This article needs to be updated.(April 2016) |
Mission type | Earth observation |
---|---|
COSPAR ID | 2003-031F |
SATCAT no. | 27845 |
Website | [1] |
Mission duration | 21 years, 3 months, 4 days (elapsed) |
Spacecraft properties | |
Spacecraft | CubeSat |
Spacecraft type | 3 CubeSat |
Manufacturer | Stanford University |
Launch mass | 5 kg (11 lb) |
Start of mission | |
Launch date | 30 June 2003, 14:15:26 UTC |
Rocket | Rockot/Briz-KM |
Launch site | Plesetsk Cosmodrome, Site 133 |
Contractor | Khrunichev State Research and Production Space Center |
Orbital parameters | |
Reference system | Geocentric orbit[1] |
Regime | Low Earth orbit |
Perigee altitude | 821 km (510 mi) |
Apogee altitude | 833 km (518 mi) |
Inclination | 98.70° |
Period | 101.40 minutes |
Instruments | |
Magnetometer | |
Quakesat is an Earth observation nanosatellite based on three CubeSats. It was designed to be a proof of concept for space-based detection of extremely low frequency signals, thought by some to be earthquake precursor signals. The science behind the concept is disputed.[2]