Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9659
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
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: 1999-025ADE
Object number (NORAD): 30391
Object ID (CCSDS): 30391
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.703 minutes
Inclination: 98.7874 deg
SMA: 7217.422 km
Apoapsis: 891.749 km
Periapsis: 786.825 km
RAAN: 337.731 deg
Eccentricy: 0.00726876
Argument of periapsis: 63.0812 deg
Mean anomaly: 20.7717 deg
Mean motion: 14.15890323 rev/day
Mean motion (dot): 0.00002929 rev/day2
B* drag term: 0.0014715918 1/REarth
Two-line elements (TLE)
Creation date: Oct. 18, 2025, 2:17 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 17, 2025, 10:52 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30391U 99025ADE 25290.95305822 .00002929 00000-0 14716-2 0 9996
TLE line 2: 2 30391 98.7874 337.7310 0072688 63.0812 20.7717 14.15890323960898
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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