Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9619
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 1999-025BG
Object number (NORAD): 29766
Object ID (CCSDS): 29766
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.116 minutes
Inclination: 98.6733 deg
SMA: 7284.123 km
Apoapsis: 1011.505 km
Periapsis: 800.471 km
RAAN: 206.5593 deg
Eccentricy: 0.0144859
Argument of periapsis: 191.3004 deg
Mean anomaly: 346.8995 deg
Mean motion: 13.96486756 rev/day
Mean motion (dot): 0.00001821 rev/day2
B* drag term: 0.0012331206 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 6:18 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 8, 2025, 3:03 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 29766U 99025BG 25251.62744117 .00001821 00000-0 12331-2 0 9996
TLE line 2: 2 29766 98.6733 206.5593 0144859 191.3004 346.8995 13.96486756944766
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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