Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025BGC
Object number (NORAD): 31082
Object ID (CCSDS): 31082
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.936 minutes
Inclination: 98.6734 deg
SMA: 7228.461 km
Apoapsis: 900.704 km
Periapsis: 799.948 km
RAAN: 176.9567 deg
Eccentricy: 0.0069694
Argument of periapsis: 3.5448 deg
Mean anomaly: 356.6204 deg
Mean motion: 14.12648174 rev/day
Mean motion (dot): 0.00000968 rev/day2
B* drag term: 0.00053332 1/REarth
Two-line elements (TLE)
Creation date: June 13, 2025, 2:45 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 12, 2025, 8:21 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31082U 99025BGC 25163.84841271 .00000968 00000-0 53332-3 0 9993
TLE line 2: 2 31082 98.6734 176.9567 0069694 3.5448 356.6204 14.12648174937274
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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