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

9398

Days in orbit

Revolutions

≈ 14.6

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: 1999-057SN

Object number (NORAD): 35334

Object ID (CCSDS): 35334

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.743 minutes

Inclination: 98.4728 deg

SMA: 7076.688 km

Apoapsis: 744.199 km

Periapsis: 652.908 km

RAAN: 243.2747 deg

Eccentricy: 0.0064501

Argument of periapsis: 5.5546 deg

Mean anomaly: 354.6354 deg

Mean motion: 14.583362 rev/day

Mean motion (dot): 0.00001653 rev/day2

B* drag term: 0.00035797 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 6:05 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 2:16 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 35334U 99057SN 25187.09493692 .00001653 00000-0 35797-3 0 9992

TLE line 2: 2 35334 98.4728 243.2747 0064501 5.5546 354.6354 14.58336200 17930

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
THOR ABLESTAR DEB LEO 2025-05-14 09:13:17 0.0001174959 766.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-02-18 10:27:36 0.000181722 161.0 (m) DEBRIS
IRIDIUM 33 DEB LEO 2024-11-12 14:08:16 0.0002974877 309.0 (m) DEBRIS

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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