Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9716
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.1
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: 1999-025CFH
Object number (NORAD): 31758
Object ID (CCSDS): 31758
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.857 minutes
Inclination: 98.0612 deg
SMA: 7129.823 km
Apoapsis: 978.328 km
Periapsis: 525.047 km
RAAN: 356.9918 deg
Eccentricy: 0.03178767
Argument of periapsis: 86.4834 deg
Mean anomaly: 277.2652 deg
Mean motion: 14.42064387 rev/day
Mean motion (dot): 0.00014398 rev/day2
B* drag term: 0.0023825989 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 11:30 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 11:34 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31758U 99025CFH 25347.98238744 .00014398 00000-0 23826-2 0 9993
TLE line 2: 2 31758 98.0612 356.9918 0317877 86.4834 277.2652 14.42064387942183
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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