Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
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: 1999-025CDP
Object number (NORAD): 31716
Object ID (CCSDS): 31716
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.656 minutes
Inclination: 98.5606 deg
SMA: 7262.466 km
Apoapsis: 978.287 km
Periapsis: 790.375 km
RAAN: 96.0837 deg
Eccentricy: 0.0129372
Argument of periapsis: 179.8915 deg
Mean anomaly: 210.987 deg
Mean motion: 14.0273803 rev/day
Mean motion (dot): 0.00001883 rev/day2
B* drag term: 0.0011558 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 4:22 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31716U 99025CDP 25187.68233964 .00001883 00000-0 11558-2 0 9999
TLE line 2: 2 31716 98.5606 96.0837 0129372 179.8915 210.9870 14.02738030919612
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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