Iapetus 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
572.88m/s
- Surface gravity
- 0.2234 m/s2
- Circular orbit speed at that altitude
- 359.14
- Orbital period
- 4:32:29
- Orbital period in minutes
- 272.49
- Stationary orbit altitude Where an orbit matches the rotation period. Meaningless for a retrograde or very slow rotator.
- 51 611
- Mean density
- 1088 kg/m3
- Orbital kinetic energy of the payload
- 64 489 000
- Energy to lift the payload out of the well
- 164 098 000
Show the working
- Orbit altitude above the surface = 200
- Payload mass = 1000
- gm = 1.2053e11 = 120 530 000 000
- radius = 7.345e5 = 734 500
- Surface gravity = 120 530 000 000 / 734 500^2 = 0.223 415
- Escape velocity = sqrt(2 * 120 530 000 000 / 734 500) = 572.884
- orbit_radius = 734 500 + 200 * 1000 = 934 500
- Circular orbit speed at that altitude = sqrt(120 530 000 000 / 934 500) = 359.135
- Orbital period = 359.135 > 0 ? 2 * pi * 934 500 / 359.135 : 0 = 16 349.4
- Orbital period in minutes = 16 349.4 / 60 = 272.49
- Orbital kinetic energy of the payload = 1000 * 120 530 000 000 / (2 * 934 500) = 64 489 000
- Energy to lift the payload out of the well = 1000 * 120 530 000 000 / 734 500 = 164 098 000
- geo_radius = (120 530 000 000 * (1903.9 * 3600 / (2*pi))^2)^(1/3) = 52 345 100
- Stationary orbit altitude = (52 345 100 - 734 500) / 1000 = 51 610.6
- Mean density = 120 530 000 000 / 6.6743e-11 / (4/3 * pi * 734 500^3) = 1087.99
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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