Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9552
Days in orbit
Revolutions
≈ 13.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
102.5
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: 1999-025CQA
Object number (NORAD): 31997
Object ID (CCSDS): 31997
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.887 minutes
Inclination: 102.5163 deg
SMA: 7414.026 km
Apoapsis: 1249.429 km
Periapsis: 822.352 km
RAAN: 183.3665 deg
Eccentricy: 0.028802
Argument of periapsis: 280.4741 deg
Mean anomaly: 76.4057 deg
Mean motion: 13.59945894 rev/day
Mean motion (dot): 0.00001139 rev/day2
B* drag term: 0.0012319 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 3:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 4:50 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31997U 99025CQA 25184.70190969 .00001139 00000-0 12319-2 0 9997
TLE line 2: 2 31997 102.5163 183.3665 0288020 280.4741 76.4057 13.59945894594809
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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