BeeSat-1

BeeSat-1

BeeSat-1
BeeSat-1 before launch
Mission type Technology
Operator TUB
COSPAR ID 2009-051C
SATCAT № 35933
Website /_overview/project/v-menue2/beesat.de.tu-berlin.raumfahrttechnikwww
Mission duration 12 months (planned)
15+ months (achieved)
Spacecraft properties
Spacecraft type 1U CubeSat
Launch mass 1 kilogram (2.2 lb)
Start of mission
Launch date 23 September 2009, 06:21 (2009-09-23T06:21Z) UTC
Rocket PSLV-CA C14
Launch site Satish Dhawan FLP
Contractor ISRO
Orbital parameters
Reference system Geocentric
Regime Sun-synchronous
Perigee 713 kilometres (443 mi)
Apogee 723 kilometres (449 mi)
Inclination 98.36 degrees
Period 99.01 minutes
Epoch 21 January 2014, 05:49:02 UTC[1]

BeeSat-1 or Berlin Experimental and Educational Satellite 1, is a German satellite operated by the Technical University of Berlin. The spacecraft is a single unit CubeSat, which was designed to test systems intended for use on future spacecraft, including a new design of reaction wheel.[2][3] It has also been used for amateur radio, and is equipped with a small camera.[4]

BeeSat-1 was launched by a Polar Satellite Launch Vehicle, serial number C14, flying in the Core Alone, or PSLV-CA, configuration.[5] The launch took place from the First Launch Pad at the Satish Dhawan Space Centre, at 06:21 UTC on 23 September 2009.[6] BeeSat-1 was a secondary payload aboard the rocket, which deployed the Oceansat-2 satellite. Five other secondary payloads were flown aboard the rocket; SwissCube-1, UWE-2, ITU-pSat1, Rubin 9.1 and Rubin 9.2.[7][8]

BeeSat-1 is operating in a sun synchronous orbit with an apogee of 723 kilometres (449 mi), a perigee of 714 kilometres (444 mi) and 98.4 degrees of inclination to the equator. It has an orbital period of 99.16 minutes.[9] BeeSat-1 was designed to operate for at least twelve months,[2] and as of January 2011 it is still operational.[4]

See also

References

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