Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9495
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.0
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: 1999-025AEV
Object number (NORAD): 30434
Object ID (CCSDS): 30434
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.565 minutes
Inclination: 98.9828 deg
SMA: 7305.279 km
Apoapsis: 1016.978 km
Periapsis: 837.309 km
RAAN: 121.3867 deg
Eccentricy: 0.0122972
Argument of periapsis: 107.7898 deg
Mean anomaly: 43.6043 deg
Mean motion: 13.9042496 rev/day
Mean motion (dot): 0.00000562 rev/day2
B* drag term: 0.00045711 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, 11 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30434U 99025AEV 25127.45858233 .00000562 00000-0 45711-3 0 9998
TLE line 2: 2 30434 98.9828 121.3867 0122972 107.7898 43.6043 13.90424960926590
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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