Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.4
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: 1999-025CPB
Object number (NORAD): 31974
Object ID (CCSDS): 31974
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.869 minutes
Inclination: 98.3841 deg
SMA: 7177.937 km
Apoapsis: 854.602 km
Periapsis: 745.003 km
RAAN: 202.9192 deg
Eccentricy: 0.0076344
Argument of periapsis: 59.7212 deg
Mean anomaly: 301.1497 deg
Mean motion: 14.27589266 rev/day
Mean motion (dot): 0.00004425 rev/day2
B* drag term: 0.0017585 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 11:40 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31974U 99025CPB 25185.48673370 .00004425 00000-0 17585-2 0 9991
TLE line 2: 2 31974 98.3841 202.9192 0076344 59.7212 301.1497 14.27589266671205
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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