Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 13.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.1
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: 1999-025CRU
Object number (NORAD): 32126
Object ID (CCSDS): 32126
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 106.133 minutes
Inclination: 99.1098 deg
SMA: 7425.526 km
Apoapsis: 1256.199 km
Periapsis: 838.583 km
RAAN: 219.2267 deg
Eccentricy: 0.0281203
Argument of periapsis: 265.4353 deg
Mean anomaly: 91.4619 deg
Mean motion: 13.56787693 rev/day
Mean motion (dot): 0.00001479 rev/day2
B* drag term: 0.0016621 1/REarth
Two-line elements (TLE)
Creation date: Dec. 9, 2025, 8:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 8, 2025, 9:03 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32126U 99025CRU 25342.87766713 .00001479 00000-0 16621-2 0 9999
TLE line 2: 2 32126 99.1098 219.2267 0281203 265.4353 91.4619 13.56787693616621
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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