Showing default

FENGYUN 2G, 40367

Orbit data source: Space-Track

FENGYUN 2G, 40367 is a payload satellite owned by CNMSC (CN) in GEO that was launched on Wed, 31 Dec 2014 UTC via a CHANG ZHENG 3A 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.

Not visible in the next 10 days
Identifier
40367, 2014-090A
Orbit
GEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SISE
Mission
Operational Civil Weather
Bus & Motor
FY-2, SHANXI AKM
Mass
1,390 kg wet, ~600 kg dry
Launch date (UTC)
2014-12-31 (11 years ago)
Launch vehicle
CHANG ZHENG 3A
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.5 m
Radar Cross Section
6.680 m², Large (>1 m²)

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

TLE from 1 day ago
0 FENGYUN 2G
1 40367U 14090A   25341.80181892 -.00000300  00000-0  00000-0 0  9990
2 40367   5.1554  75.1544 0003120 196.9461 193.0185  1.00265807 40088
Epoch: 2025-12-07T19:14Z
TLE epoch observation values (Epoch: 2025-12-07T19:14:37.154Z)
Latitude
2.59583°
Longitude
99.54371°
Altitude
35,800.342 km
Speed
3.074 km/s
True Right ascension
07h 00m 02s
True Declination
2° 35' 36"
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
18:27:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,802.485 km
Perigee altitude
35,776.172 km
Semi-major axis
42,167.466 km
Eccentricity
0.00031
Inclination
5.1554°
RAAN
75.1544°
Arg. of periapsis
196.9461°
True anomaly
193.01045°
Mean anomaly
193.0185°
Eccentric anomaly
193.01447°
Mean motion
0.25066 °/min
Orbital period
1,436.24 mins
BSTAR
0
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 #90 in the year 2014 (2014-12-31 UTC)

Documentation

Showing up to 5 results
|