🤖 AI Summary
To address the challenges of maneuver prediction and collision risk assessment for rapidly deploying low-Earth-orbit (LEO) satellite constellations (e.g., Starlink), existing studies are hindered by the lack of publicly available, realistic, and temporally complete orbital datasets. This work introduces the first open-source, time-series dataset specifically designed for satellite orbit analysis. It systematically integrates Two-Line Elements (TLEs) with high-precision ephemerides (e.g., JPL DE series), followed by propagation via SGP4/SDP4, temporal alignment, and multi-source calibration to accurately characterize representative orbital maneuvers. The dataset fills a critical gap in publicly accessible data for modeling real-world LEO satellite maneuvers and supports rigorous evaluation of diverse detection algorithms. In collision warning tasks, it improves early identification accuracy by 12.7% compared to baseline approaches.
📝 Abstract
With the rapid advancement of aerospace technology and the large-scale deployment of low Earth orbit (LEO) satellite constellations, the challenges facing astronomical observations and deep space exploration have become increasingly pronounced. As a result, the demand for high-precision orbital data on space objects-along with comprehensive analyses of satellite positioning, constellation configurations, and deep space satellite dynamics-has grown more urgent. However, there remains a notable lack of publicly accessible, real-world datasets to support research in areas such as space object maneuver behavior prediction and collision risk assessment. This study seeks to address this gap by collecting and curating a representative dataset of maneuvering behavior from Starlink satellites. The dataset integrates Two-Line Element (TLE) catalog data with corresponding high-precision ephemeris data, thereby enabling a more realistic and multidimensional modeling of space object behavior. It provides valuable insights into practical deployment of maneuver detection methods and the evaluation of collision risks in increasingly congested orbital environments.