Velocity of Satellite at Apogee in Elliptical Orbits Formulas

Velocity of Satellite at Apogee refers to the speed at which a satellite travels when it is at its farthest point from the celestial body it is orbiting, such as Earth. And is denoted by v_apogee. Velocity of Satellite at Apogee is usually measured using the Kilometer per Second for Speed. Note that the value of Velocity of Satellite at Apogee is always positive.

Formulas to find Velocity of Satellite at Apogee in Elliptical Orbits

fxApogee Velocity in Elliptic Orbit Given Angular Momentum and Apogee RadiusGo

Elliptical Orbits formulas that make use of Velocity of Satellite at Apogee

fxAngular Momentum in Elliptic Orbit Given Apogee Radius and Apogee VelocityGo

List of variables in Elliptical Orbits formulas

fx Angular Momentum of Elliptic Orbit Go

fx Apogee Radius in Elliptic Orbit Go

FAQ

What is the Velocity of Satellite at Apogee?

Velocity of Satellite at Apogee refers to the speed at which a satellite travels when it is at its farthest point from the celestial body it is orbiting, such as Earth. Velocity of Satellite at Apogee is usually measured using the Kilometer per Second for Speed. Note that the value of Velocity of Satellite at Apogee is always positive.

Can the Velocity of Satellite at Apogee be negative?

No, the Velocity of Satellite at Apogee, measured in Speed cannot be negative.

What unit is used to measure Velocity of Satellite at Apogee?

Velocity of Satellite at Apogee is usually measured using the Kilometer per Second[km/s] for Speed. Meter per Second[km/s], Meter per Minute[km/s], Meter per Hour[km/s] are the few other units in which Velocity of Satellite at Apogee can be measured.

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