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In 2000, NASA placed a satellite in orbit around an asteroid. Consider a spherical asteroid with a mass of 1.00×1016 and a radius of 8.50km .

What is the speed of a satellite orbiting 4.70km above the surface?

What is the escape speed from the asteroid?

  • Physics -

    Can i get the weight of the satellite?

  • Physics -

    You don't need the weight or mass of the satellite. Use Kepler's Third Law in Newton's form (with the asteroid mass M, and G). The distance R from the center of the asteroid is 13.2 km. That is what you will need in the formula.

    There is a standard formula for escape speed in terms of G and M, and asteroid radius R'. I believe it is
    GM/R = (1/2)V^2
    V = sqrt(2GM/R')

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