orbiidimanööver elliptilisel orbiidil kosmoseaparaadi üleviimiseks ühelt orbiidilt teisele või ühe taevakeha gravitatsiooniväljast teise taevakeha gravitatsioonivälja minimaalse kütusekuluga
orbital maneuver used to transfer a spacecraft between two orbits of different altitudes around a central body or around two different bodies
This existing solar orbit must be adjusted to cause it to take the spacecraft to Mars: The desired orbit's perihelion (closest approach to the Sun) will be at the distance of Earth's orbit, and the aphelion (farthest distance from the Sun) will be at the distance of Mars' orbit. This is called a Hohmann Transfer orbit.
