Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9496
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.3
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: 1999-025BME
Object number (NORAD): 31248
Object ID (CCSDS): 31248
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.417 minutes
Inclination: 99.283 deg
SMA: 7298.295 km
Apoapsis: 1001.826 km
Periapsis: 838.493 km
RAAN: 184.2555 deg
Eccentricy: 0.0111898
Argument of periapsis: 184.9557 deg
Mean anomaly: 205.6679 deg
Mean motion: 13.92421294 rev/day
Mean motion (dot): 0.00000941 rev/day2
B* drag term: 0.00072823 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 2:36 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31248U 99025BME 25127.10854581 .00000941 00000-0 72823-3 0 9991
TLE line 2: 2 31248 99.2830 184.2555 0111898 184.9557 205.6679 13.92421294917670
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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