Randomized trial investigates a new radar approach for cataloguing orbital debris, suggesting significant improvements.
Low Earth Orbit holds an estimated one million fragments between one and ten centimeters across. None of them appear in any catalogue. At orbital velocity, a fragment this size carries enough kinetic energy to destroy an operational spacecraft on impact, yet it sits below the detection floor of every ground-based radar and optical sensor running at a useful revisit rate. This paper asks why incremental upgrades to that ground-based architecture, built around a handful of large, fixed sensors, cannot close the gap, then proposes an alternative: a distributed constellation of low-cost CubeSats carrying small bistatic radar transceivers and wide-field optical sensors, cooperating through inter-satellite ranging to detect, triangulate, and catalogue debris from orbit rather than from the ground. Orbital geometry, radar link budget, onboard processing load, and data-fusion architecture are worked through in enough detail to run on hardware already flying on educational and commercial small satellites today. The concept is measured against the present ground-based model on coverage, cost, and resilience, and the paper closes with the specific steps needed to fly a two-satellite proof-of-concept.
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K. R. Sasmitha Kaushan Jayasiri (2026) studied this question.
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