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SES-15

From Wikipedia, the free encyclopedia
Geostationary communications satellite

SES-15
Mission typeCommunications
OperatorSES
COSPAR ID2017-026AEdit this at Wikidata
SATCATno.42709
Websitehttps://www.ses.com/
Mission duration15 years (planned)
8 years, 8 months, 25 days (elapsed)
Spacecraft properties
SpacecraftSES-15
Spacecraft typeBoeing 702
BusBSS-702P
ManufacturerBoeing Satellite Systems
Launch mass2,302 kg (5,075 lb)
Start of mission
Launch date18 May 2017, 11:54:53UTC
RocketSoyuz ST-A /Fregat-M
Launch siteCentre Spatial Guyanais,ELS
ContractorProgress Rocket Space Centre
Entered serviceJuly 2017
Orbital parameters
Reference systemGeocentric orbit
RegimeGeostationary orbit
Longitude129° West
Transponders
BandKu-band,Ka-band,Wide Area Augmentation System (WAAS-GEO 6)
Coverage areaNorth America,Latin America,Caribbean,Atlantic Ocean region
← SES-14
SES-16 →

SES-15 is ageostationarycommunications satellite operated bySES and designed and manufactured byBoeing Satellite Systems. It has a mass of 2,302 kg (5,075 lb) and has a design life of at least 15 years.[1]

See also

[edit]

References

[edit]
  1. ^"SES 15". Gunter's Space Page. 18 April 2018. Retrieved13 April 2021.
Satellites operated bySES
SES fleet
AMC fleet
NSS fleet
Astra fleet
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Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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