Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9716
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.5
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: 1999-025YT
Object number (NORAD): 30282
Object ID (CCSDS): 30282
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.913 minutes
Inclination: 98.5017 deg
SMA: 7227.342 km
Apoapsis: 1001.154 km
Periapsis: 697.26 km
RAAN: 351.2016 deg
Eccentricy: 0.02102395
Argument of periapsis: 358.4661 deg
Mean anomaly: 60.6314 deg
Mean motion: 14.12976248 rev/day
Mean motion (dot): 0.00001046 rev/day2
B* drag term: 0.00047342823 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 11:30 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 14, 2025, 12:13 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30282U 99025YT 25348.00906427 .00001046 00000-0 47343-3 0 9995
TLE line 2: 2 30282 98.5017 351.2016 0210240 358.4661 60.6314 14.12976248973695
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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