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

9339

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: 99.071 minutes

Inclination: 98.527 deg

SMA: 7092.389 km

Apoapsis: 762.918 km

Periapsis: 665.59 km

RAAN: 177.2913 deg

Eccentricy: 0.0068614

Argument of periapsis: 246.3783 deg

Mean anomaly: 113.0198 deg

Mean motion: 14.53496296 rev/day

Mean motion (dot): 0.00001962 rev/day2

B* drag term: 0.00046791 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 5:55 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26222U 99057DL 25127.74665044 .00001962 00000-0 46791-3 0 9995

TLE line 2: 2 26222 98.5270 177.2913 0068614 246.3783 113.0198 14.53496296324848

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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