Negai (satellite)

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Negai☆″
Mission typeTechnology
Operator
Soka University
COSPAR ID2010-020C Edit this at Wikidata
SATCAT no.36575
Websitekuro.t.soka.ac.jp/cube/what/index.html
Mission duration37 days
Spacecraft properties
Spacecraft type1U CubeSat
Launch mass1 kilogram (2.2 lb)[1]
Dimensions10-centimetre (3.9 in) cube
Start of mission
Launch date20 May 2010, 21:58:22 (2010-05-20UTC21:58:22Z) UTC
RocketH-IIA 202
Launch siteTanegashima Yoshinobu 1
ContractorMitsubishi
End of mission
Decay date26 June 2010
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude286 kilometres (178 mi)
Apogee altitude305 kilometres (190 mi)
Inclination29.9 degrees
Period90.42 minutes
Epoch23 May 2010[2]
 

Negai☆″ ("Wish") is a Japanese

field programmable gate array in orbit.[4] As part of an outreach programme, it will carry the names of selected children, along with wishes they have made. The satellite will return images of the Earth, which will be given to the participating children.[5]

The launch was conducted by

cryogenic propellant into the rocket's first and second stages had been completed.[6]
The launch attempt was scrubbed a few minutes before liftoff due to bad weather, but took place successfully at 21:58:22 UTC on 20 May 2010.

Negai was deployed from a

UNITEC-1 spacecraft.[7]

See also

References

  1. ^ "Negai". Soka University. Archived from the original on 8 March 2010. Retrieved 17 May 2010.
  2. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 25 December 2013.
  3. ^ Krebs, Gunter. "Negai*". Gunter's Space Page. Archived from the original on 27 April 2011. Retrieved 17 May 2010.
  4. ^ Nerlich, Steve. "A Multiple Payload" (PDF). Cheap Astronomy. Retrieved 17 May 2010.
  5. ^ "Japanese space agency selects Soka microsatellite for 2010 launch". Soka University. Archived from the original on 24 February 2012. Retrieved 17 May 2010.
  6. ^ a b "Countdown Report". H-IIA Launch Services Flight 17. Mitsubishi Heavy Industries. Archived from the original on 9 August 2016. Retrieved 17 May 2010.
  7. ^ "Overview of Secondary Payloads". Akatsuki Special Site. JAXA. Retrieved 17 May 2010.