Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9493
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.2
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: 1999-025ELC
Object number (NORAD): 37687
Object ID (CCSDS): 37687
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.168 minutes
Inclination: 98.1986 deg
SMA: 7333.582 km
Apoapsis: 1206.731 km
Periapsis: 704.162 km
RAAN: 184.3015 deg
Eccentricy: 0.0342649
Argument of periapsis: 261.05 deg
Mean anomaly: 226.0599 deg
Mean motion: 13.82383504 rev/day
Mean motion (dot): 0.0000952 rev/day2
B* drag term: 0.0056323 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: April 30, 2025, 11:31 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37687U 99025ELC 25120.97993264 .00009520 00000-0 56323-2 0 9992
TLE line 2: 2 37687 98.1986 184.3015 0342649 261.0500 226.0599 13.82383504801322
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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