SLR Validation and Evaluation of BDS-3 MEO Satellite Precise Orbits

Author:

Li Ran12ORCID,Wang Chen3ORCID,Ma Hongyang4ORCID,Zhou Yu2,Tang Chengpan5,Wu Ziqian1ORCID,Yang Guang2,Zhang Xiaolin6

Affiliation:

1. State Key Laboratory of Satellite Navigation System and Equipment Technology, Shijiazhuang 050081, China

2. Aerospace Information Research Institute (AIR), Chinese Academy of Sciences (CAS), Beijing 100094, China

3. School of Geological Engineering and Geomatics, Chang’an University, Xi’an 710064, China

4. School of Geomatics Science and Technology, Nanjing Tech University, Nanjing 210037, China

5. Shanghai Astronomical Observatory, Chinese Academy of Sciences, Shanghai 200030, China

6. Beijing Satellite Navigation Center, Beijing 100094, China

Abstract

Starting from February 2023, the International Laser Ranging Service (ILRS) began releasing satellite laser ranging (SLR) data for all BeiDou global navigation satellite system (BDS-3) medium earth orbit (MEO) satellites. SLR data serve as the best external reference for validating satellite orbits, providing a basis for comprehensive evaluation of the BDS-3 satellite orbit. We utilized the SLR data from February to May 2023 to comprehensively evaluate the orbits of BDS-3 MEO satellites from different analysis centers (ACs). The results show that, whether during the eclipse season or the yaw maneuver season, the accuracy was not significantly decreased in the BDS-3 MEO orbit products released from the Center for Orbit Determination in Europe (CODE), Wuhan University (WHU), and the Deutsches GeoForschungsZentrum (GFZ) ACs, and the STD (Standard Deviation) of SLR residuals of those three ACs are all less than 5 cm. Among these, CODE had the smallest SLR residuals, with 9% and 12% improvement over WHU and GFZ, respectively. Moreover, the WHU precise orbits exhibit the smallest systematic biases, whether during non-eclipse seasons, eclipse seasons, or satellite yaw maneuver seasons. Additionally, we found some BDS-3 satellites (C32, C33, C34, C35, C45, and C46) exhibit orbit errors related to the Sun elongation angle, which indicates that continued effort for the refinement of the non-conservative force model further to improve the orbit accuracy of BDS-3 MEO satellites are in need.

Funder

Beijing Natural Science Foundation

State Key Laboratory of Satellite Navigation System and Equipment Technology

National Natural Science Foundation of China

Foundation of Science and Technology on Complex Electronic System Simulation Laboratory

Youth Innovation Promotion Association, CAS

National Key Research Program of China

Publisher

MDPI AG

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