Compute rper and l'ap for the orbit of Earth, which has eccentricity e = 0.017 and a semi-major axis of a = 1.5 × 10° km. (Use decimal notation. Give your answer to three decimal places.) "per a x10® km lap x108 km

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Compute rper
and
l'ap
for the orbit of Earth, which has eccentricity e = 0.017 and a semi-major axis of a = 1.5 × 10° km.
(Use decimal notation. Give your answer to three decimal places.)
"per a
x10® km
lap
x108 km
Transcribed Image Text:Compute rper and l'ap for the orbit of Earth, which has eccentricity e = 0.017 and a semi-major axis of a = 1.5 × 10° km. (Use decimal notation. Give your answer to three decimal places.) "per a x10® km lap x108 km
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