Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9553
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.8
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: 1999-025EWM
Object number (NORAD): 39544
Object ID (CCSDS): 39544
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.472 minutes
Inclination: 98.763 deg
SMA: 7253.776 km
Apoapsis: 915.868 km
Periapsis: 835.415 km
RAAN: 68.203 deg
Eccentricy: 0.0055456
Argument of periapsis: 106.5165 deg
Mean anomaly: 254.2106 deg
Mean motion: 14.05259428 rev/day
Mean motion (dot): 0.00000406 rev/day2
B* drag term: 0.00027319 1/REarth
Two-line elements (TLE)
Creation date: July 2, 2025, 5:47 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 2, 2025, 9:52 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 39544U 99025EWM 25183.41180153 .00000406 00000-0 27319-3 0 9997
TLE line 2: 2 39544 98.7630 68.2030 0055456 106.5165 254.2106 14.05259428545619
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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