Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.2
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: 1999-025AZR
Object number (NORAD): 30927
Object ID (CCSDS): 30927
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.202 minutes
Inclination: 99.1824 deg
SMA: 7241.02 km
Apoapsis: 934.121 km
Periapsis: 791.649 km
RAAN: 46.5978 deg
Eccentricy: 0.00983789
Argument of periapsis: 7.6267 deg
Mean anomaly: 352.6371 deg
Mean motion: 14.0897451 rev/day
Mean motion (dot): 0.00004165 rev/day2
B* drag term: 0.0023255389 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 3:19 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30927U 99025AZR 25346.13820104 .00004165 00000-0 23255-2 0 9990
TLE line 2: 2 30927 99.1824 46.5978 0098379 7.6267 352.6371 14.08974510956757
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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