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FENGYUNG-4C, 67246

Orbit data source: Space-Track

FENGYUNG-4C, 67246 is a payload satellite owned by CNMSC (CN) in HEO that was launched on Fri, 26 Dec 2025 UTC via a CHANG ZHENG 3B 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
67246, 2025-312A
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SISE
Mission
Operational spacecraft
Bus & Motor
FY-4, LAE?
Mass
5,380 kg wet, ~3,000 kg dry
Launch date (UTC)
2025-12-26 (4 days ago)
Launch vehicle
CHANG ZHENG 3B
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: 3 days ago

TLE from 3 days ago
0 FENGYUNG-4C
1 67246U 25312A   25360.90857406  .00039214  41525-6  21251-2 0  9998
2 67246  28.4641 334.3215 7309751 179.7824 181.1675  2.27841578    17
Epoch: 2025-12-26T21:48Z
TLE epoch observation values (Epoch: 2025-12-26T21:48:20.798Z)
Latitude
Longitude
-88.41413°
Altitude
35,833.184 km
Speed
1.596 km/s
True Right ascension
22h 17m 15s
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
21:36:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,856.713 km
Perigee altitude
185.924 km
Semi-major axis
24,399.455 km
Eccentricity
0.73098
Inclination
28.4641°
RAAN
334.3215°
Arg. of periapsis
179.7824°
True anomaly
180.2659°
Mean anomaly
181.1675°
Eccentric anomaly
180.67448°
Mean motion
0.56947 °/min
Orbital period
632.16 mins
BSTAR
0.0021251
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Other satellites on launch #312 in the year 2025 (2025-12-26 UTC)

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