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

9399

Days in orbit

Revolutions

≈ 14.6

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.6

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: 1999-057DY

Object number (NORAD): 26234

Object ID (CCSDS): 26234

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.967 minutes

Inclination: 98.5847 deg

SMA: 7087.396 km

Apoapsis: 716.468 km

Periapsis: 702.054 km

RAAN: 293.7426 deg

Eccentricy: 0.0010169

Argument of periapsis: 236.5661 deg

Mean anomaly: 245.7303 deg

Mean motion: 14.55032655 rev/day

Mean motion (dot): 0.00000437 rev/day2

B* drag term: 0.00011274 1/REarth

Two-line elements (TLE)

Creation date: July 8, 2025, 2:27 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 7, 2025, 8:40 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26234U 99057DY 25188.86176712 .00000437 00000-0 11274-3 0 9991

TLE line 2: 2 26234 98.5847 293.7426 0010169 236.5661 245.7303 14.55032655340231

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 2025-01-18 18:35:33 0.0002338616 243.0 (m) DEBRIS
FREGAT R/B LEO 2024-08-14 05:00:36 0.0002715486 390.0 (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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