Geostationary communications satellite
SES-15 Mission type Communications Operator SES COSPAR ID 2017-026A SATCAT no. 42709 Website https://www.ses.com/ Mission duration 15 years (planned) 7 years, 7 months, 1 day (elapsed)
Spacecraft SES-15 Spacecraft type Boeing 702 Bus BSS-702P Manufacturer Boeing Satellite Systems Launch mass 2,302 kg (5,075 lb)
Launch date 18 May 2017, 11:54:53 UTC Rocket Soyuz ST-A / Fregat-M Launch site Centre Spatial Guyanais , ELS Contractor Progress Rocket Space Centre Entered service July 2017
Reference system Geocentric orbit Regime Geostationary orbit Longitude 129° West
Band Ku-band , Ka-band , Wide Area Augmentation System (WAAS-GEO 6)Coverage area North America , Latin America , Caribbean , Atlantic Ocean region
SES-15 is a geostationary communications satellite operated by SES and designed and manufactured by Boeing 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
References
^ "SES 15" . Gunter's Space Page. 18 April 2018. Retrieved 13 April 2021 .
January February March April May June
QZS-2
ViaSat-2 , Eutelsat 172B
Dragon CRS-11 (NICER , BRAC Onnesha , GhanaSat-1 , Mazaalai , Nigeria EduSat-1 )
GSAT-19
EchoStar 21
Progress MS-06
HXMT / Insight , ÑuSat 3
ChinaSat 9A
Cartosat-2E , Max Valier Sat , Aalto-1 , Blue Diamond , Green Diamond , Red Diamond , CICERO-6 , COMPASS-2 , InflateSail , Lemur-2 × 8 , LituanicaSAT-2 , ROBUSTA-1B
Kosmos 2519 / Nivelir, Kosmos 2521 / Sputnik Inspektor
BulgariaSat-1
Iridium NEXT × 10
EuropaSat / Hellas Sat 3 , GSAT-17
July August September October November December 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).