Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025EEG
Object number (NORAD): 37048
Object ID (CCSDS): 37048
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.484 minutes
Inclination: 98.885 deg
SMA: 7395.233 km
Apoapsis: 1204.331 km
Periapsis: 829.866 km
RAAN: 204.5179 deg
Eccentricy: 0.025318
Argument of periapsis: 159.5311 deg
Mean anomaly: 272.4204 deg
Mean motion: 13.6513296 rev/day
Mean motion (dot): 0.00000189 rev/day2
B* drag term: 0.00022488 1/REarth
Two-line elements (TLE)
Creation date: Dec. 9, 2025, 7:56 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 8, 2025, 9:18 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37048U 99025EEG 25342.88793007 .00000189 00000-0 22488-3 0 9990
TLE line 2: 2 37048 98.8850 204.5179 0253180 159.5311 272.4204 13.65132960621178
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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