Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9617
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.3
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: 1999-025LW
Object number (NORAD): 29996
Object ID (CCSDS): 29996
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.233 minutes
Inclination: 99.3096 deg
SMA: 7242.466 km
Apoapsis: 960.114 km
Periapsis: 768.548 km
RAAN: 283.9812 deg
Eccentricy: 0.01322523
Argument of periapsis: 357.3595 deg
Mean anomaly: 65.4151 deg
Mean motion: 14.08552599 rev/day
Mean motion (dot): 0.0000453 rev/day2
B* drag term: 0.0024576722 1/REarth
Two-line elements (TLE)
Creation date: Sept. 7, 2025, 3:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 6, 2025, 6:13 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29996U 99025LW 25249.75940355 .00004530 00000-0 24577-2 0 9999
TLE line 2: 2 29996 99.3096 283.9812 0132252 357.3595 65.4151 14.08552599947716
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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