Improved orbit predictions using two-line elements

TL;DR

This paper presents a method to significantly improve orbit prediction accuracy using least-squares fitting of TLE data and high-precision propagation, enhancing collision avoidance capabilities in space debris management.

Contribution

The paper introduces a novel orbit prediction method that achieves a tenfold accuracy improvement over traditional TLE propagation, aiding collision avoidance systems.

Findings

Predicted range error increases at about 100 meters per day.

Method improves orbit prediction accuracy by approximately ten times.

Potential for operational collision avoidance with debris.

Abstract

The density of orbital space debris constitutes an increasing environmental challenge. There are three ways to alleviate the problem: debris mitigation, debris removal and collision avoidance. This paper addresses collision avoidance, by describing a method that contributes to achieving a requisite increase in orbit prediction accuracy. Batch least-squares differential correction is applied to the publicly available two-line element (TLE) catalog of space objects. Using a high-precision numerical propagator, we fit an orbit to state vectors derived from successive TLEs. We then propagate the fitted orbit further forward in time. These predictions are compared to precision ephemeris data derived from the International Laser Ranging Service (ILRS) for several satellites, including objects in the congested sun-synchronous orbital region. The method leads to a predicted range error that increases at a typical rate of 100 meters per day, approximately a 10-fold improvement over TLE's propagated with their associated analytic propagator (SGP4). Corresponding improvements for debris trajectories could potentially provide initial conjunction analysis sufficiently accurate for an operationally viable collision avoidance system. We discuss additional optimization and the computational requirements for applying all-on-all conjunction analysis to the whole TLE catalog, present and near future. Finally, we outline a scheme for debris-debris collision avoidance that may become practicable given these developments.