When a planet moves around a star, the gravitational force between them provides the centripetal force necessary for the orbital motion. The planet's orbit follows Kepler's three laws of planetary motion. For a circular orbit of radius R, the orbital speed is v = √(GM/R) and the time period is T = 2π√(R³/GM), where M is the mass of the star and G is the gravitational constant.
Gravitational force provides centripetal force for planetary orbit: GMm/R² = mv²/R.
Orbital speed: v = √(GM/R) — independent of the planet's mass.
Orbital period: T = 2π√(R³/GM).
Kepler's Third Law: T² ∝ R³.
Total energy of orbiting planet: E = −GMm/(2R) (negative = bound system).
Kepler's Second Law: equal areas swept in equal times (conservation of angular momentum).
All planets orbit in ellipses with the star at one focus (Kepler's First Law).
Kepler's First Law (Law of Orbits): All planets move in elliptical orbits with the star at one focus.
Kepler's Second Law (Law of Areas): A line joining the planet to the star sweeps out equal areas in equal times.
Kepler's Third Law (Law of Periods): T² ∝ R³ (for circular orbits, R is the radius; for elliptical, R is the semi-major axis) T²/R³ = 4π²/(GM) = constant for all planets orbiting the same star
Where:
For a circular orbit:
Gravitational force = Centripetal force GMm/R² = mv²/R
Solving for orbital speed: v = √(GM/R)
Note: Orbital speed is independent of the planet's mass!
Orbital time period: T = 2πR/v = 2πR/√(GM/R) = 2π√(R³/GM)
Squaring: T² = 4π²R³/(GM) This confirms T² ∝ R³ (Kepler's Third Law)
For Earth orbiting the Sun:
For a planet of mass m in circular orbit of radius R around a star of mass M:
Kinetic Energy: KE = ½mv² = GMm/(2R) Potential Energy: PE = −GMm/R (negative, bound system) Total Mechanical Energy: E = KE + PE = GMm/(2R) − GMm/R = −GMm/(2R)
Key observations:
Escape velocity: v_esc = √(2GM/R) = √2 × v_orbital
Gravitational force between the planet and the star provides the centripetal force required for orbital motion. For a circular orbit: GMm/R² = mv²/R, where G is the gravitational constant, M is the star's mass, m is the planet's mass, and R is the orbital radius.
The orbital speed of a planet in a circular orbit is v = √(GM/R), where G = 6.674 × 10⁻¹¹ N·m²/kg², M = mass of the star, and R = orbital radius. Note that orbital speed is independent of the planet's own mass.
1st Law (Orbits): Planets move in elliptical orbits with the star at one focus. 2nd Law (Areas): The line joining planet to star sweeps equal areas in equal times. 3rd Law (Periods): The square of the orbital period is proportional to the cube of the semi-major axis: T² ∝ R³.
The total mechanical energy of a planet of mass m in a circular orbit of radius R is E = −GMm/(2R). The energy is negative, indicating the planet is gravitationally bound. KE = GMm/(2R) and PE = −GMm/R.
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