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

≈ 14.7

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.4

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: 1999-057FC

Object number (NORAD): 26266

Object ID (CCSDS): 26266

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.121 minutes

Inclination: 98.4315 deg

SMA: 7046.949 km

Apoapsis: 722.099 km

Periapsis: 615.528 km

RAAN: 209.4456 deg

Eccentricy: 0.0075615

Argument of periapsis: 271.477 deg

Mean anomaly: 87.7773 deg

Mean motion: 14.67577686 rev/day

Mean motion (dot): 0.00005637 rev/day2

B* drag term: 0.00096021 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, 6:25 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26266U 99057FC 25127.76771849 .00005637 00000-0 96021-3 0 9990

TLE line 2: 2 26266 98.4315 209.4456 0075615 271.4770 87.7773 14.67577686323651

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 LEO 2025-02-26 07:45:26 0.0004429736 102.0 (m) DEBRIS
IRIDIUM 33 DEB LEO 2024-11-09 15:35:16 0.0001604712 873.0 (m) DEBRIS
SL-8 R/B LEO 2024-11-08 01:39:44 0.0004719199 111.0 (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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