Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9500
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
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: 1999-025DUR
Object number (NORAD): 36216
Object ID (CCSDS): 36216
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.514 minutes
Inclination: 98.6228 deg
SMA: 7208.488 km
Apoapsis: 861.742 km
Periapsis: 798.964 km
RAAN: 158.5763 deg
Eccentricy: 0.0043545
Argument of periapsis: 274.6004 deg
Mean anomaly: 85.0199 deg
Mean motion: 14.18523398 rev/day
Mean motion (dot): 0.00000714 rev/day2
B* drag term: 0.00036286 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, 7:51 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 36216U 99025DUR 25132.32767357 .00000714 00000-0 36286-3 0 9996
TLE line 2: 2 36216 98.6228 158.5763 0043545 274.6004 85.0199 14.18523398613325
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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