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

9346

Days in orbit

Revolutions

≈ 14.0

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: 1999-057SE

Object number (NORAD): 35326

Object ID (CCSDS): 35326

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 102.841 minutes

Inclination: 98.4919 deg

SMA: 7271.166 km

Apoapsis: 1059.05 km

Periapsis: 727.012 km

RAAN: 21.6515 deg

Eccentricy: 0.0228325

Argument of periapsis: 357.0378 deg

Mean anomaly: 2.9422 deg

Mean motion: 14.00221278 rev/day

Mean motion (dot): 0.00000133 rev/day2

B* drag term: 0.000093682 1/REarth

Two-line elements (TLE)

Creation date: May 14, 2025, 5:20 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 14, 2025, 10:58 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 35326U 99057SE 25134.45710884 .00000133 00000-0 93682-4 0 9990

TLE line 2: 2 35326 98.4919 21.6515 0228325 357.0378 2.9422 14.00221278597968

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
OV3-3 LEO 2024-12-05 01:12:15 0.0003026928 719.0 (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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