๐Ÿ›ฐ๏ธ Neuravant Research ยท Space Domain Awareness

ORBIT-FM

A sovereign foundation model of orbital behaviour. Every object in orbit leaves a public behavioural trace โ€” continuous two-line element records since 1957, covering 60,000+ catalogued objects. ORBIT-FM is a research programme to pretrain a single model on that record, fused with space-weather indices, so that multiple Space Domain Awareness capabilities emerge from one model โ€” trained entirely on UK-owned, on-premises compute.

F1 0.628 Phase-0 prototype vs 0.568 for the classical manoeuvre detector, on strictly held-out months
+9 pts additional recall at matched precision over the classical baseline
574 real manoeuvre events as ground truth, derived from CNES/IDS DORIS precise-orbit records
100% UK trained on our own on-premises NVIDIA DGX Spark cluster โ€” no foreign cloud dependency

Phase 0: the first gate is passed

Evaluation precedes scale โ€” every claim below is backed by a frozen, versioned evidence set.

โœ“ Gate passed ยท August 2026

A self-funded Phase-0 prototype encodes orbital histories as residuals against an SGP4 physics baseline โ€” the model learns precisely what physics misses: manoeuvres, drag error, sensor artefacts. Trained on 335 low-Earth-orbit objects, it was evaluated on strictly held-out months against 574 real manoeuvre events derived from CNES/IDS DORIS precise-orbit records.

Result: F1 0.628 versus 0.568 for the standard classical detector, with equal-or-better recall at every matched precision operating point โ€” up to nine percentage points more. The result held across two model configurations trained independently, one per cluster node. Negative results are reported alongside positive ones.

Read the Phase-0 technical report โ†’

One model, many capabilities

From a single pretrained model of orbital behaviour, SDA capabilities emerge with minimal task-specific engineering.

๐Ÿ›ฐ๏ธ
Manoeuvre detection
Station-keeping, relocations and reboosts detected across whole constellations โ€” validated against precise-orbit ground truth.
โš ๏ธ
Anomaly & fault flagging
Behavioural anomalies surfaced with lead time, validated against documented satellite failures.
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Behavioural identification
Objects identified by how they behave โ€” a complement to sensor-based positive identification.
๐Ÿ“ก
Payload-activity characterisation
Activity patterns across object families and constellations, learned population-wide rather than per object.
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Lifetime & re-entry windows
Drag-aware orbital-lifetime estimation and tighter re-entry windows, benchmarked against historical TIP messages.
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Propagation-error correction
Measurable correction of SGP4 propagation error at 1โ€“7-day horizons, strengthening conjunction screening.

Sovereign by construction

Not a policy aspiration โ€” an engineering property of how the model is built and delivered.

๐Ÿ‡ฌ๐Ÿ‡ง UK-owned compute, end to end

  • Entire pretraining programme runs on our own two-node NVIDIA DGX Spark cluster โ€” on-premises, in the UK.
  • No operational data, model weights or capability roadmap depends on foreign cloud infrastructure.
  • Deliverable to government users as an air-gapped, on-premises licence on the same class of compact hardware it was trained on.

๐Ÿงญ Programme status

  • Phase 0 complete (August 2026): prototype beats the classical manoeuvre detector on held-out data.
  • Expression of Interest submitted to UKSA's National Space Innovation Programme Call 3 (Space Domain Awareness, August 2026).
  • Application to ESA Business Incubation Centre UK in preparation.
  • A public, versioned SDA benchmark and labelled manoeuvre dataset are planned for release.

Work with us

We are engaging an astrodynamics consultant (SGP4 baseline verification, manoeuvre-label validation, orbit-regime stratification) and talking to early pilot partners โ€” SSA platforms, insurers and government SDA users. If that's you, we'd like to hear from you.

team@neuravant.ai