SOCRATES (satellite)

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SOCRATES
Mission typeTechnology demonstrator
OperatorAdvanced Engineering Services Co., Ltd.
COSPAR ID2014-029C Edit this at Wikidata
SATCAT no.39768
WebsiteOfficial page (Japanese)
Spacecraft properties
Launch mass48 kg (106 lb)
Dimensions496 mm × 495 mm × 485 mm (19.5 in × 19.5 in × 19.1 in)
Power120W
Start of mission
Launch date24 May 2014; 9 years ago (2014-05-24)
RocketH-IIA 202
Launch siteTanegashima, LA-Y
Orbital parameters
Reference systemGeocentric
RegimeSun Synchronous
Eccentricity0.0013
Perigee altitude629.8 km
Apogee altitude647.4 km
Inclination97.9 
Period97.5 min
 

SOCRATES or Space Optical Communications Research Advanced Technology Satellite is a Japanese micro-satellite launched in 2014. The satellite is purely a technology demonstrator intended to help AES company to gain experience in basic mission control, attitude control and spacecraft communications. Its main experiment is SOTA (Small Optical TrAnsponder), an optical small satellite communications demonstrator.[1] All subsystems of spacecraft are powered by solar cells mounted on spacecraft body and stub wings, with estimated electrical power of 120W BOL degrading to 100W EOL.[1][2][3]

Launch

SOCRATES was launched from Tanegashima, Japan, on 24 May 2014 at 03:05:00 UTC by an H-IIA 202.[4]

See also

References

  1. ^ a b "SOCRATES". eoPortal Directory. Retrieved 2016-08-24.
  2. ^ Krebs, Gunter Dirk (2016-04-21). "SOCRATES". Gunter's Space Page. Retrieved 2016-08-24.
  3. ^ "SOCRATES". NASA Space Science Data Coordinated Archive. 27 April 2016. Retrieved 2016-08-04.
  4. ^ "SOCRATES". NASA Space Science Data Coordinated Archive. 27 April 2016. Retrieved 2016-08-04.

External links