Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9555
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: 1999-025BPE
Object number (NORAD): 31296
Object ID (CCSDS): 31296
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.519 minutes
Inclination: 99.0715 deg
SMA: 7066.018 km
Apoapsis: 707.825 km
Periapsis: 667.941 km
RAAN: 85.9987 deg
Eccentricy: 0.0028222
Argument of periapsis: 348.4504 deg
Mean anomaly: 11.6043 deg
Mean motion: 14.61640777 rev/day
Mean motion (dot): 0.00011954 rev/day2
B* drag term: 0.0023971 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 10:05 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31296U 99025BPE 25187.42070005 .00011954 00000-0 23971-2 0 9991
TLE line 2: 2 31296 99.0715 85.9987 0028222 348.4504 11.6043 14.61640777950163
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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