Orbital inclination change Guide, Meaning , Facts, Information and Description

Orbital inclination change is a orbital maneuver aimed at changing inclination of orbiting body's orbit. This meneuver requires usually delta-v.

Maximum efficiency of inclinatin change is achieved at apoapsis where orbital velocity is the lowest.

Calculation

Delta-v () required for given inclination change () can be calculated as follows:

where:

• is orbiting body's velocity at orbital position where maneuver takes place.

See also

• Inclination
• Orbital maneuver

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