Use Kuiper Belt Object Haumea's eccentricity, e = 0.189, semimajor axis, a = 43.3 AU, and Period, P = 285 yrs, values to a) calculate its perihelion and aphelion distances with Dp = a (1 e) and D₂ = a (1 + e), b) verify if Haumea's a and P satisfy Kepler's third law for all objects orbiting the Sun: p2 = a³. Show your work. Paragraph V Lato (Recom... a) Dp= Da= b) p2 = BI 19px... v U✓ A L ป Q«/> 58° ...

Use Kuiper Belt Object Haumea's eccentricity, e = 0.189, semimajor axis, a = 43.3 AU, and Period, P = 285 yrs, values to a) calculate its perihelion and aphelion distances with Dp = a (1 e) and D₂ = a (1 + e), b) verify if Haumea's a and P satisfy Kepler's third law for all objects orbiting the Sun: p2 = a³. Show your work. Paragraph V Lato (Recom... a) Dp= Da= b) p2 = BI 19px... v U✓ A L ป Q«/> 58° ...