# Resourcesat-2 3D model

> Shape built from published dimensions and pictures; details simplified.

Free 3D model of Resourcesat-2, a satellite, built from published dimensions by Space Radar. 5,288 triangles, 36 kB glTF, MIT.

- **Class:** Satellites
- **Mission:** Earth observation
- **Triangles:** 5,288
- **File:** resourcesat-2.glb, 36 kB, glTF 2.0 binary (meshopt)
- **Look:** Flat colours
- **Size:** 2.1 m across
- **Made:** Built from dimensions
- **Added:** 2026-10-27
- **NORAD:** 37387
- **Download:** https://raw.githubusercontent.com/Sara-Managed-Projects/space-radar/main/site/models/resourcesat-2.glb
- **Mirror:** https://git.sara-agent.org/sara-projects/space-radar/raw/branch/main/site/models/resourcesat-2.glb
- **Viewer:** https://www.spaceradar.ai/model/?id=resourcesat-2
- **On the live map:** https://www.spaceradar.ai/#at=sat-37387
- **Licence:** MIT (https://github.com/Sara-Managed-Projects/space-radar/blob/main/LICENSE)
- **Credit:** Resourcesat-2 3D model by Space Radar (spaceradar.ai), MIT License

Canonical: https://models.spaceradar.ai/resourcesat-2/

## How it was made

Built in code from published dimensions and photographs, with no image-to-3D generator and no one else’s mesh. 3D model: built by Space Radar from published dimensions and ISRO's render of Resourcesat-2A (ISRO, GODL-India).

built by this project in code (the private tool model-from-images: assemble.py, from a yaml of primitives), from the cited dimensions and the pictures under `references`; no image-to-3D model was used, and no published mesh: NASA's 3D Resources (1 583 paths, read 2026-10-27) has none of these craft, and no agency named here publishes a model of its own under terms that allow one

## Dimensions

- Diameter: 2 m
- Height: 2.1 m
- Mass: 1200 kg
- Panels: 6 × 1.4 × 1.8

Source: eoPortal, https://www.eoportal.org/satellite-missions/resourcesat-2, OPENED 2026-10-27: 'The overall S/C size is about 2 m in diameter and 2.1 m in height. The total S/C mass at launch is ~1200 kg'; '6 Solar panels (1.4 x 1.8 m2 each) generate 1250 W of power at EOL'; 'The S/C structure consists of two modules, the main platform and the payload module'; 'The payload module deck accommodates LISS-3, AWiFS-A and AWiFS-B camera modules. The LISS-4 camera is mounted on a rotating deck'; 'Two star trackers are mounted with skewed orientation on the top deck'. OURS: the platform's 2.0 x 2.0 x 1.1 m box, the camera boxes' 0.55 m and places, the tower's hexagon, the wings' arms.

## References

- [Render of Resourcesat-2A spacecraft in deployed configuration](https://commons.wikimedia.org/wiki/File:Render_of_Resourcesat-2A_spacecraft_in_deployed_configuration.png), Indian Space Research Organisation (ISRO) (GODL-India (Government Open Data Licence - India; attribution; commercial use and derivatives allowed), as the Commons file's LicenseShortName reads, 2026-10-27)