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  • Analysing the Influence of Photometric Filters on LEO Satellite Orbit Determination

    Paper number

    IAC-24,A6,9,4,x89278

    Author

    Dr. Simone Varanese, Sapienza University of Rome, Italy

    Coauthor

    Mr. Lorenzo Cimino, Sapienza University of Rome, Italy

    Coauthor

    Dr. Lorenzo Mariani, Sapienza University of Rome, Italy

    Coauthor

    Mr. Matteo Rossetti, University of Rome “La Sapienza”, Italy

    Coauthor

    Dr. Gaetano Zarcone, Sapienza University of Rome, Italy

    Coauthor

    Ms. Mascia Bucciarelli, Sapienza University of Rome, Italy

    Coauthor

    Dr. Fabrizio Piergentili, Sapienza University of Rome, Italy

    Coauthor

    Dr. Thomas Kelecy, United States

    Year

    2024

    Abstract
    As the space industry continues to populate the orbits near Earth, the challenge of monitoring and managing Resident Space Objects (RSOs) has become increasingly complex. The proliferation of satellites and space debris necessitates a high level of precision in tracking RSOs within crowded orbits, such as Low Earth Orbit (LEO). Space Surveillance and Tracking (SST) services are indispensable in this context, offering crucial capabilities for the accurate mapping of object trajectories, thereby ensuring the operational safety and long-term sustainability of activities in LEO.
    In response to these challenges, this paper, conducted by the research team at Sapienza Space Systems and Space Surveillance Laboratory (S5Lab), proposes a methodology for processing and analysing ground-based optical observations of LEO satellites for Orbit Determination (OD) purposes. The objective of this study is to evaluate the benefits and limitations of using optical measurements obtained through various photometric filters for precise OD. Depending on the RSOs’ surface properties, shape, and orientation, the selection of a particular filter may influence the accuracy of satellite centroid detection. By optimizing the choice of optical filter to match the specific electromagnetic spectrum segment most relevant to the target, this approach seeks to enhance the OD accuracy through more precise photometric observations. This research presents a comprehensive analysis of the collected observational data and an astrometric analysis, employing an angles-only OD technique for precise orbit estimation of LEO satellites.
    The proposed methodology focuses on the study of satellites for which accurate orbit data are available, such as Sentinel and Starlink satellites. This choice enables a direct comparison between the estimated orbits derived from the optical data and the satellites' true known states. Such comparative analysis is essential for validating the accuracy and reliability of the proposed OD procedure. Observational data for this study is acquired from telescopes directly managed by the S5Lab research team, using the Johnson V and Sloan g’, r’, i’ filters. These observations are carried out during multiple passes and nights for LEO satellites, both consecutive and non-consecutive nights, to ensure a comprehensive dataset for analysis and to assess orbit accuracy sensitivity to tracking cadence, revisits, and duration. The OD accuracy of the results is compared between data collected using the different filters to assess the performance dependence on the selected filter.
    Abstract document

    IAC-24,A6,9,4,x89278.brief.pdf

    Manuscript document

    IAC-24,A6,9,4,x89278.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.