Showing default

HJS-8A, 68687

Orbit data source: Space-Track

HJS-8A, 68687 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Sat, 11 Apr 2026 UTC via a JIELONG-3 launch vehicle from the South China Sea Launch Area (SCSLA). 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.

Loading next visibility...
Identifier
68687, 2026-078A
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown (CN)
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
2026-04-11 (1 month ago)
Launch vehicle
JIELONG-3
Launch site
South China Sea Launch Area (SCSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 3 weeks ago

TLE from 3 weeks ago
0 HJS-8A
1 68687U 26078A   26121.56499271  .00000303  00000-0  35284-3 0  9994
2 68687  86.4967 298.5999 0001401  91.1620 268.9698 13.65394683  2731
Epoch: 2026-05-01T13:33Z
TLE epoch observation values (Epoch: 2026-05-01T13:33:35.370Z)
Latitude
0.00001°
Longitude
-124.2929°
Altitude
1,019.124 km
Speed
7.342 km/s
True Right ascension
19h 54m 23s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
07:22:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,014.247 km
Perigee altitude
1,012.176 km
Semi-major axis
7,391.349 km
Eccentricity
0.00014
Inclination
86.4967°
RAAN
298.5999°
Arg. of periapsis
91.162°
True anomaly
268.95375°
Mean anomaly
268.9698°
Eccentric anomaly
268.96177°
Mean motion
3.41553 °/min
Orbital period
105.4 mins
BSTAR
0.00035284
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #78 in the year 2026 (2026-04-11 UTC)

Documentation

Showing up to 5 results
|