Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9493
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.1
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: 1999-025CVP
Object number (NORAD): 32217
Object ID (CCSDS): 32217
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.902 minutes
Inclination: 99.1176 deg
SMA: 7084.28 km
Apoapsis: 730.104 km
Periapsis: 682.187 km
RAAN: 276.7561 deg
Eccentricy: 0.0033819
Argument of periapsis: 358.0618 deg
Mean anomaly: 2.0441 deg
Mean motion: 14.5599253 rev/day
Mean motion (dot): 0.00039831 rev/day2
B* drag term: 0.0089446 1/REarth
Two-line elements (TLE)
Creation date: April 9, 2025, 5:16 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 7, 2024, 7:03 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 32217U 99025CVP 24251.29403962 .00039831 00000-0 89446-2 0 9996
TLE line 2: 2 32217 99.1176 276.7561 0033819 358.0618 2.0441 14.55992530893362
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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