Tech credibility
SBIR Phase I/II (SpaceWERX + NASA, ~$2.3M). Two LOIs in negotiation with constellation operators at $8–15M per object. Customer discovery underway: SDA, Starlink, OneWeb, Iridium. Founding CTO search active.
— Investors · Seed round · Open
A category-defining bet on the physical infrastructure of orbital sustainability.
Waypoint Dynamics is raising its seed round to commercialize Sparrow — a reusable solar-electric servicer that captures derelict satellites and rocket bodies, deorbits them, and recovers for the next cycle. Active debris removal is no longer optional for U.S.-licensed operators. The market exists. The regulation exists. The hardware heritage exists. We are pulling them together.
Stage
Seed
Round size
$2–3M directional
Instrument
SAFE YC post-money
Status
Open partner-led
01 · Why now
Three forces converging — for the first time, simultaneously.
Active debris removal has been an academic conversation for thirty years. Three things changed in the last twenty-four months that turned it into a procurable service.
2024·
Regulation
The FCC's 5-year deorbit rule replaced the prior 25-year guideline for U.S.-licensed LEO satellites. Non-discretionary. Operators are now financially exposed on every satellite they fly.
$2.31B
Market by 2033
The active debris removal SAM grows from $143M in 2025 to $2.31B in 2033 — a 41.6% CAGR. North America holds 41.2% share. On-orbit servicing TAM: $4.67B.
3×
Hardware heritage
Net (RemoveDEBRIS, 2018), magnetic dock (Astroscale ELSA-d, 2021), and drag-sail (NanoSail-D2) capture have all flown. Hall-effect propulsion is flight-qualified. The components exist; integration and operations are the work.
02 · What we're building
Sparrow — and the operations company around it.
The vehicle
Sparrow is a 12U-class servicer (~32 kg wet) built around three flight-demonstrated capture mechanisms and a flight-qualified Hall thruster. It is designed for the 500–800 km regime where natural decay takes decades and where the densest concentration of derelict objects sits.
One ~3 kg propellant load supports approximately ten capture-and-deorbit cycles. The vehicle is refuelable in orbit through the Orbit Fab RAFTI standard, extending mission life beyond the propellant constraint.
The company
Waypoint Dynamics is structured as a mission services company, not a hardware company. We sell deorbit-as-a-service: the customer signs a service-level agreement, we deliver a reentry trajectory.
The differentiator is operational discipline. Engineering-led ADR companies are well-capitalized and technically capable. Government buyers — particularly DoD — reward demonstrated operational maturity when evaluating commercial RPO providers. We import 48 years of Part 121 aviation operations culture directly into mission control.
03 · Unit economics
A multi-object refuelable bus changes the math.
Single-shot deorbit architectures are constrained by the cost of the bus. Reusing the bus across five-to-ten objects collapses cost-per-object by roughly 60% at equivalent technical maturity.
Per-mission economics
- Mission contract value 5-object deorbit$40M
- Cost per object blended~$8M
- Reduction vs single-shot peers~60%
- Cycles per propellant load~10
- Target gross margin at scale~50%
Path to recurring revenue
Three revenue lines stack as the company matures: debris removal contracts (~$150M/yr at 3 missions), life-extension and inspection for cooperative satellites (~$25M/yr), and orbital sustainability data sold to insurers, reinsurers, and SSA providers (~$5M/yr).
Steady-state EBITDA target by Year 5: $35M / 17.5% margin on $200M revenue. The unit economics work because the bus does not get thrown away every mission.
04 · Competitive position
Where we are differently positioned.
There are well-funded players in adjacent spaces. None of them sit on all four of these axes simultaneously.
Provider
U.S.-flagged
Operations-led
Unprep. debris
Reusable bus
Waypoint Dynamics · Sparrow
✓
✓
✓
✓
Astroscale
JP / UK
Engineering-led
Cooperative-first
✓
ClearSpace
CH
Engineering-led
✓
Single-shot
Starfish Space
✓
Engineering-led
Cooperative-first
✓
Northrop Grumman MEV
✓
Operations-led
GEO life-extension
✓
Read: ITAR friction prevents non-U.S.-flagged providers from servicing U.S. national-security assets. MEV operates in GEO, not LEO, and addresses life-extension rather than disposal. We sit in the gap.
05 · Roadmap & traction
Three phases. Non-dilutive-led.
SBIR runs in parallel with seed equity. The seed funds the engineering team, GNC testbed, and capture breadboard — the work that gates Series A.
First mission
TRL-7 demonstrator. First commercial 5-object deorbit at $75M ($15M/obj). STRATFI follow-on. Fleet of three spacecraft. Series A close on the back of demonstrated mission revenue.
Recurring service
Three deorbit missions per year ($150M) plus life-extension ($25M) plus orbital sustainability data ($5M). Refuelable fleet via Orbit Fab. Steady-state EBITDA $35M.
06 · Use of funds
Where the seed dollars go.
The seed buys 18–24 months of runway, the LOIs that gate Series A, and the engineering organization that executes Year 1–2. SBIR cost-share extends every dollar.
45%Engineering team — 4 FTE through TRL-4
18%RPO simulation + capture-mechanism ground demo
12%SBIR Phase II cost-share + proposal cadence
8%Regulatory, licensing, ITAR, FCC ARM authority
12%G&A — legal, accounting, IP, insurance
5%6-month operating reserve
07 · Materials
Materials available on request.
The one-pager below is downloadable directly. The full deck, financial model, and data room are available after an introductory conversation.
— Get in touch
Partner with us on the first 18–24 months.
We're partner-led on this round and we're selective about the table. If you have a thesis on space sustainability, defense space, or operations-led aerospace — we'd like to hear it. Cold inbound is welcome; warm intros are welcomer.
info@waypointdynamics.space · Sheridan, WY · Response < 2 business days
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