KIKU 3 (ETS 4)
NORAD 12295
Payload
MEO
1981-012A
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🛰️ Orbital Parameters
Perigee
288 km
Apogee
12259 km
Inclination
28.5°
Period
236.0 min
Mean Motion
6.10122987 rev/day
TLE Epoch
2026-05-08 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude6,274 km
Orbital Velocity20,213 km/h
Velocity5.61 km/s
Orbital Period3 hours 56 minutes
Orbits / Day6.10
Eccentricity0.4734
Semi-Major Axis12,645 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. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 288 km and 12,259 km with an inclination of 28.5°. It travels at approximately 20,213 km/h (5.61 km/s), completing one full orbit every 3 hours 56 minutes — that’s roughly 6.10 orbits per day. Its orbital eccentricity of 0.4734 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) operates in Medium Earth Orbit (MEO), the region between LEO and GEO spanning roughly 2,000 to 35,786 km altitude. MEO is home to navigation constellations (GPS at ~20,200 km, Galileo at ~23,222 km, GLONASS at ~19,130 km) and some communications systems. The higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer satellites are needed for global coverage, but signal latency is higher and radiation exposure — particularly from the Van Allen belts — is a significant design challenge.
❓ Frequently Asked Questions
KIKU 3 (ETS 4) orbits in Medium Earth Orbit (MEO) at altitudes between 288 km (perigee) and 12,259 km (apogee), with an average altitude of approximately 6,274 km. It completes one orbit every 3 hours 56 minutes, travelling at approximately 20,213 km/h (12,559 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.
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.
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.
KIKU 3 (ETS 4) travels at approximately 20,213 km/h (12,559 mph) — roughly 5.61 km/s. It completes 6.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 12 sunrises and sunsets every 24 hours.