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

9338

Days in orbit

Revolutions

≈ 14.6

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.4

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: 1999-057AC

Object number (NORAD): 26140

Object ID (CCSDS): 26140

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.645 minutes

Inclination: 99.3568 deg

SMA: 7072.028 km

Apoapsis: 799.386 km

Periapsis: 588.399 km

RAAN: 7.6234 deg

Eccentricy: 0.014917

Argument of periapsis: 73.9727 deg

Mean anomaly: 38.9661 deg

Mean motion: 14.59778048 rev/day

Mean motion (dot): 0.000054 rev/day2

B* drag term: 0.00097855 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, 6:33 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26140U 99057AC 25127.27298271 .00005400 00000-0 97855-3 0 9994

TLE line 2: 2 26140 99.3568 7.6234 0149170 73.9727 38.9661 14.59778048314682

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 1867 LEO 2025-03-10 14:32:09 0.0001300866 287.0 (m) PAYLOAD
CZ-4B R/B SSO 2024-10-23 07:52:27 0.0001294705 77.0 (m) ROCKET BODY

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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