Juno II | Explorer 7
Launch Successful
L - -- : -- : -- : --
Instantaneous launch window.
Launch Window
Oct. 13, 1959, 3:30 p.m. - Oct. 13, 1959, 3:30 p.m.
Instantaneous launch window.
Oct. 13, 1959, 3:30 p.m. - Oct. 13, 1959, 3:30 p.m.
Explorer 7 was designed to measure solar x-ray and Lyman-alpha flux, trapped energetic particles, and heavy primary cosmic rays. Secondary objectives included collecting data on micrometeoroid penetration, molecular sputtering and studying the Earth-atmosphere heat balance.
Juno II was an American space launch vehicle used during the late 1950s and early 1960s. It was derived from the Jupiter missile, which was used as the first stage.
The Army Ballistic Missile Agency was formed to develop the U.S. Army's first large ballistic missile. The agency was established at Redstone Arsenal on 1 February 1956, and commanded by Major General John B. Medaris with Wernher von Braun as technical director.
WIKIChinese communication satellite with name meaning "Satellite Internet - High Orbit Satellite 03" in Chinese. Details TBD.
Hera is a space mission in development at the European Space Agency in its Space Safety program. Its primary objective is to study the Didymos binary…
Replacement Vulcan test launch with inert payload, experiments, and demonstrations for certification with the USSF after delays caused by payload tes…
SpaceX Crew-9 is the ninth crewed operational flight of a Crew Dragon spacecraft to the International Space Station as part of NASA's Commercial Crew…
Shijian 19 is a Chinese recoverable satellite for hoisting various scientific experiments in microgravity. Unlike previous similar Chinese satelli…
The IGS Radar 8 is a Japanese radar reconnaissance satellite. The satellite is operated by the Cabinet Satellite Information Center. The satellite se…
A batch of 20 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Carried 5 satellites to Sun-synchronous orbit: * Zhongke-01/02 * Jilin-1 SAR-01A * Yunyao-21/22
Carried 8 satellites to a 500 km Sun-synchronous orbit: * Tianyi-41 * Luojia 4-01 * Fudan-1 * Tianyan-15 * Jitianxing A-01 * Xingshidai-15/21…
Second batch of five satellites for the French Kinéis IoT constellation designed to operate with 25 nanosatellites of 30 kg each.