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ESA’s process for the identification and assessment of high-risk conjunction events
Authors:T Flohrer  H Krag  H Klinkrad
Institution:1. Aboa Space Research Oy (ASRO) at ESA/ESOC Space Debris Office, Robert-Bosch-Straße 5, DE-64293 Darmstadt, Germany;2. ESA/ESOC Space Debris Office, Robert-Bosch-Straße 5, DE-64293 Darmstadt, Germany
Abstract:ESA’s Space Debris Office provides an operational service for the assessment of collision risks of ESA satellites. Currently, the ENVISAT and ERS-2 missions in low Earth orbits are covered by this service. If an upcoming high-risk conjunction event is predicted based on analysis of Two-Line Element (TLE) data from the US Space Surveillance Network, then independent tracking data of the potential high-risk conjunction object are acquired to improve the knowledge of its orbit. This improved knowledge and the associated small error covariances derived from the orbit determination process scale down the position error ellipsoid at the conjunction epoch. Hence, for the same miss-distance, in most cases an avoidance manoeuvre can be suppressed with an acceptable residual risk.
Keywords:Collision avoidance  Space debris  Space surveillance  Radar tracking  Orbit improvement  ENIVSAT  COSMOS
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