Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025CHF
Object number (NORAD): 31817
Object ID (CCSDS): 31817
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.489 minutes
Inclination: 98.9089 deg
SMA: 7064.576 km
Apoapsis: 734.012 km
Periapsis: 638.869 km
RAAN: 103.0726 deg
Eccentricy: 0.0067338
Argument of periapsis: 39.7077 deg
Mean anomaly: 320.9024 deg
Mean motion: 14.62088366 rev/day
Mean motion (dot): 0.00010424 rev/day2
B* drag term: 0.0020172 1/REarth
Two-line elements (TLE)
Creation date: May 5, 2025, 6:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 4:08 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31817U 99025CHF 25124.67287316 .00010424 00000-0 20172-2 0 9994
TLE line 2: 2 31817 98.9089 103.0726 0067338 39.7077 320.9024 14.62088366943396
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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