Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 14.7
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: 1999-025CDM
Object number (NORAD): 31714
Object ID (CCSDS): 31714
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 97.813 minutes
Inclination: 99.0389 deg
SMA: 7032.189 km
Apoapsis: 674.541 km
Periapsis: 633.567 km
RAAN: 67.4597 deg
Eccentricy: 0.0029133
Argument of periapsis: 70.2479 deg
Mean anomaly: 319.8138 deg
Mean motion: 14.72200603 rev/day
Mean motion (dot): 0.00019371 rev/day2
B* drag term: 0.003053 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 2:31 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31714U 99025CDM 25186.60504611 .00019371 00000-0 30530-2 0 9990
TLE line 2: 2 31714 99.0389 67.4597 0029133 70.2479 319.8138 14.72200603936849
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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