Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.1
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: 1999-025AGJ
Object number (NORAD): 30471
Object ID (CCSDS): 30471
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.943 minutes
Inclination: 99.0584 deg
SMA: 7228.799 km
Apoapsis: 909.205 km
Periapsis: 792.123 km
RAAN: 272.9355 deg
Eccentricy: 0.0080983
Argument of periapsis: 345.7253 deg
Mean anomaly: 73.314 deg
Mean motion: 14.1254894 rev/day
Mean motion (dot): 0.000021 rev/day2
B* drag term: 0.0011251 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 4:16 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30471U 99025AGJ 25187.17792797 .00002100 00000-0 11251-2 0 9997
TLE line 2: 2 30471 99.0584 272.9355 0080983 345.7253 73.3140 14.12548940941899
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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