Inactive Tutor answered 12/08/23
Average radius orbit R = (0.829 + 0.992)/2 = 0.9105 AU.
For Earth radius orbit R0 = 1 AU and period T0 = 1 year.
By 3rd Keppler's Law: T2/ T02 = R3/R03. T = T0(R/R0)3/2 = 1year·(0.9105AU/1AU)3/2 = 0.8688 years
Elle B.
asked 12/08/23Duende has an elliptical orbit about the Sun, with a perihelion distance of 0.829 AU and aphelion distance of 0.992 AU. What is the period of its orbit (in years)?
Inactive Tutor answered 12/08/23
Average radius orbit R = (0.829 + 0.992)/2 = 0.9105 AU.
For Earth radius orbit R0 = 1 AU and period T0 = 1 year.
By 3rd Keppler's Law: T2/ T02 = R3/R03. T = T0(R/R0)3/2 = 1year·(0.9105AU/1AU)3/2 = 0.8688 years
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