Atlas of Useful Space · mission planning & operational advisory · compiled 2026-08-17 Space Weather Workshop 2026 poster →

ATLAS OF USEFUL SPACE

A map of certainty in space.

Space operations run on models that predict density, dose, charging. Good ones. But a model can’t tell you what it doesn’t know. That has to be measured from the outside. From LEO to the Mars surface, this atlas draws the frontier by calculating certainty where it can be earned from measurement, and recording gaps where it can’t. With five decades of model heritage, LEO is the most mature environment, but even there, storms locally drive the standard model's error to ten times its everyday miss. We flag these errors about three days ahead, at 92% precision, where drag residual is available from live satellites. The gaps are even bigger in GEO, cislunar, and the Mars corridor.

61
storm sectors where the drivers are certified · 2 satellites, 3 bands
2 / 3
independent satellites / altitude bands confirming
40
geomagnetic storms back-tested · incl. Gannon 2024
41.5M
in-orbit measurements ingested · 8 years
131
orbital regions assessed & classified
3
flight & data opportunities to close top gaps
Low Earth Orbit · 420–850 km · 2018–2025

Storm-time density certainty, cell by cell.

Latitude × altitude × local time. Every measured cell was tested on storms the model never saw. Solid cells are certainty earned from Swarm and GRACE-FO drag observations; dashed cells are waiting on a partner satellite’s drag signal.

Dawn (03–09)
Noon (09–15)
Dusk (15–21)
Midnight (21–03)
Polar N (60–90°) Mid-Lat N (30–60°) Tropical N (0–30°) Tropical S (0–30°) Mid-Lat S (30–60°) Polar S (60–90°)
420 460 510 550 600 650 700 800 850 km
certified out-of-sample
measured, not yet trusted
awaiting a partner satellite’s drag signal
SW·GF source satellite (Swarm / GRACE-FO)
Deep dive: how the LEO density grid was earned ↗
Every dashed cell is a satellite-shaped hole in the map. The signal that fills it isn’t telemetry or proprietary state — it’s the drag residual a satellite’s GPS already computes for navigation. Three source bands lit their columns; a contributing fleet fills the grid wherever it flies. We also audit the baseline model itself: its solar-EUV term is corrected in 13 of 13 cells out-of-sample, and its failure windows are flagged in real time at 92% precision (the audits ↗).
Beyond the thermosphere

Radiation, from the South Atlantic Anomaly to the Mars surface.

Three environments, one standard. Measured means we made a prediction and scored the residual outcome. Modeled means there is a registered stake with a named measurement that would score it. Hover on any cell.

LEO Radiation — SAA & belts ↗

dose environment · SAA to polar
SAA core
South Atlantic Anomaly core
MEASURED — during storms, radiation dose here does the opposite of everywhere else. It drops first, then recovers. We predicted that in advance, and it held in exactly this one cell and nowhere else. We trust the direction; we are still earning confidence in the size.
Slot region
Slot region
MEASURED — we measured how long dose takes to settle after a storm passes (the question crews and planners actually ask). The shape of the recovery is earned; confidence in the exact numbers is still building.
Belt edges
Belt edges (outer/polar)
MEASURED — storms push dose UP here (unlike the SAA core), with the strongest solar-particle coupling at the poles. Direction earned; confidence still building.
Polar inner
Polar inner boundary
NO MEASUREMENTS YET — our source orbit never samples this cell.
What closes it: data from a different orbit, or a hosted sensor.

Geostationary — electrons ↗

spacecraft-charging driver · 36,000 km
Calm ×4
GEO electrons · calm conditions
MEASURED — faster solar wind reliably pumps up the electron flux about two days later, in all four local-time sectors, strongest on the midnight side — exactly the shape spacecraft-charging planning needs, and we called the ordering before we saw it. We trust the direction and the ordering; we do not yet claim the amplitude. A longer observing window earns that.
Storm ×4
GEO electrons · storm conditions
MODELED, UNVERIFIED — one longitude sees each sector only ~6 storm-hours a day, so the storm side cannot be certified from measurement yet. NOAA's operational forecaster (REFM) puts a storm response near 5.7×10⁸ e/cm²·day·sr (2-day peak ~1.1×10⁹) — stamped with its own published skill, which is modest at one day out.
The measurement that scores this stake: electron feeds from additional GEO longitudes.

Cislunar · Moon · Transit · Mars ↗

radiation dose · 384,000 km → 1.5 AU
cislunar
Cislunar orbit
MEASURED — we followed the Moon's radiation dose across 17 years and learned how it answers solar-particle floods; the storm-vs-quiet model structure we built for it held over the entire archive. Two honest caveats: extreme floods are so rare that no one can yet be confident about them, and one geometry effect (the magnetotail's influence on dose) behaves opposite to what the textbooks suggested. This is an open question we publish in the gap register.
Mars orbit
Mars orbit
MEASURED — one relationship earned so far: the electron-driven dose signal that shows up in Mars orbit disappears at the surface, under 20 g/cm² of atmosphere. This isa direct read on how much shielding matters. The rest of this cell's structure is mapped as six named open questions, each with a planned next step.
Mars surface
Mars surface
MEASURED — surface dose followed across two separate years (2023 and 2024–25). The dependable finding: solar-particle events SUPPRESS dose at the surface where the atmosphere filters the flood. This occurredthe same way in both years, and in one season we certified the effect is essentially zero, firmly (knowing a solid zero is real knowledge). We also caught two solar-storm arrivals at Mars that appear in no official catalog, confirmed against an orbiting spacecraft. The puzzle we published is a seasonal dose signal that showed up in BOTH years and survived every explanation we tested. This is our best open mystery, with the tests on record.
Earth→Mars transit
Earth→Mars transfer corridor
MODELED, UNVERIFIED — no continuous measurement exists (4 one-way snapshots in 25 years). Here's what the current models stake: ~0.28–0.29 mGy/day free-space GCR silicon dose (BON2020 + HZETRN2020, current-cycle conditions) — a model pair that came within ~4% of the one modern point-check that exists.
The measurement needed to score this stake is a hosted dosimeter on any Mars-bound rideshare, hourly, one solar rotation.
Lunar surface
Lunar surface
NO MEASUREMENTS AVAILABLE — the instrument exists (LND); archive access is blocked.
What closes it: a data-access agreement. Cheapest cell on the map.
measured — direction earned, size still building
modeled, unverified — a stake on the books
no measurements yet — the close is named in the tooltip
Operational outlook · 2026–2027 and beyond

What this map means for the missions ahead.

Here is how the atlas reads against what’s actually on the manifest. Which numbers you can schedule around, which are stakes awaiting a score, and which are gaps.

2026–2027 · Constellations · Stations · Reentry Certified to 550 km

LEO: the next few thousand satellites deploy into the dashed cells.

The big deployments of the next two years — Kuiper’s shells at 590–630 km, Starlink’s continuing build-out, and everything that rides with them — fly almost entirely in the 550–850 km rows of the grid above; The rows where nobody is measuring and the standard density models disagree with themselves by 4–13%. Storm-time drag error lands directly on conjunction screening and reentry prediction, and the declining phase of Solar Cycle 25 is historically rich in the recurrent high-speed streams that drive it.

What the atlas already offers that fleet: below 550 km — where the first commercial stations and most crewed LEO operations fly — storm response is certified cell by cell, and when the standard model is about to fail, we flag it in real time at 92% precision. The rest is closable. A fleet that shares the drag residual its GPS already computes lights up its own corridor. More participating satellites lights up more cells.

2026–2027 · GEO fleet · Declining phase Storm side staked

GEO: a two-day heads-up on charging, earned on the calm side.

The declining phase of the solar cycle is when high-speed streams recur every solar rotation and GEO’s relativistic-electron episodes — the spacecraft-charging environment — are historically at their strongest. What was earned: faster solar wind pumps electron flux about two days later, in all four local-time sectors, strongest on the midnight side. That is a usable two-day heads-up for anomaly attribution and scheduling charging-sensitive operations.

What we couldn't earn (yet): the storm-time response is modeled, not certified — one longitude sees each sector only ~6 storm-hours a day — so storm charging margins should stay conservative until additional GEO longitude feeds close the cell.

2026–2027 · Artemis · Gateway · CLPS landers Surface archive blocked

The Moon: dose behavior is earned; the surface archive is the cheapest close.

As crews return to cislunar space — the Artemis flights, Gateway assembly, a steady lander cadence through 2027 — the atlas holds 17 years of measured lunar-orbit dose response to solar-particle floods, with the storm-vs-quiet structure intact across the whole archive. Two caveats matter operationally. Extreme floods are so rare that nobody can certify shelter margins for them from data. And, the magnetotail’s effect on dose runs opposite to textbook expectation; the Moon spends days of every month inside it, so for a long-stay base that is a real open question about the monthly dose rhythm, published in the gap register.

For the surface itself: the instrument exists (LND), the archive is blocked, and one data agreement converts base-siting dose assumptions from inference to measurement. It should happen before anyone pours regolith.

Late-2026 window · Earth→Mars transit · Surface Corridor unmeasured

The corridor: crews will spend months in the one region never continuously measured.

Every crewed Mars architecture spends six to nine months each way in the transfer corridor where four one-way snapshots in 25 years is the entire measurement record. Our current stake: ~0.28–0.29 mGy/day of free-space galactic-cosmic-ray dose (silicon), which compounds to roughly 50–80 mGy per leg before a single solar storm — if the stake is right. That “if” is the point. The late-2026 Mars departure window is the nearest chance to close the biggest hole on this map. Any rideshare hosting a small dosimeter, reporting hourly for one solar rotation, scores the stake. The analysis is pre-committed on our side and waiting for the signal.

At Mars, the measured results already carry weight for a base: ~20 g/cm² of atmosphere erases the electron-driven dose signal seen in orbit — a flight-data anchor for habitat shielding mass — and solar-particle events suppress surface dose rather than spike it, the kind of fact a storm-shelter strategy can be sited on. One outstanding mystery in the gap register: a seasonal surface-dose signal that has survived every explanation we’ve tested.

The gap register

Where do the Gaps exist & What data closes them?

Every existing gap has a named target that is a flight opportunity, a data agreement, or a feed that already exists in someone’s flight-dynamics logs.

ref gap what closes it detail
TRANSIT Earth→Mars corridor radiation Flight opportunity Crew transit dose has never been continuously measured. Any Mars-bound rideshare hosting a small dosimeter closes the biggest hole on this map. The analysis is pre-committed on our side.
LUNAR Lunar surface dose Data agreement The measurements exist (LND instrument); access is blocked. One archive agreement converts this from gap to coverage, and it now carries a second justification. 17 years of CRaTER hold only 46 magnetotail-flood days, so a farside stream is the only way to close that cell.
LEO-FLEET Upper-LEO density (550–850 km) Live drag signals Every dashed cell in the LEO grid is a satellite-shaped hole. The signal that fills it is the GPS drag residual every operating satellite already computes. We don't need the raw telemetry or proprietary state. Just that one signal lights up certainty where current models disagree and frequently miss at storm time.
LEO-STORM Low-altitude storm seasons Scheduled data Severe-storm hours are rare; storm certainty grows each solar-cycle season. Next data window identified (declining phase).
GEO-STORM GEO storm-time electrons More longitudes One satellite = 6 storm-hours/day/sector. Additional GEO longitude feeds certify the storm side.
SAA-POLAR Polar inner-belt boundary Different orbit Never sampled from our current source orbit; a hosted sensor or alternate-orbit dataset closes it.
STORM-TYPES Fast storm-train events Advisory A small class of storm sequences (notably 2023 storm trains) degrades our model; flagged for conservative margins until characterized.
The bigger picture

Assured autonomy starts with navigating an evolving ecosystem.

Nervous Machine learns the causal drivers of local environments — whether they live inside a machine like a satellite, a drone, a robot, or a quantum computer, or in an open environment like space. We believe the intersection where internal and external drivers influence each other is where some of the most unexpected edge cases arise. Assurance there has to be earned, not assumed.

This atlas is that conviction applied to the largest open environment there is. Certainty earned from measurement, models stamped and validated, and every gap named with the measurement that closes it.