Satellite Period Near Earth's Surface and Earth's Density

Physics · Gravitation · NEET

A satellite orbiting just above Earth's surface (orbit radius nearly equal to Earth's radius R) has a period that depends ONLY on Earth's mean density d, not on R: T = sqrt(3pi / (G d)), so T squared = 3pi / (G d). Memory hook: "skimming satellite = density only" — the R cancels out, so a denser planet always gives a shorter period.
Earthdensity dsatelliteRv (orbit)T (period)density dT = sqrt(3*pi / (G*d))higher d gives smaller TOrbit radius = R, so R cancels: period set by density d only.
A satellite skimming Earth's surface has orbit radius equal to R. Because mass hides an R^3 through density, R cancels and the period follows T = sqrt(3*pi/(G*d)) — falling as density d rises.

Your doubts, answered

Why does the radius R cancel out for a near-surface satellite?

Start with T = 2*pi*sqrt(R^3 / (G*M)). Replace the mass using density: M = (4/3)*pi*R^3*d. Substituting gives T = 2*pi*sqrt(R^3 / (G*(4/3)*pi*R^3*d)). The R^3 in the top and bottom cancel completely, leaving T = sqrt(3*pi / (G*d)). So for a satellite skimming the surface, only the mean density d matters, not the planet's size.

What is the exact formula linking period and density?

For an orbit radius equal to R (just above the surface): T = sqrt(3*pi / (G*d)), which is the same as T^2 = 3*pi / (G*d). Here G is the gravitational constant and d is the mean density of the planet. This is the form NEET tests directly.

Does this formula work for a satellite far above the surface?

No. This clean result only holds when the orbit radius equals the planet's radius R (satellite just above the surface). For a satellite at height h, the orbit radius is r = R + h and R does NOT cancel, so you must use the full T = 2*pi*sqrt(r^3 / (G*M)) and the period grows with height.

How is T^2 = 3pi/(Gd) connected to Kepler's third law?

Kepler's third law says T^2 is proportional to r^3. For a near-surface orbit r = R, and because M itself contains R^3 through density, the R^3 factors cancel and the proportionality collapses to a constant that depends only on d. So this is Kepler's law specialised to the surface orbit.

A denser planet gives a shorter or longer period?

Shorter. Since T = sqrt(3*pi / (G*d)), a larger density d makes the denominator bigger, so T becomes smaller. A denser planet pulls harder for the same size, so the skimming satellite must move faster and completes an orbit in less time.

⚠️ The NEET trap
Plugging a height h into T = sqrt(3pi/(Gd)) and expecting R to always cancel, or thinking a bigger planet must give a bigger period.
R cancels ONLY when the orbit radius equals R (satellite just above surface). Then the period depends solely on mean density d, so two planets of equal density but different sizes give the SAME near-surface period.
🧠 R cancels only at the surface — the moment there is height h, R comes back.

Real NEET questions

NEET 2023 Phase 1

A satellite orbits just above the earth's surface with period T. If d is the mean density of the earth and G the gravitational constant, the quantity 3*pi/(G*d) represents:

A · T
B · T^2
C · T^3
D · sqrt(T)
Solution: Step 1: Period of a near-surface satellite, T = 2*pi*sqrt(R^3 / (G*M)). Step 2: Write mass from density, M = (4/3)*pi*R^3*d. Step 3: Substitute, T^2 = 4*pi^2*R^3 / (G*(4/3)*pi*R^3*d). Step 4: Cancel R^3 and simplify: T^2 = 4*pi^2 / ((4/3)*pi*G*d) = 3*pi/(G*d). So 3*pi/(G*d) equals T^2. Answer: B.
NEET 2023 Phase 2

If R is the radius of the earth and g the acceleration due to gravity on its surface, the mean density of the earth is:

A · 3g/(4*pi*R*G)
B · 4*pi*g*R/(3G)
C · 12*pi*g/(R*G)
D · 4*pi*g*G/(3R)
Solution: Step 1: g = G*M/R^2. Step 2: M = (4/3)*pi*R^3*d, so g = (4/3)*pi*G*R*d. Step 3: Solve for density: d = 3g/(4*pi*G*R). This same density d is what feeds the satellite period formula T = sqrt(3*pi/(G*d)). Answer: A.

Solved Gravitation NEET PYQs

Try the real previous-year questions from this chapter — each with the answer and a full solution.

See all 27 Gravitation NEET PYQs ›
Next concept: Energy of an Orbiting SatelliteKeep learning — 2 minFeeling ready? Solve the Gravitation NEET PYQs ›Or practice on your phone — get the free MedicNEET app ›

Frequently asked

What is the period of a satellite just above Earth's surface?

About 84 to 85 minutes. Using T = sqrt(3*pi/(G*d)) with Earth's mean density d = 5500 kg/m^3 and G = 6.67e-11, you get roughly 5060 seconds, close to 84 minutes. This is the shortest possible period for an Earth satellite.

Is the formula T = sqrt(3pi/(Gd)) in the NEET syllabus?

Yes. It is a standard derived result from the Gravitation chapter and has been asked directly in NEET 2023. It combines the satellite period formula with the density expression for mass, both from NCERT Class 11 Physics.

Why does only density matter and not mass or radius?

Mass and radius are linked through density: M = (4/3)*pi*R^3*d. When both appear in the period formula for a surface orbit, the R^3 terms cancel, and mass gets absorbed into density. What is left is a single dependence on d.

How does this differ from the geostationary satellite period?

A geostationary satellite has a period of 24 hours at a height of about 36000 km, so its orbit radius is much larger than R and R does not cancel. The near-surface case gives the minimum period of about 84 minutes and depends only on density.