Calculate the eccentricity, e, of Haumea's orbit knowing that its semimajor axis, a = 43.3 AU, and its aphelion distance, D, = 51.5 AU. Start by solving for "e" the formula for its aphelion distance: D₁ = a (1 + e). Wait with plugging in the values until you have isolated "e" on one side of the equation. Hint: In this equation, "e" is added to the 1 so you can leave "e" on the right side since it is already in its positive form. Show your work. Paragraph Lato (Recom... V V B I 19px... e= U v 7 A/ <> ► 11 OB 0⁰ + v ... 11.

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Calculate the eccentricity, e, of Haumea's orbit knowing that its semimajor axis, a = 43.3 AU, and its aphelion
distance, D₂ = 51.5 AU. Start by solving for "e" the formula for its aphelion distance: D₁ = a (1 + c). Wait with
plugging in the values until you have isolated "e" on one side of the equation. Hint: In this equation, "e" is added to
the 1 so you can leave "e" on the right side since it is already in its positive form. Show your work.
Paragraph V
Lato (Recom... V
e
B I
19px...
U v
T
A/
<>
► 11
OB
0⁰
+ v
...
11.
Transcribed Image Text:Calculate the eccentricity, e, of Haumea's orbit knowing that its semimajor axis, a = 43.3 AU, and its aphelion distance, D₂ = 51.5 AU. Start by solving for "e" the formula for its aphelion distance: D₁ = a (1 + c). Wait with plugging in the values until you have isolated "e" on one side of the equation. Hint: In this equation, "e" is added to the 1 so you can leave "e" on the right side since it is already in its positive form. Show your work. Paragraph V Lato (Recom... V e B I 19px... U v T A/ <> ► 11 OB 0⁰ + v ... 11.
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