Quakesat

Quakesat
Mission typeEarth observation
COSPAR ID2003-031F Edit this at Wikidata
SATCAT no.27845
Website[1]
Mission duration21 years, 3 months, 4 days (elapsed)
Spacecraft properties
SpacecraftCubeSat
Spacecraft type3 CubeSat
ManufacturerStanford University
Launch mass5 kg (11 lb)
Start of mission
Launch date30 June 2003, 14:15:26 UTC
RocketRockot/Briz-KM
Launch sitePlesetsk Cosmodrome, Site 133
ContractorKhrunichev State Research and Production Space Center
Orbital parameters
Reference systemGeocentric orbit[1]
RegimeLow Earth orbit
Perigee altitude821 km (510 mi)
Apogee altitude833 km (518 mi)
Inclination98.70°
Period101.40 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]

  1. ^ "Trajectory: Quakesat 2003-031F". NASA. 14 May 2020. Retrieved 16 December 2020. Public Domain This article incorporates text from this source, which is in the public domain.
  2. ^