Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.2
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: 1999-025AVA
Object number (NORAD): 30816
Object ID (CCSDS): 30816
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.551 minutes
Inclination: 98.9145 deg
SMA: 7210.251 km
Apoapsis: 869.912 km
Periapsis: 794.32 km
RAAN: 56.6708 deg
Eccentricy: 0.005242
Argument of periapsis: 56.893 deg
Mean anomaly: 2.7743 deg
Mean motion: 14.18003155 rev/day
Mean motion (dot): 0.00005023 rev/day2
B* drag term: 0.0024397141 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 4:39 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30816U 99025AVA 25346.19411139 .00005023 00000-0 24397-2 0 9999
TLE line 2: 2 30816 98.9145 56.6708 0052420 56.8930 2.7743 14.18003155963865
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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