Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9556
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.3
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: 1999-025CS
Object number (NORAD): 29800
Object ID (CCSDS): 29800
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.044 minutes
Inclination: 98.3017 deg
SMA: 7280.728 km
Apoapsis: 998.075 km
Periapsis: 807.111 km
RAAN: 224.7441 deg
Eccentricy: 0.0131144
Argument of periapsis: 314.4017 deg
Mean anomaly: 74.4256 deg
Mean motion: 13.97463722 rev/day
Mean motion (dot): 0.00002138 rev/day2
B* drag term: 0.0014395 1/REarth
Two-line elements (TLE)
Creation date: July 7, 2025, 6:34 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 12:48 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29800U 99025CS 25188.03371388 .00002138 00000-0 14395-2 0 9999
TLE line 2: 2 29800 98.3017 224.7441 0131144 314.4017 74.4256 13.97463722933598
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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