Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9659
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: 1999-025EBR
Object number (NORAD): 36743
Object ID (CCSDS): 36743
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.801 minutes
Inclination: 98.6586 deg
SMA: 7174.687 km
Apoapsis: 832.233 km
Periapsis: 760.87 km
RAAN: 338.0493 deg
Eccentricy: 0.0049732
Argument of periapsis: 178.6312 deg
Mean anomaly: 181.5014 deg
Mean motion: 14.28559574 rev/day
Mean motion (dot): 0.0000379 rev/day2
B* drag term: 0.001508 1/REarth
Two-line elements (TLE)
Creation date: Oct. 17, 2025, 6:56 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 16, 2025, 8:44 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 36743U 99025EBR 25289.36389803 .00003790 00000-0 15080-2 0 9999
TLE line 2: 2 36743 98.6586 338.0493 0049732 178.6312 181.5014 14.28559574599182
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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