The orbit in time, part 2: a position angle that changes linearly in time.

Why Another Anomaly

  • The true anomaly 𝜃 is useful geometrically, but its time dependence is unknown
  • The mean anomaly 𝑀 will change linearly in time

Areal Angle

  • Define 𝑀 as the fraction of the ellipse’s area swept out since perigee, times 2𝜋 (an “areal angle”):
    • 𝑀=𝐴(𝑡)𝜋𝑎𝑏⋅2𝜋=2𝐴(𝑡)𝑎𝑏
  • By Kepler’s second law 𝐴(𝑡) grows linearly in time, so

Mean Motion

  • ̇𝑀=𝑛=const
  • Mean motion 𝑛 is a constant

Mean Anomaly in Time

  • Measuring time from perigee passage 𝑡𝑝:
    • 𝑀(𝑡)=𝑛(𝑡−𝑡𝑝)
  • After one orbital period the full area is swept out:
    • 2𝜋=𝑀(𝒫︀)=𝑛𝒫︀⇒𝑛=2𝜋𝒫︀
  • With 𝒫︀=2𝜋𝑎32√𝜇 this is 𝑛=√𝜇𝑎3
  • The relationship between mean and true anomaly is complex: it goes through the eccentric anomaly and Kepler’s Equation