Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9715
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.2
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: 1999-025ANM
Object number (NORAD): 30630
Object ID (CCSDS): 30630
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.239 minutes
Inclination: 99.1728 deg
SMA: 7195.469 km
Apoapsis: 836.017 km
Periapsis: 798.651 km
RAAN: 159.3038 deg
Eccentricy: 0.0025965
Argument of periapsis: 75.9619 deg
Mean anomaly: 49.3985 deg
Mean motion: 14.22374914 rev/day
Mean motion (dot): 0.00002986 rev/day2
B* drag term: 0.0013579915 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 6:50 a.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 30630U 99025ANM 25346.28472515 .00002986 00000-0 13580-2 0 9995
TLE line 2: 2 30630 99.1728 159.3038 0025965 75.9619 49.3985 14.22374914972062
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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