Mechanics of particles and systems Orbital mechanics Problem
Lambert's problem
Builds on Kepler orbitKepler problem
Problem
Let , let be two positions that are not on a common line through , and let . Find the Kepler orbits with gravitational parameter that go from to in time . That is, find the velocities such that the solution of the Kepler problem with and satisfies .
Remarks
Lambert's theorem states that the time of flight depends only on the semi-major axis of the orbit, on the sum and on the chord . This reduces the problem to one scalar equation for , or for a related variable. For a fixed direction of motion and a transfer of less than one revolution, the problem has exactly one solution. For longer times of flight there are also solutions that make one or more full revolutions first. The problem is the core of the planning of interplanetary trajectories and of rendezvous, and of the determination of an orbit from two positions. Practical solvers use universal variables and Newton-type iterations.
Reading path
To understand this page from the ground up, read these 7 pages in order. The foundations come first.
Show the path as a graph
- no evidence level
- Conic section concept
- Ellipse concept
- First integral concept
- Focus of a conic concept
- Kepler orbit concept
- Kepler problem example
- Lambert's problem problem
Further reading
About this page
| Tag | NY83V7S6VP |
|---|---|
| URI | m2://NY83V7S6VP |
| Kind | problem |
| Writing | W0 stub |
| MSC | 70F05, 70M20 |
| Status | This copy of the site has no build data. Run m2 status NY83V7S6VP. |
| About | Kepler orbit |
| Uses | Kepler orbit, Kepler problem |
| Same as | |
| Changed | 3 November 2026 |
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