BS-3B (YURI 3B)
NORAD 21668
Payload
GEO
1991-060A
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GEO · NORAD 21668
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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
36190 km
Apogee
36223 km
Inclination
13.4°
Period
1457.6 min
Mean Motion
0.98792781 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,207 km
Orbital Velocity11,015 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0004
Semi-Major Axis42,578 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1991-08-25
Launch Site
TNSTA
Int'l Designator
1991-060A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
BS-3B (YURI 3B) is an active satellite operated by Japan, launched on 1991-08-25 from TNSTA. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,190 km and 36,223 km with an inclination of 13.4°. It travels at approximately 11,015 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-3B (YURI 3B) 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-3B (YURI 3B) 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 13.4°, 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-3B (YURI 3B)’s average altitude, there are currently 97 active payloads and 17 tracked debris or rocket body fragments. Japan operates approximately 189 active satellites in total, of which 9 share a similar altitude band with BS-3B (YURI 3B).
❓ Frequently Asked Questions
BS-3B (YURI 3B) orbits at approximately 36,207 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 11,015 km/h — it just keeps pace with the ground below. With an inclination of 13.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
BS-3B (YURI 3B) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21668. You can track BS-3B (YURI 3B) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
BS-3B (YURI 3B) was launched on 1991-08-25 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks BS-3B (YURI 3B) (NORAD ID 21668) 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-3B (YURI 3B) travels at approximately 11,015 km/h (6,844 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.