[SA1-2-10-1] Keplerian elements (Two-Body Problem)

Keplerian elements describe ideal two-body orbital motion using semimajor axis, eccentricity, inclination, right ascension of ascending node, argument of periapis, and true anomaly. They form a standard orbit representation.

External resources

• Sanz Subirana, J., Juan Zornoza, J.M. and Hernández-Pajares, M. (2013) GNSS Data Processing, Vol. 1: Fundamentals and Algorithms (ESA TM-23/1, May 2013) ESA Communications, Noordwijk, The Netherlands.

Outgoing relations

• [SA1-2-10-1] Keplerian elements (Two-Body Problem) is subconcept of [SA1-2-10] Orbital elements

Contributors

• Adria Rovira Garcia
  https://wwwdfen.webs.upc.edu/php_pagina_web/person_id.php?id=adria.rovira
• Adriano Camps
  https://prs.upc.edu/2018/08/17/adriano-camps/