QZS-1R is a Japanese
navigation satellite consisting part of the
Quasi-Zenith Satellite System (QZSS). QZS-1R will replace the
QZS-1 (Michibiki-1) satellite launched in September 2010. QZS-1 has a design life of ten years. As QZS-1 is an experimental satellite, it did not broadcast the MADOCA (Multi-GNSS Advanced Demonstration tool for Orbit and Clock Analysis) signal, which can be used for centimeter-order navigation.[2][3] With the launch of QZS-1R, all satellites of QZSS will be capable of transmitting in the MADOCA signal, reaching operational capacity.[2]
Satellite
QZS-1R is the fourth operational Quasi-Zenith Satellite to be launched. The design of the satellite is based on
QZS-2 and 4, with minor differences such as an increase in the number of temperature sensors on board.[4][5]
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
