Rocket: H-IIA; Payload: Michibiki No. 4; Date: 9 October 2017, 2201 UTC; Launch site: Tanegashima Space Center, Japan. The satellite, which will become part of Japan’s navigational Quasi-Zenith Satellite System, separated from the launch vehicle approx. 29 minutes after lift-off.
The RSS feed has been moved to http://www.sat-index.co.uk/feed/rssoutput.xml and https://www.sat-nd.com/feed/rssoutput.xml
Rocket: Chang Zheng 11; Payload: two GECAM astronomy satellites; Date: 9 December 2020, 2014 UTC; Launch site: Xichang Satellite Launch…
The first mockup of the RD-0124MS rocket engine, developed for use in the Soyuz-5 perspective rocket was built at Voronezh…
NASA and Boeing are targeting 29 March for the launch of Starliner’s second uncrewed flight test to the International Space…
Supporting a rideshare manifest with a mix of small and large satellites, TriSept Corporation has selected Relativity Space for a…
Airbus has successfully qualified Europe’s first five metre deployable antenna reflector. The 70 kilogram deployable reflector will help enable higher…