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

9507

Days in orbit

Revolutions

≈ 14.6

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: 1999-057DR

Object number (NORAD): 26227

Object ID (CCSDS): 26227

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 98.947 minutes

Inclination: 98.5033 deg

SMA: 7086.444 km

Apoapsis: 759.279 km

Periapsis: 657.338 km

RAAN: 348.4611 deg

Eccentricy: 0.0071927

Argument of periapsis: 96.7262 deg

Mean anomaly: 67.8346 deg

Mean motion: 14.55325855 rev/day

Mean motion (dot): 0.00002761 rev/day2

B* drag term: 0.00062613 1/REarth

Two-line elements (TLE)

Creation date: Oct. 23, 2025, 10:16 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 23, 2025, 2:24 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26227U 99057DR 25296.60025909 .00002761 00000-0 62613-3 0 9991

TLE line 2: 2 26227 98.5033 348.4611 0071927 96.7262 67.8346 14.55325855349085

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
SS 2 LEO 2025-06-15 21:25:05 0.0006479973 239.0 (m) PAYLOAD
STEX LEO 2025-06-14 14:35:09 0.0005257339 34.0 (m) PAYLOAD

Associated space launch

The CBERS (China Brazil Earth Resources Satellite) or ZY 1 (Zi Yuan) satellites are designed for global coverage and include cameras to make optical observations and a data collecting system to gather data on the environment. They are unique systems due to the use of on-board sensors which combine features that are especially designed to resolve the broad range of space and time scales involved in the monitoring and preservation of the ecosystem. They are operated jointly by the China Centre for Resources Satellite Data and Application (CRESDA) and the Brazilian INPE (Instituto Nacional de Pesquisas Espaciais, National Institute of Space Research).

CZ-4 DEB was lifted into orbit during the mission ‘Long March 4B | Zi Yuan 1-1’, on board a Long March 4B space rocket.

The launch took place on Oct. 14, 1999, 3:15 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 4B | Zi Yuan 1-1
Long March 4B | Zi Yuan 1-1

Agency: N/A

Status: Launch Successful

Launch date: Oct. 14, 1999, 3:15 a.m. UTC

Rocket: Long March 4B

Launch pad: Launch Complex 7

Location: Taiyuan Satellite Launch Center, People's Republic of China

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