Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
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: 102.126 minutes
Inclination: 98.7268 deg
SMA: 7237.438 km
Apoapsis: 912.342 km
Periapsis: 806.265 km
RAAN: 143.4407 deg
Eccentricy: 0.0073283
Argument of periapsis: 149.2165 deg
Mean anomaly: 211.3335 deg
Mean motion: 14.10020536 rev/day
Mean motion (dot): 0.00000301 rev/day2
B* drag term: 0.00018976 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 6:34 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31890U 99025CKR 25125.27376842 .00000301 00000-0 18976-3 0 9998
TLE line 2: 2 31890 98.7268 143.4407 0073283 149.2165 211.3335 14.10020536610318
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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