Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9617
Days in orbit
Revolutions
≈ 14.6
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: 1999-025CLR
Object number (NORAD): 31914
Object ID (CCSDS): 31914
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.939 minutes
Inclination: 99.0394 deg
SMA: 7086.053 km
Apoapsis: 837.702 km
Periapsis: 578.133 km
RAAN: 103.285 deg
Eccentricy: 0.01831555
Argument of periapsis: 7.1122 deg
Mean anomaly: 353.2607 deg
Mean motion: 14.55446384 rev/day
Mean motion (dot): 0.00001389 rev/day2
B* drag term: 0.00026687631 1/REarth
Two-line elements (TLE)
Creation date: Sept. 5, 2025, 7:38 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 5, 2025, 7:45 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31914U 99025CLR 25248.32358968 .00001389 00000-0 26688-3 0 9992
TLE line 2: 2 31914 99.0394 103.2850 0183155 7.1122 353.2607 14.55446384670417
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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