Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9620
Days in orbit
Revolutions
≈ 13.4
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
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: 1999-025EGP
Object number (NORAD): 37421
Object ID (CCSDS): 37421
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 107.429 minutes
Inclination: 98.8696 deg
SMA: 7485.85 km
Apoapsis: 1413.316 km
Periapsis: 802.114 km
RAAN: 215.1212 deg
Eccentricy: 0.04082378
Argument of periapsis: 332.4162 deg
Mean anomaly: 25.5828 deg
Mean motion: 13.40420551 rev/day
Mean motion (dot): 0.00001083 rev/day2
B* drag term: 0.0012561443 1/REarth
Two-line elements (TLE)
Creation date: Sept. 6, 2025, 2:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 5, 2025, 2:58 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 37421U 99025EGP 25248.62395283 .00001083 00000-0 12561-2 0 9990
TLE line 2: 2 37421 98.8696 215.1212 0408238 332.4162 25.5828 13.40420551596314
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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