Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9618
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
100.8
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: 1999-025CXG
Object number (NORAD): 32315
Object ID (CCSDS): 32315
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.409 minutes
Inclination: 100.7915 deg
SMA: 7391.717 km
Apoapsis: 1182.921 km
Periapsis: 844.244 km
RAAN: 355.463 deg
Eccentricy: 0.0229092
Argument of periapsis: 50.7323 deg
Mean anomaly: 311.3898 deg
Mean motion: 13.66107094 rev/day
Mean motion (dot): 0.00000056 rev/day2
B* drag term: 0.0001099 1/REarth
Two-line elements (TLE)
Creation date: Aug. 15, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 14, 2025, 2:15 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32315U 99025CXG 25226.09409728 .00000056 00000-0 10990-3 0 9998
TLE line 2: 2 32315 100.7915 355.4630 0229092 50.7323 311.3898 13.66107094908736
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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