Unisat 1
General
| Designation | 26547 / 00057C |
| Launch date | 26 Sep 2000 |
| Country of origin | Italy |
| Mission | Technology |
| Perigee/Apogee | 637/663 km |
| Inclination | 64.6° |
| Period | |
| Launch vehicle | Dnepr #2 |
| Launch site | Tyuratam |
It carries NiMH batteries, a magnetometer, and a payload consisting of a space debris sensor and a camera.
External resources
sat-index articles
Technical data
Specifications
| Prime contractor | GAUSS (Gruppo di Astrodinamica dell' Universita degli Studi "la Sapienza") in Roma |
| Platform | |
| Mass at launch | 10 kg |
| Mass in orbit | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |
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V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly
V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly