Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9494
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.2
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: 1999-025CHU
Object number (NORAD): 31830
Object ID (CCSDS): 31830
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.168 minutes
Inclination: 99.1559 deg
SMA: 7333.591 km
Apoapsis: 1094.727 km
Periapsis: 816.185 km
RAAN: 237.8262 deg
Eccentricy: 0.0189908
Argument of periapsis: 183.7864 deg
Mean anomaly: 202.5327 deg
Mean motion: 13.82380928 rev/day
Mean motion (dot): 0.00003513 rev/day2
B* drag term: 0.0028641 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, 7:03 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31830U 99025CHU 25126.29392836 .00003513 00000-0 28641-2 0 9993
TLE line 2: 2 31830 99.1559 237.8262 0189908 183.7864 202.5327 13.82380928896937
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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