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`r_(ap) = (1+ e ) a `

Enter a value for all fields

The **Apsis-Apocenter Maximum Distance** calculator computes the maximum distance from the center of gravity in an orbit at apogee based on the semi-major axis (a) and eccentricity (e).

**INSTRUCTION:** Choose units and enter the following:

- (
**a**) This is the semi-major axis of the orbit - (
**e**) This is the eccentricity of the the orbit

**Maximum Distance (r _{ap}):** The calculator returns the distance in meters. However this can be automatically converted to compatible units via the pull-down menu.

The apsides indicate the nearest

and furthest points of an

orbiting body around its host.

- Force of Gravity computes the force of gravity between two bodies.
- Apsis-Apocenter (minimum speed) computes the minimum velocity at the maximum distance of an orbit.
- Apsis-Apocenter (maximum distance) computes the greatest distance from the center of gravity in an orbit.
- Apsis-Pericenter (maximum speed) computes maximum velocity at the minimum distance of an orbit.
- Apsis-Pericenter (minimum distance) computes the minimum distance from the center of mass in an orbit.
- Standard Gravitational Parameter

The **Apsis-Apocenter **is an extreme point in an object's orbit. For elliptical orbits about a larger body, there are two apsides. This is commonly known as the apogee. The apocenter is the point furthest away from the object being orbited.

The formula for the Apsis-Apocenter maximum distance is:

`r_(ap)=(1+e)a`

where:

- r
_{ap}is distance at apogee - e = eccentricity
- a = semi-major axis

Wikipedia (https://en.wikipedia.org/wiki/Apsis)