Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.6
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: 1999-025AYE
Object number (NORAD): 30892
Object ID (CCSDS): 30892
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.511 minutes
Inclination: 99.6478 deg
SMA: 7208.356 km
Apoapsis: 857.439 km
Periapsis: 803.002 km
RAAN: 113.4949 deg
Eccentricy: 0.003776
Argument of periapsis: 283.7059 deg
Mean anomaly: 75.9911 deg
Mean motion: 14.18562433 rev/day
Mean motion (dot): 0.00000469 rev/day2
B* drag term: 0.00024976 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 5:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 12:47 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30892U 99025AYE 25184.53283486 .00000469 00000-0 24976-3 0 9996
TLE line 2: 2 30892 99.6478 113.4949 0037760 283.7059 75.9911 14.18562433620035
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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