Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9497
Days in orbit
Revolutions
≈ 14.3
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: 1999-025GH
Object number (NORAD): 29887
Object ID (CCSDS): 29887
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.546 minutes
Inclination: 98.7281 deg
SMA: 7162.572 km
Apoapsis: 992.874 km
Periapsis: 575.999 km
RAAN: 209.5297 deg
Eccentricy: 0.0291009
Argument of periapsis: 277.9941 deg
Mean anomaly: 207.1963 deg
Mean motion: 14.32185547 rev/day
Mean motion (dot): 0.00001986 rev/day2
B* drag term: 0.00047505 1/REarth
Two-line elements (TLE)
Creation date: May 10, 2025, 2:32 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 9, 2025, 6:20 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29887U 99025GH 25129.76440152 .00001986 00000-0 47505-3 0 9995
TLE line 2: 2 29887 98.7281 209.5297 0291009 277.9941 207.1963 14.32185547948677
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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