GLOBALSTAR M067

Additional information GLOBALSTAR M067

The GLOBALSTAR M067 satellite, also known as Globalstar M067, was launched on October 20, 2007, from Tyuratam (Baikonur Cosmodrome), using a Soyuz-FG launch vehicle from LC31. It is part of the US communication constellation and has a configuration based on the LS-400 bus with a shape described as Box + 2 Pan. The satellites dimensions are 1.5 meters in length, 0.6 meters in diameter, and it spans up to 12 meters when fully deployed, indicating the presence of deployable solar arrays. Its dry mass is approximately 380 kilograms, while its launch mass was around 450 kilograms. The satellite is equipped with a motor called LS-400 AOCS for attitude control and uses batteries alongside two deployable solar arrays to power its operations. GLOBALSTAR M067 has an expected operational lifetime of 7.5 years and serves as part of the communication network operated by Globalstar, manufacturing was done by LOR (Lockheed Martin Commercial Space Systems).

Average inclination GLOBALSTAR M067

Mean right ascension of the ascending node (RAAN) GLOBALSTAR M067

Mean argument of perigee GLOBALSTAR M067

Mean semi-major axis of the orbit GLOBALSTAR M067

Mean orbital eccentricity GLOBALSTAR M067