Titania 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
760.90m/s
- Surface gravity
- 0.3672 m/s2
- Circular orbit speed at that altitude
- 480.53
- Orbital period
- 3:35:24
- Orbital period in minutes
- 215.40
- Stationary orbit altitude Where an orbit matches the rotation period. Meaningless for a retrograde or very slow rotator.
- 14 054
- Mean density
- 1666 kg/m3
- Orbital kinetic energy of the payload
- 115 454 000
- Energy to lift the payload out of the well
- 289 485 000
Show the working
- Orbit altitude above the surface = 200
- Payload mass = 1000
- gm = 2.2823e11 = 228 230 000 000
- radius = 7.884e5 = 788 400
- Surface gravity = 228 230 000 000 / 788 400^2 = 0.367 18
- Escape velocity = sqrt(2 * 228 230 000 000 / 788 400) = 760.901
- orbit_radius = 788 400 + 200 * 1000 = 988 400
- Circular orbit speed at that altitude = sqrt(228 230 000 000 / 988 400) = 480.529
- Orbital period = 480.529 > 0 ? 2 * pi * 988 400 / 480.529 : 0 = 12 923.9
- Orbital period in minutes = 12 923.9 / 60 = 215.398
- Orbital kinetic energy of the payload = 1000 * 228 230 000 000 / (2 * 988 400) = 115 454 000
- Energy to lift the payload out of the well = 1000 * 228 230 000 000 / 788 400 = 289 485 000
- geo_radius = (228 230 000 000 * (208.9 * 3600 / (2*pi))^2)^(1/3) = 14 842 200
- Stationary orbit altitude = (14 842 200 - 788 400) / 1000 = 14 053.8
- Mean density = 228 230 000 000 / 6.6743e-11 / (4/3 * pi * 788 400^3) = 1665.86
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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