Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.2
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: 1999-025BMU
Object number (NORAD): 31262
Object ID (CCSDS): 31262
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.639 minutes
Inclination: 99.0096 deg
SMA: 7214.382 km
Apoapsis: 877.259 km
Periapsis: 795.236 km
RAAN: 269.166 deg
Eccentricy: 0.0056847
Argument of periapsis: 186.6385 deg
Mean anomaly: 300.5793 deg
Mean motion: 14.16785288 rev/day
Mean motion (dot): 0.00002313 rev/day2
B* drag term: 0.00116 1/REarth
Two-line elements (TLE)
Creation date: July 7, 2025, 5:18 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 7:06 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31262U 99025BMU 25187.79605436 .00002313 00000-0 11600-2 0 9991
TLE line 2: 2 31262 99.0096 269.1660 0056847 186.6385 300.5793 14.16785288934571
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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