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QZS-7

NORAD 100270 Payload GEO 2026-182A ● Active
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🛰️ Orbital Parameters
Perigee
35466 km
Apogee
36095 km
Inclination
2.9°
Period
1435.8 min
Mean Motion
1.00292925 rev/day
TLE Epoch
2026-09-24 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,781 km
Orbital Velocity11,070 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0075
Semi-Major Axis42,152 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2026-08-10
Launch Site
Tanegashima Space Center, Japan
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 Tanegashima Space Center, Japan on the QZS 7 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Geostationary Orbit (GEO) at altitudes between 35,466 km and 36,095 km with an inclination of 2.9°. It travels at approximately 11,070 km/h (3.08 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. 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 occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 2.9°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of QZS-7’s average altitude, there are currently 724 active payloads and 49 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Japan operates approximately 207 active satellites in total, of which 27 share a similar altitude band with QZS-7.
🔗 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 at approximately 35,781 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,070 km/h — it just keeps pace with the ground below. With an inclination of 2.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
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 Tanegashima Space Center, Japan, Japan’s primary launch site, operated by JAXA on a small island south of Kyushu. 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 11,070 km/h (6,879 mph) — roughly 3.08 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.