Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9499
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.2
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: 1999-025DEG
Object number (NORAD): 33647
Object ID (CCSDS): 33647
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.971 minutes
Inclination: 98.2288 deg
SMA: 7324.334 km
Apoapsis: 1131.242 km
Periapsis: 761.156 km
RAAN: 183.0751 deg
Eccentricy: 0.0252641
Argument of periapsis: 205.932 deg
Mean anomaly: 152.8998 deg
Mean motion: 13.85002521 rev/day
Mean motion (dot): 0.0001952 rev/day2
B* drag term: 0.013459 1/REarth
Two-line elements (TLE)
Creation date: April 9, 2025, 5:06 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 8, 2024, 12:04 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 33647U 99025DEG 24282.50309509 .00019520 00000-0 13459-1 0 9997
TLE line 2: 2 33647 98.2288 183.0751 0252641 205.9320 152.8998 13.85002521842483
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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