Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.3
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: 1999-025CLU
Object number (NORAD): 31917
Object ID (CCSDS): 31917
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.232 minutes
Inclination: 98.3499 deg
SMA: 7147.661 km
Apoapsis: 906.331 km
Periapsis: 632.721 km
RAAN: 124.2471 deg
Eccentricy: 0.0191398
Argument of periapsis: 236.3357 deg
Mean anomaly: 182.2877 deg
Mean motion: 14.36669348 rev/day
Mean motion (dot): 0.000016 rev/day2
B* drag term: 0.00045435 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 2:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 5:16 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31917U 99025CLU 25125.21996851 .00001600 00000-0 45435-3 0 9993
TLE line 2: 2 31917 98.3499 124.2471 0191398 236.3357 182.2877 14.36669348933398
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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