Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9620
Days in orbit
Revolutions
≈ 14.8
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: 1999-025CJB
Object number (NORAD): 31837
Object ID (CCSDS): 31837
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.328 minutes
Inclination: 98.1104 deg
SMA: 7008.922 km
Apoapsis: 699.05 km
Periapsis: 562.525 km
RAAN: 326.5478 deg
Eccentricy: 0.00973938
Argument of periapsis: 323.5119 deg
Mean anomaly: 35.9481 deg
Mean motion: 14.79537293 rev/day
Mean motion (dot): 0.00005815 rev/day2
B* drag term: 0.0007243484 1/REarth
Two-line elements (TLE)
Creation date: Sept. 9, 2025, 10:35 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 9, 2025, 12:10 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31837U 99025CJB 25252.00727454 .00005815 00000-0 72435-3 0 9995
TLE line 2: 2 31837 98.1104 326.5478 0097394 323.5119 35.9481 14.79537293969574
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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