Engineering:Perseus-M
From HandWiki
Mission type | Maritime surveillance |
---|---|
Operator | Aquila Space |
COSPAR ID | M1: 2014-033AF M2: 2014-033AD |
SATCAT no. | M1: 40039 M2: 40037 |
Mission duration | 10 years, 2 months and 20 days (ongoing) |
Spacecraft properties | |
Manufacturer | Elecnor Deimos |
Start of mission | |
Launch date | 19 June 2014 |
Rocket | Dnepr |
Launch site | Dombarovsky |
Orbital parameters | |
Reference system | Geocentric |
Eccentricity | 0 |
Perigee altitude | 620 km (390 mi) |
Apogee altitude | 620 km (390 mi) |
Inclination | 97.9° |
Perseus-M is a pair of microsatellite developed by Russian-American company Dauria Aerospace and launched in 2014. The satellite is built in 6U Cubesat bus (0.3x0.2x0.1m), optimized for piggy-back launch. All instruments are powered by solar cells mounted on the one side of spacecraft, providing approximately 6W average power.[1]
Launch
Perseus-M1 and Perseus-M2 were launched from Dombarovsky site 13, Russia, on 19 June 2014 by a Dnepr rocket. Telemetry beacons were received and decoded by multiple amateur ground station operators starting on 6 July 2014. [2]
Mission
The satellites are intended primarily for radio-frequency maritime surveillance under contract with Russian Federation.[3]
See also
- 2014 in spaceflight
References
External links
![]() | Original source: https://en.wikipedia.org/wiki/Perseus-M.
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