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

9453

Days in orbit

Revolutions

≈ 13.8

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.1

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: 1999-057AL

Object number (NORAD): 26150

Object ID (CCSDS): 26150

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 104.26 minutes

Inclination: 99.114 deg

SMA: 7337.924 km

Apoapsis: 1212.185 km

Periapsis: 707.393 km

RAAN: 325.5134 deg

Eccentricy: 0.03439611

Argument of periapsis: 138.1697 deg

Mean anomaly: 33.6342 deg

Mean motion: 13.81156644 rev/day

Mean motion (dot): 0.00002531 rev/day2

B* drag term: 0.001548872 1/REarth

Two-line elements (TLE)

Creation date: Aug. 30, 2025, 11:24 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 29, 2025, 11:43 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26150U 99057AL 25241.98876171 .00002531 00000-0 15489-2 0 9995

TLE line 2: 2 26150 99.1140 325.5134 0343961 138.1697 33.6342 13.81156644275187

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
CZ-4 DEB SSO 2025-04-16 01:23:32 0.0001981297 262.0 (m) DEBRIS

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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