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QZS-1 (MICHIBIKI)

NORAD 37158 Payload GEO 2010-045A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
39691 km
Apogee
39750 km
Inclination
44.2°
Period
1641.7 min
Mean Motion
0.87714915 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude39,721 km
Orbital Velocity10,587 km/h
Velocity2.94 km/s
Orbital Period27.4 hours
Orbits / Day0.88
Eccentricity0.0006
Semi-Major Axis46,092 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan Aerospace Exploration Agency (JAXA) (Japan)
Launch Date
2010-09-11
Launch Site
TNSTA
Int'l Designator
2010-045A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
QZS-1 (MICHIBIKI) is an active satellite operated by Japan Aerospace Exploration Agency (JAXA) (Japan), launched on 2010-09-11 from TNSTA. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 39,691 km and 39,750 km with an inclination of 44.2°. It travels at approximately 10,587 km/h (2.94 km/s), completing one full orbit every 27.4 hours — that’s roughly 0.88 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-1 (MICHIBIKI) 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-1 (MICHIBIKI) 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 44.2°, 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-1 (MICHIBIKI)’s average altitude, there are currently 3 active payloads and 0 tracked debris or rocket body fragments. Japan operates approximately 189 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-1 (MICHIBIKI) orbits at approximately 39,721 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 10,587 km/h — it just keeps pace with the ground below. With an inclination of 44.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
QZS-1 (MICHIBIKI) is operated by Japan Aerospace Exploration Agency (JAXA) (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 37158. You can track QZS-1 (MICHIBIKI) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
QZS-1 (MICHIBIKI) was launched on 2010-09-11 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks QZS-1 (MICHIBIKI) (NORAD ID 37158) 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-1 (MICHIBIKI) travels at approximately 10,587 km/h (6,578 mph) — roughly 2.94 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.