 4.9 m downward per 7.7 km. Fall 8 m, ground drops ~5 m: it stays up. Match the two numbers and you orbit.
Draw Earth as a circle and the orbit as a ring around it. The satellite is ALWAYS on the ring, always falling (arrow pointing to Earth’s centre), always moving sideways (arrow along the ring). The two arrows never cancel — they cooperate to make the path curve exactly as much as Earth curves.
Throw a ball sideways — it lands a few metres away. Throw harder — it lands farther. Now imagine throwing extremely hard, from a very high mountain. Here’s the key: the Earth is round, so its surface curves downward. As the ball flies farther, the ground beneath it drops away. If the ball flies fast enough, its falling matches the Earth’s curving — the ball falls forever and never touches ground. That’s an orbit.
Feels wrong, right? Higher = farther from Earth = fighting more gravity? No — it’s the opposite. Farther from Earth, gravity is weaker , so the satellite needs less speed to keep circling. vₒ shrinks as r grows: doubling the orbit distance cuts the speed by √2.
From Part 1: escape velocity 11.2 km/s, orbit velocity 7.9 km/s. The ratio is always √2, for any planet, at any height. Memorise the pair, and any question about either one hands you the other.
Shortcut form (when the question gives g instead of M): vₒ = √(gR). Using R instead of R + h. The question says ‘height 400 km’ — students plug in Earth’s radius alone. Fix it forever: r = R + h, distance from the CENTRE. This is the most-lost mark in satellites.
Moreover, your Google Maps pin: GPS satellites fly at 20,200 km at 3.9 km/s. Circling exactly twice a day — that orbit was chosen with this formula. Your phone is talking to objects obeying it right now. Starlink internet: thousands of satellites in the low fast lane (550 km, ~95 minutes per lap) — low = fast = low signal delay.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.
Quick answer: Kepler's three laws — ellipse orbits, equal areas, T² ∝ r³ — with the 15-second ratio method that turns them into guaranteed marks, and how they discovered Neptune…
In one line: Kepler's Laws — exam-ready notes in one glance.
In one line: kepler’s laws: JEE/NEET Physics · Gravitation series · Part 3 of 8 · All parts →✪ Key points — the 30-second versionLaw 1: ellipses, Sun at a focus ·.
In fact, JEE/NEET Physics · Gravitation series · Part 3 of 9 · All parts →
Notably, in 1609, a man with no telescope predicted the motion of every planet using three simple rules. NASA still uses them to plan missions today. In fact, kepler's laws look like boring history — they're actually three of the easiest marks in NEET and JEE Main. Meanwhile, part 3 of the Gravitation series , told simply.
Overall, everyone pictures orbits as perfect circles. Meanwhile, they're not — they're ellipses : circles gently squashed, like a slightly oval roti. And the Sun doesn't sit in the middle — it sits slightly off-centre, at a point called a focus .
Consequently, what this means: a planet's distance from the Sun keeps changing through the year. Meanwhile, earth is closest in January (147 million km) and farthest in July (152 million km). Moreover, a perfect circle is just the special case where the squash is zero.
Furthermore, picture a ball rolling in a large round bowl. Indeed, near the edges (high up) it rolls slowly. Therefore, near the centre it whizzes fast. Planets do the same: closer to the Sun = faster; farther = slower.
Likewise, earth runs at 30.3 km/s in January and 29.3 km/s in July. As a result, the reason (angular momentum) is Part 4 's story.
Sun (focus)
fast (perihelion)
slow (aphelion)
equal areas
in equal times
| Letter | What it means (plain words) | Value / unit |
|---|---|---|
| T | In short, the time for one complete round — the planet's 'year' | Subsequently, earth: 1 year; Jupiter: 12 years |
| r | In fact, the average distance from the Sun (centre to centre) | Earth: 1.5×10¹¹ m |
| M | Moreover, mass of the big central body being orbited | Sun: 2×10³⁰ kg |
| G | gravity's fixed strength number | 6.67 × 10⁻¹¹ |
Therefore, why does distance matter SO much? Meanwhile, two reasons stack up: a bigger orbit is a longer track AND the planet moves slower on it (Part 2's rule). Meanwhile, longer track + slower speed = much, much more time. That's why the r is raised to the power 1.5.
Meanwhile, almost every exam question on Rule 3 is a comparison. Meanwhile, don't compute full years — compare: year ratio = (distance ratio)^1.5.
Indeed, apply the trick: 4^1.5 = 4 × √4 = 4 × 2 = 8.
Specifically, reality check: Jupiter orbits ~5× farther out and takes 12 years — same pattern.
Answer: 8 Earth-years
Similarly, flip the power: distance ratio = 8^(2/3) = (2³)^(2/3) = 2² = 4.
Overall, remember: distance→year uses power 1.5; year→distance uses power 2/3. Flip one, flip the other.
Answer: 4× farther
Rearrange: M = 4π²r³/(GT²).
Consequently, piece by piece: r³ = 3.4×10³³; T² = 9.9×10¹⁴; 4π² ≈ 39.5.
As a result, combine: M = 39.5 × 3.4×10³³ ÷ (6.67×10⁻¹¹ × 9.9×10¹⁴) ≈ 2×10³⁰ kg.
Think about this: this IS how the Sun's mass is known — a timer and a ruler. You just weighed a star with Class 11 maths.
Answer: M ≈ 2×10³⁰ kg
A planet is like a ball on an invisible string attached to the Sun. When the planet is close, the string's 'pull' is strong, so it moves fast — like a skater whipping through the tight end of a slalom. When far, the pull is weak and slow. Speed exactly compensates distance.
Numbers on the sweep: at its closest, Earth moves ~30.3 km/s; at its farthest, ~29.3 km/s. Near: fast. Far: slow. Multiply speed × distance in each case and you get the same number — the 'area speed' — which is exactly what Kepler's second law demands: equal areas in equal times.
Picture the Sun-planet line as a broom sweeping the floor of the orbit. In any fixed number of days, the broom sweeps a triangle of IDENTICAL area — a fat short triangle near the Sun, a thin long one far away. The broom never sweeps more or less, ever.
Everyone pictures orbits as perfect circles. They're not — they're ellipses : circles gently squashed, like a slightly oval roti. And the Sun doesn't sit in the middle — it sits slightly off-centre, at a point called a focus .
Picture a ball rolling in a large round bowl. Near the edges (high up) it rolls slowly. Near the centre it whizzes fast. Planets do the same: closer to the Sun = faster; farther = slower.
Why does distance matter SO much? Two reasons stack up: a bigger orbit is a longer track AND the planet moves slower on it (Part 2's rule). Longer track + slower speed = much, much more time. That's why the r is raised to the power 1.5.
Almost every exam question on Rule 3 is a comparison. Don't compute full years — compare: year ratio = (distance ratio)^1.5.
Apply the trick: 4^1.5 = 4 × √4 = 4 × 2 = 8. Reality check: Jupiter orbits ~5× farther out and takes 12 years — same pattern. ✔ Comparing across different centres. The trick only works for bodies orbiting the same big mass. Earth vs Mars (both around Sun): fine. A Moon-orbiter vs a Sun-orbiter: not allowed — different M.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.
Quick answer: Why central forces conserve angular momentum (τ = 0), the L = mvr shortcut for elliptical-orbit speed problems, and how pulsars, satellites and ice skaters all obey the…
In one line: angular momentum: JEE/NEET Physics · Gravitation series · Part 4 of 8 · All parts →✪ Key points — the 30-second versionCentral force ⟹ zero torque ⟹ L = mv.
In fact, JEE/NEET Physics · Gravitation series · Part 4 of 9 · All parts →
In other words, watch an ice skater spin: arms stretched out — slow. Meanwhile, arms pulled in — suddenly whirling fast. No push, no engine. In fact, where did the extra spin come from? That’s the secret — a rule so strict the whole universe obeys it. Part 4 of the Gravitation series , the rule behind planets, skaters and pulsars.
Similarly, some things in physics can be changed by pushing harder. But a few are locked. Moreover, one locked thing: if no outside ‘twist’ (torque) acts on a spinning system, its turning quantity — angular momentum — cannot change. Meanwhile, not by pulling arms in, not by exploding, not by any internal trick.
Overall, why can’t gravity change it for a planet? Meanwhile, because gravity pulls the planet straight toward the Sun — along the string connecting them. Therefore, a pull aimed straight at the centre can speed you up or slow you down, but it can never twist you around. In one line: gravity can pull, but it cannot twist. So a planet’s turning quantity is locked for eternity.
| Letter | What it means (plain words) | Value / unit |
|---|---|---|
| L | Consequently, angular momentum — the ‘amount of turning’ the system has | unit: kg·m²/s |
| m | Furthermore, mass of the moving object (planet, skater’s arm, satellite) | kg |
| v | Likewise, the object’s sideways speed (the part that goes around, not toward or away) | m/s |
| r | In short, distance from the centre of the motion (planet to Sun, skater’s arm to body centre) | m |
Subsequently, read it as a see-saw: v × r must stay constant (m doesn’t change). Indeed, shrink r, and v must grow to pay for it. Grow r, and v must drop. That’s the entire rule.
In fact, arms out: her hands are far from the spin axis (big r), moving at modest speed (v). Meanwhile, she pulls her arms in: r shrinks — and since v × r is locked, v rises automatically. She spins faster without doing any rotational work. Her muscles worked to pull the arms in, but the spin-up is pure rule, not push.
Moreover, a comet on its long oval orbit is a skater with invisible arms. Meanwhile, far from the Sun: big r, slow crawl. Falling closer: r shrinks — v must rise. The comet whips around the Sun at maximum speed at closest approach, then slows again on the way out. This IS Kepler’s Rule 2 from Part 3 — ‘faster near the Sun’ was this locked quantity all along. Kepler saw the pattern; this rule explains it.
Therefore, apply the see-saw: v × r constant → 2 × 24,000 = v × 8,000.
Solve: v = 6 km/s. Meanwhile, closer = faster, exactly like the comet.
Answer: 6 km/s
As a result, the locked thing: turning resistance × spin rate = constant. Meanwhile, half the resistance → double the spin rate.
Answer: 4 rounds/s.
In other words, bonus truth: her spinning energy DOUBLED — paid for by her muscles pulling the arms in. Meanwhile, the turning rule and the energy rule are separate books; both must balance.
Answer: 4 rounds/s (and her muscles paid the extra energy)
Notably, the string pulls through the centre — it can’t twist. Meanwhile, v × r is locked: half the radius → double the speed .
Similarly, energy: speed energy = ½mv² → quadruples. Your hand did that work pulling the string — you can feel the ball yank back.
Answer: speed ×2; energy ×4 — your pulling hand pays
Open a door by pushing near the hinge: nothing. The same push at the handle: the door swings. What matters is not force alone but force × leverage — the twist. Gravity always pulls through the centre, so its leverage is zero: gravity is a push at the hinge.
Compare: a rocket thrusting sideways gives angular momentum L = mvr; change any factor and the orbit twists into a new shape. Gravity gives ΔL = 0 every second of the orbit — pull it as hard as you like, the twisting effect is exactly zero because the lever arm (perpendicular distance to the line of pull) is zero.
Draw the planet with two arrows: the velocity arrow (long near the Sun, short far away) and the gravity arrow (pointing dead at the Sun’s centre). The gravity arrow only tilts the velocity arrow — it can rotate it, never lengthen or shorten the sweep the path makes around the Sun.
Some things in physics can be changed by pushing harder. But a few are locked. One locked thing: if no outside ‘twist’ (torque) acts on a spinning system, its turning quantity — angular momentum — cannot change. Not by pulling arms in, not by exploding, not by any internal trick.
Read it as a see-saw: v × r must stay constant (m doesn’t change). Shrink r, and v must grow to pay for it. Grow r, and v must drop. That’s the entire rule.
Arms out: her hands are far from the spin axis (big r), moving at modest speed (v). She pulls her arms in: r shrinks — and since v × r is locked, v rises automatically. She spins faster without doing any rotational work. Her muscles worked to pull the arms in, but the spin-up is pure rule, not push.
A comet on its long oval orbit is a skater with invisible arms. Far from the Sun: big r, slow crawl. Falling closer: r shrinks — v must rise. The comet whips around the Sun at maximum speed at closest approach, then slows again on the way out. This IS Kepler’s Rule 2 from Part 3 — ‘faster near the Sun’ was this locked quantity all along. Kepler saw the pattern; this rule explains it.
Apply the see-saw: v × r constant → 2 × 24,000 = v × 8,000. Solve: v = 6 km/s. Closer = faster, exactly like the comet. ✔ ‘Angular momentum is always conserved.’ Only when no outside twist acts. Add friction (a twist) and it drains away — a spinning top slows and stops.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.
Quick answer: U = −GMm/r explained: zero at infinity, negative means bound, mgh is its near-surface shadow — with a 3 GJ worked numerical and the sign traps that cost…
In one line: gravitational potential energy: JEE/NEET Physics · Gravitation series · Part 5 of 8 · All parts →✪ Key points — the 30-second versionU = −GMm/r with U = 0.
In fact, JEE/NEET Physics · Gravitation series · Part 5 of 9 · All parts →
Notably, there’s a minus sign in gravity’s energy formula, and it decides marks. Meanwhile, remove it and every answer goes wrong. But the minus isn’t there to torture you — it has a beautifully simple meaning: negative energy = trapped. In fact, part 5 of the Gravitation series , explained like a bank account.
Similarly, potential energy always needs a ‘zero’ chosen by us. Meanwhile, near the ground, you choose the ground as zero — that’s why mgh is positive when you climb. But for planets, ‘the ground’ is a bad choice (every planet has different ground!). So physics chooses the only universal zero: infinite distance apart = zero energy.
Overall, now think like a bank account. Meanwhile, far away (at infinity): balance zero. Moreover, bring a satellite closer to Earth — gravity pulls it in. Doing work for free — like receiving free money, your balance goes below zero (into debt). Closer = deeper debt. That debt is the minus sign:
And here’s the elegant connection: to escape. Consequently, your throwing energy must exactly pay off the debt: ½mv² = GMm/R — which rearranges to v = √(2GM/R) . Indeed, part 1’s escape velocity was a debt repayment all along!
| Letter | What it means (plain words) | Value / unit |
|---|---|---|
| U | Furthermore, gravitational potential energy — the ‘debt’ stored in the pair of masses | Likewise, unit: joules (J); negative by design |
| G | gravity’s fixed strength number | 6.67 × 10⁻¹¹ |
| M | In short, mass of the big body (planet) | kg |
| m | Subsequently, mass of the small body (satellite) | kg |
| r | distance between the two centres | m |
In fact, follow the steps: (1) We declared U = 0 at infinite distance. Meanwhile, (2) Gravity is attractive — it pulls masses together for free , doing positive work as r shrinks. Therefore, (3) Energy conservation then forces stored energy to drop below its zero mark as they come together. Result: at any finite distance, U is negative. The minus sign is bookkeeping for ‘gravity already paid. You’re in debt.’ Closer = more negative = deeper trap.
Is mgh wrong? Moreover, no — it’s a local approximation. Meanwhile, near the surface, the big formula expands to: U ≈ (a big negative constant) + mgh. Meanwhile, the ‘big constant’ is invisible to us (we only measure changes ), so we see just mgh. That’s why mgh works for a shelf and fails for a satellite: for a 400-km orbit, the full −GMm/r must be used.
Therefore, apply U = −GMm/r with r = 2R: the debt halves.
Meanwhile, common-sense check: farther away = shallower trap = less negative.
Answer: −U₀/2
As a result, think: energy needed = final debt minus initial debt = (−GMm/2R) − (−GMm/R) = +GMm/2R.
Notably, numbers: GMm/R = 6.67×10⁻¹¹ × 6×10²⁴ × 100 ÷ 6.4×10⁶ ≈ 6.25×10⁹ J → answer is half.
Indeed, common-sense check: ≈3 GJ ≈ 870 kWh — the right order for launch-scale budgets.
Answer: ≈ 3.1 × 10⁹ J
Specifically, build each: KE = GMm/2r; |PE| = GMm/r; total = −GMm/2r.
Similarly, the pattern: the debt is always exactly 2× the speed-energy. Meanwhile, the total is negative — trapped, with the debt winning by exactly 2:1.
Overall, this −2:+1 pattern is the whole story of Part 6 .
Answer: |PE| : KE : |total| = 2 : 1 : 1
Climbing out of a well costs energy — and we set the well’s top as zero. Every height inside the well is BELOW zero, so every ‘energy bank account’ in gravity starts in debt. Negative potential energy isn’t weird physics; it’s honest accounting from inside a well.
Lift 1 kg to infinity and you’d pay 62.7 million joules (for Earth). So a 1 kg rock sitting on Earth’s surface is 62.7 MJ in debt: U = −62.7 MJ. Halfway up the energy ladder, the debt shrinks to −31 MJ. Zero is only reached at infinite distance, where the well finally ends.
Picture the classic ‘gravity well’ funnel drawing: a dip with the planet at the bottom. Height above the pit floor = potential energy. Every orbit is a ball rolling on the funnel’s wall — and everything inside the funnel has negative height relative to the flat rim.
Potential energy always needs a ‘zero’ chosen by us. Near the ground, you choose the ground as zero — that’s why mgh is positive when you climb. But for planets, ‘the ground’ is a bad choice (every planet has different ground!). So physics chooses the only universal zero: infinite distance apart = zero energy.
Follow the steps: (1) We declared U = 0 at infinite distance. (2) Gravity is attractive — it pulls masses together for free , doing positive work as r shrinks. (3) Energy conservation then forces stored energy to drop below its zero mark as they come together. Result: at any finite distance, U is negative. The minus sign is bookkeeping for ‘gravity already paid. You’re in debt.’ Closer = more negative = deeper trap.
Is mgh wrong? No — it’s a local approximation. Near the surface, the big formula expands to: U ≈ (a big negative constant) + mgh. The ‘big constant’ is invisible to us (we only measure changes ), so we see just mgh. That’s why mgh works for a shelf and fails for a satellite: for a 400-km orbit, the full −GMm/r must be used.
Apply U = −GMm/r with r = 2R: the debt halves. Common-sense check: farther away = shallower trap = less negative. ✔ Assuming energy at the surface is zero. Zero lives at infinity! The surface sits at −GMm/R (deep debt). Every escape-energy question dies on this.
The price of a rocket launch (₹3–5 lakh per kg to orbit) is literally this card: you’re paying cash to clear a gravitational debt of ~63 million joules per kilogram. Voyager 2’s free speed boost at Jupiter: it stole a tiny sliver of Jupiter’s orbital energy — transfers between gravity ‘bank accounts’ that mission designers trade like currency.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.
Quick answer: The −2 : +1 : −1 ratio (PE : KE : E) that solves every satellite-energy question, the halve-the-radius pattern, and why a satellite that loses energy speeds…
In one line: satellite energy: JEE/NEET Physics · Gravitation series · Part 6 of 8 · All parts →✪ Key points — the 30-second versionThe ratio that solves everything: PE.
In fact, JEE/NEET Physics · Gravitation series · Part 6 of 9 · All parts →
Notably, every satellite in orbit is in debt — and the size of that debt follows one fixed pattern that solves nearly every exam question on this topic. If Part 5 was the bank account, this card is the repayment schedule. In fact, part 6 of the Gravitation series .
Similarly, a satellite in a circular orbit has two energies: speed-energy (positive — it’s moving) and gravity-debt (negative — it’s trapped). Meanwhile, using the orbit speed from Part 2 , the maths gives a fixed pattern:
| Letter. | What it means (plain words). | Value / unit. |
|---|---|---|
| G. | gravity’s fixed strength number. | 6.67 × 10⁻¹¹. |
| M, m. | planet’s mass, satellite’s mass. | kg. |
| r. | Overall, distance from the planet’s centre to the orbit. | m. |
| total (E). | Consequently, the whole account: negative = trapped, zero = just barely free. | −GMm/2r. |
Furthermore, read the pattern as a sentence: ‘the debt is always exactly twice the speed-energy. Meanwhile, the account is negative by exactly the amount of the speed-energy.’ Escape means paying off exactly the speed-energy you have. That single sentence answers most questions.
Likewise, here’s the strangest fact in this chapter: when a satellite loses energy (to air drag), it speeds up. Indeed, losing energy deepens the debt → deeper debt = smaller orbit r → smaller orbit = faster orbit speed (Part 2’s rule). So the satellite descends and speeds up while its account gets worse. As a result, space stations fight this constantly — drag bleeds them downward, and re-supply craft re-pay the debt.
In short, apply 2:1:1: debt = −2E₀, total = −E₀.
Check: total is negative (trapped) and equals the speed-energy in size.
Answer: debt = −2E₀; total = −E₀
Subsequently, all three scale as 1/r: every one doubles in size.
But think: moving closer needs energy removed (a retro-burn or drag) — the account worsens — and the satellite ends up faster . Yes: that’s the drag paradox.
Answer: all double in size; total more negative; satellite faster
In fact, use totals, never pieces: new total − old total = (−GMm/4r) − (−GMm/2r) = +GMm/4r.
Moreover, why totals: the move changes both speed-energy (down) and debt (up) — only the net is what the thrusters pay. Meanwhile, students who compute only one piece get the wrong options.
Therefore, common-sense check: positive (climbing costs energy). Meanwhile, less than the full debt change — the satellite gives back some speed-energy as it settles.
Answer: +GMm/4r
Orbiting is a strange bargain: to climb higher, you must SLOW DOWN. Gain potential energy and you lose twice as much kinetic — so the total sinks. Falling toward the Sun, the reverse: you speed up, but the total energy climbs less than your speed suggests.
Low orbit: KE = +3.2 MJ/kg, PE = −6.4 MJ/kg, total = −3.2 MJ/kg (exactly −KE/2). Geostationary orbit: KE smaller, total −0.5 MJ/kg. Check the pattern: E = −KE/2 at every radius — the two energies are locked in a 2:1 marriage by the mathematics of circular orbits.
Draw a bar chart at two orbit heights: at low orbit the KE bar is tall, the PE bar twice as tall downward, total bar a short stub below zero. At high orbit all three bars shrink together, same 2:1 shape. The chart is self-similar at every altitude.
A satellite in a circular orbit has two energies: speed-energy (positive — it’s moving) and gravity-debt (negative — it’s trapped). Using the orbit speed from Part 2, the maths gives a fixed pattern:
Apply 2:1:1: debt = −2E₀, total = −E₀. Check: total is negative (trapped) and equals the speed-energy in size. ✔ ‘Closer = lazier.’ The opposite: closer orbits are faster (Part 2) with MORE speed-energy. The mistake comes from everyday ‘nearer the ground = slower’ feelings. Computing only the speed-energy or only the debt for orbit shifts. Thruster budgets = change in TOTAL. Every wrong MCQ option is a partial answer.
The ISS loses ~2 km of height per month to drag and gets re-boosted by visiting spacecraft — a monthly subscription payment against this exact debt schedule. Retired TV satellites are pushed UP to a ‘graveyard orbit’, not down — the debt maths makes burial-in-space cheaper than a controlled fall.
🧠 The 2:1:1 chant: ‘debt twice the speed-energy, total negative by exactly the speed-energy’ — one pattern, every question. 🧠 Paradox line: ‘lose energy, speed up’ — the drag paradox in four words. 🏠 Daily: the ISS falls ~2 km per month and gets re-boosted — a monthly debt payment you can watch on launch schedules.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.
Quick answer: How g changes with height, depth and latitude — three formulas, one 15-second free-mark numerical, and how gold traders and mineral surveys quietly use them.
In one line: variation of g: JEE/NEET Physics · Gravitation series · Part 7 of 8 · All parts →✪ Key points — the 30-second versionHeight: g' ≈ g(1 − 2h/R) — exact: gR²/.
Therefore, JEE/NEET Physics · Gravitation series · Part 7 of 9 · All parts →
Consequently, Stand on a spring balance at the equator, then at the North Pole — the same you weighs about 350 grams more at the Pole. Meanwhile, Not an instrument trick: g itself genuinely changes with height , depth , and latitude . NEET asks all three as direct formula questions. Part 7 of the Gravitation series — with one recipe behind all three.
Furthermore, Your gravity depends on only two things: how much planet is beneath you. Meanwhile, How far you are from its centre. Specifically, Climb: mass same, distance bigger → g falls. Dig: distance smaller BUT mass beneath you shrinks too → g still falls. Spin: some gravity gets ‘spent’ holding you on the circle → felt g falls. Three variations, one recipe.
However, Climbing to height h moves you farther from the centre: divide by (R+h)² instead of R². Meanwhile, Calibration: at Everest’s top, g drops only 0.03 m/s² — tiny, because 8.8 km is truly tiny next to 6,400 km. But at h = R (one full radius up), the exact formula gives g/4 — while the shortcut would absurdly give −g. If h isn’t tiny, use the exact form. A wrong-sign answer is your alarm bell.
Moreover, Descend to depth d and something lovely happens: all the rock ABOVE your head cancels its own pull (a shell of uniform rock pulls you equally in all directions from inside — net zero). Only the ball of rock beneath you counts — and that ball shrinks as you descend. At the centre of the Earth: nothing beneath, pulls from every side cancel — g = 0. You would float at the centre of the Earth.
In fact, The spinning Earth carries you around a circle (biggest circle at the equator, shrinking to nothing at the poles). Going in a circle needs some inward pull — part of gravity is ‘spent’ as that inward pull. The balance you stand on reads less. The discount is small (0.34% at the equator) but permanent — and combined with Earth’s slight equatorial bulge, real g runs 9.780 (equator) to 9.832 (poles).
| Letter. | What it means (plain words). | Value / unit. |
|---|---|---|
| g. | gravity strength at the surface (the starting value). | Earth: 9.8 m/s². |
| h / d. | height climbed / depth dug. | in metres. |
| ω. | spin rate of Earth in radians per second (2π ÷ 24 hours). | 7.29 × 10⁻⁵. |
| λ (lambda). | latitude — 0° at the equator, 90° at the poles. | degrees. |
Notably, One substitution: g’ = 9.8 × (1 − ½) = 4.9 m/s².
In other words, Check: halfway down, half the ‘effective planet’ beneath you — linear, clean.
Answer: 4.9 m/s² (= g/2)
Specifically, Exact: g’ = g·R²/(2R)² = g/4 = 2.45 m/s².
Indeed, Shortcut would say: g(1 − 2) = −g — nonsense! That’s the alarm: big h demands the exact formula. JEE tests exactly this discrimination.
Answer: g/4 = 2.45 m/s²
In short, Step 1 — spin rate: ω = 2π/86,400 = 7.27×10⁻⁵ per second.
Similarly, Step 2 — the spent part: ω²R = (7.27×10⁻⁵)² × 6.4×10⁶ ≈ 0.034 m/s².
Therefore, Step 3 — fraction: 0.034/9.8 ≈ 0.34%.
Fun limit: if Earth spun ~17× faster (a day of 1.4 hours). The spent part would equal g itself — objects at the equator would float!
Answer: ≈ 0.34% reduction at the equator
Sit on a spinning merry-go-round: you feel flung outward. Earth is a giant merry-go-round, and at the equator you ride the widest circle — maximum outward fling, subtracting from gravity’s pull. At the poles you stand on the axis: no spin, no fling, full weight.
Earth’s pull is ~9.83 m/s² at the poles and effectively ~9.78 m/s² at the equator — a 0.05 difference, of which spin contributes 0.034. On a 70 kg person that’s ~350 g lighter at the equator: a bag of flour’s worth, measurable on a good scale.
Picture Earth as a spinning top seen from above the pole: circles of daily travel at every latitude, shrinking to a point at the pole. Each circle’s outward fling is biggest at the equator’s fat circle, zero at the pole’s point. Weigh yourself on different circles, get different weights.
Moreover, One substitution: g’ = 9.8 × (1 − ½) = 4.9 m/s². Check: halfway down, half the ‘effective planet’ beneath you — linear, clean. ✔ Using the small-h shortcut for big h. It quietly returns nonsense (like −g). If h is a serious fraction of R, use gR²/(R+h)² exactly.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.
Quick answer: The series finale: how the Class 11 formulas run today's biggest experiments — the 9 mm Schwarzschild radius of Earth, LIGO's proton-width measurement, Aditya-L1 at Lagrange point L1,…
In one line: Black Holes, LIGO and Lagrange Points — exam-ready notes in one glance.
One-page formula card (PDF) — print it, pin it, revise from it. Free, no signup.
In one line: Black holes, LIGO and Lagrange points — the finale of the JEE/NEET Physics · Gravitation series · Part 8 of 8 · All parts →
JEE/NEET Physics · Gravitation series · Part 8 of 8 · All parts →
In 2015, humanity “heard” two black holes collide — 1.3 billion years after the event actually happened. Every formula used in that detection is over a century old at most, and the core mathematics traces straight back to the gravitation you have revised across this series. This finale of the Gravitation series shows exactly how the syllabus connects to modern astrophysics — and then hands you the complete revision card.
Start with escape velocity from Part 1: vₑ = √(2GM/R). Now imagine shrinking R while keeping M fixed. As the radius decreases, the escape velocity climbs. At some critical radius, vₑ equals c — the speed of light. Beyond that boundary, nothing escapes, not even light itself:
R_s = 2 × 6.67×10⁻¹¹ × 6×10²⁴ ÷ (3×10⁸)² = 8×10¹⁴ ÷ 9×10¹⁶
Answer: ≈ 9 mm — all of Earth, squeezed into a marble.
Try it yourself: repeat the calculation for the Sun (M = 2×10³⁰ kg). You should get about 3 km — the entire Sun compressed to the size of a small town. This is a classic one-mark exam question.
Here is the exam-relevant correction most students miss: at a distance, a black hole’s gravity is identical to that of any object of equal mass. If you swapped the Sun for a Sun-mass black hole tomorrow, Earth’s orbit would not change by a metre. Black holes do not “suck things in” — they simply have gravity, and their horror lies only in how close you can get to the mass.
In September 2015, two black holes — 36 and 29 solar masses — spiralled into each other and merged. In the final moments, three entire solar masses converted directly into pure energy as gravitational waves: E = mc², Part 5’s bookkeeping applied at cosmic scale. For a few hundredths of a second, that merger out-radiated all the stars in the observable universe combined.
LIGO — the Laser Interferometer Gravitational-Wave Observatory — caught the signal. Its two 4-km detector arms measured a length change of roughly one ten-thousandth of a proton’s width, a precision so extreme that engineers must account for quantum noise, thermal vibration of the mirrors, and even the rumble of trucks hundreds of kilometres away. This is energy and momentum conservation verified at 22 decimal places.
And the story is coming home: LIGO-India is under development as India’s flagship gravitational observatory, which will sharpen the sky-localisation of every future detection dramatically. Expect this in the “current science” flavour of exam questions.
There are five special points in the Sun–Earth system where the Sun’s gravity, the Earth’s gravity and the orbital motion balance out. A satellite parked there holds station with almost no fuel — these are the Lagrange points.
The placement math is Parts 2, 3 and 5 working together: gravitational force balance plus centripetal orbital conditions plus energy bookkeeping. If a question gives you the Sun–Earth distance and asks for the L1 distance, you are equating the net force toward the Sun with the required centripetal force for a 1-year orbital period — a beautiful synthesis problem.
How do we know the black hole at our galaxy’s centre, Sgr A*, weighs about four million Suns? We watch a star orbit it. The star S2 completes a full 16-year loop around a point where nothing visible sits. Measure the orbital period T and the semi-major radius r, then apply Kepler’s third law from Part 3: M = 4π²r³/GT².
That is the astonishing part: a law published in 1619, derived from planetary observations by naked-eye-era astronomy, weighs a four-million-solar-mass monster. Kepler’s third law works equally for Mars and for black holes because gravity is gravity — the same inverse-square force everywhere in the universe. This technique, watching things orbit invisible masses, is also how astronomers first inferred dark matter in galaxies.
| Quantity. | Formula. | Note. |
|---|---|---|
| Escape velocity. | vₑ = √(2GM/R) = √(2gR). | surface launch; mass-independent. |
| Orbital velocity. | vₒ = √(GM/r) = √(gR). | Furthermore, r = R + h; vₑ = √2·vₒ. |
| Kepler’s third law. | T² = 4π²r³/GM. | same central body only. |
| Angular momentum. | L = mvr = constant. | central force ⟹ τ = 0. |
| Gravitational PE. | U = −GMm/r. | U = 0 at infinity. |
| Orbit energies. | KE = GMm/2r, E = −GMm/2r. | |PE| = 2|KE|. |
| g with depth. | g’ = g(1 − d/R). | g = 0 at centre. |
| g with height. | g’ ≈ g(1 − 2h/R). | exact: gR²/(R+h)². |
| g with latitude. | Likewise, g’ = g − ω²R cos²λ. | max reduction at equator. |
Revision tip: memorise the escape and orbital velocity pair together — the relation vₑ = √2·vₒ is tested far more often than either formula alone. The energy relations are the second-highest-yield row: remember that for a circular orbit, the total energy is negative and equal to half the potential energy in magnitude.
In short, the angular momentum conservation from Part 4 becomes the most powerful problem-solving tool in the next chapter — Rotational Motion: torque, moment of inertia and rolling bodies. The central-force argument (τ = 0 ⟹ L = constant) reappears everywhere in rotation, so the mental machinery you built here transfers directly. Gravitation, it turns out, was rotation’s rehearsal.
Imagine the well of gravity dug so deep that even light — the fastest thing there is — lacks the launch speed to climb out. That’s a black hole: not a vacuum cleaner, just a pit with walls steeper than light can climb. And when two such pits crash together, the well itself shakes — space quivers like a struck drumskin.
Light escapes at 300,000 km/s; Earth would trap it only if compressed to 9 mm across (its ‘photon sphere’ logic). LIGO measured two black holes of 36 and 29 solar masses merging 1.3 billion light-years away — the wobble it detected in a 4-km laser arm was 10,000× smaller than a proton.
Picture spacetime as a stretched rubber sheet: masses make dents, a black hole a bottomless poke. Two pokes spiralling together launch waves across the sheet — and a detector is just two rulers at right angles, each stretching and squeezing a hair’s breadth as the wave passes.
A black hole is nothing more exotic than escape velocity taken to its limit. Start from Part 1: vₑ = √(2GM/R). Shrink R while keeping M fixed, and at some radius vₑ = c. That radius is the Schwarzschild radius, R_s = 2GM/c². Worked example for Earth: R_s = 2 × 6.67×10⁻¹¹ × 6×10²⁴ ÷ (3×10⁸)² = 8×10¹⁴ ÷ 9×10¹⁶ ≈ 9 mm. Remember also that at a distance, a black hole’s gravity equals that of any equal mass — orbiting bodies notice nothing special until they venture close.
Two black holes of 36 and 29 solar masses merged in 2015, converting three solar masses directly into gravitational-wave energy — E = mc² from Part 5 at cosmic scale. LIGO’s 4-km detector arms measured a length change of one ten-thousandth of a proton’s width, confirming energy conservation to extraordinary precision. LIGO-India is under development and will become India’s flagship gravitational observatory, dramatically improving source localisation on the sky.
There are five Lagrange points in the Sun–Earth system where gravitational pulls and orbital motion balance, letting satellites hold station with almost no fuel. L1 (1.5 million km sunward) hosts Aditya-L1, ISRO’s solar observatory, because it enjoys a continuous, eclipse-free view of the Sun. L2 hosts the James Webb Space Telescope, which needs a permanently dark, cold sky. L4 and L5 sit 60° ahead of and behind Earth’s orbit. The placement math combines Parts 2, 3 and 5 — force balance plus centripetal conditions.
How do we know the black hole Sgr A* weighs about four million Suns? Watch a star orbit it: the star S2 completes a 16-year loop around an invisible point. Measure T and r, then apply Part 3: M = 4π²r³/GT². It is remarkable that Kepler’s 1619 law — derived from naked-eye planetary data — weighs million-solar-mass monsters today, but gravity’s inverse-square nature makes it universal.
The angular momentum conservation from Part 4 becomes the most powerful problem-solving tool in the next chapter — Rotational Motion: torque, moment of inertia and rolling bodies. The central-force argument (zero torque ⟹ constant angular momentum) transfers directly, so the intuition built across Gravitation becomes rotation’s foundation.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.
Quick answer: The side streets of Gravitation: field intensity E = GM/r², the shell theorem, potential inside a planet, true weightlessness, and the geostationary conditions — Part 9 (bonus) of…
In one line: Gravitation Bonus — exam-ready notes in one glance.
In one line: JEE/NEET Physics · Gravitation series · Part 9 (bonus) · All parts →✪ Key points — the 30-second versionField intensity E = GM/r² = −dV/dr — force per.
In fact, JEE/NEET Physics · Gravitation series · Part 9 of 9 · All parts →
In other words, eight cards covered the main roads. Meanwhile, this bonus card completes the chapter’s side streets — gravity ‘field’, the hollow-shell surprise, true weightlessness. Why your TV satellite sits at exactly 36,000 km. All simple, all exam-tested. Moreover, part 9 (bonus) of the Gravitation series .
Similarly, you know g = 9.8 m/s². Therefore, generalise: the field at any point is the pull a 1-kg test mass would feel there: E = GM/r², direction: toward the planet. The subtle point: the field exists whether or not anything is there to feel it — it’s a property of space around a mass, an invisible arrow at every point. Meanwhile, (E and g are the same number; exams swap the names.)
Overall, stand anywhere inside a hollow spherical shell of rock. Which way do you fall? As a result, nowhere — gravity is exactly zero, everywhere inside. Not approximately — exactly.
Consequently, look at a patch of shell on your right: close, so it pulls hard. Meanwhile, a cone of vision catches only a small patch. The same cone extended left catches a bigger but farther patch that pulls weakly. Small-near-strong exactly cancels big-far-weak. Every direction cancels. Notably, this is why, when you dig into the Earth ( Part 7 ). Only the rock BENEATH you counts — the shell above you cancels itself out.
Furthermore, combine the ideas: at the centre, pulls cancel from all sides (field = 0. Meanwhile, you’d float) — but the gravity trap is at its deepest (energy −1.5GMm/R). No pull ≠ shallow trap. Specifically, a favourite conceptual MCQ: zero field, deepest well — both at once.
Likewise, astronauts float not because gravity is absent (at ISS height it’s 89% of surface value) but because they and their spacecraft fall together — nothing presses against anything. Meanwhile, same as a lift with a snapped cable: you’d float inside it, in full gravity. Weight is a contact force; weightlessness is absence of contact.
In short, for a satellite to hover over one fixed spot (so your dish never moves), it must circle exactly once per day. Meanwhile, part 3’s rule then FIXES its distance — no choice: r³ = GMT²/4π² gives r ≈ 42,300 km from Earth’s centre, i.e. Plus two more conditions: circle directly above the equator, moving eastward. All three together = ‘geostationary’.
Subsequently, direct: E = GM/(2R)² = GM/4R².
Check: double the distance, quarter the field — the same inverse-square as gravity always.
Answer: GM/4R², pointing at the planet
In fact, step 1 — Kepler solved for r: r³ = GMT²/4π² = 6.67×10⁻¹¹ × 6×10²⁴ × (8.64×10⁴)² ÷ 39.5 ≈ 7.55×10²².
Moreover, step 2 — cube root: r ≈ 4.23×10⁷ m.
Therefore, step 3 — minus Earth’s radius: h = 42,300 − 6,400 ≈ 36,000 km.
Meanwhile, you just derived the most famous number in satellite TV.
Answer: h ≈ 36,000 km
A field is gravity’s version of a smell: you don’t need to touch the source to know it’s there. Every mass fills space around it with ‘if you were here, you’d fall THIS way’ information. And GEO satellites are the perfect trick: orbit exactly once a day, and you circle at the same speed the Earth spins — parked over one spot forever.
Field strength: Earth’s field is 9.8 N/kg at the surface, but only 0.22 N/kg at GEO height (42,000 km from Earth’s centre). Exactly one strength exists where the orbital period equals 24 hours — and that’s where all TV satellites must live. Inside a shell (Shell Theorem), the field is exactly zero: the walls pull you in all directions at once, cancelling perfectly.
Draw arrows pointing at Earth in every location — a hedgehog of fall-directions. Long arrows near, stubby arrows far. Inside a hollow planet, no arrows at all. A GEO satellite sits where its arrow is just the right length for a 24-hour loop — the only such spot in the sky.
Stand anywhere inside a hollow spherical shell of rock. Which way do you fall? Nowhere — gravity is exactly zero, everywhere inside. Not approximately — exactly. Look at a patch of shell on your right: close, so it pulls hard. A cone of vision catches only a small patch. The same cone extended left catches a bigger but farther patch that pulls weakly. Small-near-strong exactly cancels big-far-weak. Every direction cancels. This is why, when you dig into the Earth (Part 7), only the rock BENEATH you counts — the shell above you cancels itself out.
For a satellite to hover over one fixed spot (so your dish never moves), it must circle exactly once per day. Part 3’s rule then FIXES its distance — no choice: r³ = GMT²/4π² gives r ≈ 42,300 km from Earth’s centre, i.e. Plus two more conditions: circle directly above the equator, moving eastward. All three together = ‘geostationary’.
Source: compiled from official notifications, standard textbooks and our own mock-test analytics; last reviewed September 2026.