1. Correcting TLEs at epoch: Application to the GPS constellation
- Author
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Romain Lucken, Delphine Ly, Damien Giolito, Laboratoire de Physique des Plasmas (LPP), Observatoire de Paris, and Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-École polytechnique (X)-Sorbonne Université (SU)-Université Paris-Saclay-Centre National de la Recherche Scientifique (CNRS)
- Subjects
020301 aerospace & aeronautics ,Series (stratigraphy) ,Computer science ,business.industry ,Epoch (reference date) ,Conjunction (astronomy) ,Aerospace Engineering ,02 engineering and technology ,Geodesy ,01 natural sciences ,[SPI]Engineering Sciences [physics] ,0203 mechanical engineering ,0103 physical sciences ,Global Positioning System ,Satellite ,Safety, Risk, Reliability and Quality ,business ,010303 astronomy & astrophysics ,Medium Earth orbit ,Constellation ,Space debris - Abstract
Two-Line Elements (TLEs) issued by the space-track catalog are still the most extensive public data source for space debris tracking to date. However, TLEs accuracy at epoch is typically larger than 1 km in Low Earth Orbit (LEO) and 3 km in Medium Earth Orbit (MEO). Therefore, TLEs are too coarse to enable collision avoidance maneuvers. The present work aims at correcting TLEs orbits at epoch to enable operational conjunction assessment and help satellite operators better protect their assets at moderate cost. Using only Moon-Earth and Sun-Earth distance time series, as well as 2018 TLE data for 14 GPS satellites and SGP4 propagation over a short period, we were able to correct the TLEs of the 29 operational GPS satellites by 65% on average for year 2019, reducing the 3D RMS error at epoch from 2.2 km to 680 m. In other words, we improved TLEs accuracy from 5 km to 1.5 km with a 95% confidence level.
- Published
- 2020
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