HIMAWARI 5 AKM
NORAD 23524
Rocket Body
GEO
1995-011D
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GEO · NORAD 23524
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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
34595 km
Apogee
36429 km
Inclination
13.6°
Period
1422.1 min
Mean Motion
1.01259277 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,512 km
Orbital Velocity11,106 km/h
Velocity3.08 km/s
Orbital Period23 hours 42 minutes
Orbits / Day1.01
Eccentricity0.0219
Semi-Major Axis41,883 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1995-03-18
Launch Site
TNSTA
Int'l Designator
1995-011D
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
HIMAWARI 5 AKM is a spent rocket body associated with Japan, launched on 1995-03-18 from TNSTA on the SFU launch. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 34,595 km and 36,429 km with an inclination of 13.6°. It travels at approximately 11,106 km/h (3.08 km/s), completing one full orbit every 23 hours 42 minutes — that’s roughly 1.01 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 5 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 5 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 13.6°, 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 5 AKM’s average altitude, there are currently 2 active payloads and 36 tracked debris or rocket body fragments. Japan operates approximately 190 active satellites in total.
🔗 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 5 AKM orbits at approximately 35,512 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 11,106 km/h — it just keeps pace with the ground below. With an inclination of 13.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
HIMAWARI 5 AKM (NORAD ID 23524) 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 5 AKM was launched on 1995-03-18 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks HIMAWARI 5 AKM (NORAD ID 23524) 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 5 AKM travels at approximately 11,106 km/h (6,901 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.