Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 11.9
Per day
Orbit
MEO
Medium Earth Orbit
Inclination
99.0
Latest
Satellite identification and parameters
Extended collection of information and parameters for FENGYUN 1C DEB.
Object identification
Identified? True
Debris? True
Object name: FENGYUN 1C DEB
International designator: 1999-025EJW
Object number (NORAD): 37476
Object ID (CCSDS): 37476
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 120.946 minutes
Inclination: 98.9613 deg
SMA: 8101.286 km
Apoapsis: 2597.46 km
Periapsis: 848.842 km
RAAN: 256.7393 deg
Eccentricy: 0.1079222
Argument of periapsis: 187.5332 deg
Mean anomaly: 170.8276 deg
Mean motion: 11.90616273 rev/day
Mean motion (dot): 0.00002109 rev/day2
B* drag term: 0.0055642 1/REarth
Two-line elements (TLE)
Creation date: June 30, 2025, 5:29 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 29, 2025, 11:12 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37476U 99025EJW 25180.96730666 .00002109 00000-0 55642-2 0 9997
TLE line 2: 2 37476 98.9613 256.7393 1079222 187.5332 170.8276 11.90616273654701
Live tracking on map
Real-time ground track for satellite FENGYUN 1C DEB.
Associated space launch
Chinese polar orbiting meteorological satellite
FENGYUN 1C DEB was lifted into orbit during the mission ‘Long March 4B | Feng Yun 1C’, on board a Long March 4B space rocket.
The launch took place on May 10, 1999, 1:33 a.m. from Launch Complex 7.
For more information about the launch, click the button.

Long March 4B | Feng Yun 1C
Agency: N/A
Status: Launch Successful
Launch date: May 10, 1999, 1:33 a.m. UTC
Rocket: Long March 4B
Launch pad: Launch Complex 7
Location: Taiyuan Satellite Launch Center, People's Republic of China
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