HIMAWARI 5 (GMS 5)
NORAD 23522
Payload
GEO
1995-011B
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GEO · NORAD 23522
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🛰️ Orbital Parameters
Perigee
36004 km
Apogee
36059 km
Inclination
14.3°
Period
1448.6 min
Mean Motion
0.99405452 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,032 km
Orbital Velocity11,038 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day0.99
Eccentricity0.0006
Semi-Major Axis42,403 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
1995-011B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
HIMAWARI 5 (GMS 5) is an active satellite operated by Japan, launched on 1995-03-18 from TNSTA. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,004 km and 36,059 km with an inclination of 14.3°. It travels at approximately 11,038 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 0.99 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 HIMAWARI 5 (GMS 5) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HIMAWARI 5 (GMS 5) 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 14.3°, 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 (GMS 5)’s average altitude, there are currently 74 active payloads and 29 tracked debris or rocket body fragments. Japan operates approximately 189 active satellites in total, of which 10 share a similar altitude band with HIMAWARI 5 (GMS 5).
❓ Frequently Asked Questions
HIMAWARI 5 (GMS 5) orbits at approximately 36,032 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 11,038 km/h — it just keeps pace with the ground below. With an inclination of 14.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
HIMAWARI 5 (GMS 5) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23522. You can track HIMAWARI 5 (GMS 5) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HIMAWARI 5 (GMS 5) was launched on 1995-03-18 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks HIMAWARI 5 (GMS 5) (NORAD ID 23522) 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 (GMS 5) travels at approximately 11,038 km/h (6,858 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.