ETS 8
NORAD 29656
Payload
GEO
2006-059A
● Active
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GEO · NORAD 29656
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
36138 km
Apogee
36152 km
Inclination
11.6°
Period
1454.4 min
Mean Motion
0.99007369 rev/day
TLE Epoch
2026-06-18 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,145 km
Orbital Velocity11,023 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0002
Semi-Major Axis42,516 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2006-12-18
Launch Site
TNSTA
Int'l Designator
2006-059A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ETS 8 is an active satellite operated by Japan, launched on 2006-12-18 from TNSTA. With over 20 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,138 km and 36,152 km with an inclination of 11.6°. It travels at approximately 11,023 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 ETS 8 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 8 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 11.6°, 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 ETS 8’s average altitude, there are currently 174 active payloads and 9 tracked debris or rocket body fragments. Japan operates approximately 189 active satellites in total, of which 19 share a similar altitude band with ETS 8.
❓ Frequently Asked Questions
ETS 8 orbits at approximately 36,145 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 11,023 km/h — it just keeps pace with the ground below. With an inclination of 11.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ETS 8 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 29656. You can track ETS 8 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ETS 8 was launched on 2006-12-18 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks ETS 8 (NORAD ID 29656) 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 8 travels at approximately 11,023 km/h (6,849 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.