Satellite catalog

Working, current, and decommissioned Earth satellites.

A separate satellite page with a lightweight 3D Earth orbit view, catalog filters, active same-origin satellite snapshots, and a decommissioned archive for study and comparison.

Drag to rotate. Wheel to zoom. Same-origin satellite snapshots are downsampled for fast rendering.

Catalog controls

Filter satellite records

- shown- source- latest epoch

The 3D view renders a performance-safe sample of the selected group. It is for visual study, not certified collision analysis.

Orbit view

What the 3D view shows

Inclination

Orbit rings are tilted from catalog inclination when available.

Orbit shell

Mean motion estimates a compact LEO, MEO, or GEO radius for visualization.

Status

Current groups load same-origin data; decommissioned entries use a curated local archive.

Satellite rows

Current table view

Switch groups to compare current, working, thematic, and decommissioned satellites.

ObjectStatus / groupNORAD / operatorObject id / launchInclinationPeriod / orbitEpoch / note

Satellite Study Notes

How to use the catalog responsibly

Current satellites

Active, station, science, weather, resource, GPS, GEO, and Starlink groups are loaded from compact same-origin JSON snapshots.

Decommissioned satellites

The archive shows retired, inactive, reentered, graveyard, and historically important objects as mission-study references.

Performance

The chart draws a bounded sample so the VPS and browser remain responsive even when the active catalog contains thousands of records.

Precision warning

This is not an SGP4 flight-dynamics console. Operational work needs fresh elements, a validated propagator, and collision-risk tools.

Mathematical model

Satellite orbit propagation model

Satellite and observatory maps use orbital period, mean motion, altitude, and coordinate transforms. The model is a lightweight educational propagator, not a pixel drawing of a ground track.

Mean motion

\[n=\frac{2\pi}{P}\]

The phase angle advances from orbital period P. This keeps speed and repeat timing consistent with the catalog shell.

Circular speed check

\[v=\sqrt{\frac{\mu}{r}}\]

For circular shells, speed follows the gravitational parameter mu and orbital radius r. Displayed speed is checked against this relation.

Ground-track projection

\[\lambda=\operatorname{atan2}(y,x)-\omega_E t\]

Earth rotation is subtracted from the inertial longitude to draw the map track. The proof is a coordinate transform from orbit frame to rotating Earth frame.

Verification standard: the rendered object must be reproducible from stated equations, catalog parameters, or explicit geometric transforms. Visual reference images may inform presentation only; they are not the source of orbital positions, field vectors, accretion-disk gradients, timing, or engineering layout.

Limitations: browser scenes may use bounded scale, compressed distances, simplified two-body dynamics, schematic transfer curves, or educational approximations where full numerical ephemerides, CFD, finite-element models, or general-relativistic ray tracing are outside the page scope. Those simplifications are part of the model contract, not hidden image-based construction.

Open the full site-wide mathematical verification policy