Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9500
Days in orbit
Revolutions
≈ 14.3
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: 1999-025BPP
Object number (NORAD): 31311
Object ID (CCSDS): 31311
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.857 minutes
Inclination: 98.8581 deg
SMA: 7177.33 km
Apoapsis: 811.456 km
Periapsis: 786.935 km
RAAN: 210.3295 deg
Eccentricy: 0.0017082
Argument of periapsis: 349.7202 deg
Mean anomaly: 39.7593 deg
Mean motion: 14.27770324 rev/day
Mean motion (dot): 0.00004063 rev/day2
B* drag term: 0.0016602 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 7:41 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 12, 2025, 4:22 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31311U 99025BPP 25132.18261729 .00004063 00000-0 16602-2 0 9993
TLE line 2: 2 31311 98.8581 210.3295 0017082 349.7202 39.7593 14.27770324931586
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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