| COSPAR ID | 1995-033C |
|---|---|
| SATCAT no. | 1995-033C |
| Mission duration | 213 days |
| Spacecraft properties | |
| Manufacturer | Technical University of Madrid |
| Launch mass | 47 kilograms (104 lb) |
| Start of mission | |
| Launch date | July 7, 1995 |
| Rocket | Ariane IV-40 |
| Launch site | Guiana Space Centre |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-synchronous polar orbit |
| Perigee altitude | 670 kilometres (420 mi) |
| Apogee altitude | 670 kilometres (420 mi) |
| Inclination | 98.1 degrees |
| Period | 98 minutes |
| COSPAR ID | 1995-033C |
|---|---|
| SATCAT no. | 2020-061E |
| Mission duration | 2 years (expected) |
| Spacecraft properties | |
| Manufacturer | Technical University of Madrid |
| Launch mass | 45 kilograms (99 lb) |
| Start of mission | |
| Launch date | September 3, 2020 |
| Rocket | Vega |
| Launch site | Guiana Space Centre |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-synchronous polar orbit |
| Perigee altitude | 600 kilometres (370 mi) |
| Apogee altitude | 600 kilometres (370 mi) |
UPM-Sat is a series of Spanish microsatellites developed by the Technical University of Madrid (UPM), in collaboration with the Instituto Nacional de Técnica Aeroespacial (INTA), for educational, scientific and technological purposes.[1]
- ^ "Programa de satélites UPM-Sat". Instituto Universitario de Microgravedad “Ignacio Da Riva” (in Spanish).