High-orbit optical remote sensing satellite structure

A high-orbit optical remote sensing satellite structure comprises a force bearing cylinder (1), fuel tanks (2), an oxygen tank (3), a satellite platform (8), solar wings (11), a load adaption structure (14), a camera (15) and the like. The oxygen tank (3) is mounted in the force bearing cylinder (1), and the fuel tanks (2) are mounted on the two sides of the force bearing cylinder (1) through fueltank supports (4) located at the two ends of the fuel tanks (2) and fuel tank top pull plates (5) correspondingly. The force bearing cylinder (1), the fuel tanks (2), the oxygen tank (3), the fuel tank supports (4) and the fuel tank top pull plates (5) are mounted in the satellite platform (8). The camera (15) is mounted at the top of the satellite platform (8) through the load adaption structure(14), and the solar wings (11) are mounted on the two sides of the satellite platform (8) correspondingly. According to the high-orbit optical remote sensing satellite structure, the whole mass center of a satellite is lowered, the load mounting face environment condition is improved, and meanwhile the mounting requirements of control propelling equipment such as the fuel tanks (2) and the oxygentank (3) are met.