Pallas 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
334.24m/s
- Surface gravity
- 0.2182 m/s2
- Circular orbit speed at that altitude
- 177.09
- Orbital period
- 4:29:39
- Orbital period in minutes
- 269.65
- Stationary orbit altitude Where an orbit matches the rotation period. Meaningless for a retrograde or very slow rotator.
- 403
- Mean density
- 3049 kg/m3
- Orbital kinetic energy of the payload
- 15 679 800
- Energy to lift the payload out of the well
- 55 859 400
Show the working
- Orbit altitude above the surface = 200
- Payload mass = 1000
- gm = 1.43e10 = 14 300 000 000
- radius = 2.56e5 = 256 000
- Surface gravity = 14 300 000 000 / 256 000^2 = 0.218 201
- Escape velocity = sqrt(2 * 14 300 000 000 / 256 000) = 334.244
- orbit_radius = 256 000 + 200 * 1000 = 456 000
- Circular orbit speed at that altitude = sqrt(14 300 000 000 / 456 000) = 177.087
- Orbital period = 177.087 > 0 ? 2 * pi * 456 000 / 177.087 : 0 = 16 179.3
- Orbital period in minutes = 16 179.3 / 60 = 269.655
- Orbital kinetic energy of the payload = 1000 * 14 300 000 000 / (2 * 456 000) = 15 679 800
- Energy to lift the payload out of the well = 1000 * 14 300 000 000 / 256 000 = 55 859 400
- geo_radius = (14 300 000 000 * (7.813 * 3600 / (2*pi))^2)^(1/3) = 659 284
- Stationary orbit altitude = (659 284 - 256 000) / 1000 = 403.284
- Mean density = 14 300 000 000 / 6.6743e-11 / (4/3 * pi * 256 000^3) = 3048.75
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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