Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9658
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.3
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: 1999-025ASJ
Object number (NORAD): 30724
Object ID (CCSDS): 30724
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.219 minutes
Inclination: 99.3189 deg
SMA: 7147.034 km
Apoapsis: 836.511 km
Periapsis: 701.286 km
RAAN: 110.8486 deg
Eccentricy: 0.00946015
Argument of periapsis: 62.8707 deg
Mean anomaly: 308.8761 deg
Mean motion: 14.36858609 rev/day
Mean motion (dot): 0.00001427 rev/day2
B* drag term: 0.00047539195 1/REarth
Two-line elements (TLE)
Creation date: Oct. 18, 2025, 2:17 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 17, 2025, 6:35 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30724U 99025ASJ 25290.77444584 .00001427 00000-0 47539-3 0 9997
TLE line 2: 2 30724 99.3189 110.8486 0094602 62.8707 308.8761 14.36858609976494
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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