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Orbital Speed, Escape Velocity and Satellites

concepthard~45 min study9 MCQ

Orbital speed vo = √(GM/r); escape speed ve = √(2GM/R) = 11.2 km/s for Earth; total orbital energy is negative.

What is Orbital Speed, Escape Velocity and Satellites?

Orbital speed vo = √(GM/r); escape speed ve = √(2GM/R) = 11.2 km/s for Earth; total orbital energy is negative.

Key formula / rule: ve = √(2) × vo at the same radius.

Key points

  • Derive orbital and escape speeds from energy considerations.
  • Evaluate whether a given launch speed produces a bound orbit.

Common exam trap

Assuming escape velocity depends on the mass of the escaping body.

Definitions

Term

Orbital Speed, Escape Velocity and Satellites

Meaning

Orbital speed vo = √(GM/r); escape speed ve = √(2GM/R) = 11.2 km/s for Earth; total orbital energy is negative.

Term

Orbital Speed, Escape Velocity and Satellites — explanation

Meaning

A bound satellite has negative total energy, and the escape condition is precisely total energy reaching zero. Geostationary satellites need a 24-hour period, which fixes their altitude at about 36000 km.

Learning objectives

  • Derive orbital and escape speeds from energy considerations.

  • Evaluate whether a given launch speed produces a bound orbit.

Formulae

Key point

ve = √(2) × vo at the same radius.

Key point

Total orbital energy E = -GMm/2r, negative for bound orbits.

Key point

Escape speed is independent of the mass and direction of the projectile.

Prerequisites

  • PHY-U2-GRAV-T2-S1-C1

  • PHY-U2-GRAV-T1-S1-C2

Common mistakes

  • Assuming escape velocity depends on the mass of the escaping body.

  • Using R instead of the orbital radius r in orbital speed.

Keywords

  • Orbital

  • Speed

  • Escape

  • Velocity

  • Satellites

Practice preview

  • A satellite of mass 'm' orbits a planet of mass 'M' in a circular orbit of radius 'r'. Which of the following statements about its energy is INCORRECT?

    medium

  • Which of the following statements is true regarding a geostationary satellite?

    easy

  • A satellite is orbiting Earth at a height of 3600 km above the surface. Given Earth's radius R = 6400 km and acceleration due to gravity g = 9.8 m/s^2, what is its orbital speed? (Assume G = 6.67 x 10^-11 Nm^2/kg^2 and M

    medium