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

9503

Days in orbit

Revolutions

≈ 14.5

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: 1999-057DL

Object number (NORAD): 26222

Object ID (CCSDS): 26222

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.028 minutes

Inclination: 98.5115 deg

SMA: 7090.328 km

Apoapsis: 762.015 km

Periapsis: 662.371 km

RAAN: 345.428 deg

Eccentricy: 0.00702677

Argument of periapsis: 101.4541 deg

Mean anomaly: 259.4557 deg

Mean motion: 14.54130167 rev/day

Mean motion (dot): 0.00003183 rev/day2

B* drag term: 0.00074002059 1/REarth

Two-line elements (TLE)

Creation date: Oct. 20, 2025, 2:10 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 19, 2025, 11:59 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26222U 99057DL 25292.99957830 .00003183 00000-0 74002-3 0 9995

TLE line 2: 2 26222 98.5115 345.4280 0070268 101.4541 259.4557 14.54130167348857

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
COSMOS 2251 DEB LEO 2024-11-26 07:21:56 0.0003268685 138.0 (m) DEBRIS
XSS 10 LEO 2024-10-31 14:46:15 0.0005218469 393.0 (m) PAYLOAD
FENGYUN 1C DEB SSO 2024-09-28 12:49:28 0.0002199664 697.0 (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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