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Quakesat

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Earth Observation nanosatellite
This article needs to be updated. Please help update this article to reflect recent events or newly available information. (April 2016)
Quakesat
Mission typeEarth observation
COSPAR ID 2003-031F Edit this at Wikidata
SATCAT no. 27845
Website[1]
Mission duration1 year and 185 days (elapsed)
Spacecraft properties
SpacecraftCubeSat
Spacecraft type3 CubeSat
ManufacturerQuakeFinder, LLC
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 altitude 821 km (510 mi)
Apogee altitude 833 km (518 mi)
Inclination 98.70°
Period 101.40 minutes
Instruments
Magnetometer

Quakesat was an Earth observation nanosatellite based on three CubeSats. It was designed to be a "proof-of-concept" for collecting space-based detection of extremely low frequency signals, theorized to be earthquake precursor signals. The science behind the concept was disputed at the time of launch.[2]

Stanford University and Stellar Solutions released a 10-year, longitudinal study in 2022 in collaboration with Google using earth-based instrumentation that confirmed the science behind the theory for forecasting purposes, but not to the level sufficient to meet the USGS standard of an earthquake prediction.[3]

Mission

[edit ]

The mission goal of Quakesat was to determine if there were any ultra low frequency (ULF) magnetic signals, associated with large earthquakes, that could be detected using a satellite-based, induction magnetometer flying in low-earth-orbit (LEO).[4] QuakeFinder LLC, the company that put the satellites together, was from Palo Alto, California. They were gathering data on the ultra low frequency magnetic field fluctuations that are associated with earthquakes to help better understand this area of study. The primary instrument was a magnetometer housed in a 2 ft (0.6 m) telescoping boom.

On 30 June 2003, deployment of Quakesat was alongside other university CubeSats and one commercial CubeSat. The launch occurred on a Rokot rocket from Russia's Plesetsk Cosmodrome.

The mission was planned to last one year, but ended up lasting 1 and a half years.[5]

See also

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References

[edit ]
  1. ^ "Trajectory: Quakesat 2003-031F". NASA. 14 May 2020. Archived from the original on 28 March 2023. Retrieved 16 December 2020. Public Domain This article incorporates text from this source, which is in the public domain.
  2. ^
  3. ^ Heavlin, William D.; Kappler, Karl; Yang, Lusann; Fan, Minjie; Hickey, Jason; Lemon, James; MacLean, Laura; Bleier, Thomas; Riley, Patrick; Schneider, Daniel (2022). "Case-Control Study on a Decade of Ground-Based Magnetometers in California Reveals Modest Signal 24–72 hr Prior to Earthquakes". Journal of Geophysical Research: Solid Earth. 127 (10) e2022JB024109. doi:10.1029/2022JB024109 . ISSN 2169-9356.
  4. ^ "QuakeFinder » About QuakeSat" . Retrieved 29 January 2025.
  5. ^ "QuakeSat". eoPortal. 12 June 2012. Archived from the original on 23 August 2024. Retrieved 4 December 2024.

QuakeFinder LLC Single axis search coil, small E-field dipole [2]

Science instruments on satellites and spacecraft
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Near-Earth
Interplanetary
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Near-Earth
Interplanetary
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Near-Earth
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Near-Earth
Interplanetary
UV-visible (UVVS)
Interplanetary
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Interplanetary
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Near-Earth
Interplanetary
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Near-Earth
Interplanetary
Helium vapor
Near-Earth
Interplanetary
Particle
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Near-Earth
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Interplanetary
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Interplanetary
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