Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025CNR
Object number (NORAD): 31964
Object ID (CCSDS): 31964
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.041 minutes
Inclination: 98.695 deg
SMA: 7090.934 km
Apoapsis: 737.814 km
Periapsis: 687.783 km
RAAN: 303.2329 deg
Eccentricy: 0.0035278
Argument of periapsis: 159.5985 deg
Mean anomaly: 200.6628 deg
Mean motion: 14.53943847 rev/day
Mean motion (dot): 0.00009052 rev/day2
B* drag term: 0.0021418 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, 6:41 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31964U 99025CNR 25186.27848482 .00009052 00000-0 21418-2 0 9997
TLE line 2: 2 31964 98.6950 303.2329 0035278 159.5985 200.6628 14.53943847651757
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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