Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9554
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
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: 1999-025EVK
Object number (NORAD): 38819
Object ID (CCSDS): 38819
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.482 minutes
Inclination: 98.6073 deg
SMA: 7206.955 km
Apoapsis: 885.969 km
Periapsis: 771.671 km
RAAN: 184.0474 deg
Eccentricy: 0.0079297
Argument of periapsis: 297.085 deg
Mean anomaly: 186.7056 deg
Mean motion: 14.18975847 rev/day
Mean motion (dot): 0.00000579 rev/day2
B* drag term: 0.00028936 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 7:15 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 38819U 99025EVK 25186.80240948 .00000579 00000-0 28936-3 0 9993
TLE line 2: 2 38819 98.6073 184.0474 0079297 297.0850 186.7056 14.18975847666877
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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