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KIKU 3 (ETS 4)

NORAD 12295 Payload MEO 1981-012A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
293 km
Apogee
12201 km
Inclination
28.4°
Period
235.3 min
Mean Motion
6.11993176 rev/day
TLE Epoch
2026-08-03 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude6,247 km
Orbital Velocity20,234 km/h
Velocity5.62 km/s
Orbital Period3 hours 55 minutes
Orbits / Day6.12
Eccentricity0.4719
Semi-Major Axis12,618 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1981-02-11
Launch Site
TNSTA
Int'l Designator
1981-012A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
KIKU 3 (ETS 4) is an active satellite operated by Japan, launched on 1981-02-11 from TNSTA on the ETS-4 launch. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 293 km and 12,201 km with an inclination of 28.4°. It travels at approximately 20,234 km/h (5.62 km/s), completing one full orbit every 3 hours 55 minutes — that’s roughly 6.12 orbits per day. Its orbital eccentricity of 0.4719 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks KIKU 3 (ETS 4) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
KIKU 3 (ETS 4) orbits at an average altitude of 6,247 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of KIKU 3 (ETS 4)’s average altitude, there are currently 1 active payload and 3 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 28.4°, KIKU 3 (ETS 4) passes over latitudes between 28.4°N and 28.4°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Japan operates approximately 200 active satellites in total.
❓ Frequently Asked Questions
KIKU 3 (ETS 4) orbits in Medium Earth Orbit (MEO) at altitudes between 293 km (perigee) and 12,201 km (apogee), with an average altitude of approximately 6,247 km. It completes one orbit every 3 hours 55 minutes, travelling at approximately 20,234 km/h (12,573 mph).
KIKU 3 (ETS 4) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 12295. You can track KIKU 3 (ETS 4) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
KIKU 3 (ETS 4) was launched on 1981-02-11 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks KIKU 3 (ETS 4) (NORAD ID 12295) 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.
KIKU 3 (ETS 4) travels at approximately 20,234 km/h (12,573 mph) — roughly 5.62 km/s. It completes 6.12 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 12 sunrises and sunsets every 24 hours.