Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.6
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: 1999-025EV
Object number (NORAD): 29851
Object ID (CCSDS): 29851
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.087 minutes
Inclination: 99.6039 deg
SMA: 7329.79 km
Apoapsis: 1055.475 km
Periapsis: 847.835 km
RAAN: 225.3741 deg
Eccentricy: 0.0141641
Argument of periapsis: 287.4483 deg
Mean anomaly: 189.7521 deg
Mean motion: 13.83456291 rev/day
Mean motion (dot): 0.00000201 rev/day2
B* drag term: 0.00020955 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 3:57 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29851U 99025EV 25187.66519828 .00000201 00000-0 20955-3 0 9995
TLE line 2: 2 29851 99.6039 225.3741 0141641 287.4483 189.7521 13.83456291931783
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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