BS-2B (YURI 2B)
NORAD 16597
Payload
GEO
1986-016A
● Active
CONNECTING…
GEO · NORAD 16597
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
36009 km
Apogee
36119 km
Inclination
12.3°
Period
1450.3 min
Mean Motion
0.99290443 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,064 km
Orbital Velocity11,033 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0013
Semi-Major Axis42,435 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1986-02-12
Launch Site
TNSTA
Int'l Designator
1986-016A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
BS-2B (YURI 2B) is an active satellite operated by Japan, launched on 1986-02-12 from TNSTA. With over 40 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,009 km and 36,119 km with an inclination of 12.3°. It travels at approximately 11,033 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 BS-2B (YURI 2B) 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-2B (YURI 2B) 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 12.3°, 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-2B (YURI 2B)’s average altitude, there are currently 123 active payloads and 21 tracked debris or rocket body fragments. Japan operates approximately 189 active satellites in total, of which 19 share a similar altitude band with BS-2B (YURI 2B).
❓ Frequently Asked Questions
BS-2B (YURI 2B) orbits at approximately 36,064 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 11,033 km/h — it just keeps pace with the ground below. With an inclination of 12.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
BS-2B (YURI 2B) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 16597. You can track BS-2B (YURI 2B) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
BS-2B (YURI 2B) was launched on 1986-02-12 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks BS-2B (YURI 2B) (NORAD ID 16597) 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-2B (YURI 2B) travels at approximately 11,033 km/h (6,856 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.