Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9613
Days in orbit
Revolutions
≈ 14.1
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: 1999-025ETR
Object number (NORAD): 38724
Object ID (CCSDS): 38724
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.93 minutes
Inclination: 98.7407 deg
SMA: 7228.159 km
Apoapsis: 943.325 km
Periapsis: 756.722 km
RAAN: 252.2637 deg
Eccentricy: 0.01290806
Argument of periapsis: 14.2646 deg
Mean anomaly: 346.2117 deg
Mean motion: 14.12736705 rev/day
Mean motion (dot): 0.00011257 rev/day2
B* drag term: 0.0056188493 1/REarth
Two-line elements (TLE)
Creation date: Aug. 29, 2025, 9:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 28, 2025, 11:43 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38724U 99025ETR 25240.98851633 .00011257 00000-0 56188-2 0 9991
TLE line 2: 2 38724 98.7407 252.2637 0129081 14.2646 346.2117 14.12736705551306
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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