HIMAWARI 3 AKM
NORAD 22266
Rocket Body
GEO
1984-080E
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GEO · NORAD 22266
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35346 km
Apogee
36518 km
Inclination
9.5°
Period
1443.5 min
Mean Motion
0.99756971 rev/day
TLE Epoch
2026-06-26 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,932 km
Orbital Velocity11,051 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0139
Semi-Major Axis42,303 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1984-08-02
Launch Site
TNSTA
Int'l Designator
1984-080E
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
HIMAWARI 3 AKM is a spent rocket body associated with Japan, launched on 1984-08-02 from TNSTA on the GMS 3 launch. With over 42 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,346 km and 36,518 km with an inclination of 9.5°. It travels at approximately 11,051 km/h (3.07 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. Spent rocket bodies like HIMAWARI 3 AKM are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
HIMAWARI 3 AKM 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 9.5°, 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 HIMAWARI 3 AKM’s average altitude, there are currently 62 active payloads and 18 tracked debris or rocket body fragments. Japan operates approximately 190 active satellites in total, of which 2 share a similar altitude band with HIMAWARI 3 AKM.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
HIMAWARI 3 AKM orbits at approximately 35,932 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 11,051 km/h — it just keeps pace with the ground below. With an inclination of 9.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
HIMAWARI 3 AKM (NORAD ID 22266) is a spent rocket body — the upper stage of a launch vehicle attributed to Japan. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
HIMAWARI 3 AKM was launched on 1984-08-02 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks HIMAWARI 3 AKM (NORAD ID 22266) 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.
HIMAWARI 3 AKM travels at approximately 11,051 km/h (6,867 mph) — roughly 3.07 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.