General Administration of Quality Supervision, Inspection and Quarantine of the People‘s Republic of China
Latest
GB/T 32300-2015
Scope
This standard specifies the calculation method for the orbital elements of the launch vehicle and payload separation point, including orbital elements and calculation conditions, orbital element calculation methods, and orbital element error calculation methods. This standard is applicable to the calculation method of the orbit elements of different payloads such as satellites, manned spacecraft, and space stations, and is applicable to different orbits such as low earth orbit, sun synchronous orbit, medium earth orbit, geosynchronous transfer orbit, and geosynchronous orbit.
GB/T 32300-2015 history
2015GB/T 32300-2015 Best practices for orbit elements at payload-launch vehicle separation