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HJS-9B, 68832

Orbit data source: Space-Track

HJS-9B, 68832 is a Chinese payload satellite in LEO that was launched on Fri, 24 Apr 2026 UTC via a CHANG ZHENG 2D launch vehicle from the Xichang Space Center, China (XSC). 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
68832, 2026-091B
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-04-24 (1 week ago)
Launch vehicle
CHANG ZHENG 2D
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 HJS-9B
1 68832U 26091B   26120.69958377  .00001895  00000-0  10392-3 0  9991
2 68832  55.0011 229.1963 0008863 291.9985  68.0093 15.19148891   981
Epoch: 2026-04-30T16:47Z
TLE epoch observation values (Epoch: 2026-04-30T16:47:24.037Z)
Latitude
0.00001°
Longitude
118.70372°
Altitude
507.221 km
Speed
7.613 km/s
True Right ascension
15h 16m 47s
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
19:14:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.477 km
Perigee altitude
502.27 km
Semi-major axis
6,886.511 km
Eccentricity
0.00089
Inclination
55.0011°
RAAN
229.1963°
Arg. of periapsis
291.9985°
True anomaly
68.10351°
Mean anomaly
68.0093°
Eccentric anomaly
68.0564°
Mean motion
3.79791 °/min
Orbital period
94.79 mins
BSTAR
0.00010392
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Other satellites on launch #91 in the year 2026 (2026-04-24 UTC)

Documentation

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