Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 14.0
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: 1999-025QJ
Object number (NORAD): 30081
Object ID (CCSDS): 30081
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.001 minutes
Inclination: 98.9153 deg
SMA: 7278.719 km
Apoapsis: 955.447 km
Periapsis: 845.721 km
RAAN: 130.9646 deg
Eccentricy: 0.0075374
Argument of periapsis: 220.0492 deg
Mean anomaly: 254.1435 deg
Mean motion: 13.98042353 rev/day
Mean motion (dot): 0.00000694 rev/day2
B* drag term: 0.00050644 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 2:30 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30081U 99025QJ 25128.60477306 .00000694 00000-0 50644-3 0 9999
TLE line 2: 2 30081 98.9153 130.9646 0075374 220.0492 254.1435 13.98042353933202
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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