Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9493
Days in orbit
Revolutions
≈ 14.2
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: 1999-025KR
Object number (NORAD): 29967
Object ID (CCSDS): 29967
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.27 minutes
Inclination: 98.8718 deg
SMA: 7196.945 km
Apoapsis: 875.832 km
Periapsis: 761.788 km
RAAN: 200.2805 deg
Eccentricy: 0.0079231
Argument of periapsis: 209.6496 deg
Mean anomaly: 170.0591 deg
Mean motion: 14.21937373 rev/day
Mean motion (dot): 0.0000417 rev/day2
B* drag term: 0.0018494 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 4:29 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29967U 99025KR 25125.18686126 .00004170 00000-0 18494-2 0 9991
TLE line 2: 2 29967 98.8718 200.2805 0079231 209.6496 170.0591 14.21937373940726
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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