Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9610
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.0
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: 1999-025AVM
Object number (NORAD): 30827
Object ID (CCSDS): 30827
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.341 minutes
Inclination: 98.9934 deg
SMA: 7152.869 km
Apoapsis: 808.9 km
Periapsis: 740.567 km
RAAN: 220.5818 deg
Eccentricy: 0.00477666
Argument of periapsis: 128.4859 deg
Mean anomaly: 232.0624 deg
Mean motion: 14.35100742 rev/day
Mean motion (dot): 0.00009358 rev/day2
B* drag term: 0.0032494392 1/REarth
Two-line elements (TLE)
Creation date: Aug. 28, 2025, 2:53 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 27, 2025, 9:48 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30827U 99025AVM 25239.90875674 .00009358 00000-0 32494-2 0 9991
TLE line 2: 2 30827 98.9934 220.5818 0047767 128.4859 232.0624 14.35100742950154
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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