Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.8
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: 1999-025CDE
Object number (NORAD): 31696
Object ID (CCSDS): 31696
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.604 minutes
Inclination: 97.8119 deg
SMA: 7307.08 km
Apoapsis: 1039.098 km
Periapsis: 818.791 km
RAAN: 331.5621 deg
Eccentricy: 0.0150749
Argument of periapsis: 148.8684 deg
Mean anomaly: 212.1518 deg
Mean motion: 13.89911059 rev/day
Mean motion (dot): 0.00004746 rev/day2
B* drag term: 0.0035409 1/REarth
Two-line elements (TLE)
Creation date: April 9, 2025, 5:16 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 14, 2024, 10:39 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31696U 99025CDE 24258.94424001 .00004746 00000-0 35409-2 0 9999
TLE line 2: 2 31696 97.8119 331.5621 0150749 148.8684 212.1518 13.89911059882877
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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