Key statistics
Satellite CZ-4 DEB at a glance.
Uptime
12890
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.9
Latest
Satellite identification and parameters
Extended collection of information and parameters for CZ-4 DEB.
Object identification
Identified? True
Debris? True
Object name: CZ-4 DEB
International designator: 1990-081DN
Object number (NORAD): 37626
Object ID (CCSDS): 37626
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.937 minutes
Inclination: 98.9245 deg
SMA: 7369.627 km
Apoapsis: 1110.997 km
Periapsis: 871.987 km
RAAN: 303.6562 deg
Eccentricy: 0.01621587
Argument of periapsis: 157.9182 deg
Mean anomaly: 357.5874 deg
Mean motion: 13.72254067 rev/day
Mean motion (dot): 0.00000267 rev/day2
B* drag term: 0.00030589039 1/REarth
Two-line elements (TLE)
Creation date: Dec. 15, 2025, 8:47 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 15, 2025, 8:40 a.m. UTC
TLE line 0: 0 CZ-4 DEB
TLE line 1: 1 37626U 90081DN 25349.36165457 .00000267 00000-0 30589-3 0 9995
TLE line 2: 2 37626 98.9245 303.6562 0162159 157.9182 357.5874 13.72254067116076
Live tracking on map
Real-time ground track for satellite CZ-4 DEB.
Associated space launch
Chinese polar orbiting meteorological satellite
CZ-4 DEB was lifted into orbit during the mission ‘Long March 4A | Feng Yun 1B’, on board a Long March 4A space rocket.
The launch took place on Sept. 3, 1990, 12:53 a.m. from Launch Complex 7.
For more information about the launch, click the button.
Long March 4A | Feng Yun 1B
Agency: N/A
Status: Launch Successful
Launch date: Sept. 3, 1990, 12:53 a.m. UTC
Rocket: Long March 4A
Launch pad: Launch Complex 7
Location: Taiyuan Satellite Launch Center, People's Republic of China
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