The true anomaly is the angle at the focus from periapsis to the current position of an orbiting body, measured in the direction of motion.
Ancestors (7)
Incoming links (29)
- Barker equation
- Conjunction longitude from a transit time lag
- Exoplanet transit
- Facing geometry of synchronous rotation
- Gauss planetary equation for the semi-major axis
- High-eccentricity angular-speed crossover
- Kepler's first law
- Line density on a Kepler orbit
- Orbit averaging
- Osculating-element evolution under isotropic mass loss
- Past exam of the mathematics course of the University of Cambridge / 2010 / iii / Paper 61 / 1 / Solution
- Past exam of the mathematics course of the University of Cambridge / 2012 / iii / Paper 64 / 1 / Solution
- Past exam of the mathematics course of the University of Cambridge / 2012 / iii / Paper 64 / 2 / Solution
- Past exam of the mathematics course of the University of Cambridge / 2015 / iii / Paper 65 / 2 / Solution
- Past exam of the mathematics course of the University of Cambridge / 2016 / iii / Paper 316 / 1 / Solution
- Past exam of the mathematics course of the University of Cambridge / 2017 / iii / Paper 316 / 1 / ii / Solution
- Past exam of the mathematics course of the University of Cambridge / 2017 / iii / Paper 316 / 1 / i / Solution
- Past exam of the mathematics course of the University of Cambridge / 2017 / iii / Paper 316 / 2 / i / Solution
- Past exam of the mathematics course of the University of Cambridge / 2017 / iii / Paper 316 / 3 / vi / Solution
- Past exam of the mathematics course of the University of Cambridge / 2017 / iii / Paper 316 / 4 / ii / Solution
- Past exam of the mathematics course of the University of Cambridge / 2018 / iii / Paper 316 / 3 / vii / Solution
- Past exam of the mathematics course of the University of Cambridge / 2018 / iii / Paper 316 / 4 / iii / Solution
- Past exam of the mathematics course of the University of Cambridge / 2018 / iii / Paper 316 / 4 / i / Solution
- Past exam of the mathematics course of the University of Cambridge / 2022 / iii / Paper 322 / 2 / Solution
- Pericentre-to-crossover flight time
- Polar equation of a Kepler orbit
- Resonant conjunction geometry
- Tangential launch trajectories across the escape threshold
- True longitude
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