Planets and Satellites: Kepler's Laws — Question 9

Section 13-6 · Physics pages 2008–2009

Question 9 A projected ellipse need not be an eccentric physical orbit A circular orbit of radius a is viewed at inclination i from face-on. Under orthographic projection its apparent semiaxes are a and a cos i. The observed minor-to-major ratio is .60. face-on projected Schematic; labels, not drawing lengths, specify the data. (a) Find i and the eccentricity of the apparent ellipse. (b) Can that apparent eccentricity be inserted into the physical periapsis formula a(1 −e)?
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Question 9 - Solution A projected ellipse need not be an eccentric physical orbit face-on projected (a) Derivation and calculation The projection ratio is bapp aapp = cos i = .60, i = cos−1(.60) = 53.1301◦. Its apparent eccentricity is eapp = √ 1 −(bapp/aapp)2 = √ 1 −.36 = .80 . (b) Result and interpretation The physical orbit is circular: ephysical = 0, rp = ra = a . Incorrectly using the projected eccentricity would give a(1 −eapp) = .2a, which contradicts the actual constant radius. Inclination changes the image, not the orbit’s source distance. Physical check Viewed face-on, i = 0 and the apparent eccentricity returns to zero; viewing geometry must be removed before orbital interpretation.

Question 9

A projected ellipse need not be an eccentric physical orbit

A circular orbit of radius aa is viewed at inclination ii from face-on. Under orthographic projection its apparent semiaxes are aa and acos⁡ia\cos i. The observed minor-to-major ratio is .60.60.

Diagram shown in the original SVG worksheet.

  1. Find ii and the eccentricity of the apparent ellipse.

  2. Can that apparent eccentricity be inserted into the physical periapsis formula a(1−e)a(1-e)?

Question 9 - Solution

A projected ellipse need not be an eccentric physical orbit

Diagram shown in the original SVG worksheet.

(a) Derivation and calculation

The projection ratio is bappaapp=cos⁡i=.60,i=cos⁡−1(.60)=53.1301∘.\frac{b_{\mathrm{app}}}{a_{\mathrm{app}}}=\cos i=.60,\qquad \boxed{i=\cos^{-1}(.60)=53.1301^\circ}. Its apparent eccentricity is eapp=1−(bapp/aapp)2=1−.36=.80.\boxed{e_{\mathrm{app}}=\sqrt{1-(b_{\mathrm{app}}/a_{\mathrm{app}})^2} =\sqrt{1-.36}=.80}.

(b) Result and interpretation

The physical orbit is circular: ephysical=0,rp=ra=a.e_{\mathrm{physical}}=0,\qquad \boxed{r_p=r_a=a}. Incorrectly using the projected eccentricity would give a(1−eapp)=.2a,a(1-e_{\mathrm{app}})=.2a, which contradicts the actual constant radius. Inclination changes the image, not the orbit’s source distance.

Physical check

Viewed face-on, i=0i=0 and the apparent eccentricity returns to zero; viewing geometry must be removed before orbital interpretation.