QZS-6 (Michibiki No.6) is a Japanese navigation satellite consisting part of the Quasi-Zenith Satellite System (QZSS). QZS-6 was deployed to a geostationary orbit (GEO). With the launch of QZS-5, QZS-6, and QZS-7, the QZSS will expand from a GNSS augmentation service to an independent regional navigation satellite system (RNSS) covering the Asia-Pacific region.
Satellite QZS-6 is the first of three Michibiki satellites to be launched to expand QZSS to a seven-satellite constellation. In 2017, Michibiki's four-satellite constellation was established, and with it there are at a minimum two Michibiki satellites (one in QZO and one in GEO) constantly visible from Japan. Satellite navigation requires at least four satellites to be visible, so users need to receive signals from QZSS and other global navigation satellite system (GNSS) at the same time. In its seven-satellite constellation, four Michibiki satellites (one in QZO, two in GEO, and one in quasi-geostationary orbit (QGEO)) will be constantly visible from Japan, thus eliminating the system's dependency on other GNSS. QZS-6 joined QZS-3 in geostationary orbit.
QZS-6 was manufactured by Mitsubishi Electric (MELCO), and its positioning mission payload was manufactured by NEC. QZS-6 has a design life of 15 years. The satellite has a Precise Ranging Payload (PRP) consisting of Inter-satellite ranging (ISR) and satellite/ground bi-directional ranging. PRP enables the satellite to achieve a precise positioning measurement compared to previous Michibiki satellites. The Japan Aerospace Exploration Agency's Advanced Satellite Navigation System (ASNAV) project is responsible for Michibiki's PRP. For ISR, QZS-6 will receive signals sent from QZS-5 and will measure the distance between them.
Secondary payload
Following a Memorandum of Understanding between the governments of Japan and the United States made on 15 December 2020 regarding hosted payloads, QZS-6 hosts a secondary payload from the United States Space Force as part of the Quasi-Zenith Satellite System Hosted Payload (QZSS-HP) framework, called QZS6-HP1. The US Space Force Mission Delta 2's Situational Awareness Camera Hosted Instrument (SĀCHI, meaning 'search' in Japanese), developed by MIT Lincoln Laboratory, is a space domain awareness (SDA) payload that will monitor objects in geosynchronous orbit and send the data in near real time to the SDA database at Schriever Space Force Base. QZS-6 is the third foreign-owned satellite to carry a US Space Force payload, following Space Norway's ASBM 1 and 2.
Launch QZS-6 was launched on 2 February 2025. By May 2025, the US Space Force's QZS6-HP1 achieved first light.
Comparison of QZS-5, 6, and 7 +Comparison of QZS-5, 6, and 7Schematics of satelliteQZS-5QZS-6QZS-7Design life (after launch)15 yearsLaunch date22 December 20252 February 20252026OrbitQZOGEOQGEORocketH3-22SMass (dry/launch)1.8t/4.8t1.9t/4.9t2.0t/5.0tBlock typeIII-QIII-GIII-GPayload electricity consumption2.4kW2.7kW3.0kWPosition, Navigation, and Timing (PNT)L1-C/A (L1-C/B), L1C, L5Precise Point Positioning (PPP)L6Position Technology Verification Service (PTV)—L1Sb, L5SL-band antenna typePatch antennaPrecise Ranging Payload (PRP)Inter-satellite ranging (ISR), satellite/ground bi-directional rangingMessage Communication Payload (MCP)—S-band (MCP developed by MELCO)Secondary Payload—SĀCHI
References
External links Special website of launch Michibiki seven-satellite constellation special website