Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9494
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.1
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: 1999-025AGJ
Object number (NORAD): 30471
Object ID (CCSDS): 30471
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.967 minutes
Inclination: 99.0557 deg
SMA: 7229.94 km
Apoapsis: 914.256 km
Periapsis: 789.353 km
RAAN: 211.8717 deg
Eccentricy: 0.0086379
Argument of periapsis: 154.4595 deg
Mean anomaly: 328.8515 deg
Mean motion: 14.12214793 rev/day
Mean motion (dot): 0.00004017 rev/day2
B* drag term: 0.002133 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 6:19 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30471U 99025AGJ 25126.76351637 .00004017 00000-0 21330-2 0 9997
TLE line 2: 2 30471 99.0557 211.8717 0086379 154.4595 328.8515 14.12214793933365
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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