ESA’s process for the identification and assessment of high-risk conjunction events |
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Authors: | T. Flohrer H. Krag H. Klinkrad |
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Affiliation: | 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 |
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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. |
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Keywords: | Collision avoidance Space debris Space surveillance Radar tracking Orbit improvement ENIVSAT COSMOS |
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