Key statistics
Satellite CZ-4 DEB at a glance.
Uptime
12671
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: 1990-081BY
Object number (NORAD): 20915
Object ID (CCSDS): 20915
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.925 minutes
Inclination: 98.5314 deg
SMA: 7180.586 km
Apoapsis: 829.28 km
Periapsis: 775.623 km
RAAN: 129.4866 deg
Eccentricy: 0.0037362
Argument of periapsis: 114.9545 deg
Mean anomaly: 308.0829 deg
Mean motion: 14.26799301 rev/day
Mean motion (dot): 0.00000971 rev/day2
B* drag term: 0.00041499 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 2:31 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 11, 2025, 4:19 p.m. UTC
TLE line 0: 0 CZ-4 DEB
TLE line 1: 1 20915U 90081BY 25131.68035064 .00000971 00000-0 41499-3 0 9996
TLE line 2: 2 20915 98.5314 129.4866 0037362 114.9545 308.0829 14.26799301791543
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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