Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
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: 101.986 minutes
Inclination: 98.7392 deg
SMA: 7230.8 km
Apoapsis: 947.63 km
Periapsis: 757.701 km
RAAN: 194.6829 deg
Eccentricy: 0.0131333
Argument of periapsis: 177.8352 deg
Mean anomaly: 182.3416 deg
Mean motion: 14.11962657 rev/day
Mean motion (dot): 0.00004301 rev/day2
B* drag term: 0.002188 1/REarth
Two-line elements (TLE)
Creation date: July 1, 2025, 6:11 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: June 30, 2025, 11:22 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38724U 99025ETR 25181.97428462 .00004301 00000-0 21880-2 0 9997
TLE line 2: 2 38724 98.7392 194.6829 0131333 177.8352 182.3416 14.11962657542974
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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