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Concept
True anomaly
Summary
In celestial mechanics, true anomaly is an angular parameter that defines the position of a body moving along a Keplerian orbit. It is the angle between the direction of periapsis and the current position of the body, as seen from the main focus of the ellipse (the point around which the object orbits).
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^c).
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.
For elliptic orbits, the true anomaly ν can be calculated from orbital state vectors as:
(if r ⋅ v < 0 then replace ν by 2pi − ν)
where:
v is the orbital velocity vector of the orbiting body,
e is the eccentricity vector,
r is the orbital position vector (segment FP in the figure) of the orbiting body.
For circular orbits the true anomaly is undefined, because circular orbits do not have a uniquely determined periapsis. Instead the argument of latitude u is used:
(if rz < 0 then replace u by 2pi − u)
where:
n is a vector pointing towards the ascending node (i.e. the z-component of n is zero).
rz is the z-component of the orbital position vector r
For circular orbits with zero inclination the argument of latitude is also undefined, because there is no uniquely determined line of nodes. One uses the true longitude instead:
(if vx > 0 then replace l by 2pi − l)
where:
rx is the x-component of the orbital position vector r
vx is the x-component of the orbital velocity vector v.
The relation between the true anomaly ν and the eccentric anomaly is:
or using the sine and tangent:
or equivalently:
so
Alternatively, a form of this equation was derived by that avoids numerical issues when the arguments are near , as the two tangents become infinite. Additionally, since and are always in the same quadrant, there will not be any sign problems.
where
so
The true anomaly can be calculated directly from the mean anomaly via a Fourier expansion:
with Bessel functions and parameter .
Official source
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