Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9500
Days in orbit
Revolutions
≈ 14.5
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: 1999-025BEE
Object number (NORAD): 31036
Object ID (CCSDS): 31036
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.405 minutes
Inclination: 98.907 deg
SMA: 7108.277 km
Apoapsis: 829.245 km
Periapsis: 631.04 km
RAAN: 227.0748 deg
Eccentricy: 0.0139418
Argument of periapsis: 187.339 deg
Mean anomaly: 239.0771 deg
Mean motion: 14.48625765 rev/day
Mean motion (dot): 0.00000964 rev/day2
B* drag term: 0.00023983 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 7:41 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 12, 2025, 12:09 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31036U 99025BEE 25132.50643612 .00000964 00000-0 23983-3 0 9995
TLE line 2: 2 31036 98.9070 227.0748 0139418 187.3390 239.0771 14.48625765542058
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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