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

9344

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.0

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: 1999-057AU

Object number (NORAD): 26158

Object ID (CCSDS): 26158

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 100.857 minutes

Inclination: 98.9915 deg

SMA: 7177.357 km

Apoapsis: 930.001 km

Periapsis: 668.444 km

RAAN: 186.0672 deg

Eccentricy: 0.018221

Argument of periapsis: 79.3014 deg

Mean anomaly: 335.3656 deg

Mean motion: 14.27762305 rev/day

Mean motion (dot): 0.00003472 rev/day2

B* drag term: 0.0011938 1/REarth

Two-line elements (TLE)

Creation date: May 14, 2025, 3:37 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 13, 2025, 9:17 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26158U 99057AU 25133.88733656 .00003472 00000-0 11938-2 0 9992

TLE line 2: 2 26158 98.9915 186.0672 0182210 79.3014 335.3656 14.27762305296727

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
METEOR 2-14 LEO 2025-03-03 17:53:16 0.0001590869 364.0 (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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