OrbitReclaim is pre-flight and developing a proposed dual-use rendezvous concept. Starfish Space's $52.5M Space Force award and LeoLabs' $60M STRATFI are market context only; they do not indicate an OrbitReclaim award, relationship, or operational result.
OrbitReclaim's OLE v2.0 nano-swarm is proposed as more than an environmental cleanup concept: it is an in-development dual-use rendezvous and proximity-operations architecture with prospective commercial and defense mission profiles. A future five-drone formation could be designed to inspect and characterize a 1–10kg fragment for a constellation operator or support on-orbit servicing and inspection scenarios for a government mission. This is outreach positioning, not a current customer pipeline, activated relationship, or operational capability. Targeting Space Force, NRL and NASA NIAC research calls.
The public Monte Carlo collision model and Kessler cascade stress test are simulation-only physics artifacts — not validation of the OrbitReclaim swarm consensus, coordination algorithm, or flight system. Those simulations use Clohessy-Wiltshire (CW) relative-motion equations, a closed-form framework for modeling chaser-spacecraft rendezvous, formation-keeping, and proximity operations in LEO. The 2,000-object catalog and modeled collision probabilities are illustrative; they are not current telemetry or mission-grade predictions. The proprietary swarm consensus and decentralized GNC stack remain in development and under validation. No current government relationship, customer, funding award, flight heritage, or on-orbit result is implied. Consensus and coordination algorithm: proprietary to Orbital Reclaim LLC / Polsia Inc.; not licensed under any open-source or community-extensible terms.
The proposed five-drone mission concept is paired with a v3.0 cold-gas chassis design that remains in development and under validation. It is an engineering concept, not a shipped or flight-qualified hardware artifact, and no current mission is funded to fly. Chassis design, propellant manifold stack, and rendezvous sequence: proprietary to Orbital Reclaim LLC / Polsia Inc.; not licensed under any open-source or community-extensible terms; full schematics released only under NDA-protected technical interchange.
Positioned against the existing IQT portfolio, OLE v2.0 runs alongside ClearSpace (large-object deorbit), Starfish Space (tug-style remediation), and Kurs Orbital (inspection) — filling the small-object / tight-formation lane none of them address, rather than competing head-on with any single one.
The FCC's 2022 five-year-disposal rule and public Space Force, SpaceWERX, and SDA program activity provide context for prospective outreach. They do not establish an OrbitReclaim relationship, contract, award, or operational result. The dual-use framing is a research and partnership hypothesis for future validation and funding discussions.
Space Force, SpaceWERX, SDA, STRATFI, Orbital Prime, and In-Q-Tel are prospective outreach routes only. OrbitReclaim has no current government relationship, customer, funding award, flight heritage, or on-orbit result implied by this page. Any commercial or defense mission profile would require future funding, hardware development, validation, approvals, and an executed agreement.
This page is the canonical pre-read for In-Q-Tel outreach. Share it ahead of any intro call. Inbound capture happens on the demo form.
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The four questions below come up in every In-Q-Tel, Shield Capital, and Seraphim first-pass review. Answers are short on purpose; deeper material is on the linked technical-narrative page.
The OrbitReclaim / Polsia proprietary swarm consensus and coordination algorithm — implemented as a decentralized GNC stack — together with the v3.0 cold-gas chassis, the propellant manifold stack, the rendezvous sequence, and the underlying engineering schematics, are held in-house and are not licensed under any open-source or community-extensible terms. Schematics and detailed technical material are released only under NDA-protected technical interchange at the appropriate counterparty stage.
Consensus and coordination algorithm: proprietary to Orbital Reclaim LLC / Polsia Inc.; not licensed under any open-source or community-extensible terms.
OrbitReclaim proposes a rideshare secondary-payload architecture rather than a dedicated launch-license vehicle program. If the concept advances, FAA/AST (Federal Aviation Administration / Office of Commercial Space Transportation) payload review and the FCC's 2022 five-year-disposal rule would shape the future regulatory path; no approval or launch is claimed.
The proposed sequence is hardware-in-the-loop validation, then FAA/AST payload review, FCC RPO characterization, and an ITAR/EAR export-control baseline if funding and mission partners are secured. Any commercial or defense mission would depend on those future approvals and executed agreements.
OLE v2.0 has three public development references, not flight heritage. First, the v3.0 cold-gas chassis is a proposed bus design in development, not a shipped or flight-qualified artifact. Second, the MIT-licensed Monte Carlo collision model and Kessler cascade stress test are simulation-only physics models, with the consensus and coordination algorithm explicitly carved out as proprietary. Third, the on-board GNC stack is planned for hardware-in-the-loop validation against the closed-form CW regime referenced in the narrative and glossary.
The carve-out is deliberate: the open-source physics models are the validator; the consensus and coordination layer that protects against single-point failure modes is the proprietary asset.
The proposed capital plan is conditional: a future Phase I $150–225K / 6 months scope would support autonomy-stack maturation and subsystem validation, followed—only if funded and technically successful—by a potential Phase II $750K+ request through an eligible NASA SBIR (Small Business Innovation Research) or SpaceWERX Orbital Prime opportunity.
Within that conditional plan, dollars would trace to three buckets: (i) simulation + autonomy-stack maturation — extending the open-source physics models with the proprietary consensus and coordination layer, then testing it in hardware-in-the-loop; (ii) v3.0 cold-gas chassis development — advancing the proposed bus toward future qualification; and (iii) regulatory + legal preparation — future FAA/AST, FCC RPO, and ITAR/EAR work if a mission is funded. No IQT portfolio pipeline or current underwriting is implied.
Three prospective scenarios, all contingent on future validation and agreements. (a) Strategic acquisition. A defense prime or large-constellation operator could evaluate OrbitReclaim after rendezvous and proximity-operations capability is validated on orbit. (b) Prime-contractor partnership through STRATFI / Orbital Prime. Future outreach could seek a role as the small-object / tight-formation lane inside a prime-contractor structure. (c) Continued independent development. Future non-dilutive capital and commercial service contracts could fund the platform toward flight qualification; none of these routes is a current relationship, award, customer commitment, or operating result.
An IQT introduction would be a prospective outreach opportunity, not an activation trigger or current portfolio relationship.
OLE v2.0 — Orbital Lane Enforcement, OrbitReclaim's preserve-and-organize debris framing.
RPO — rendezvous & proximity operations.
GNC — guidance, navigation, and control (the on-board stack that steers the swarm; on the OrbitReclaim nano-swarm, the consensus and coordination layer of the GNC stack is proprietary to Orbital Reclaim LLC / Polsia Inc.).
CW / Clohessy-Wiltshire — the closed-form relative-motion equations used to model chaser-target approach in LEO.
LEO — low Earth orbit (~160–2,000 km altitude).
ADR — Active Debris Removal (capture & relocation, not deorbit-and-destroy).
DoD — U.S. Department of Defense.
SDA — Space Development Agency.
STRATFI — Strategic Financing program, a SpaceWERX investment vehicle.
SpaceWERX — U.S. Space Force technology accelerator.
IQT — In-Q-Tel, the CIA-affiliated strategic-investor network.
Orbital Prime — U.S. Space Force program funding operational ADR.
Warfighter — military end-user / mission operator.
Dual-use — a single capability stack with both commercial and government customers.
Chaser-spacecraft — the active servicing vehicle that approaches a target.
Formation-keeping — maintaining coordinated relative position across the swarm (on the OrbitReclaim nano-swarm, the control law that maintains formation is part of the proprietary swarm consensus and coordination algorithm — proprietary to Orbital Reclaim LLC / Polsia Inc.).
v3.0 cold-gas chassis — OrbitReclaim's third-generation nano-satellite bus; mechanical layout, propellant manifold stack, and seal architecture are proprietary to Orbital Reclaim LLC / Polsia Inc., released only under NDA-protected technical interchange.
Engineering schematics — proprietary trade-secret documentation describing the v3.0 cold-gas chassis, propellant manifold, and rendezvous sequence; not covered by the MIT-licensed open-source physics models and not licensed under any community-extensible terms. proprietary to Orbital Reclaim LLC / Polsia Inc.