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HMU-SAT2, 67688

Orbit data source: Space-Track

HMU-SAT2, 67688 is a payload satellite owned by Kyutech (JP) in LEO that was delivered to the ISS. Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
67688, 1998-067YE
Orbit
LEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
Kyutech
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
1998-11-20 (28 years ago)
Launch vehicle
H3-24W
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 HMU-SAT2
1 67688U 98067YE  26165.66873790  .00062747  00000-0  67767-3 0  9993
2 67688  51.6296 305.7514 0006259 190.5533 169.5331 15.63005499 19829
Epoch: 2026-06-14T16:02Z
TLE epoch observation values (Epoch: 2026-06-14T16:02:58.954Z)
Latitude
-0.00002°
Longitude
162.03958°
Altitude
383.884 km
Speed
7.679 km/s
True Right ascension
20h 23m 00s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:34:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
383.723 km
Perigee altitude
375.264 km
Semi-major axis
6,757.63 km
Eccentricity
0.00063
Inclination
51.6296°
RAAN
305.7514°
Arg. of periapsis
190.5533°
True anomaly
169.54612°
Mean anomaly
169.5331°
Eccentric anomaly
169.53961°
Mean motion
3.90707 °/min
Orbital period
92.14 mins
BSTAR
0.00067767
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