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N-STAR a

N-STAR a
Mission typeCommunications
OperatorSKY Perfect JSAT Group
COSPAR ID1995-044A[1]
SATCAT no.23651
Mission duration10 years (planned)
Spacecraft properties
SpacecraftN-STAR a
BusSSL 1300
ManufacturerSpace Systems/Loral
Launch mass3,400 kg (7,500 lb)[2]
BOL mass2,050 kg (4,520 lb)
Dry mass1,617 kg (3,565 lb)
Start of mission
Launch date29 August 1995, 06:41:00 UTC[1]
RocketAriane 44P H10-3
Launch siteKourou, ELA-2
ContractorArianespace
Orbital parameters
Reference systemGeocentric orbit[3]
RegimeGeostationary orbit
Transponders
Band6 C-band
11 Ka-band
8 Ku-band
1 S-band[4]
Coverage areaJapan
 

N-STAR a, was a geostationary communications satellite originally ordered by a consortium including NTT DoCoMo and JSAT Corporation, and later fully acquired by JSAT, which was merged into SKY Perfect JSAT Group. It was designed and manufactured by Space Systems/Loral on the SSL 1300 platform.[2] It had a launch weight of 3,400 kg (7,500 lb), and a 10-year design life.[2] Its payload is composed of 6 C-band, 11 Ka-band, 8 Ku-band and 1 S-band transponders.

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  2. ^ a b c Cite error: The named reference gsp-nstara was invoked but never defined (see the help page).
  3. ^ Cite error: The named reference nyo-23651date20160819 was invoked but never defined (see the help page).
  4. ^ Cite error: The named reference soumu-wp1999chapter2 was invoked but never defined (see the help page).

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