Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
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: 100.848 minutes
Inclination: 98.666 deg
SMA: 7176.913 km
Apoapsis: 835.545 km
Periapsis: 762.011 km
RAAN: 235.3505 deg
Eccentricy: 0.005123
Argument of periapsis: 122.5139 deg
Mean anomaly: 238.1007 deg
Mean motion: 14.2789486 rev/day
Mean motion (dot): 0.00002424 rev/day2
B* drag term: 0.00098259 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 7:06 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 9:16 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 36743U 99025EBR 25185.88667149 .00002424 00000-0 98259-3 0 9996
TLE line 2: 2 36743 98.6660 235.3505 0051230 122.5139 238.1007 14.27894860868111
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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