HALCA

HALCA
HALCA after the final assembly during a solar battery check at Uchinoura
NamesMUSES-B
VSOP
Haruka (はるか)
Mission typeAstronomy
OperatorISAS
COSPAR ID1997-005A Edit this at Wikidata
SATCAT no.24720
WebsiteHALCA Home
Mission duration8 years, 9 months, 18 days
Spacecraft properties
ManufacturerNEC Toshiba Space Systems
Launch mass830 kg (1,830 lb)
Dimensions1.5 m × 1 m (4.9 ft × 3.3 ft)
Start of mission
Launch date04:50, February 12, 1997 (UTC) (1997-02-12T04:50Z)
RocketM-5-1
Launch siteKagoshima M-V Pad
End of mission
DisposalDecommissioned
DeactivatedNovember 30, 2005 (2005-11-30)
Orbital parameters
Reference systemGeocentric
RegimeHighly elliptical
Semi-major axis17,259 km (10,724 mi)
Eccentricity0.5999671
Perigee altitude533.5 km (331.5 mi)
Apogee altitude21,244.1 km (13,200.5 mi)
Inclination31.1880 degrees
Period376.1 minutes
RAAN127.6566 degrees
Argument of perigee143.9533 degrees
Mean anomaly358.3371 degrees
Mean motion3.82867831 rev/day
Epoch28 April 2016, 09:56:58 UTC[1]
Revolution no.26766
Main telescope
TypeMesh antenna
Diameter8 m (26 ft)
Wavelengths1.3, 6, 18 cm (radio)

HALCA (Highly Advanced Laboratory for Communications and Astronomy), also known for its project name VSOP (VLBI Space Observatory Programme), the code name MUSES-B (for the second of the Mu Space Engineering Spacecraft series), or just Haruka (はるか)[2] was a Japanese 8 meter diameter radio telescope satellite which was used for Very Long Baseline Interferometry (VLBI). It was the first such space-borne dedicated VLBI mission.

  1. ^ "HALCA (MUSES-B) Satellite details 1997-005A NORAD 24720". N2YO. 28 April 2016. Retrieved 28 April 2016.
  2. ^ ""Haruka" large antenna and space VLBI (「はるか」大型アンテナとスペースVLBI)". ISAS JAXA + translate.google.com. Retrieved 2020-01-24.

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