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° ...
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Transcribed Image Text:a) Dp =
Da =
b) p² =
a³-
Transcribed Image Text: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
Lato (Recom...
a) Dp=
Da=
V
b) p2=
BI
19px... v
U A
L
EQ </>
58°
...
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