Key statistics
Satellite CZ-4 DEB at a glance.
Uptime
12666
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.3
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: 1990-081W
Object number (NORAD): 20858
Object ID (CCSDS): 20858
Country: PEOPLES REPUBLIC OF CHINA (PRC)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 98.986 minutes
Inclination: 98.2801 deg
SMA: 7088.327 km
Apoapsis: 730.645 km
Periapsis: 689.739 km
RAAN: 165.0463 deg
Eccentricy: 0.0028854
Argument of periapsis: 269.3855 deg
Mean anomaly: 238.6731 deg
Mean motion: 14.54745951 rev/day
Mean motion (dot): 0.00004133 rev/day2
B* drag term: 0.00097025 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 4:33 p.m. UTC
TLE line 0: 0 CZ-4 DEB
TLE line 1: 1 20858U 90081W 25127.69015845 .00004133 00000-0 97025-3 0 9993
TLE line 2: 2 20858 98.2801 165.0463 0028854 269.3855 238.6731 14.54745951806877
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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