Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9619
Days in orbit
Revolutions
≈ 14.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.0
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: 1999-025DA
Object number (NORAD): 29808
Object ID (CCSDS): 29808
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 96.771 minutes
Inclination: 99.0303 deg
SMA: 6982.166 km
Apoapsis: 615.385 km
Periapsis: 592.676 km
RAAN: 154.2571 deg
Eccentricy: 0.00162624
Argument of periapsis: 71.4317 deg
Mean anomaly: 91.0266 deg
Mean motion: 14.88050027 rev/day
Mean motion (dot): 0.00064711 rev/day2
B* drag term: 0.0069691228 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 9:49 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 8, 2025, 4:33 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29808U 99025DA 25251.18962448 .00064711 00000-0 69691-2 0 9991
TLE line 2: 2 29808 99.0303 154.2571 0016262 71.4317 91.0266 14.88050027967920
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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