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Eccentricity (orbit)__NOTOC__ :''This page refers to eccentricity in astrodynamics. For other uses, see the disambiguation page eccentricity.'' In astrodynamics, under standard assumptions in astrodynamics any orbit must be of conic section shape. The eccentricity (mathematics) of this conic section, the '''orbit's eccentricity, is an important parameter of the orbit that defines its absolute shape. Eccentricity may be interpreted as a measure of how much this shape deviates from a circle. Under standard assumptions in astrodynamics eccentricity () is strictly defined for all circular orbit, elliptic orbit, parabolic trajectory and hyperbolic trajectory orbits and may take following values: *for circular orbits: , *for elliptic orbits: Eccentricity''' of an orbit can be calculated from orbital state vectors as a magnitude (mathematics) of eccentricity vector: : See other meanings of words starting from letter: EEA | EB | EC | ED | EF | EG | EH | EI | EJ | EK | EL | EM | EN | EO | EP | ER | ES | ET | EU | EW | EX | EY | EZ |Words begining with Eccentricity_(orbit): Eccentricity_(orbit) |
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