CZ-4 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite CZ-4 DEB at a glance.

Uptime

12725

Days in orbit

Revolutions

≈ 13.8

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: 1990-081BC

Object number (NORAD): 20892

Object ID (CCSDS): 20892

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 104.146 minutes

Inclination: 98.9269 deg

SMA: 7332.559 km

Apoapsis: 1071.25 km

Periapsis: 837.599 km

RAAN: 35.9913 deg

Eccentricy: 0.0159324

Argument of periapsis: 185.9196 deg

Mean anomaly: 201.4679 deg

Mean motion: 13.82672663 rev/day

Mean motion (dot): 0.00000594 rev/day2

B* drag term: 0.00053027 1/REarth

Two-line elements (TLE)

Creation date: July 5, 2025, 5:45 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 5, 2025, 1:24 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 20892U 90081BC 25186.55840356 .00000594 00000-0 53027-3 0 9995

TLE line 2: 2 20892 98.9269 35.9913 0159324 185.9196 201.4679 13.82672663742735

Live tracking on map

Real-time ground track for satellite CZ-4 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object CZ-4 DEB.

Target Orbit TCA Probability of collision Miss distance Type
METEOR 1-19 LEO 2025-02-22 05:19:41 0.0007690474 908.0 (m) PAYLOAD
CZ-6A DEB LEO 2024-11-10 07:27:37 0.0001329362 260.0 (m) DEBRIS
COSMOS 1531 LEO 2024-10-16 05:32:45 0.0002778144 896.0 (m) PAYLOAD
FENGYUN 1C DEB SSO 2024-09-25 17:37:06 0.0003051791 676.0 (m) DEBRIS
SL-3 R/B LEO 2024-09-16 11:18:39 0.0001182632 489.0 (m) ROCKET BODY

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.

Launch to space Long March 4A | Feng Yun 1B
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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