SES-4
SES-4 Names NSS-14 Mission type Communications Operator SES New Skies / SES COSPAR ID 2012-007A SATCAT no. 38087 Website https://www.ses.com/ Mission duration 15 years (planned) 12 years, 8 months, 13 days (elapsed)
Spacecraft NSS-14 Bus SSL-1300 Manufacturer Space Systems/Loral Launch mass 6,180 kg (13,620 lb) Power 20 kW [ 1]
Launch date 14 February 2012, 19:36:37 UTC [ 2] Rocket Proton-M / Briz-M Launch site Baikonur , Site 200/39 Contractor Khrunichev State Research and Production Space Center Entered service April 2012
Reference system Geocentric orbit [ 3] Regime Geostationary orbit Longitude 22° West
Band 124 transponders : 52 C-band 72 Ku-band Bandwidth 36 MHz Coverage area North America , South America , Europe, Middle East , West Africa
SES-4 is a communications satellite operated by SES World Skies (now SES ).
Spacecraft
SES-4 was built by Space Systems/Loral (SSL), and is based on the SSL-1300 satellite bus . It is equipped with 52 C-band , and 72 Ku-band transponders , and at launch it had a mass of 6,180 kg (13,620 lb). It has a design life of fifteen years.[ 4]
Launch
It was launched on 14 February 2012, at 19:36:37 UTC on a Proton-M / Briz-M launch vehicle , the launch was arranged by International Launch Services (ILS), since Baikonour , Site 200/39 .[ 4]
Mission
It is positioned at 22° West orbital location over Atlantic Ocean , replacing NSS-7 .[ 4]
References
^ "Display: SES 4 2012-007A" . NASA. 5 April 2021. Retrieved 12 April 2021 . This article incorporates text from this source, which is in the public domain .
^ "Launch Log" . Jonathan's Space Report. 14 March 2021. Retrieved 12 April 2021 .
^ "SES 4" . N2YO.com. Retrieved 12 April 2021 .
^ a b c "SES 4" . Gunter's Space Page. 11 December 2017. Retrieved 12 April 2021 .
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EchoStar XVII , MSG-3
SES-5
Soyuz TMA-05M
Kounotori 3 (Raiko , We-Wish , Niwaka , TechEdSat , F-1 )
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Tianlian I-03
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