DART Mission Simulation

Settings

Grid
Central body M
Body m
Orbit
Orbit type:
Time t: 0h 00m 00s
ucirc = √(GM/r₀):
uesc = √(2GM/r₀):
Energy E = u²/2 − GM/r:
Distance M–m (r):
Eccentricity e:
Period T:

Charts

Total energy E(t). Units: J/kg - h