Volume 43, Issue 4 No AccessClassical Orbit Element Differences Determination Using Relative Position CoordinatesZhe Dong, Zheng You and Xiaomin ZhangZhe Dong Tsinghua University, 100084 Beijing, People’s Republic of ChinaSearch for more papers by this author, Zheng You Tsinghua University, 100084 Beijing, People’s Republic of ChinaSearch for more papers by this author and Xiaomin Zhang DFH Satellite Corporation, 100086 Beijing, People’s Republic of ChinaSearch for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/1.17172SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous article FiguresReferencesRelatedDetailsSee PDF for referencesCited byMultistep Iterative Tracking Filter for Relative Orbit Determination in an Arbitrarily Orbit31 January 2023Distance-based relative orbital elements determination for formation flying system1 Jan 2016 | Acta Astronautica, Vol. 118Determination and Estimation of Differential Mean Orbital Elements for Formation-Flying MissionsKai Wang, Tong Chen and Shijie Xu10 January 2014 | Journal of Guidance, Control, and Dynamics, Vol. 37, No. 1 What's Popular Volume 43, Number 4July 2006 Metrics Crossmark TopicsAerospace SciencesAstrodynamicsAstronauticsAstronomyCelestial Coordinate SystemCelestial MechanicsOrbital ManeuversOrbital PropertyPlanetary Science and ExplorationPlanetsSpace OrbitSpace Science and Technology KeywordsPerigeeEarth Centered InertialRight AscensionEarthSatellitesSearch AlgorithmEccentric AnomalySpacecraft FormationRelative KinematicsFormation FlyingDigital Published online23 May 2012