Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9615
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.9
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: 1999-025CDX
Object number (NORAD): 31724
Object ID (CCSDS): 31724
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.561 minutes
Inclination: 97.8585 deg
SMA: 7115.746 km
Apoapsis: 849.862 km
Periapsis: 625.36 km
RAAN: 260.2535 deg
Eccentricy: 0.01577502
Argument of periapsis: 188.2497 deg
Mean anomaly: 171.61 deg
Mean motion: 14.4634556 rev/day
Mean motion (dot): 0.00012336 rev/day2
B* drag term: 0.0029513065 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 10:13 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 4, 2025, 7:10 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31724U 99025CDX 25247.29922797 .00012336 00000-0 29513-2 0 9996
TLE line 2: 2 31724 97.8585 260.2535 0157750 188.2497 171.6100 14.46345560630539
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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