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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: 5 hours ago

TLE from 5 hours ago
0 HONGYAN 1
1 43914U 18112F   25310.28249677 -.00000093  00000-0  62621-4 0  9994
2 43914  50.0086 336.8802 0006644 298.1349  61.8857 13.43806627336566
Epoch: 2025-11-06T06:46Z
TLE epoch observation values (Epoch: 2025-11-06T06:46:47.720Z)
Latitude
-0.0001°
Longitude
-170.56176°
Altitude
1,093.306 km
Speed
7.308 km/s
True Right ascension
22h 27m 31s
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
07:41:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,100.808 km
Perigee altitude
1,090.876 km
Semi-major axis
7,473.979 km
Eccentricity
0.00066
Inclination
50.0086°
RAAN
336.8802°
Arg. of periapsis
298.1349°
True anomaly
61.95288°
Mean anomaly
61.8857°
Eccentric anomaly
61.91929°
Mean motion
3.35904 °/min
Orbital period
107.17 mins
BSTAR
0.000062621
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