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

9517

Days in orbit

Revolutions

≈ 13.4

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: 1999-057AN

Object number (NORAD): 26152

Object ID (CCSDS): 26152

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 107.604 minutes

Inclination: 99.1483 deg

SMA: 7493.979 km

Apoapsis: 1505.183 km

Periapsis: 726.504 km

RAAN: 330.9527 deg

Eccentricy: 0.05195363

Argument of periapsis: 156.3467 deg

Mean anomaly: 270.9023 deg

Mean motion: 13.38240237 rev/day

Mean motion (dot): 0.0000073 rev/day2

B* drag term: 0.00065869677 1/REarth

Two-line elements (TLE)

Creation date: Nov. 2, 2025, 5:34 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Nov. 2, 2025, midnight UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26152U 99057AN 25306.00065705 .00000730 00000-0 65870-3 0 9994

TLE line 2: 2 26152 99.1483 330.9527 0519536 156.3467 270.9023 13.38240237247719

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-6A DEB SSO 2025-03-03 00:33:43 0.0001070696 196.0 (m) DEBRIS
COSMOS 1159 LEO 2024-11-01 13:48:13 0.005757427 113.0 (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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