QZS-5

Japanese navigation satellite From Wikipedia, the free encyclopedia

QZS-5 (Michibiki No.5) was a Japanese navigation satellite lost during launch. It was intended to form part of the Quasi-Zenith Satellite System (QZSS). QZS-5 was to be deployed to a quasi-zenith orbit (QZO).

Quick facts Mission type, Operator ...
QZS-5
Artist's rendering of QZS-5 in orbit
Mission typeNavigation
OperatorCAO
COSPAR ID2025-308A Edit this at Wikidata
SATCAT no.67231Edit this on Wikidata
Websitehttps://qzss.go.jp/
Spacecraft properties
Spacecraft typeQZS Block III-Q[1]
BusDS2000
ManufacturerMitsubishi Electric
Launch mass4.8t
Dry mass2.0t
Payload mass647kg[2]
Power6.7kW
Start of mission
Launch date22 December 2025, 01:51:00 (2025-12-22UTC01:51Z) UTC
RocketH3-22S
Launch siteTanegashima, LA-Y2
ContractorJAXA
Orbital parameters
Reference systemGeocentric
RegimeMedium Earth orbit
 QZS-6
QZS-7 
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Satellite

QZS-5 was the second 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.[3] 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 dependancy on other GNSS. QZS-5 was to join QZS-2 and 4, QZS-1R in Quasi Zenith Orbit.

QZS-5 was manufactured by Mitsubishi Electric (MELCO), and its positioning mission payload was manufactured by NEC.[4] QZS-5 had an intended design life of 15 years.[2] Like QZS-6 and QZS-7, the satellite had a Precise Ranging Payload (PRP) consisting of Inter-satellite ranging (ISR) and satellite/ground bi-directional ranging. PRP enabled 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.[5] For ISR, QZS-5 was to be the source of the signals. QZS-6 and QZS-7 were to receive QZS-5's signal to measure the distance between them.[6]

Launch

QZS-5 was launched aboard an H3-22S rocket on 22 December 2025. An anomaly occurred during the second-stage burn that led to a premature engine cutoff and the subsequent loss of the QZS-5 satellite.[7][8]

Comparison of QZS-5, 6, and 7

More information Schematics of satellite, Design life (after launch) ...
Comparison of QZS-5, 6, and 7[2][1]
Schematics of satellite QZS-5 QZS-6 QZS-7
Design life (after launch) 15 years
Launch date 22 December 2025 2 February 2025 2026
Orbit QZO GEO QGEO
Rocket H3-22S
Mass (dry/launch) 1.8t/4.8t 1.9t/4.9t 2.0t/5.0t
Block type III-Q III-G III-G
Payload electricity consumption 2.4kW 2.7kW 3.0kW
Position, Navigation, and Timing (PNT) L1-C/A (L1-C/B), L1C, L5
Precise Point Positioning (PPP) L6
Position Technology Verification Service (PTV) L1Sb, L5S
L-band antenna type Patch antenna
Precise Ranging Payload (PRP) Inter-satellite ranging (ISR), satellite/ground bi-directional ranging
Message Communication Payload (MCP) S-band (MCP developed by MELCO)
Secondary Payload SĀCHI
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References

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