Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025CKR
Object number (NORAD): 31890
Object ID (CCSDS): 31890
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.124 minutes
Inclination: 98.7233 deg
SMA: 7237.35 km
Apoapsis: 911.346 km
Periapsis: 807.085 km
RAAN: 202.6463 deg
Eccentricy: 0.007203
Argument of periapsis: 338.0689 deg
Mean anomaly: 21.7404 deg
Mean motion: 14.10046267 rev/day
Mean motion (dot): 0.00000068 rev/day2
B* drag term: 0.000061388 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 7:10 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31890U 99025CKR 25186.29908448 .00000068 00000-0 61388-4 0 9996
TLE line 2: 2 31890 98.7233 202.6463 0072030 338.0689 21.7404 14.10046267618911
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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