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The equation to find the semi-minor axis of elliptical orbit is b=a*sqrt(1 - e^2), where b is the semi-minor axis, a is the semi-major axis, and e is the eccentricity. Therefore, using 17.8AU as the semi-major axis and 0.967 as the eccentricity, the semi-minor axis is calculated to be 4.53AU or 6.62*10^11 m.

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14y ago
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13y ago

i hope its 149.5562786 giga-meters because that's the answer i got for my calculus homework

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Q: What is the semi minor axis length of earths elliptic orbit?
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