Key statistics
Satellite CZ-4 DEB at a glance.
Uptime
12786
Days in orbit
Revolutions
≈ 14.1
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: 1990-081AZ
Object number (NORAD): 20889
Object ID (CCSDS): 20889
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 102.375 minutes
Inclination: 98.9114 deg
SMA: 7249.167 km
Apoapsis: 920.1 km
Periapsis: 821.964 km
RAAN: 331.341 deg
Eccentricy: 0.00676879
Argument of periapsis: 288.238 deg
Mean anomaly: 71.143 deg
Mean motion: 14.06599904 rev/day
Mean motion (dot): 0.00001466 rev/day2
B* drag term: 0.00089230642 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 10:13 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 4, 2025, 4:20 a.m. UTC
TLE line 0: 0 CZ-4 DEB
TLE line 1: 1 20889U 90081AZ 25247.18115513 .00001466 00000-0 89231-3 0 9993
TLE line 2: 2 20889 98.9114 331.3410 0067688 288.2380 71.1430 14.06599904780178
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
...
Latest news about this satellite
There are no fresh news available about this satellite. Check back as we update our databases every day.
Newsletter sign-up
Weekly statistics, charts and insights to help you stay on top of the space industry.
