Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 13.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025GV
Object number (NORAD): 29899
Object ID (CCSDS): 29899
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 107.664 minutes
Inclination: 98.6617 deg
SMA: 7496.771 km
Apoapsis: 1383.717 km
Periapsis: 853.556 km
RAAN: 142.4193 deg
Eccentricy: 0.03535928
Argument of periapsis: 78.4908 deg
Mean anomaly: 285.5699 deg
Mean motion: 13.37492488 rev/day
Mean motion (dot): 0.00000174 rev/day2
B* drag term: 0.00027482953 1/REarth
Two-line elements (TLE)
Creation date: Dec. 13, 2025, 4:32 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 10:26 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29899U 99025GV 25346.93517734 .00000174 00000-0 27483-3 0 9990
TLE line 2: 2 29899 98.6617 142.4193 0353593 78.4908 285.5699 13.37492488920873
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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