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ETS 6

NORAD 23230 Payload MEO 1994-056A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
8447 km
Apogee
38794 km
Inclination
12.5°
Period
861.8 min
Mean Motion
1.67089522 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude23,621 km
Orbital Velocity13,124 km/h
Velocity3.65 km/s
Orbital Period14 hours 22 minutes
Orbits / Day1.67
Eccentricity0.5059
Semi-Major Axis29,992 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1994-08-28
Launch Site
TNSTA
Int'l Designator
1994-056A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ETS 6 is an active satellite operated by Japan, launched on 1994-08-28 from TNSTA. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 8,447 km and 38,794 km with an inclination of 12.5°. It travels at approximately 13,124 km/h (3.65 km/s), completing one full orbit every 14 hours 22 minutes — that’s roughly 1.67 orbits per day. Its orbital eccentricity of 0.5059 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks ETS 6 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ETS 6 orbits at an average altitude of 23,621 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 ETS 6’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 12.5°, ETS 6 passes over latitudes between 12.5°N and 12.5°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Japan operates approximately 189 active satellites in total.
❓ Frequently Asked Questions
ETS 6 orbits in Medium Earth Orbit (MEO) at altitudes between 8,447 km (perigee) and 38,794 km (apogee), with an average altitude of approximately 23,621 km. It completes one orbit every 14 hours 22 minutes, travelling at approximately 13,124 km/h (8,155 mph).
ETS 6 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23230. You can track ETS 6 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ETS 6 was launched on 1994-08-28 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks ETS 6 (NORAD ID 23230) 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.
ETS 6 travels at approximately 13,124 km/h (8,155 mph) — roughly 3.65 km/s. It completes 1.67 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.