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Home Library Satellite Directory HIMAWARI 1 (GMS 1)

HIMAWARI 1 (GMS 1)

NORAD 10143 Payload GEO 1977-065A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36007 km
Apogee
36145 km
Inclination
6.5°
Period
1450.9 min
Mean Motion
0.99247881 rev/day
TLE Epoch
2026-06-19 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,076 km
Orbital Velocity11,032 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0016
Semi-Major Axis42,447 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1977-07-14
Launch Site
Cape Canaveral, Florida
Int'l Designator
1977-065A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
HIMAWARI 1 (GMS 1) is an active satellite operated by Japan, launched on 1977-07-14 from Cape Canaveral, Florida. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,007 km and 36,145 km with an inclination of 6.5°. It travels at approximately 11,032 km/h (3.06 km/s), completing one full orbit every 24.2 hours — 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 1 (GMS 1) 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 1 (GMS 1) 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 6.5°, 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 1 (GMS 1)’s average altitude, there are currently 137 active payloads and 13 tracked debris or rocket body fragments. Japan operates approximately 189 active satellites in total, of which 19 share a similar altitude band with HIMAWARI 1 (GMS 1).
❓ Frequently Asked Questions
HIMAWARI 1 (GMS 1) orbits at approximately 36,076 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 11,032 km/h — it just keeps pace with the ground below. With an inclination of 6.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
HIMAWARI 1 (GMS 1) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 10143. You can track HIMAWARI 1 (GMS 1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HIMAWARI 1 (GMS 1) was launched on 1977-07-14 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks HIMAWARI 1 (GMS 1) (NORAD ID 10143) 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 1 (GMS 1) travels at approximately 11,032 km/h (6,855 mph) — roughly 3.06 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.