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Review key Why Do Satellites Stay in Orbit Instead of Falling to Earth? exam facts and rate your mastery to track revision.
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#1
Satellites remain in orbit not by escaping gravity, but through continuous freefall matched with high tangential velocity.
#2
Gravity in Low Earth Orbit (LEO at 400 km) is still roughly 90% as strong as gravity on Earth's surface (g ≈ 8.7 m/s²).
#3
Sir Isaac Newton explained orbital mechanics in 1687 through his famous Cannonball Thought Experiment in the 'Principia'.
#4
An orbit occurs when a projectile's downward fall matches the geometric curvature of the spherical Earth beneath it.
#5
Earth's surface curves downward approximately 5 meters for every 8,000 meters (8 kilometers) traveled horizontally.
#6
In orbital mechanics, gravitational pull supplies the exact Centripetal Force required to maintain a curved circular trajectory.
#7
The formula for orbital velocity in a circular orbit is v = √(GM / r), where M is Earth's mass and r is orbital radius.
#8
Orbital velocity is independent of the satellite's mass; a tiny CubeSat and the 450-ton ISS orbit at the identical speed at the same altitude.
#9
In Low Earth Orbit (LEO), satellites travel at approximately 7.8 km/s (roughly 28,000 km/h), orbiting Earth every ~90 minutes.
#10
Astronauts aboard the ISS experience 'weightlessness' because they and the station fall freely together at the same acceleration.
#11
Geostationary Orbit (GEO) is located at an altitude of exactly 35,786 kilometers directly above Earth's equator.
#12
At GEO, a satellite's orbital period matches Earth's sidereal rotation period (23 hours, 56 minutes, 4 seconds), appearing stationary.
#13
Arthur C. Clarke popularized the concept of geostationary communications satellites in 1945, leading GEO to be called the Clarke Orbit.
#14
Escape Velocity from Earth's surface is approximately 11.2 km/s; exceeding this velocity propels a spacecraft into interplanetary space.
#15
Johannes Kepler's First Law states that all orbits are ellipses with the central body (Earth) located at one focal point.
#16
According to Kepler's Second Law, satellites move fastest at Perigee (closest approach) and slowest at Apogee (farthest point).
#17
Kepler's Third Law proves that orbital period squared is directly proportional to the semi-major axis cubed (T² ∝ a³).
#18
Orbital decay is caused by atmospheric drag from sparse gas molecules in the upper thermosphere colliding with LEO satellites.
#19
Atmospheric drag bleeds kinetic energy, causing satellites to spiral downward unless re-boosted via station-keeping thrusters.
#20
Sun-synchronous orbits (SSO) pass over any given point on Earth's surface at the same local solar time, ideal for imaging satellites.
#21
The Kármán line (100 km altitude) is the internationally recognized boundary where aerodynamic lift becomes insufficient to support flight.
#22
Kessler Syndrome describes a catastrophic scenario where orbital space debris cascades in collisions, rendering orbits unusable.
Subject Specialist Commentary
Analytical perspective & practical exam advice from the Master10 academic board
Satellites stay in orbit not because they escape Earth's gravity, but because they are constantly in free fall around it. Sir Isaac Newton explained this with his famous cannonball thought experiment. If a satellite travels forward at high horizontal speed—roughly eight kilometers per second in Low Earth Orbit—its downward plunge matches Earth's spherical curvature. As it falls toward the planet, the ground curves away at the exact same rate.
In UPSC and SSC physics questions, examiners frequently test orbital mechanics. A major misconception trap is believing gravity is zero in space; at the altitude of the International Space Station, gravity is still ninety percent of its surface strength. Astronauts float because they and the station fall together. For numerical prelims MCQs, remember that orbital velocity depends strictly on altitude and Earth's mass, completely independent of the satellite's weight.
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