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Starlink Downlinks Become a Mock Navigation Constellation

Beam-specific orbit and clock models turn live Ku-band arrivals into meter-scale positioning and nanosecond timing in a field test.

Published Updated Story ID: mp-2026-11-12-012
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Summary

Beam-specific orbit and clock models turn live Ku-band arrivals into meter-scale positioning and nanosecond timing in a field test.

A field experiment extracted time-of-arrival measurements from live Starlink downlinks and paired them with high-fidelity, beam-specific orbit and clock models distributed as though the constellation operator supplied them. The mock fused low-Earth-orbit navigation system reported 95% error bounds of 2.33 meters horizontally, 3.37 meters vertically and 11.19 nanoseconds in timing. Actual errors in the campaign remained inside those bounds despite consumer-grade receiver constraints. The method depends on precision data not available in ordinary opportunistic reception, so it demonstrates an architecture rather than a current public service.

Why it matters

Beam-specific orbit and clock models turn live Ku-band arrivals into meter-scale positioning and nanosecond timing in a field test.

Limits and context

  • The method depends on precision data not available in ordinary opportunistic reception, so it demonstrates an architecture rather than a current public service.

Key claims

  1. Beam-specific orbit and clock models turn live Ku-band arrivals into meter-scale positioning and nanosecond timing in a field test.

    Qualification: The method depends on precision data not available in ordinary opportunistic reception, so it demonstrates an architecture rather than a current public service.

    Evidence: source-2026-11-12-012

Sources

  1. arXiv:2611.13655v1arXiv / Cornell University · primary research

Corrections

No corrections have been recorded for this story.