Key statistics
Satellite FENGYUN 1C DEB at a glance.
Uptime
9615
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
99.1
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: 1999-025BZV
Object number (NORAD): 31615
Object ID (CCSDS): 31615
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.533 minutes
Inclination: 99.1396 deg
SMA: 7161.972 km
Apoapsis: 907.995 km
Periapsis: 659.678 km
RAAN: 292.6675 deg
Eccentricy: 0.01733582
Argument of periapsis: 247.1226 deg
Mean anomaly: 111.1573 deg
Mean motion: 14.32365559 rev/day
Mean motion (dot): 0.0001383 rev/day2
B* drag term: 0.0043414279 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 4:29 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 3, 2025, 8:54 p.m. UTC
TLE line 0: 0 FENGYUN 1C DEB
TLE line 1: 1 31615U 99025BZV 25246.87100288 .00013830 00000-0 43414-2 0 9997
TLE line 2: 2 31615 99.1396 292.6675 0173358 247.1226 111.1573 14.32365559638473
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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