Dione surface gravity, escape velocity and orbit calculator

Everything about orbiting a body follows from one number, its gravitational parameter GM, together with its radius.

Escape velocity
510.36m/s
≈ Rounded Dione gravity and escape velocity
Surface gravity
0.2320 m/s2
Circular orbit speed at that altitude
309.88
Orbital period
4:17:18
Orbital period in minutes
257.31
Stationary orbit altitude Where an orbit matches the rotation period. Meaningless for a retrograde or very slow rotator.
4135
Mean density
1478 kg/m3
Orbital kinetic energy of the payload
48 012 200
Energy to lift the payload out of the well
130 233 000
Show the working
  1. Orbit altitude above the surface = 200
  2. Payload mass = 1000
  3. gm = 7.3113e10 = 73 113 000 000
  4. radius = 5.614e5 = 561 400
  5. Surface gravity = 73 113 000 000 / 561 400^2 = 0.231 98
  6. Escape velocity = sqrt(2 * 73 113 000 000 / 561 400) = 510.359
  7. orbit_radius = 561 400 + 200 * 1000 = 761 400
  8. Circular orbit speed at that altitude = sqrt(73 113 000 000 / 761 400) = 309.878
  9. Orbital period = 309.878 > 0 ? 2 * pi * 761 400 / 309.878 : 0 = 15 438.4
  10. Orbital period in minutes = 15 438.4 / 60 = 257.306
  11. Orbital kinetic energy of the payload = 1000 * 73 113 000 000 / (2 * 761 400) = 48 012 200
  12. Energy to lift the payload out of the well = 1000 * 73 113 000 000 / 561 400 = 130 233 000
  13. geo_radius = (73 113 000 000 * (65.686 * 3600 / (2*pi))^2)^(1/3) = 4 696 000
  14. Stationary orbit altitude = (4 696 000 - 561 400) / 1000 = 4134.6
  15. Mean density = 73 113 000 000 / 6.6743e-11 / (4/3 * pi * 561 400^3) = 1478.03

Values are shown to six significant figures here; the arithmetic itself runs on exact fractions and is only rounded where a number is printed.

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    The formula

    • g = GM / r^2
    • escape velocity = sqrt(2 GM / r)
    • circular orbit speed = sqrt(GM / r)
    • period = 2 pi r / v
    • escape velocity is always sqrt(2) times the circular orbit speed at the same radius

    Escape velocity assumes no atmosphere and no further thrust. It is the speed at which kinetic energy equals the depth of the gravity well.

    Mean density is derived by dividing GM by G, so it inherits the uncertainty in G — about one part in twenty thousand.

    Where the numbers come from

    • GM and mean radius from planetary ephemeris and spacecraft tracking solutions.

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