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HONGYAN 1, 43914

Orbit data source: Space-Track

HONGYAN 1, 43914 is a payload satellite owned by Yidong Tongxin (CN) in LEO that was launched on Sat, 29 Dec 2018 UTC via a CHANG ZHENG 2D/YZ-3 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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
43914, 2018-112F
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
DFH Shenzhen
Mission
Operational Commercial Communications
Bus & Motor
HONGYAN, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
2018-12-29 (7 years ago)
Launch vehicle
CHANG ZHENG 2D/YZ-3
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
3.085 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 HONGYAN 1
1 43914U 18112F   26172.40311843 -.00000078  00000-0  88255-4 0  9994
2 43914  50.0073 221.5065 0006794 268.7912  91.2188 13.43821403367105
Epoch: 2026-06-21T09:40Z
TLE epoch observation values (Epoch: 2026-06-21T09:40:29.432Z)
Latitude
-0.00002°
Longitude
166.77995°
Altitude
1,095.7 km
Speed
7.306 km/s
True Right ascension
14h 46m 01s
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
21:42:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,100.865 km
Perigee altitude
1,090.709 km
Semi-major axis
7,473.924 km
Eccentricity
0.00068
Inclination
50.0073°
RAAN
221.5065°
Arg. of periapsis
268.7912°
True anomaly
91.29663°
Mean anomaly
91.2188°
Eccentric anomaly
91.25772°
Mean motion
3.35908 °/min
Orbital period
107.17 mins
BSTAR
0.000088255
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