Key statistics
Satellite CZ-4 DEB at a glance.
Uptime
12664
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.2
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: 1990-081CF
Object number (NORAD): 20973
Object ID (CCSDS): 20973
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.453 minutes
Inclination: 98.2035 deg
SMA: 7062.834 km
Apoapsis: 710.592 km
Periapsis: 658.807 km
RAAN: 178.7367 deg
Eccentricy: 0.003666
Argument of periapsis: 26.3009 deg
Mean anomaly: 27.9965 deg
Mean motion: 14.62629225 rev/day
Mean motion (dot): 0.00006616 rev/day2
B* drag term: 0.0012976 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 7:40 p.m. UTC
TLE line 0: 0 CZ-4 DEB
TLE line 1: 1 20973U 90081CF 25125.81957022 .00006616 00000-0 12976-2 0 9994
TLE line 2: 2 20973 98.2035 178.7367 0036660 26.3009 27.9965 14.62629225810905
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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