Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 13.9
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: 1999-025CFB
Object number (NORAD): 31752
Object ID (CCSDS): 31752
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.46 minutes
Inclination: 98.9883 deg
SMA: 7300.306 km
Apoapsis: 1186.435 km
Periapsis: 657.906 km
RAAN: 261.283 deg
Eccentricy: 0.0361991
Argument of periapsis: 59.4002 deg
Mean anomaly: 304.2341 deg
Mean motion: 13.91846025 rev/day
Mean motion (dot): 0.00002094 rev/day2
B* drag term: 0.00098133 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 7:06 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 2, 2025, 10:43 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31752U 99025CFB 25183.94662956 .00002094 00000-0 98133-3 0 9991
TLE line 2: 2 31752 98.9883 261.2830 0361991 59.4002 304.2341 13.91846025913241
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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