Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9616
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025CEA
Object number (NORAD): 31727
Object ID (CCSDS): 31727
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.331 minutes
Inclination: 98.8642 deg
SMA: 7152.353 km
Apoapsis: 798.306 km
Periapsis: 750.129 km
RAAN: 358.0133 deg
Eccentricy: 0.00336792
Argument of periapsis: 264.8707 deg
Mean anomaly: 253.3754 deg
Mean motion: 14.3525601 rev/day
Mean motion (dot): 0.00008407 rev/day2
B* drag term: 0.0029309556 1/REarth
Two-line elements (TLE)
Creation date: Sept. 6, 2025, 2:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 5, 2025, 6:13 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31727U 99025CEA 25248.75912015 .00008407 00000-0 29310-2 0 9992
TLE line 2: 2 31727 98.8642 358.0133 0033679 264.8707 253.3754 14.35256010702627
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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