QZS-7
NORAD 100270
Payload
MEO
2026-182A
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MEO · NORAD 100270
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
390 km
Apogee
35372 km
Inclination
22.9°
Period
626.7 min
Mean Motion
2.29741957 rev/day
TLE Epoch
2026-08-10 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude17,881 km
Orbital Velocity14,595 km/h
Velocity4.05 km/s
Orbital Period10 hours 27 minutes
Orbits / Day2.30
Eccentricity0.7212
Semi-Major Axis24,252 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2026-08-10
Launch Site
TNSTA
Int'l Designator
2026-182A
Object Type
Payload
RCS Size
Unknown
📖 About This Object
QZS-7 is an active satellite operated by Japan, launched on 2026-08-10 from TNSTA. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Medium Earth Orbit (MEO) at altitudes between 390 km and 35,372 km with an inclination of 22.9°. It travels at approximately 14,595 km/h (4.05 km/s), completing one full orbit every 10 hours 27 minutes — that’s roughly 2.30 orbits per day. Its orbital eccentricity of 0.7212 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks QZS-7 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
QZS-7 orbits at an average altitude of 17,881 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of QZS-7’s average altitude, there are currently 2 active payloads and 18 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 22.9°, QZS-7 passes over latitudes between 22.9°N and 22.9°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Japan operates approximately 202 active satellites in total.
🔗 Quasi-Zenith Satellite System (QZSS)
This satellite is part of Japan's Quasi-Zenith Satellite System (QZSS), a regional satellite navigation augmentation system providing centimetre-level positioning accuracy over Japan and the Asia-Oceania region. QZSS supplements GPS with satellites in highly inclined geosynchronous and geostationary orbits, ensuring at least one satellite is always near-zenith over Japan.
❓ Frequently Asked Questions
QZS-7 orbits in Medium Earth Orbit (MEO) at altitudes between 390 km (perigee) and 35,372 km (apogee), with an average altitude of approximately 17,881 km. It completes one orbit every 10 hours 27 minutes, travelling at approximately 14,595 km/h (9,069 mph).
QZS-7 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 100270. You can track QZS-7 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
QZS-7 was launched on 2026-08-10 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks QZS-7 (NORAD ID 100270) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
QZS-7 travels at approximately 14,595 km/h (9,069 mph) — roughly 4.05 km/s. It completes 2.30 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.