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  2. Eccentric anomaly - Wikipedia

    en.wikipedia.org/wiki/Eccentric_anomaly

    In orbital mechanics, the eccentric anomaly is an angular parameter that defines the position of a body that is moving along an elliptic Kepler orbit.The eccentric anomaly is one of three angular parameters ("anomalies") that define a position along an orbit, the other two being the true anomaly and the mean anomaly.

  3. Mean anomaly - Wikipedia

    en.wikipedia.org/wiki/Mean_anomaly

    where M 0 is the mean anomaly at the epoch t 0, which may or may not coincide with τ, the time of pericenter passage. The classical method of finding the position of an object in an elliptical orbit from a set of orbital elements is to calculate the mean anomaly by this equation, and then to solve Kepler's equation for the eccentric anomaly.

  4. Kepler's equation - Wikipedia

    en.wikipedia.org/wiki/Kepler's_equation

    where is the mean anomaly, is the eccentric anomaly, and is the eccentricity. The 'eccentric anomaly' E {\displaystyle E} is useful to compute the position of a point moving in a Keplerian orbit.

  5. Orbital elements - Wikipedia

    en.wikipedia.org/wiki/Orbital_elements

    Unlike with mean anomaly, mean longitude is defined relative to the vernal point, which means it is defined for circular orbits. Eccentric anomaly at epoch (E 0) — the eccentric anomaly at the epoch time. Eccentric anomaly is defined at the angular displacement along the auxiliary circle of the ellipse (circle tangent to the ellipse both at ...

  6. Equation of the center - Wikipedia

    en.wikipedia.org/wiki/Equation_of_the_center

    On the computation of the eccentric anomaly, equation of the centre and radius vector of a planet, in terms of the mean anomaly and eccentricity. Monthly Notices of the Royal Astronomical Society, Vol. 43, p. 345. Gives the equation of the center to order e 12. Morrison, J. (1883). Errata. Monthly Notices of the Royal Astronomical Society, Vol ...

  7. True anomaly - Wikipedia

    en.wikipedia.org/wiki/True_anomaly

    The true anomaly is usually denoted by the Greek letters ν or θ, or the Latin letter f, and is usually restricted to the range 0–360° (0–2π rad). The true anomaly f is one of three angular parameters (anomalies) that defines a position along an orbit, the other two being the eccentric anomaly and the mean anomaly.

  8. NYT ‘Connections’ Hints and Answers Today, Wednesday, February 19

    www.aol.com/nyt-connections-hints-answers-today...

    We mean it. Read no further until you really want some clues or you've completely given up and want the answers ASAP. Get ready for all of today's NYT 'Connections’ hints and answers for #619 on ...

  9. Mean motion - Wikipedia

    en.wikipedia.org/wiki/Mean_motion

    where M 1 and M 0 are the mean anomalies at particular points in time, and Δt (≡ t 1-t 0) is the time elapsed between the two. M 0 is referred to as the mean anomaly at epoch t 0, and Δt is the time since epoch.