Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.2
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: 1999-025ADP
Object number (NORAD): 30400
Object ID (CCSDS): 30400
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.32 minutes
Inclination: 99.1531 deg
SMA: 7246.569 km
Apoapsis: 1033.84 km
Periapsis: 703.029 km
RAAN: 52.4475 deg
Eccentricy: 0.0228253
Argument of periapsis: 225.1947 deg
Mean anomaly: 288.9815 deg
Mean motion: 14.07356336 rev/day
Mean motion (dot): 0.00003272 rev/day2
B* drag term: 0.0015573 1/REarth
Two-line elements (TLE)
Creation date: May 9, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 6:35 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30400U 99025ADP 25128.27461481 .00003272 00000-0 15573-2 0 9990
TLE line 2: 2 30400 99.1531 52.4475 0228253 225.1947 288.9815 14.07356336924392
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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