BS-3A (YURI 3A)
NORAD 20771
Payload
GEO
1990-077A
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GEO · NORAD 20771
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Altitude (km)
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🛰️ Orbital Parameters
Perigee
36150 km
Apogee
36251 km
Inclination
15.6°
Period
1457.3 min
Mean Motion
0.98812771 rev/day
TLE Epoch
2026-06-18 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,201 km
Orbital Velocity11,016 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0012
Semi-Major Axis42,572 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1990-08-28
Launch Site
TNSTA
Int'l Designator
1990-077A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
BS-3A (YURI 3A) is an active satellite operated by Japan, launched on 1990-08-28 from TNSTA. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,150 km and 36,251 km with an inclination of 15.6°. It travels at approximately 11,016 km/h (3.06 km/s), completing one full orbit every 24.3 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 BS-3A (YURI 3A) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
BS-3A (YURI 3A) 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 15.6°, 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 BS-3A (YURI 3A)’s average altitude, there are currently 104 active payloads and 15 tracked debris or rocket body fragments. Japan operates approximately 189 active satellites in total, of which 9 share a similar altitude band with BS-3A (YURI 3A).
❓ Frequently Asked Questions
BS-3A (YURI 3A) orbits at approximately 36,201 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 11,016 km/h — it just keeps pace with the ground below. With an inclination of 15.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
BS-3A (YURI 3A) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 20771. You can track BS-3A (YURI 3A) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
BS-3A (YURI 3A) was launched on 1990-08-28 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks BS-3A (YURI 3A) (NORAD ID 20771) 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.
BS-3A (YURI 3A) travels at approximately 11,016 km/h (6,845 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.