Key statistics
Satellite CZ-4 DEB at a glance.
Uptime
12724
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: 102.382 minutes
Inclination: 98.9138 deg
SMA: 7249.502 km
Apoapsis: 922.613 km
Periapsis: 820.121 km
RAAN: 270.311 deg
Eccentricy: 0.0070689
Argument of periapsis: 102.4374 deg
Mean anomaly: 258.4716 deg
Mean motion: 14.06502412 rev/day
Mean motion (dot): 0.0000075 rev/day2
B* drag term: 0.00046851 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 5:20 a.m. UTC
TLE line 0: 0 CZ-4 DEB
TLE line 1: 1 20889U 90081AZ 25185.22250635 .00000750 00000-0 46851-3 0 9990
TLE line 2: 2 20889 98.9138 270.3110 0070689 102.4374 258.4716 14.06502412771465
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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