Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 13.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025GV
Object number (NORAD): 29899
Object ID (CCSDS): 29899
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 107.67 minutes
Inclination: 98.6504 deg
SMA: 7497.021 km
Apoapsis: 1384.347 km
Periapsis: 853.425 km
RAAN: 3.8234 deg
Eccentricy: 0.0354089
Argument of periapsis: 127.0335 deg
Mean anomaly: 236.3743 deg
Mean motion: 13.37425728 rev/day
Mean motion (dot): 0.00000096 rev/day2
B* drag term: 0.00017037 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 5:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 10:50 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29899U 99025GV 25184.45199254 .00000096 00000-0 17037-3 0 9997
TLE line 2: 2 29899 98.6504 3.8234 0354089 127.0335 236.3743 13.37425728899153
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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