Skip to content
Home Library Satellite Directory HMU-SAT2

HMU-SAT2

NORAD 67688 Payload LEO 1998-067YE ● Active
CONNECTING… LEO · NORAD 67688
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
374 km
Apogee
382 km
Inclination
51.6°
Period
92.1 min
Mean Motion
15.63349670 rev/day
TLE Epoch
2026-06-17 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude378 km
Orbital Velocity27,666 km/h
Velocity7.69 km/s
Orbital Period92 minutes
Orbits / Day15.63
Eccentricity0.0006
Semi-Major Axis6,749 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1998-11-20
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1998-067YE
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
HMU-SAT2 is an active satellite operated by Japan, launched on 1998-11-20 from Baikonur, Kazakhstan. With over 28 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 374 km and 382 km with an inclination of 51.6°. It travels at approximately 27,666 km/h (7.69 km/s), completing one full orbit every 92 minutes — that’s roughly 15.63 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Orbital Radar tracks HMU-SAT2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HMU-SAT2 orbits at an average altitude of 378 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of HMU-SAT2’s average altitude, there are currently 1,312 active payloads and 57 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.5% of all active satellites. With an inclination of 51.6°, HMU-SAT2 passes over latitudes between 51.6°N and 51.6°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Japan operates approximately 189 active satellites in total, of which 5 share a similar altitude band with HMU-SAT2.
❓ Frequently Asked Questions
HMU-SAT2 orbits in Low Earth Orbit (LEO) at altitudes between 374 km (perigee) and 382 km (apogee), with an average altitude of approximately 378 km. It completes one orbit every 92 minutes, travelling at approximately 27,666 km/h (17,191 mph).
HMU-SAT2 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 67688. You can track HMU-SAT2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HMU-SAT2 was launched on 1998-11-20 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks HMU-SAT2 (NORAD ID 67688) 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.
HMU-SAT2 travels at approximately 27,666 km/h (17,191 mph) — roughly 7.69 km/s. It completes 15.63 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.