Merge additive analyst and satellite tools into walkthrough train

docs/CURRENT-STATE.md

@@ -2,6 +2,10 @@
 
 Wind is an optional GFS 10 m forecast overlay. Source acquisition has deadline and body budgets, disconnect cancellation and one-minute failure backoff. The row distinguishes model issue time from forecast valid time. Animation starts only with a field, stops on disable/destruction, preserves trails between unchanged canvas dimensions and scales from 200 to 4,000 particles with viewport area. Application catalog construction owns each instance.
 
+Voice and HUD snapshots reuse the existing feedState classifier. Analyst follow-ups retain their original data provenance; current-view results append provenance without replacing legacy fields. HUD context and deterministic telemetry include non-nominal feed state.
+
+Satellite and local infrastructure layers expose on-demand analyst records through their current factory owners. Analyst counts and ranks explicitly cover only bounded examined loaded records (default 2,000 per new layer, core satellite rows before dense extras); omitted records can change nearest/count and satellite distance is ground distance. Existing tools and result fields remain available.
+
 Search framing and annotations request semantic map features from an explicit source. The Overpass adapter owns bounded queries, member/tag decoding and request deadlines; callers retain candidate ranking, outline caching, deferred retries and scene placement. Empty, transient and throttled outcomes remain distinct. Traffic sources return road records and installation sources return mapped records with freshness/saturation metadata, so their layers no longer decode upstream elements. ALPR already normalizes its records in the source. Default providers, footprints, road directions, exact-viewport retries and source attribution are unchanged.
 
 Nepal media preloads survive repeated camera-flight updates, but Stop, event disable and replacement remove abandoned frames and revoke pending Facebook sessions. Fallback evidence-card clicks respect the shared drawing-tool pointer lease.
@@ -40,7 +44,7 @@ Source factories have dedicated `layers/<family>/source` exports. ALPR and earth
 
 Voice controls bind to a protocol-independent session factory. The default WebRTC adapter preserves the existing Realtime connection, push-to-talk, cost controls and radio handoff. Session subscriptions expose state, transcript, action call/result, interruption and completion events; stopping or replacing a session cancels pending actions. Alternate adapters can use the same controls and action runner.
 
-Voice action argument schemas have one portable owner under `src/voice/actionSchemas.js`. The Realtime provider builds the same 28 tools using separate description-only metadata. Description customization cannot replace argument types, enum values or required fields.
+Voice action argument schemas have one portable owner under `src/voice/actionSchemas.js`. The Realtime provider builds 29 tools, retaining the existing 28 names and argument contracts apart from the three additive analyst-layer enum values using separate description-only metadata. Description customization cannot replace argument types, enum values or required fields.
 
 Portable source exports provide Radio Browser station normalization, CCTV feed types and regional records independently of HTTP middleware. Radio normalization accepts an explicit URL policy; the standalone directory retains its existing HTTPS rules. Tile coordinate validation accepts explicit zoom bounds with unchanged traffic defaults. Cache, request and rendering owners remain unchanged.
 
@@ -3087,7 +3091,7 @@ silently demoting every later lookup for the session.
   `activeCameraCardEnabled` presentation option can publish the retained
   protected-card path. Disable tears the tier down completely.
   Coverage/viewshed semantics unchanged.
-- **Satellites**: orbit rings rotate about Earth's Z by ΔGMST every ~1s (exact inertial→ECEF compensation; no SGP4 re-runs); the tracked satellite propagates per frame with one shared epoch for dot/label/camera. Verified: ISS holds <1km perpendicular to its ring while tracked.
+- **Satellites**: orbit rings rotate about Earth's Z by ΔGMST every ~1s (exact inertial→ECEF compensation; no SGP4 re-runs); the tracked satellite propagates per frame with one shared epoch for dot/label/camera. Verified: ISS holds <1km perpendicular to its ring while tracked. Pass prediction (`src/data/satellitePass.js`; `getNextSatellitePass`, `getNextIssPass`) scans at 20s, bisects rise/set to ~0.2s, fits the peak with a parabola, and marks a pass visible when the satellite is outside a cylindrical Earth shadow while the observer's Sun is at or below −6°. `next_iss_pass` preserves its geometric-pass ordering and appends visibility metadata. General `next_satellite_pass` accepts a loaded NORAD ID or unambiguous name, searches 24 hours and optionally requires estimated visibility. These estimates do not account for weather or satellite brightness.
 - **Space Missions (30d)**: recent launches render as bounded shared-host, horizon-occluded mission markers using Launch Library 2 v2.3 detailed records. Enabling the layer selects the unified right-side Context panel's Space Missions mode and enables the required satellite layer. Before applying its temporary dense/hidden Satellite mode, Space Missions snapshots the complete standalone Satellite parameter set and exact enabled-layer set. Disabling Space Missions from either Context or the left Data Layers rail restores those parameters and the exact prior enabled state, so a Satellite layer that was already on stays on while a mode-owned dependency returns off; enabling Satellites by itself remains independent. Selecting a mission isolates its launch-to-orbit transfer and dashed satellite orbit, fills that same panel with navigation/details, and animates a small phase-colored marker along the exact displayed Cartesian samples. Marker hit testing drill-picks through photorealistic tiles so the depth-test-free tactical dot remains reliably selectable; its text is non-interactive shared-host presentation. The selected pad is the camera's zoom pivot: the overview remains centered on its launch site, wheel zoom approaches that site instead of drifting elsewhere, and camera pitch progressively changes from global nadir to an oblique close 3D view. Its protected shared-host callout remains visible and expands to include both mission and launch-site names. `FOCUS` flies directly to a 12 km oblique frame around the selected launch site and retains the same anchored zoom/orbit behavior. `REPLAY ASCENT` resets the selected marker at the pad, frames it from an oblique third-person angle, and follows it through the mission-specific compressed ascent directly into one orbital lap at the default `1×` rate. A live `0.25×`–`4×` slider changes ascent and orbit playback speed; adjusting it mid-replay preserves the current path position and historical mission timestamp. Re-entry/recovery cannot be inserted into replay. At orbit insertion the camera smoothly pulls back over the first fifth of the orbital replay and pitches to a globe-scale nadir view while continuing to target the moving replay point. Replay Cancel, mission navigation, deselection, layer disable, and data refresh all release camera ownership. Reconstructed paths are one continuous 128-sample geodetic curve: horizontal departure begins near zero while altitude rises quickly, then the climb progressively bends toward insertion without the former hard 120 km corner. Unmatched orbit fallbacks are smooth planar inclined rings rather than longitude/latitude ground-track curves. The panel lists disclosed payload names, types, operators/manufacturers, mass, multiplicity, and destination when supplied; an empty LL2 payload collection is shown as `CLASSIFIED / MULTI-PAYLOAD`. Launcher, spacecraft, and recoverable payload stages appear in a compact stage table with serial/flight/reuse details, recovery outcome/type, destination, and final coordinates when those records exist; an empty recovery collection omits the section. Stage recoveries with confirmed coordinates use those coordinates; return-to-launch-site records use the pad; downrange-only records receive an explicitly labeled estimated endpoint along the ascent azimuth. Available endpoints render as static 2 px dashed descent/recovery paths with a fixed final-position dot and an estimated atmospheric-interface segment when applicable. The ascent is geodetically densified above the ellipsoid toward the orbit's nearest insertion point, then rendered with `ArcType.NONE`, so it neither cuts through Earth nor separates from the marker. Because LL2 does not normally supply continuous ascent telemetry, pad-to-insertion paths without upstream trajectory samples are labeled `RECONSTRUCTED ESTIMATE` / `ASCENT ESTIMATE`; only supplied trajectory samples receive the replay wording. Selected-orbit framing fits the complete ring, rear-side linework uses normal scene depth occlusion, and current distance, speed, and callout data come only from a launch-year-validated satellite match. Speed is the magnitude of the SGP4 inertial velocity vector at the same propagation epoch as position, displayed in km/s with km/h available as hover detail. Unavailable operator, site, launch-time, orbit, current-altitude, and speed values omit their detail rows instead of reserving panel space with placeholders. Newly launched payloads absent from the core operational groups use CelesTrak's cached active TLE feed as a lookup-only fallback; weak constellation-name matches are rejected. The replay callout maps compressed animation progress onto Launch Library's mission-relative timeline, showing the historical UTC date/time at the marker's current path position; unavailable timelines remain explicit. Matched live satellite positions propagate at one-second cadence and use a distinct green dot/callout with the current UTC date/time.
   When no mission is selected, the Context panel presents a scrollable newest-first roster of every launch in the rolling window, including the smaller 5 px operator-colored marker, provider, and launch date. Hovering or keyboard-focusing a row shows four compact cyan corner brackets on both that roster row and its corresponding globe dot, rotates the globe at the current zoom to center it, and gives its label declutter priority without selecting it; the globe label remains unbracketed. Selecting a roster row invokes the same mission isolation and full-orbit framing as clicking its globe marker. The replay vehicle is one screen-space SVG/CSS HUD overlay rather than separate Cesium billboard, label, and reticle graphics. It is hidden during ordinary Focus and manual close views, where the standard selected launch-site label remains visible, and exists only while ascent replay is active. Its fixed pixel scale is shared by ascent and insertion, so camera range never resizes the rocket on screen before the phase boundary. Generic Launch Library pad names are reduced to their identifying suffix, and replay timestamps use a cyan state title over unprefixed white UTC date/time values. `REPLAY ASCENT` holds the unframed cyan/white rocket at the pad for a real-time `T−10` countdown, transitions through `LIFTOFF`, and attaches six tapered cyan/white ellipse waves directly below it from liftoff through insertion to convey thrust without adding scene geometry. While replay is active, the single start button is replaced by compact Play, Pause, and Cancel icon controls. Pause freezes countdown or mission time, vehicle/stage positions, camera target, labels, and thrust-wave animation; Play resumes from that exact frame, and Cancel releases replay camera ownership. The rocket and thrust group rotates from the path's live screen-space tangent, so its nose follows the visible ascent curve while the adjacent text remains upright. The camera begins as a close oblique launch chase, then smoothly widens between roughly 120 and 420 km vehicle altitude into a higher oblique context view that keeps the moving rocket targeted while exposing the ascent bend and orbit connection. At insertion the rocket/thrust glyph is replaced by the fixed-size cyan orbit dot, which the camera follows through the existing globe-scale orbit pullback. The chase camera limits per-frame yaw changes across heading wraps so it cannot abruptly cross in front of the vehicle and make ascent read in reverse; the replay-speed slider affects mission playback but not countdown duration.
   Mission world text has no native `LabelGraphics`: overview launch markers publish at most 48 ambient candidates for a 24-winner budget, while selecting a mission clears that overview source and publishes its launch-site callout, stage re-entry annotations, live/estimated payload-position readout, and orbit annotation as protected selected-lane entries. The source retains the exact former strings and colors. Static anchors reuse the Cartesian values used to build their mission geometry; the moving payload entry reads the layer's per-frame live-position cache; catalog-backed orbit annotation positions are cached in the same one-second matrix update that realigns the orbit primitive. Keyhole edge fade, horizon culling, final collision placement, and UI exclusion are owned by the shared host. Deselect restores the bounded overview, and refresh, disable, and destroy replace or clear both mission sources.

docs/INFRASTRUCTURE-LAYERS.md

@@ -36,7 +36,8 @@ const layers = createInfrastructureLayers({
 | `governorRequestRender` | `(reason)`; request a frame through the existing render scheduler |
 
 Each returned layer supports `init(viewer)`, `enable(viewer)`, `disable(viewer)`,
-`update(viewer)`, `destroy(viewer)`, `getStats()` and `getLodDiagnostics()`.
+`update(viewer)`, `destroy(viewer)`, `getStats()`, `getLodDiagnostics()` and
+`getAnalystRecords()`.
 Use the same viewer for the instance's entire lifetime. Each viewer/context/overlay
 host permits one live instance per layer ID; destroy an old instance before
 replacing it. Separate applications may use identical IDs with separate hosts.