|  |  GeoAstro Applets |  Astronomy |  Chaos Game |  Java |  Miscel- laneous | 
| The Lagrangian points are the five
                      positions in an orbital configuration where a
                      small object affected only by gravity can
                      theoretically be stationary relative to two larger
                      objects (such as a satellite with respect to the
                      Sun and Earth): | 
An article of N. Treitz inspired me to write this applet.

| A circular orbit
                      around the common center of mass bc of the
                      two bodies is assumed (circular restricted three
                      body problem). The distance of the bodies M and m
                      is a = rM + rm. The barycenter bc of the masses M and m is at distance rM = a·m/(M+m) from the center of M. The three curves of my applet represent the accelerations (positive to the right, negative to the left). At the position x=r of the Lagrange point L1 we have: aM (red) by the mass M (red), at distance r+rM from the center of M | 

|   | Select from the view options of the menu. | 
|    | You may use the key
                  "r", or "R" (shift key and "r", faster) to rotate the system around the
                    center of mass. 
 | 

      
Select "Data Sun-Earth" from the menu:



      
|  | 
| N.
                    Treitz:  am Himmel, Spektrum der
                      Wissenschaft, Oktober 2006 The Lagrange Points The Lagrangian Points for a Planetary
                      Orbit Satellite
in
                      the triangular libration point (example 7) Lagrange
points
                      for two similar masses Satellites Orrery:
Solar
                          System Simulator The Lagrange points in the Earth-Moon
                      system Th. Münch: The
                      Three-Body Problem and the Lagrangian Points
                      system | 
        
Updated:
2023,
            Oct 06