UME 2 (ISS-B)
NORAD 10674
Payload
LEO
1978-018A
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🛰️ Orbital Parameters
Perigee
974 km
Apogee
1217 km
Inclination
69.4°
Period
107.2 min
Mean Motion
13.43713355 rev/day
TLE Epoch
2026-05-08 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,096 km
Orbital Velocity26,303 km/h
Velocity7.31 km/s
Orbital Period107 minutes
Orbits / Day13.44
Eccentricity0.0163
Semi-Major Axis7,467 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1978-02-16
Launch Site
TNSTA
Int'l Designator
1978-018A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
UME 2 (ISS-B) is an active satellite operated by Japan, launched on 1978-02-16 from TNSTA. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 974 km and 1,217 km with an inclination of 69.4°. It travels at approximately 26,303 km/h (7.31 km/s), completing one full orbit every 107 minutes — that’s roughly 13.44 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Orbital Radar tracks UME 2 (ISS-B) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
UME 2 (ISS-B) occupies the mid-LEO band between 600 and 1,000 km, where atmospheric drag is minimal but radiation exposure remains low. This altitude range balances orbital longevity (decades to centuries) with reasonable ground coverage, making it popular for remote sensing constellations, scientific instruments and weather satellites. Debris concerns are significant here because objects persist far longer than in lower orbits.
❓ Frequently Asked Questions
UME 2 (ISS-B) orbits in Low Earth Orbit (LEO) at altitudes between 974 km (perigee) and 1,217 km (apogee), with an average altitude of approximately 1,096 km. It completes one orbit every 107 minutes, travelling at approximately 26,303 km/h (16,344 mph).
UME 2 (ISS-B) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 10674. You can track UME 2 (ISS-B) in real time on Orbital Radar’s live tracker.
UME 2 (ISS-B) was launched on 1978-02-16 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years.
Yes — Orbital Radar tracks UME 2 (ISS-B) (NORAD ID 10674) 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.
UME 2 (ISS-B) travels at approximately 26,303 km/h (16,344 mph) — roughly 7.31 km/s. It completes 13.44 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.