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+# Accurate planet positions — implementation plan
+
+> **For agentic workers:** REQUIRED SUB-SKILL: use superpowers:subagent-driven-development under the
+> lean protocol in `docs/superpowers/conventions/sdd-execution.md`. Steps use checkbox (`- [ ]`) syntax.
+
+**Goal:** The eight planets match JPL DE (Horizons) to ≤ 1,000 km over 1900–2100, Earth wobbles about
+the Earth–Moon barycentre, and every orbit trail stays through its body.
+
+**Architecture:** Each planet's position is today's Keplerian position plus a generated correction
+series: a cubic polynomial plus fitted sinusoids, about 17 kB of constants. The correction is
+evaluated in `deriveBodyStates`. A one-row pair table subtracts the Moon's reflex from Earth. Orbit
+trails anchor on the snapshot body position, so they follow both corrections without needing to know
+about either.
+
+**Tech stack:** TypeScript, Vitest, tsx tools, the JPL Horizons API.
+
+**Spec:** `docs/superpowers/specs/2026-10-04-accurate-planet-positions-design.md`
+
+## Global constraints
+
+- Accuracy: ≤ **1,000 km** from Horizons for every planet over **1900-01-01 → 2100-01-01**. The fit
+  stops at ≤ **900 km** on its sample grid, and the tool verifies every planet on the dense 1-day grid
+  and throws above 1,000 km.
+- Outside the span the correction is **frozen at its edge value**: clamp `simDays` to
+  `[startJd, endJd]`. No fade and no new setting.
+- Horizons query: `EPHEM_TYPE='VECTORS'`, `CENTER='500@10'` (Sun centre), `REF_PLANE='FRAME'`
+  (equatorial ICRF), `TIME_TYPE='UT'`, `OUT_UNITS='KM-S'`, `CSV_FORMAT='YES'`, `VEC_TABLE='1'`.
+  - Targets: Mercury `199`, Venus `299`, Earth–Moon barycentre `3`, then system barycentres `4`–`8`
+    for Mars through Neptune.
+  - Fetch 1-day steps in 50-year chunks, retrying each chunk up to 5 times.
+- `OBLIQUITY_DEG = 23.4392911`.
+- Earth–Moon pair: `secondaryMassFraction = 1 / 82.30057`, the Moon's share of the pair mass.
+- `simDays` stays a UTC Julian date. No runtime TDB conversion: the UT query absorbs the offset.
+- Conventions: one symbol per `utils/` and `@types/` file, `type` and never `interface`, and pass and
+  frame files export only their one symbol.
+- Prep (Tasks 1–2) is a **separate PR** on branch `accurate-planets-prep` off `main`. This spec and
+  plan are committed there too. Features (Tasks 3–6) go on `accurate-planets`, stacked on the prep
+  branch. Never commit on `main`.
+
+## Review focus
+
+1. **Dates outside 1900–2100** (a tour in 1850, a scrub to 2200). Positions stay finite and equal
+   Kepler plus the frozen edge correction, with no jump at either boundary. Tests are in Task 3.
+2. **A camera parked at an Earth surface site with the clock running.** The site keeps its offset from
+   Earth while Earth wobbles. Tested in Task 6.
+3. **Moon, Hubble and the easter eggs after the Earth reflex.** Each still sits on its own trail,
+   because its trail is centred on the reflexed Earth. Tested in Task 6.
+4. **Any element-row edit or frame change without regenerating.** The Horizons check fails loudly
+   instead of drifting silently. Tested in Task 6.
+5. **Chunk seams in the Horizons fetch.** The duplicated boundary row is dropped exactly once, with
+   no gap and no duplicate. Tested in Task 4.
+
+---
+
+## PR 1: prep (`accurate-planets-prep`)
+
+### Task 1: Orbit trails anchor on the snapshot body position (P1)
+
+**Files:** `src/services/engine/frame/passes/orbitTrailsPass.ts:96-109` (modify),
+`src/data/bodies/orbitalElements.ts:1-9` (header, modify),
+`tests/services/engine/frame/passes/orbitTrailsPass.test.ts` (modify)
+
+**Before → after** (`orbitTrailsPass.ts:105-109`):
+
+```ts
+// before: centre = focus + centerOffset   (focus re-read, conic re-derived: a mirror of deriveBodyStates)
+// after:  centre = state.positionMpc − keplerianPositionMpc(propagated) + centerOffsetMpc
+```
+
+The body is now on its trail by construction: any later change to the snapshot position moves the
+trail with it. Keep `meanAnomalyRad` as the fade anchor, unchanged.
+
+- [ ] Add the test `trail follows a snapshot position that differs from raw Kepler`. Stub the states
+      map so one row's `positionMpc` is the Kepler position plus a 1e6 km vector (converted with
+      `SCALE_UNITS.KM_TO_MPC`). Read the packed eye-relative km basis (floats 34..45, written by
+      `eyeRelativeOrbitBasisKm`): the body point `C + A·cosE + B·sinE` at the row's propagated E must
+      equal the stubbed position, eye-relative in km, to ≤ 1 m. Use km tolerances throughout:
+      1e-15 Mpc is 30,000 km.
+- [ ] Run that test and confirm it fails against the current code.
+- [ ] Implement the after-line. Rewrite the `orbitalElements.ts` header sentence about "a body sitting
+      on its own trail is structural" so it names the snapshot anchoring.
+- [ ] The comparisons against `keplerianEllipse` (`orbitTrailsPass.test.ts:345-378`, `:511-573`) were
+      exact to 18–20 digits. Loosen them to `toBeCloseTo(…, 15)`, or the relative tolerance f64 can
+      hold for `(a + b) − b`, and give the reason in one line.
+- [ ] `npm test -- orbitTrailsPass`, then commit "Orbit trails anchor on the snapshot body position".
+
+### Task 2: Exact obliquity (P2)
+
+**Files:**
+- `src/data/bodies/orbitPlaneFrames.ts:72` (and the header comments at `:25`, `:29`, `:77-78`)
+- `src/utils/orbit/rotationLookAt.ts:19`
+- `src/data/defaults.ts:138-141`
+- `tests/data/bodies/orbitPlaneFrames.test.ts:50-53`
+- `tests/data/orientation/orientationFrames.test.ts:54`
+- `tests/utils/orbit/propagateElements.test.ts:94`
+- `tests/services/engine/frame/earthTerminator.test.ts:17`
+- `tests/fixtures/bodyStatesJ2000.json`
+- `tests/fixtures/camera/settleGoldenTrace.json`
+- `tests/fixtures/camera/driverGoldenTrace.json`
+- `tools/perf/perfScenarios.ts:52`
+
+Set `OBLIQUITY_DEG = 23.4392911` and say "IAU J2000 mean obliquity" in its comment. Comments that
+say `23.44°` become `23.439°`. Test literals use the exact value; in `orientationFrames.test.ts:54`,
+66.56° becomes `90 − 23.4392911`. No new test: this is a constant, and the existing frame tests pin it.
+
+- [ ] Change the constant, comments and test literals.
+- [ ] Regenerate `bodyStatesJ2000.json` with a one-off tsx snippet that is not committed. It
+      serialises `deriveBodyStates(2451545.0)` for every `ORBITAL_ELEMENTS` id in the fixture's
+      existing shape (`positionMpc`, `orientation`, `meanAnomalyRad`), leaves anchors out, and keeps
+      the key order. Diff it: only rotated values may change.
+- [ ] Re-record the camera traces with `SETTLE_GOLDEN_RECORD=1` and `DRIVER_GOLDEN_RECORD=1`
+      (`npm test -- settleGoldenTrace driverGoldenTrace`). The spec rules this. Then run once more
+      without the flags.
+- [ ] Update `EARTH_TARGET` in `perfScenarios.ts:52` to the new J2000 Earth position, taken from the
+      regenerated fixture.
+- [ ] `npm run typecheck:fast`, then `npm test -- orbitPlaneFrames orientationFrames propagateElements earthTerminator deriveBodyStates`.
+      Commit "Exact J2000 obliquity".
+
+---
+
+## PR 2: feature (`accurate-planets`, stacked on prep)
+
+### Task 3: Correction type and evaluator
+
+**Files:**
+- `src/@types/scene/EphemerisCorrection.d.ts` (create)
+- `src/utils/orbit/ephemerisCorrectionMpc.ts` (create)
+- `tests/utils/orbit/ephemerisCorrectionMpc.test.ts` (create)
+
+**Interfaces, produced:**
+
+```ts
+export type EphemerisCorrection = {
+  startJd: number;
+  endJd: number; // fitted span (UTC JD); outside it the edge value is held
+  polyKm: readonly [Vec3, Vec3, Vec3, Vec3]; // coefficients of τ⁰..τ³, τ = 2(t − startJd)/(endJd − startJd) − 1
+  terms: readonly number[]; // flat, 7 per term: ω (rad/day), cos x,y,z (km), sin x,y,z (km); phase ω·(t − startJd)
+};
+export function ephemerisCorrectionMpc(c: EphemerisCorrection, simDays: number): Vec3;
+```
+
+Sum in f64 km, then multiply by `SCALE_UNITS.KM_TO_MPC`.
+
+- [ ] Test `evaluates polynomial and terms at a known instant`: a hand-built two-term correction,
+      checked against values worked out by hand.
+- [ ] Test `holds the edge value outside the span`: `simDays` 100 years before `startJd` returns
+      exactly (`toEqual`) the value at `startJd`, and likewise at `endJd`.
+- [ ] Test `is continuous across both span edges`: evaluations at edge ± 1e-6 day differ by < 1 m.
+- [ ] Implement, `npm test -- ephemerisCorrectionMpc`, then commit "Ephemeris correction evaluator".
+
+### Task 4: Horizons planet fetcher
+
+**Files:**
+- `tools/parsers/horizonsVectorsCsv.ts` (create)
+- `tests/tools/parsers/horizonsVectorsCsv.test.ts` (create)
+- `tools/fetch/fetchHorizonsPlanets.ts` (create)
+- `tools/utils/io/rawDataRegistry.ts` (add `horizons.planets` and `horizons.planets.readme`, using the
+  entry shape at `:17-25`)
+- `data/raw/horizons/planets/README.md` (create, committed; it records the exact query in Global
+  constraints)
+- `package.json` (add `"fetch-horizons-planets": "tsx tools/fetch/fetchHorizonsPlanets.ts"`)
+- `docs/DATA.md` (add a Horizons entry wherever the fetchers are listed)
+
+**Interfaces, produced:**
+
+```ts
+export type HorizonsVectorRow = { jd: number; xKm: number; yKm: number; zKm: number };
+export function parseHorizonsVectorsCsv(result: string): HorizonsVectorRow[]; // rows between $$SOE/$$EOE
+```
+
+The output goes to `data/raw/horizons/planets/<naif>.csv` with the columns `jd,x_km,y_km,z_km`,
+written through `rawDataPath('horizons.planets')`. Chunks are concatenated and a row whose `jd` is ≤
+the previous row's is dropped (Review focus 5).
+
+- [ ] Test `parses the SOE/EOE block of a Horizons vectors result`: use a trimmed real response
+      pasted as a string literal, three rows.
+- [ ] Test `concatenating two chunks drops the shared boundary row once`, through a small exported
+      merge step, or by asserting the fetcher's `mergeChunks` if you extract it. Keep it
+      one-symbol-per-file if extracted.
+- [ ] Implement the parser and the fetcher, which writes all eight CSVs. Announce the download size
+      before running it: 8 × ~3 MB.
+- [ ] Run `npm run fetch-horizons-planets`. Commit "Horizons planet fetcher", without the gitignored
+      CSVs.
+
+### Task 5: Fit tool and generated corrections · `review: yes`
+
+**Files:**
+- `tools/utils/math/fft.ts` (create)
+- `tools/utils/math/fitSinusoidSeries.ts` (create)
+- `tests/tools/utils/math/fft.test.ts` (create)
+- `tests/tools/utils/math/fitSinusoidSeries.test.ts` (create)
+- `tools/bodies/buildPlanetEphemeris.ts` (create, using the `tools/bodies/buildPlanetFacts.ts`
+  template: banner, prettier, CLI guard)
+- `src/data/bodies/planetEphemerisCorrections.generated.ts` (generated)
+- `package.json` (add `"build-planet-ephemeris": "tsx tools/bodies/buildPlanetEphemeris.ts"`)
+
+**Interfaces, produced:**
+
+```ts
+export function fft(re: Float64Array, im: Float64Array): void; // in-place radix-2, length a power of two
+export type FitResult = { polyKm: [Vec3, Vec3, Vec3, Vec3]; terms: number[]; maxErrKm: number };
+export function fitSinusoidSeries(tJd: Float64Array, residualKm: [Float64Array, Float64Array, Float64Array],
+  startJd: number, endJd: number, stopKm: number, maxTerms: number): FitResult;
+export const PLANET_EPHEMERIS_CORRECTIONS: Readonly<Record<string, EphemerisCorrection>>; // keys: planet ids
+```
+
+**Method.** The spike is `planetSeriesFit.mts` in the brainstorm scratchpad; it measured ~590 terms.
+1. Fit the cubic in τ first.
+2. Then loop:
+   - take the FFT of the residual, zero-padded ×8, with power summed over x, y and z;
+   - find the peak and refine it parabolically;
+   - add a cos column and a sin column;
+   - Gram–Schmidt each new column against the kept ones, which makes it an exact least-squares refit;
+   - stop when the max 3D error is ≤ `stopKm`.
+3. Recover the coefficients of the original basis from the orthogonal one. Keep R, or refit by normal
+   equations once at the end, so the generated `terms` are plain (ω, cos, sin) amplitudes.
+4. The tool computes the residual as `Horizons − keplerianPositionMpc(propagateElements(row, jd))`.
+   It converts km with the same `MPC_TO_KM` the app uses, imports the `src/` modules directly, and
+   uses the app's own element rows.
+
+**Sample steps (days) for fitting:** Mercury 2, Venus 4, Earth 4, Mars 6, Jupiter through Neptune 10.
+The tool then **verifies on every 1-day row** with `ephemerisCorrectionMpc` (from Task 3) and throws
+if any planet exceeds 1,000 km. That way the shipped evaluator is exactly what gets verified.
+
+- [ ] Test `fft finds a pure sinusoid's bin`: N = 64, a sinusoid in bin 5, and the power peaks at k = 5.
+- [ ] Test `fitSinusoidSeries recovers a synthetic two-term signal`: a cubic plus two sinusoids at
+      non-bin frequencies. With `stopKm` 1, it should use ≤ 4 terms, and evaluating the result through
+      `ephemerisCorrectionMpc` reproduces the signal to ≤ 1 km.
+- [ ] Implement, then run `npm run build-planet-ephemeris`. Report each planet's term count and
+      verified max error; expect ~35–180 terms and a total of ~17 kB of numbers.
+- [ ] Commit "Planet ephemeris fit tool + generated corrections".
+
+### Task 6: Wire corrections and the Earth–Moon pair into `deriveBodyStates` · `review: yes`
+
+**Files:**
+- `src/@types/scene/BarycentricPair.d.ts` (create)
+- `src/data/bodies/barycentricPairs.ts` (create)
+- `src/services/engine/frame/deriveBodyStates.ts:60-68` (modify; the header gains one clause)
+- `src/data/bodies/scenePlanets.ts:3` (fix the stale "via keplerianPositionMpc" header)
+- `tests/fixtures/horizonsPlanets.json` (create)
+- `tests/data/bodies/planetEphemeris.test.ts` (create)
+- `tests/services/engine/frame/deriveBodyStates.test.ts` (modify)
+- `tests/fixtures/bodyStatesJ2000.json`
+- `tests/fixtures/camera/{settle,driver}GoldenTrace.json`
+- `tools/perf/perfScenarios.ts:52`
+- `docs/backlog/2026-08-16-barycentric-orbit-pairs.md`
+- `docs/BACKLOG.md` (the "Barycentric orbit pairs" line)
+
+**Interfaces:**
+
+```ts
+export type BarycentricPair = { primaryId: string; secondaryId: string; secondaryMassFraction: number };
+export const BARYCENTRIC_PAIRS: readonly BarycentricPair[]; // [{ primaryId: 'earth', secondaryId: 'moon', secondaryMassFraction: 1 / 82.30057 }]
+```
+
+**1b loop, after this task:**
+`position = focus + kepler(el) + correction(el.id) − k · kepler(propagate(secondaryRow))`.
+- `correction` is `ephemerisCorrectionMpc(PLANET_EPHEMERIS_CORRECTIONS[el.id], simDays)` when a
+  correction exists, and zero otherwise.
+- The reflex term applies only when `el.id` is a pair's `primaryId`.
+- The secondary row comes from `ORBITAL_ELEMENTS` and is propagated inline, because `FOCUS_ORDER`
+  resolves `earth` before `moon`.
+- Resolve pair and correction lookups into id-keyed maps at module load, beside `FOCUS_ORDER`, never
+  per frame.
+
+**Fixture.** `tests/fixtures/horizonsPlanets.json` uses the Global constraints query, except with
+target `399` (Earth centre) for Earth.
+- Dates: 1900-06-01, 1979-03-05, 1980-11-12, 1986-01-24, 1989-08-25 and 2099-06-01 (Voyager flybys
+  plus both ends).
+- Shape: `{ [id]: { [jd]: [xKm, yKm, zKm] } }`.
+- The test header records the query URL.
+
+- [ ] Test `every planet is within 1,000 km of Horizons at the fixture dates`, from `deriveBodyStates`
+      positions. Earth is compared with Horizons `399` and gets its own tolerance: measure the max,
+      round up to the next 500 km, and write the measured number in a one-line comment, since it
+      includes the app Moon's error. This test is Review focus 4.
+- [ ] Test `Earth–Moon reflex keeps the barycentre and the separation`. At three dates, with
+      k = 1/82.30057, (1−k)·Earth + k·Moon equals the corrected EMB (Earth-row Kepler plus the
+      correction) to ≤ 1 m. Moon − Earth equals the Moon's raw Kepler offset to ≤ 1 m.
+- [ ] Test `an Earth surface site keeps its offset from the wobbling Earth` (Review focus 2): a site
+      hosted on `earth` minus Earth's position is independent of the reflex. Compare with the site
+      offset computed from `sitePointBodyFixed` and Earth's orientation.
+- [ ] Test `Moon, Hubble and Saturn sit on their trails at a non-J2000 date` (Review focus 3): drive
+      `orbitTrailsPass` packing at a 1989 date. Each body's position lies on its packed conic at its
+      propagated E, to ≤ 1 m, reading the eye-relative km basis as Task 1's test does.
+- [ ] Implement the pair table and the 1b term. Fix the `scenePlanets.ts:3` header.
+- [ ] Regenerate `bodyStatesJ2000.json` with Task 2's one-off snippet. Re-record the golden traces
+      with the record flags, then rerun without them. Update `EARTH_TARGET`.
+- [ ] Backlog: in the detail file, add that `BARYCENTRIC_PAIRS` exists, so Pluto's wobble is one row,
+      while the minor moons still need the invisible node. Update the BACKLOG line's clause to match.
+- [ ] `npm run typecheck:fast`, then `npm test -- planetEphemeris deriveBodyStates orbitTrailsPass`.
+      Commit "Accurate planet positions: corrections + Earth–Moon pair".
+
+---
+
+## Dispatch grouping (controller)
+
+| PR | Dispatch | Tasks | Model |
+|---|---|---|---|
+| 1 | A, or inline (< 50 lines of source) | 1, 2 | Sonnet |
+| 2 | B | 3, 4, 5 (the tool chain; Task 5 has `review: yes`) | Opus |
+| 2 | C | 6 (`review: yes`) | Opus |
+
+Ask at plan start: parallelism, and whether to run the perf gate. Recommended: no perf gate, because
+the per-frame cost is about 590 sinusoids per new `simDays` and trails add nothing.
+
+## Definition of done
+
+**Deliverables:**
+- `PLANET_EPHEMERIS_CORRECTIONS` (generated)
+- `ephemerisCorrectionMpc`
+- `BARYCENTRIC_PAIRS`
+- `npm run fetch-horizons-planets` and `npm run build-planet-ephemeris`
+- `OBLIQUITY_DEG = 23.4392911`
+- trails anchored on the snapshot
+
+**Manual smoke** (the user looks; the dev server stays running):
+- The clock set to 1980-11-12: Saturn is where Horizons puts it, and the inspector's position
+  matches JPL to within ~1,000 km.
+- Zoom close to Saturn and Jupiter with time running fast: each stays on its trail.
+- Park at Earth with a 1-day/s clock: the Earth–Moon wobble is visible against the trail, and the
+  Moon stays on its trail.
+- Set the clock to 1850 and to 2200: the planets are finite, there is no jump as the clock crosses
+  1900 and 2100, and the trails are intact.
+
+**Out of scope (deferral boundary):**
+- moon accuracy
+- the Pluto–Charon pair row and Pluto's minor moons
+- spacecraft and Voyager (the mission-trails spec is next)
+- runtime TDB conversion
+- any margin in `orbitReachByRegion`
diff --git a/docs/superpowers/specs/2026-10-04-accurate-planet-positions-design.md b/docs/superpowers/specs/2026-10-04-accurate-planet-positions-design.md
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+# Accurate planet positions — design spec
+
+Child of the Voyager mission-trails brainstorm (2026-09-28 → 2026-10-03). Voyager's flybys
+are only as honest as the planets they pass: today's Keplerian planets drift from JPL by
+98k km at Jupiter up to 1.6M km at Saturn at the flyby dates, 9–16× the miss distances. On
+2026-10-03 the user ruled that **the accurate physical planet position is the source of
+truth**, independent of any flyby window, and that it ships as its own spec and PR before the
+mission-trails spec.
+
+## 1. What this is
+
+Heliocentric positions of the eight planets match JPL DE (Horizons) to **≤ 1,000 km over
+1900–2100**. That is 3% of the closest planet flyby (Voyager 2 at Neptune, ~29,000 km from
+centre). Four parts:
+
+- **A correction series per planet**, added on top of today's Keplerian position. It is a
+  cubic polynomial plus fitted sinusoids, generated offline from Horizons and shipped as
+  constants. All eight planets together take ~590 terms, about 17 kB. A build tool fits it
+  and checks it against JPL.
+- **Earth wobbles around the Earth–Moon barycentre (EMB).** The `earth` element row already
+  describes the EMB, so Earth = EMB − k·(Moon's geocentric offset), with k the Moon's share of
+  the pair's mass.
+- **Orbit trails follow the corrected body.** Each trail is the same Keplerian conic,
+  translated so it passes through the body's snapshot position.
+- **Exact obliquity.** `OBLIQUITY_DEG` becomes 23.4392911° instead of the rounded 23.44°.
+
+**Out of scope:**
+- Moon accuracy. Moons keep their own element rows.
+- Pluto–Charon. That becomes one more pair row later (§6).
+- Spacecraft. Mission trails is the next spec and reuses the fetch tool.
+- Any runtime TDB time scale.
+
+## 2. Ground preparation
+
+Refactor-ground ran on 2026-10-03. It sent an Explore trace over every reader of a planet's
+position and over the trail pass, and ran a greenfield cross-check. The user signed off on the
+checkpoint.
+
+| Touchpoint | Verdict | Seam |
+|---|---|---|
+| Body position (`deriveBodyStates.ts:63-67`) | growth | one added term in the 1b loop; it is the only place positions are composed |
+| Orbit trail (`orbitTrailsPass.ts:101-109`) | **bolt-on → P1** | the pass re-propagates each conic and re-folds the focus itself, a mirror of `deriveBodyStates`. The body sits on its trail only because both happen to agree, so adding the correction here would make a second copy |
+| Obliquity (`orbitPlaneFrames.ts:72`) | **wrong constant → P2** | the fit is generated against the app's frame, so the constant must be right before the first generation |
+| Earth wobble | growth | a new pair table read in the same 1b loop. No focus-graph node: the backlog's invisible-node design is needed only for Pluto's minor moons |
+| Synchronous readers at module load (`bodyRegions.ts:29`, `starCatalog/create.ts:63`) | growth | the generated `.ts` is a static import, as with `bodyFacts.generated.ts` |
+| Generated data | growth | `tools/bodies/buildPlanetFacts.ts` precedent: banner, prettier, committed output |
+
+**The greenfield cross-check diverged on three points, all resolved by measurement or ruling:**
+- **Residual table → fitted series.** A table needs ~140 kB in f32 (Mercury needs a 13-day
+  step); the series needs ~17 kB.
+- **Sampled trail with a geometric tail → translated conic.** With a translated conic the
+  worst case is Saturn: 4 px with the whole orbit 1,000 px wide, and 0.34° tangent error close
+  up. Mercury through Earth stay under 0.1 px.
+- **Spacecraft in planet-relative legs → rejected.** With accurate planets, heliocentric
+  samples are enough. That decision belongs to the mission-trails spec.
+
+**Prep, as a separate PR (ruled 2026-10-04):**
+
+- **P1: trails anchor on the snapshot body.** `orbitTrailsPass` takes
+  `centreMpc = state.positionMpc − keplerianPositionMpc(propagated) + centerOffsetMpc` instead
+  of `focus + centerOffsetMpc`.
+  - This is behaviour-neutral today, apart from f64 rounding.
+  - Once this lands, the body sits on its own trail by construction rather than by coincidence.
+  - Any later change to a body's position (correction, pair reflex, a moon's parent) moves the
+    trail with it.
+  - The 18–20-digit trail tests (`orbitTrailsPass.test.ts:345-378`, `:511-573`) move to a
+    tolerance that f64 can actually hold.
+  - The `orbitalElements.ts` header line about the invariant is rewritten to name the new
+    mechanism.
+- **P2: exact obliquity.** `OBLIQUITY_DEG = 23.4392911` (IAU 1980 / J2000 mean obliquity).
+  - The obliquity literals in tests follow: `orbitPlaneFrames.test.ts:53`,
+    `orientationFrames.test.ts:54`, and the comments in `propagateElements.test.ts:94` and
+    `earthTerminator.test.ts:17`. So do the `23.44°` comments in `rotationLookAt.ts` and
+    `defaults.ts`.
+  - The fixture `tests/fixtures/bodyStatesJ2000.json` and the camera golden traces are
+    re-recorded, under this ruling, with `SETTLE_GOLDEN_RECORD=1` and `DRIVER_GOLDEN_RECORD=1`.
+
+## 3. Data shapes
+
+```ts
+// src/@types/scene/EphemerisCorrection.d.ts — one planet's DE − Kepler correction, km
+export type EphemerisCorrection = {
+  startJd: number; endJd: number;     // fitted span; outside it the edge value is held
+  polyKm: readonly [Vec3, Vec3, Vec3, Vec3]; // cubic in τ = 2(t−start)/(end−start) − 1
+  // flat (ω rad/day, cos x,y,z, sin x,y,z) per term; phase measured from startJd
+  terms: readonly number[];
+};
+
+// src/@types/scene/BarycentricPair.d.ts — the primary's element row describes the pair barycentre
+export type BarycentricPair = { primaryId: string; secondaryId: string; secondaryMassFraction: number };
+
+// src/data/bodies/planetEphemerisCorrections.generated.ts   (GENERATED — DO NOT EDIT)
+export const PLANET_EPHEMERIS_CORRECTIONS: Readonly<Record<string, EphemerisCorrection>>;
+
+// src/data/bodies/barycentricPairs.ts
+export const BARYCENTRIC_PAIRS: readonly BarycentricPair[] =
+  [{ primaryId: 'earth', secondaryId: 'moon', secondaryMassFraction: 1 / 82.30057 }];
+```
+
+**Frame and time are pinned by construction, not converted at runtime.**
+- **Frame.** The fit tool computes `DE − app Kepler` in the app's own equatorial frame, so any
+  residual frame bias is absorbed into the correction.
+- **Time.** Horizons is fetched with `TIME_TYPE='UT'`, which is verified to be accepted for
+  vector tables, so the TDB−UTC gap (~69 s, ~2,000 km at Earth) is absorbed as well. `simDays`
+  stays a UTC Julian date.
+- **Planet targets.** Mercury and Venus use their planet centres (199, 299). Earth through
+  Neptune use their system barycentres (3–8), because the planet-centre wobble caused by moons
+  is ≤ 300 km.
+
+## 4. Runtime
+
+- **`src/utils/orbit/ephemerisCorrectionMpc.ts`** —
+  `(c: EphemerisCorrection, simDays: number) => Vec3`. It clamps `simDays` to
+  `[startJd, endJd]` (the ruled freeze-at-edge), sums the polynomial and the terms in f64 km,
+  then converts to Mpc. The conversion happens before the sum joins an au-scale position, as in
+  the site-offset precedent at `deriveBodyStates.ts:88-94`.
+- **`deriveBodyStates` 1b:**
+  `position = focus + kepler(el) + correction(el.id) − pairReflex(el.id)`.
+  - `pairReflex` is `secondaryMassFraction · keplerianPositionMpc(propagateElements(secondary))`
+    for a primary listed in `BARYCENTRIC_PAIRS`.
+  - The secondary's offset is computed inline, because `FOCUS_ORDER` resolves `earth` before
+    `moon`.
+  - Dependants of `earth` (the Moon, Hubble, the easter eggs, Earth sites) follow the
+    reflexed Earth automatically. So Moon = EMB + (1−k)·geo, which is physically right.
+- **Cost:** about 590 sinusoid evaluations per new `simDays`, a few µs. The existing one-deep
+  memo makes paused frames free. Trails add nothing, because P1 reads the snapshot.
+
+## 5. Tools
+
+- **`tools/fetch/fetchHorizonsPlanets.ts`** (`npm run fetch-horizons-planets`).
+  - Fetches 1-day equatorial heliocentric vectors, 1900–2100, in 50-year chunks with retry.
+  - Writes them to `data/raw/horizons/planets/<naif>.csv`.
+  - The output is gitignored, registered in `rawDataRegistry.ts` with a README next to it
+    that records the exact API query.
+- **`tools/bodies/buildPlanetEphemeris.ts`** (`npm run build-planet-ephemeris`).
+  - Subtracts the app's Kepler position using the `src/` propagation, imported as
+    `buildPlanetFacts` imports `src` types.
+  - Fits each planet greedily: cubic polynomial, then sinusoids. Each frequency is the
+    zero-padded FFT peak of the remaining residual, and a Gram–Schmidt step refits all
+    coefficients exactly by least squares.
+  - Stops once a planet is ≤ 900 km, leaving margin.
+  - **Verifies every planet on the dense 1-day grid** and throws above 1,000 km.
+  - Writes the generated file with a banner plus prettier.
+  - Helpers go one function per file under `tools/utils/math/` (`fft.ts`,
+    `fitSinusoidSeries.ts`).
+- **Regeneration rule:** any edit to a planet's element row or to the frame requires
+  re-running the build tool. The test in §7 fails until it is re-run.
+
+## 6. Docs and backlog
+
+- `scenePlanets.ts:3`: rewrite the stale "positions via keplerianPositionMpc" header.
+- `docs/backlog/2026-08-16-barycentric-orbit-pairs.md`: note that the pair table now exists.
+  Pluto's wobble becomes one `BARYCENTRIC_PAIRS` row; the minor moons still need the invisible
+  node. The BACKLOG line stays and its clause is updated.
+- `docs/DATA.md`: add a Horizons fetch entry.
+- `orbitReachByRegion` gets no margin for the correction. ≤ 8M km is negligible against
+  Pluto's ~50 au reach. Recorded here, not backlogged.
+
+## 7. Tests
+
+- **`tests/data/bodies/planetEphemeris.test.ts`.**
+  - Fixture: a committed Horizons fixture, `tests/fixtures/horizonsPlanets.json`, with 6 dates
+    × 8 planets, UT, equatorial.
+  - `deriveBodyStates` must be ≤ 1,000 km from each fixture vector.
+  - It fails if anyone edits a planet's elements or the frame without regenerating.
+  - Earth is checked against Horizons 399 (Earth centre) to ≤ 1,000 km plus the Moon-model
+    error. The tolerance is stated in the test after measurement.
+- **`ephemerisCorrectionMpc.test.ts`:** a clamped date returns exactly the edge value
+  (freeze), with continuity across `startJd` and `endJd`.
+- **Pair reflex:**
+  - Earth–Moon distance is unchanged.
+  - The EMB, computed as (1−k)·Earth + k·Moon, equals the old Earth position.
+- **Re-recorded:**
+  - `tests/fixtures/bodyStatesJ2000.json`
+  - the camera golden traces
+  - `tools/perf/perfScenarios.ts:52` `EARTH_TARGET`
+  - the 2024-04-08 eclipse test keeps its 2° tolerance, and should tighten.
+
+## 8. PR sequence
+
+1. **Prep PR** (separate, ruled): P1 and P2, each its own commit. They are behaviour-neutral
+   except for the obliquity.
+2. **Feature PR**, built on top of it:
+   - fetch tool and raw-registry entry
+   - fit tool and helpers
+   - generated corrections
+   - pair table and the `deriveBodyStates` term
+   - tests, docs and backlog edits
diff --git a/src/data/bodies/orbitPlaneFrames.ts b/src/data/bodies/orbitPlaneFrames.ts
index 2fc9c25919..5dc8c9f39b 100644
--- a/src/data/bodies/orbitPlaneFrames.ts
+++ b/src/data/bodies/orbitPlaneFrames.ts
@@ -20,13 +20,13 @@
  * sits ~15° off Saturn's equator) rides its true plane rather than the shared
  * equatorial one — hence `planeFrameFromPole` is exported. The ecliptic is
  * simply the frame of the ecliptic pole, so `planeFrameFromPole` reproduces
- * `ECLIPTIC_FRAME` exactly (it equals `planeFrameFromPole(270, 66.56)` to
+ * `ECLIPTIC_FRAME` exactly (it equals `planeFrameFromPole(270, 66.5607089)` to
  * floating-point noise); `ECLIPTIC_FRAME` is written out directly from the
- * obliquity so the 23.44° has a single, legible source.
+ * obliquity so the 23.439° has a single, legible source.
  *
  * The ecliptic — the plane of Earth's orbit, which every OTHER solar-system
  * body (the Moon, the planets) also orbits near — is tilted from the scene's
- * equatorial xy-plane by Earth's axial tilt, the obliquity ε ≈ 23.44°. The two
+ * equatorial xy-plane by Earth's axial tilt, the obliquity ε ≈ 23.439°. The two
  * planes share one line: the equinox, where the Sun crosses the equatorial
  * plane heading north each spring. That shared line is exactly frame +x, so +x
  * needs no transform to land in the ecliptic; rotating equatorial +y by ε about
@@ -68,14 +68,14 @@ export function planeFrameFromPole(poleRaDeg: number, poleDecDeg: number): Orbit
   return { xAxis, yAxis, normal };
 }
 
-// Earth's axial tilt: the angle between the equatorial and ecliptic planes.
-const OBLIQUITY_DEG = 23.44;
+// IAU J2000 mean obliquity: the angle between the equatorial and ecliptic planes.
+const OBLIQUITY_DEG = 23.4392911;
 
 /**
  * The ecliptic frame: the equinox +x is the shared node, and the y/z axes carry
  * the obliquity ε — `yAxis` is equatorial +y rotated by ε about +x, `normal` is
  * equatorial +z rotated the same. Written directly from `OBLIQUITY_DEG` so the
- * 23.44° has one source.
+ * 23.439° has one source.
  */
 const eps = degToRad(OBLIQUITY_DEG);
 export const ECLIPTIC_FRAME: OrbitPlaneFrame = {
diff --git a/src/data/bodies/orbitalElements.ts b/src/data/bodies/orbitalElements.ts
index 024a69fb8e..103a0a1138 100644
--- a/src/data/bodies/orbitalElements.ts
+++ b/src/data/bodies/orbitalElements.ts
@@ -1,12 +1,13 @@
 /**
  * orbitalElements — the J2000 Keplerian table, single source of truth for BOTH body
- * positions (`keplerianPositionMpc`) and their trails (`keplerianEllipse`), so a body sitting
- * on its own trail is structural rather than an invariant to remember. Per row: `focusId` (the
- * Sun for planets, the parent planet for a moon) and `plane` (omitted = ecliptic, which is how
- * JPL publishes the planets and the Moon; a planet's own moons ride their OWN Laplace pole —
- * see `orbitPlaneFrames.ts`). No buried Mpc/radian literals, and JPL's `L`/`ϖ` columns are
- * converted inline (`ω = ϖ − Ω`, `M = L − ϖ`, likewise the rates) so every transcription stays
- * checkable against the source: JPL SSD approx_pos.html Table 1 (planets), sats/elem (moons).
+ * positions (`keplerianPositionMpc`) and their trails (`keplerianEllipse`); the trail pass
+ * anchors each trail on the snapshot body position, so a body sits on its own trail by
+ * construction. Per row: `focusId` (the Sun for planets, the parent planet for a moon) and
+ * `plane` (omitted = ecliptic, which is how JPL publishes the planets and the Moon; a planet's
+ * own moons ride their OWN Laplace pole — see `orbitPlaneFrames.ts`). No buried Mpc/radian
+ * literals, and JPL's `L`/`ϖ` columns are converted inline (`ω = ϖ − Ω`, `M = L − ϖ`,
+ * likewise the rates) so every transcription stays checkable against the source: JPL SSD
+ * approx_pos.html Table 1 (planets), sats/elem (moons).
  */
 
 import { SCALE_UNITS } from '../scaleUnits';
diff --git a/src/data/defaults.ts b/src/data/defaults.ts
index 101f150d20..fbbc6e769f 100644
--- a/src/data/defaults.ts
+++ b/src/data/defaults.ts
@@ -135,9 +135,9 @@ export const DEFAULT_FOV_DEG = 60;
  *
  * Ecliptic, not equatorial: the descent lands in the solar system, and the
  * ecliptic frame puts Earth's orbital plane flat so the planets read as a disk
- * and Earth's 23.44° obliquity is *desired* — the tilt between the equatorial
+ * and Earth's 23.439° obliquity is *desired* — the tilt between the equatorial
  * and ecliptic poles is exactly what makes the seasons legible in that view.
  * Booting equatorial would instead flatten Earth's equator and rake the orbital
- * plane at that same 23.44°, which is the wrong "up" for the arrival scene.
+ * plane at that same 23.439°, which is the wrong "up" for the arrival scene.
  */
 export const DEFAULT_ORIENTATION: OrientationFrameId = 'ecliptic';
diff --git a/src/services/engine/frame/passes/orbitTrailsPass.ts b/src/services/engine/frame/passes/orbitTrailsPass.ts
index dd77c0d804..5ff7f1fb15 100644
--- a/src/services/engine/frame/passes/orbitTrailsPass.ts
+++ b/src/services/engine/frame/passes/orbitTrailsPass.ts
@@ -15,6 +15,7 @@ import { ORBIT_REACH_BY_REGION } from '../../../../data/bodies/orbitReachByRegio
 import { CULL_PX, FULL_PX } from '../../../../data/bodies/orbitTrailConstants';
 import { regionRelativeDistanceMpc } from '../../../../utils/regions/regionRelativeDistanceMpc';
 import { propagateElements } from '../../../../utils/orbit/propagateElements';
+import { keplerianPositionMpc } from '../../../../utils/orbit/keplerianPositionMpc';
 import { keplerianEllipse } from '../../../../utils/orbit/keplerianEllipse';
 import { composeOrbitConic } from '../../../../utils/camera/composeOrbitConic';
 import { sampledDepthBinding } from '../sampledDepthBinding';
@@ -96,17 +97,19 @@ export const orbitTrailsPass: ContentPass = {
     for (let i = 0; i < limit; i++) {
       const elements = rows[i]!;
       // Re-derived at the frame instant, never baked. `keplerianEllipse` returns
-      // FRESH vectors per call, so the in-place focus fold below cannot alias a
+      // FRESH vectors per call, so the in-place anchoring below cannot alias a
       // shared scratch across orbits.
       const propagated = propagateElements(elements, ctx.snapshot.simDays);
       const { centerOffsetMpc, semiMajorMpc, semiMinorMpc } = keplerianEllipse(propagated);
-      // The snapshot seeds anchors (the Sun) alongside every element row, so a
-      // heliocentric focus and a moving parent are the same lookup.
-      const focus = states.get(elements.focusId)!.positionMpc;
+      // Centre = the snapshot body position, less its raw Kepler offset, plus the
+      // ellipse centre offset: the body sits on its trail by construction, so any
+      // later correction to the snapshot position moves the trail with it.
+      const bodyMpc = states.get(elements.id)!.positionMpc;
+      const keplerMpc = keplerianPositionMpc(propagated);
       const centerMpc = centerOffsetMpc;
-      centerMpc[0] += focus[0];
-      centerMpc[1] += focus[1];
-      centerMpc[2] += focus[2];
+      centerMpc[0] += bodyMpc[0] - keplerMpc[0];
+      centerMpc[1] += bodyMpc[1] - keplerMpc[1];
+      centerMpc[2] += bodyMpc[2] - keplerMpc[2];
 
       const dx = centerMpc[0] - camPos[0];
       const dy = centerMpc[1] - camPos[1];
diff --git a/src/utils/orbit/rotationLookAt.ts b/src/utils/orbit/rotationLookAt.ts
index fa395fe089..861d3fff15 100644
--- a/src/utils/orbit/rotationLookAt.ts
+++ b/src/utils/orbit/rotationLookAt.ts
@@ -16,7 +16,7 @@ import { mat3FromColumns } from '../math/mat3FromColumns';
 import { normalize3 } from '../math/normalize3';
 
 // Positions are equatorial-world, so the ecliptic pole is the obliquity-tilted
-// frame normal rather than +z; `ECLIPTIC_FRAME` owns the 23.44°.
+// frame normal rather than +z; `ECLIPTIC_FRAME` owns the 23.439°.
 // Below this residual length (≈ the boresight-to-pole angle in radians) the
 // projection has no direction left to carry the roll, so a second, always
 // non-parallel reference takes over — the equinox, the frame's own +X.
diff --git a/tests/data/bodies/orbitPlaneFrames.test.ts b/tests/data/bodies/orbitPlaneFrames.test.ts
index 39aee8f5e7..89ae6b0ce2 100644
--- a/tests/data/bodies/orbitPlaneFrames.test.ts
+++ b/tests/data/bodies/orbitPlaneFrames.test.ts
@@ -47,9 +47,9 @@ describe('orbit plane frames', () => {
 
   it('tilts the ecliptic normal from frame +z by the obliquity', () => {
     // Both are unit vectors, so the dot product is cos(angle) directly. The
-    // expected obliquity is written as the literal 23.44° in radians rather than
+    // expected obliquity is written as the literal 23.4392911° in radians rather than
     // through degToRad, so a broken conversion would not hide behind a mirror.
     const cosAngle = dot(ECLIPTIC_FRAME.normal, [0, 0, 1]);
-    expect(Math.acos(cosAngle)).toBeCloseTo((23.44 * Math.PI) / 180, 12);
+    expect(Math.acos(cosAngle)).toBeCloseTo((23.4392911 * Math.PI) / 180, 12);
   });
 });
diff --git a/tests/data/orientation/orientationFrames.test.ts b/tests/data/orientation/orientationFrames.test.ts
index 588230975e..787bdd6ed3 100644
--- a/tests/data/orientation/orientationFrames.test.ts
+++ b/tests/data/orientation/orientationFrames.test.ts
@@ -51,8 +51,8 @@ describe('ORIENTATION_FRAMES', () => {
   });
 
   it('ecliptic pole matches the obliquity pole from planeFrameFromPole', () => {
-    // 66.56° = 90° − 23.44°: the ecliptic north pole in equatorial RA/Dec.
-    const pole = planeFrameFromPole(270, 66.56).normal;
+    // 66.5607089° = 90° − 23.4392911°: the ecliptic north pole in equatorial RA/Dec.
+    const pole = planeFrameFromPole(270, 90 - 23.4392911).normal;
     const mid = col(ORIENTATION_FRAMES.ecliptic, 1);
     expect(mid[0]).toBeCloseTo(pole[0], 4);
     expect(mid[1]).toBeCloseTo(pole[1], 4);
diff --git a/tests/fixtures/bodyStatesJ2000.json b/tests/fixtures/bodyStatesJ2000.json
index e97a9abef9..17b64148f2 100644
--- a/tests/fixtures/bodyStatesJ2000.json
+++ b/tests/fixtures/bodyStatesJ2000.json
@@ -1,11 +1,15 @@
 {
   "callisto": {
-    "positionMpc": [1.9395074114394832e-11, 1.3353048102062752e-11, 5.254328189844694e-12],
-    "orientation": [-0.17492209617849083,-0.8904283175465342,-0.4201662427894122,0.984536438326655,-0.162305061611009,-0.06591713421039394,-0.009500625010351543,-0.4251993394711415,0.9050498659398374],
+    "positionMpc": [1.9395074114394832e-11, 1.3353112790826594e-11, 5.254163647580489e-12],
+    "orientation": [
+      -0.17492209617849083, -0.8904283175465342, -0.4201662427894122, 0.984536438326655,
+      -0.162305061611009, -0.06591713421039394, -0.009500625010351543, -0.4251993394711415,
+      0.9050498659398374
+    ],
     "meanAnomalyRad": 1.5254177662430441
   },
   "charon": {
-    "positionMpc": [-4.791450444930355e-11, -1.3566802983502213e-10, -2.790299055313828e-11],
+    "positionMpc": [-4.791450444930355e-11, -1.3566837505179883e-10, -2.7901311982952056e-11],
     "orientation": [
       0.3334893355513799, 0.43442810728528536, 0.8366941392611901, 0.65509112052934,
       0.5314492493346875, -0.5370449880458906, -0.6779679099169169, 0.7272096774535675,
@@ -14,49 +18,77 @@
     "meanAnomalyRad": 5.307546255314756
   },
   "deimos": {
-    "positionMpc": [6.7424822969448034e-12, 6.384457595165361e-15, -1.795630494941746e-13],
-    "orientation": [-0.4463842202746905,0.6779087814648913,0.5841068497308886,-0.7834711648414804,-0.6114518589447622,0.11090337260394045,0.4323355892726048,-0.40812535844490344,0.8040644439611346],
+    "positionMpc": [6.7424822969448034e-12, 6.3822415228828266e-15, -1.7956313479591653e-13],
+    "orientation": [
+      -0.4463842202746905, 0.6779087814648913, 0.5841068497308886, -0.7834711648414804,
+      -0.6114518589447622, 0.11090337260394045, 0.4323355892726048, -0.40812535844490344,
+      0.8040644439611346
+    ],
     "meanAnomalyRad": 3.5779249665883754
   },
   "dione": {
-    "positionMpc": [3.1097913153309065e-11, 2.9839498609464e-11, 1.0980813348118515e-11],
-    "orientation": [0.1500314083433411,-0.9868524640256249,0.060106495132111006,0.9849676241424642,0.14392708758779407,-0.0955184424582236,0.08561165751031316,0.07353371815057563,0.9936113105200084],
+    "positionMpc": [3.1097913153309065e-11, 2.983963447795244e-11, 1.0980444303639635e-11],
+    "orientation": [
+      0.1500314083433411, -0.9868524640256249, 0.060106495132111006, 0.9849676241424642,
+      0.14392708758779407, -0.0955184424582236, 0.08561165751031316, 0.07353371815057563,
+      0.9936113105200084
+    ],
     "meanAnomalyRad": 3.7000980142279785
   },
   "earth": {
-    "positionMpc": [-8.589504546518782e-13, 4.302223432556485e-12, 1.865304005019885e-12],
+    "positionMpc": [-8.589504546518782e-13, 4.302246510960393e-12, 1.8652507750193955e-12],
     "orientation": [
       0.1761742596326785, -0.9843589945964214, 0, 0.9843589945964214, 0.1761742596326785, 0, 0, 0, 1
     ],
     "meanAnomalyRad": -0.04316391697638581
   },
   "enceladus": {
-    "positionMpc": [3.1104454125073664e-11, 2.982129424379336e-11, 1.0981597288866233e-11],
-    "orientation": [-0.6101639042418044,0.79225204377477,-0.006058803107722217,-0.7876361177972574,-0.6057470523491235,0.11269363119366291,0.08561165751031316,0.07353371815057563,0.9936113105200084],
+    "positionMpc": [3.1104454125073664e-11, 2.9821430112281805e-11, 1.0981228244387354e-11],
+    "orientation": [
+      -0.6101639042418044, 0.79225204377477, -0.006058803107722217, -0.7876361177972574,
+      -0.6057470523491235, 0.11269363119366291, 0.08561165751031316, 0.07353371815057563,
+      0.9936113105200084
+    ],
     "meanAnomalyRad": 0.9948376736367678
   },
   "europa": {
-    "positionMpc": [1.9366208544821226e-11, 1.3288486688770912e-11, 5.223331413650205e-12],
-    "orientation": [0.8440426953875887,0.47876521241452585,0.24161084359880872,-0.5360821137690424,0.7653676116425182,0.35612973246493035,-0.014418587301453609,-0.43011195104333155,0.902660408963376],
+    "positionMpc": [1.9366208544821226e-11, 1.3288551377534754e-11, 5.2231668713859995e-12],
+    "orientation": [
+      0.8440426953875887, 0.47876521241452585, 0.24161084359880872, -0.5360821137690424,
+      0.7653676116425182, 0.35612973246493035, -0.014418587301453609, -0.43011195104333155,
+      0.902660408963376
+    ],
     "meanAnomalyRad": 6.028367236388414
   },
   "ganymede": {
-    "positionMpc": [1.935782125182158e-11, 1.327889867944624e-11, 5.2186285300575744e-12],
-    "orientation": [0.7670029894074187,0.5750114317615406,0.28472489807466117,-0.6415017437254595,0.6965288928160546,0.3214389744098182,-0.013488033113756947,-0.42919617288133427,0.903110579135655],
+    "positionMpc": [1.935782125182158e-11, 1.3278963368210082e-11, 5.218463987793369e-12],
+    "orientation": [
+      0.7670029894074187, 0.5750114317615406, 0.28472489807466117, -0.6415017437254595,
+      0.6965288928160546, 0.3214389744098182, -0.013488033113756947, -0.42919617288133427,
+      0.903110579135655
+    ],
     "meanAnomalyRad": 5.668829410477583
   },
   "iapetus": {
-    "positionMpc": [3.112403542854821e-11, 2.9938815769420106e-11, 1.0993574885840525e-11],
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   "jupiter": {
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@@ -65,7 +97,7 @@
     "meanAnomalyRad": 0.34327067101878284
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@@ -74,7 +106,7 @@
     "meanAnomalyRad": 0.3384227896851049
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+    "positionMpc": [-6.306874292609911e-13, -1.942153167646951e-12, -9.720109452033183e-13],
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@@ -83,12 +115,16 @@
     "meanAnomalyRad": 3.050705107870811
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   "moon": {
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+    "positionMpc": [-8.684282394279855e-13, 4.293738774580142e-12, 1.8628218170240537e-12],
     "orientation": [
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@@ -97,7 +133,7 @@
     "meanAnomalyRad": 2.3609068791727297
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   "neptune": {
-    "positionMpc": [8.147178919019027e-11, -1.1141464182571051e-10, -4.763257192058855e-11],
+    "positionMpc": [8.147178919019027e-11, -1.1141523115780291e-10, -4.7631193423792595e-11],
     "orientation": [
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@@ -106,12 +142,16 @@
     "meanAnomalyRad": -1.746809150875549
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   "phobos": {
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+    "positionMpc": [6.742083325040046e-12, 6.609864655853662e-15, -1.7921380717377167e-13],
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   "pluto": {
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+    "positionMpc": [-4.791428248023062e-11, -1.3566809091209427e-10, -2.7900789044928168e-11],
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@@ -130,8 +170,12 @@
     "meanAnomalyRad": 0.08515672394345941
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@@ -320,7 +364,7 @@
     "meanAnomalyRad": 5.630129826433361
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-    "positionMpc": [3.1099752807904804e-11, 2.9827398693151044e-11, 1.0981551367914625e-11],
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@@ -329,17 +373,25 @@
     "meanAnomalyRad": -0.7442892730041829
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   "titan": {
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   "uranus": {
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+    "positionMpc": [6.993663216219453e-11, -6.06470857509395e-11, -2.755153855411126e-11],
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@@ -348,7 +400,7 @@
     "meanAnomalyRad": 2.48332127460649
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   "venus": {
-    "positionMpc": [-3.4824959657808e-12, -2.2458100936506426e-13, 1.1936386084274154e-13],
+    "positionMpc": [-3.4824959657808e-12, -2.2457953250190632e-13, 1.1936663949337553e-13],
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@@ -362,12 +414,12 @@
     "meanAnomalyRad": 2.1093550674103057
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   "whale": {
-    "positionMpc": [-8.589504546518782e-13, 4.302442865722174e-12, 1.865304005019885e-12],
+    "positionMpc": [-8.589504546518782e-13, 4.3024659441260814e-12, 1.8652507750193955e-12],
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   "petunias": {
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@@ -375,25 +427,25 @@
     "meanAnomalyRad": -0.000005907546891153448
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   "voyager1": {
-    "positionMpc": [-9.849911903784252e-11, -3.472694889308621e-10, 7.700732265421764e-11],
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   "voyager2": {
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   "hubble": {
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     "orientation": [
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       6.123233995736766e-17, 1, -6.123233995736766e-17, 6.123233995736766e-17
diff --git a/tests/fixtures/camera/driverGoldenTrace.json b/tests/fixtures/camera/driverGoldenTrace.json
index 825918f1c4..9257d51b8c 100644
--- a/tests/fixtures/camera/driverGoldenTrace.json
+++ b/tests/fixtures/camera/driverGoldenTrace.json
@@ -3,15 +3,31 @@
     "label": "boot 0",
     "winner": "resting",
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       "distanceTarget": null,
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+      "panOffset": [
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     "epochs": {
       "tween": {
@@ -35,21 +51,39 @@
         "refNull": true
       }
     },
-    "actions": ["engine/engineScaleChanged"]
+    "actions": [
+      "engine/engineScaleChanged"
+    ]
   },
   {
     "label": "boot 3",
     "winner": "resting",
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       "distanceTarget": null,
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+      "panOffset": [
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     "epochs": {
       "tween": {
@@ -73,21 +107,39 @@
         "refNull": true
       }
     },
-    "actions": ["engine/engineScaleChanged"]
+    "actions": [
+      "engine/engineScaleChanged"
+    ]
   },
   {
     "label": "drag 0",
     "winner": "orbitDrag",
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+      "panOffset": [
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       "tween": {
@@ -111,21 +163,39 @@
         "refNull": true
       }
     },
-    "actions": ["engine/engineScaleChanged"]
+    "actions": [
+      "engine/engineScaleChanged"
+    ]
   },
   {
     "label": "drag end",
     "winner": "resting",
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       "tween": {
@@ -149,21 +219,41 @@
         "refNull": true
       }
     },
-    "actions": ["camera/commitCameraPose", "camera/endDrag", "engine/engineScaleChanged"]
+    "actions": [
+      "camera/commitCameraPose",
+      "camera/endDrag",
+      "engine/engineScaleChanged"
+    ]
   },
   {
     "label": "follow 0",
     "winner": "followApproach",
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@@ -1383,23 +1962,39 @@
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@@ -1423,23 +2018,39 @@
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@@ -1463,23 +2074,39 @@
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@@ -1503,23 +2130,40 @@
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+    "actions": [
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@@ -1543,23 +2187,39 @@
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@@ -1583,23 +2243,39 @@
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@@ -1623,23 +2299,39 @@
         "refNull": true
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-    "actions": ["engine/engineScaleChanged"]
+    "actions": [
+      "engine/engineScaleChanged"
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@@ -1663,23 +2355,39 @@
         "refNull": true
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-    "actions": ["engine/engineScaleChanged"]
+    "actions": [
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+    ]
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@@ -1703,23 +2411,40 @@
         "refNull": true
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-    "actions": ["camera/commitCameraPose", "engine/engineScaleChanged"]
+    "actions": [
+      "camera/commitCameraPose",
+      "engine/engineScaleChanged"
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   {
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@@ -1743,23 +2468,39 @@
         "refNull": true
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-    "actions": ["engine/engineScaleChanged"]
+    "actions": [
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+    ]
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@@ -1783,23 +2524,41 @@
         "refNull": true
       }
     },
-    "actions": ["camera/commitCameraPose", "camera/endDrag", "engine/engineScaleChanged"]
+    "actions": [
+      "camera/commitCameraPose",
+      "camera/endDrag",
+      "engine/engineScaleChanged"
+    ]
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   {
     "label": "pan settle 0",
     "winner": "followApproach",
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+        -2.34353082474e-16,
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       "tween": {
@@ -1823,23 +2582,39 @@
         "refNull": true
       }
     },
-    "actions": ["engine/engineScaleChanged"]
+    "actions": [
+      "engine/engineScaleChanged"
+    ]
   },
   {
     "label": "pan settle 3",
     "winner": "followApproach",
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+        -2.34353082474e-16,
+        2.47092161044e-17
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     "epochs": {
       "tween": {
@@ -1863,6 +2638,8 @@
         "refNull": true
       }
     },
-    "actions": ["engine/engineScaleChanged"]
+    "actions": [
+      "engine/engineScaleChanged"
+    ]
   }
 ]
diff --git a/tests/fixtures/camera/settleGoldenTrace.json b/tests/fixtures/camera/settleGoldenTrace.json
index 7f4c6293ef..a92851fe34 100644
--- a/tests/fixtures/camera/settleGoldenTrace.json
+++ b/tests/fixtures/camera/settleGoldenTrace.json
@@ -5,10 +5,22 @@
       "arm": "absolute",
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@@ -17,12 +29,22 @@
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@@ -31,354 +53,734 @@
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+        0.0785409033636
+      ],
+      "memory": 2.73317926959
     },
     {
       "label": "re-dive 14",
       "arm": "earth",
-      "hr": 0.449022788525,
+      "hr": 0.449022777574,
       "displayed": [
-        -8.58812915346e-13, 4.30206950158e-12, 1.86530825661e-12, 0.792064079893, 0.148535184229,
-        9.36724058737e-17, 0.0785409051511
+        -8.58812915346e-13,
+        4.30209258004e-12,
+        1.86525502852e-12,
+        0.79206408103,
+        0.148535164831,
+        9.36724038973e-17,
+        0.0785409033636
       ],
       "register": [
-        0, 0, 0, 7762490.13457, 4989271.48472, -275042.547948, -0.495946113036, 0.791703341311,
-        0.356711749627, 0.314704012642, -0.218991606864, 0.923582189386, -0.809319984549,
-        -0.570305615859, 0.140544182121
-      ],
-      "memory": 2.73317926564
+        0,
+        0,
+        0,
+        7762493.42556,
+        4989270.84689,
+        -274958.882602,
+        -0.495950457609,
+        0.791704119425,
+        0.356703982153,
+        0.314692779118,
+        -0.218989581328,
+        0.923586497325,
+        -0.809321690287,
+        -0.570305313456,
+        0.14053558651
+      ],
+      "memory": 2.73317926959
     },
     {
       "label": "re-dive engaged 0",
       "arm": "earth",
-      "hr": 0.404742861533,
+      "hr": 0.404742850815,
       "displayed": [
-        -8.58813375988e-13, 4.30206906302e-12, 1.86530706557e-12, 0.801544273355, 0.0594168216069,
-        8.55816312919e-17, 0.0775559827398
+        -8.58813375989e-13,
+        4.30209214146e-12,
+        1.86525383748e-12,
+        0.801544274338,
+        0.0594167972848,
+        8.55816295471e-17,
+        0.0775559811744
       ],
       "register": [
-        0, 0, 0, 7485120.5034, 4881334.78478, -491102.955744, -0.497894230725, 0.790278686588,
-        0.357156733852, 0.38579097349, -0.167005848978, 0.907344681574, -0.776702426792,
-        -0.589549526276, 0.221731135123
-      ],
-      "memory": 2.73317926564
+        0,
+        0,
+        0,
+        7485126.427,
+        4881333.67662,
+        -491022.434865,
+        -0.49789858041,
+        0.790279465874,
+        0.357148945741,
+        0.385779940944,
+        -0.167003855664,
+        0.907349739273,
+        -0.776705118299,
+        -0.589549046315,
+        0.221722983015
+      ],
+      "memory": 2.73317926959
     },
     {
       "label": "re-dive engaged 3",
       "arm": "earth",
-      "hr": 0.266757755343,
+      "hr": 0.266757742279,
       "displayed": [
-        -8.58814922354e-13, 4.30206767835e-12, 1.86530523177e-12, 0.863342306848, -0.376693539653,
-        6.70660395683e-17, 0.0879707615574
+        -8.58814922355e-13,
+        4.30209075677e-12,
+        1.8652520037e-12,
+        0.863342306569,
+        -0.376693585659,
+        6.70660385912e-17,
+        0.0879707620004
       ],
       "register": [
-        0, 0, 0, 6556743.55339, 4560834.9573, -1158054.05414, -0.514400153683, 0.774691173384,
-        0.367758164793, 0.677083432359, 0.103729462365, 0.728559005341, -0.526260874013,
-        -0.62377382481, 0.577889010075
-      ],
-      "memory": 2.73317926564
+        0,
+        0,
+        0,
+        6556757.59107,
+        4560832.38104,
+        -1157984.13863,
+        -0.514404629972,
+        0.774691977732,
+        0.367750209111,
+        0.67707458349,
+        0.103731078593,
+        0.72856699879,
+        -0.526267883359,
+        -0.623772557084,
+        0.577883995256
+      ],
+      "memory": 2.73317926959
     }
   ]
 }
diff --git a/tests/services/engine/camera/cameraFraming.test.ts b/tests/services/engine/camera/cameraFraming.test.ts
index 18f8c43be9..3b7b7679a5 100644
--- a/tests/services/engine/camera/cameraFraming.test.ts
+++ b/tests/services/engine/camera/cameraFraming.test.ts
@@ -22,7 +22,9 @@ describe('GALACTIC_DISC_FORWARD', () => {
       GALACTIC_DISC_FORWARD,
       ORIENTATION_FRAMES.ecliptic,
     );
-    expect(yaw).toBeCloseTo(-1.4208, 6);
-    expect(pitch).toBeCloseTo(-0.1783, 6);
+    // 4 places, not 6: the exact J2000 obliquity re-tilts the ecliptic frame by
+    // ~2e-6 rad, still well inside a mistyped fourth decimal.
+    expect(yaw).toBeCloseTo(-1.4208, 4);
+    expect(pitch).toBeCloseTo(-0.1783, 4);
   });
 });
diff --git a/tests/services/engine/frame/earthTerminator.test.ts b/tests/services/engine/frame/earthTerminator.test.ts
index a87a0cec9d..9c46cb06fd 100644
--- a/tests/services/engine/frame/earthTerminator.test.ts
+++ b/tests/services/engine/frame/earthTerminator.test.ts
@@ -14,7 +14,7 @@ import { cubeSphereMesh } from '../../../../src/utils/math/cubeSphereMesh';
  * Sub-solar longitude at 14:00 UTC: the Sun crosses the Greenwich meridian near
  * 12:00 UTC and the sub-solar point moves 15°/hour westward, so at 14:00 it sits
  * near -30°. Cross-checked via sidereal time: GMST ≈ 149.3°, the Sun's apparent
- * right ascension ≈ 120.6° (ecliptic longitude ~118.5°, obliquity 23.44°), so the
+ * right ascension ≈ 120.6° (ecliptic longitude ~118.5°, obliquity 23.439°), so the
  * sub-solar geographic longitude = RA - GMST ≈ -28.7°. Sub-solar latitude ≈ +20.5°
  * (late-July solar declination). Denmark at (10°E, 56°N) is ~39° of longitude east
  * of that meridian — well inside the 90° day hemisphere — so it MUST be lit.
diff --git a/tests/services/engine/frame/passes/orbitTrailsPass.test.ts b/tests/services/engine/frame/passes/orbitTrailsPass.test.ts
index 683b3b32eb..0ad439b246 100644
--- a/tests/services/engine/frame/passes/orbitTrailsPass.test.ts
+++ b/tests/services/engine/frame/passes/orbitTrailsPass.test.ts
@@ -33,6 +33,7 @@ import { ORBITAL_ELEMENTS } from '../../../../../src/data/bodies/orbitalElements
 import { CORE_TRAIL_ELEMENTS } from '../../../../../src/data/bodies/coreTrailElements';
 import { SCENE_ANCHORS } from '../../../../../src/data/bodies/sceneAnchors';
 import { deriveBodyStates } from '../../../../../src/services/engine/frame/deriveBodyStates';
+import { eccentricAnomalyFromMean } from '../../../../../src/utils/orbit/eccentricAnomalyFromMean';
 import { propagateElements } from '../../../../../src/utils/orbit/propagateElements';
 import { keplerianEllipse } from '../../../../../src/utils/orbit/keplerianEllipse';
 import { keplerianPositionMpc } from '../../../../../src/utils/orbit/keplerianPositionMpc';
@@ -76,6 +77,21 @@ vi.mock('../../../../../src/utils/camera/composeOrbitConic', () => ({
 }));
 import { composeOrbitConic } from '../../../../../src/utils/camera/composeOrbitConic';
 
+// Lets one test hand the pass a snapshot that differs from raw Kepler; unset, the
+// real map passes through untouched.
+const snapshotOverride = vi.hoisted(() => ({ states: undefined as unknown }));
+vi.mock('../../../../../src/services/engine/frame/sceneBodyStates', async (importOriginal) => {
+  const actual =
+    await importOriginal<
+      typeof import('../../../../../src/services/engine/frame/sceneBodyStates')
+    >();
+  return {
+    sceneBodyStates: ((...args: Parameters<typeof actual.sceneBodyStates>) =>
+      (snapshotOverride.states as ReturnType<typeof actual.sceneBodyStates> | undefined) ??
+      actual.sceneBodyStates(...args)) as typeof actual.sceneBodyStates,
+  };
+});
+
 const composeMock = composeOrbitConic as unknown as ReturnType<typeof vi.fn>;
 
 // The J2000 oracle `SCENE_ORBIT_CONICS` used to provide, hand-derived here with
@@ -585,6 +601,58 @@ describe('orbitTrailsPass.draw', () => {
     expect(drift).toBeGreaterThan(1e-13);
   });
 
+  it('trail follows a snapshot position that differs from raw Kepler', () => {
+    const simDays = CONST_J2000 + 100;
+    const real = deriveBodyStates(simDays);
+    const moonEl = CORE_TRAIL_ELEMENTS.find((e) => e.id === 'moon')!;
+    const moonState = real.get('moon')!;
+    // 1e6 km off raw Kepler, asymmetric so a dropped axis shows.
+    const shiftMpc = [1e6, -4e5, 2.5e5].map((km) => km * SCALE_UNITS.KM_TO_MPC);
+    const stubbed: Vec3 = [
+      moonState.positionMpc[0] + shiftMpc[0]!,
+      moonState.positionMpc[1] + shiftMpc[1]!,
+      moonState.positionMpc[2] + shiftMpc[2]!,
+    ];
+    snapshotOverride.states = new Map(real).set('moon', { ...moonState, positionMpc: stubbed });
+    try {
+      // Eye 100 km off the body. The basis is packed in f32, whose ulp at the Moon's
+      // ~4e5 km semi-major axis is 30 m, so 0.1 km is the tightest honest bound; the
+      // injected 1e6 km offset is four orders above it.
+      const eye: Vec3 = [stubbed[0] + 100 * SCALE_UNITS.KM_TO_MPC, stubbed[1], stubbed[2]];
+      const ctx = {
+        snapshot: {
+          simDays,
+          focusBlend: 0,
+          nowMs: 0,
+          renderTargets: { farDepthView: () => FAR_DEPTH_VIEW_STUB },
+        },
+        bodyPose: () => null,
+        drawCamPos: eye,
+        drawPxPerRad: FIXTURE_PX_PER_RAD,
+        cam: { distance: 1e-13 },
+      } as unknown as FrameView;
+      const renderer = makeRendererSpy();
+      orbitTrailsPass.draw(PASS_STUB, makeNear0View(), ctx, {
+        ...makeState(renderer),
+        orbitTrailRows: [moonEl],
+      } as unknown as EngineState);
+
+      const [, { instances: staging, count }] = renderer.draw.mock.calls[0]!;
+      expect(count).toBe(1);
+      const { eccentricity, meanAnomalyRad } = propagateElements(moonEl, simDays);
+      const eAnom = eccentricAnomalyFromMean(meanAnomalyRad, eccentricity);
+      const [cosE, sinE] = [Math.cos(eAnom), Math.sin(eAnom)];
+      const kmPerMpc = 1 / SCALE_UNITS.KM_TO_MPC;
+      for (let axis = 0; axis < 3; axis++) {
+        const bodyKm =
+          staging[34 + axis]! + staging[38 + axis]! * cosE + staging[42 + axis]! * sinE;
+        expect(Math.abs(bodyKm - (stubbed[axis]! - eye[axis]!) * kmPerMpc)).toBeLessThan(0.1);
+      }
+    } finally {
+      snapshotOverride.states = undefined;
+    }
+  });
+
   it('stages no conic for the mesh bodies (whale, petunias) even when the Moon trail is emitted', () => {
     // Same pose as "rides a moon trail on its propagated parent" above — parking
     // the camera at Earth is what makes the Moon's tiny geocentric orbit survive
diff --git a/tests/services/engine/frame/settleGoldenTrace.test.ts b/tests/services/engine/frame/settleGoldenTrace.test.ts
index 9cd61162ca..ce8c85e4b4 100644
--- a/tests/services/engine/frame/settleGoldenTrace.test.ts
+++ b/tests/services/engine/frame/settleGoldenTrace.test.ts
@@ -231,7 +231,7 @@ describe('settle golden trace (byte bar for the orientation settles)', () => {
       const trace = thin(runScript(northUp));
       if (process.env['SETTLE_GOLDEN_RECORD']) {
         recorded[key] = trace;
-        writeFileSync(FIXTURE_PATH, `${JSON.stringify(recorded)}\n`);
+        writeFileSync(FIXTURE_PATH, `${JSON.stringify(recorded, null, 2)}\n`);
         return;
       }
       expectTraceMatches(trace, (GOLDEN as Record<string, Trace>)[key]!);
diff --git a/tests/utils/orbit/propagateElements.test.ts b/tests/utils/orbit/propagateElements.test.ts
index 123152deb9..b4cbade8e5 100644
--- a/tests/utils/orbit/propagateElements.test.ts
+++ b/tests/utils/orbit/propagateElements.test.ts
@@ -90,9 +90,9 @@ describe('propagateElements', () => {
     // The scene frame is equatorial J2000 (keplerianEllipse rotates the ecliptic
     // elements through ECLIPTIC_FRAME), matching Horizons' ICRF frame to sub-
     // arcsecond bias. Tolerance is arcminute-class: the mean-element model differs
-    // from the true DE ephemeris by ~1 arcmin (~2e-4 au at 1 au), and the scene's
-    // rounded 23.44° obliquity adds ~2 arcsec. A frame swap, unit slip, or sign
-    // error in a rate would miss by ≥0.05 au and fail loudly.
+    // from the true DE ephemeris by ~1 arcmin (~2e-4 au at 1 au); the scene's J2000
+    // obliquity is exact, so it adds none. A frame swap, unit slip, or sign error in a
+    // rate would miss by ≥0.05 au and fail loudly.
     const simDays = 2_460_676.5;
     const horizonsAu: Vec3 = [-1.786710910310161e-1, 8.871846912692936e-1, 3.845832338744293e-1];
     const expectedMpc = horizonsAu.map((au) => au * SCALE_UNITS.AU_TO_MPC) as Vec3;
diff --git a/tools/perf/perfScenarios.ts b/tools/perf/perfScenarios.ts
index 1e201da978..0e652fb789 100644
--- a/tools/perf/perfScenarios.ts
+++ b/tools/perf/perfScenarios.ts
@@ -49,7 +49,7 @@ export type PerfScenario = { readonly name: string; readonly pose: PerfPose };
 // time).
 // Factored out so those poses differ only in the axes that actually vary
 // (distance/yaw/pitch) and the target can never drift between them.
-const EARTH_TARGET: Vec3 = [-8.5895045e-13, 4.3022234e-12, 1.865304e-12];
+const EARTH_TARGET: Vec3 = [-8.5895045e-13, 4.3022465e-12, 1.8652508e-12];
 
 // The shared look-at point for `milky-way-outside` and `milky-way-close`: the
 // galactic centre (~8 kpc off the origin — contrast `EARTH_TARGET`'s ~1 AU).