Key statistics
Satellite CZ-4 DEB at a glance.
Uptime
12665
Days in orbit
Revolutions
≈ 14.3
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.5
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: 1990-081CQ
Object number (NORAD): 23259
Object ID (CCSDS): 23259
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.494 minutes
Inclination: 98.5391 deg
SMA: 7160.138 km
Apoapsis: 795.925 km
Periapsis: 768.081 km
RAAN: 124.9901 deg
Eccentricy: 0.0019444
Argument of periapsis: 113.2956 deg
Mean anomaly: 247.0277 deg
Mean motion: 14.32915833 rev/day
Mean motion (dot): 0.00001982 rev/day2
B* drag term: 0.00073962 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 9:49 a.m. UTC
TLE line 0: 0 CZ-4 DEB
TLE line 1: 1 23259U 90081CQ 25126.40953059 .00001982 00000-0 73962-3 0 9990
TLE line 2: 2 23259 98.5391 124.9901 0019444 113.2956 247.0277 14.32915833751936
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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