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

9458

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: 1999-057SF

Object number (NORAD): 35327

Object ID (CCSDS): 35327

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.59 minutes

Inclination: 98.482 deg

SMA: 7069.374 km

Apoapsis: 743.799 km

Periapsis: 638.68 km

RAAN: 320.515 deg

Eccentricy: 0.00743484

Argument of periapsis: 296.5596 deg

Mean anomaly: 62.7996 deg

Mean motion: 14.60599992 rev/day

Mean motion (dot): 0.00004512 rev/day2

B* drag term: 0.00090281197 1/REarth

Two-line elements (TLE)

Creation date: Aug. 31, 2025, 2:26 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 30, 2025, 11:09 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 35327U 99057SF 25242.46519459 .00004512 00000-0 90281-3 0 9993

TLE line 2: 2 35327 98.4820 320.5150 0074348 296.5596 62.7996 14.60599992670856

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
IRIDIUM 33 DEB LEO 2024-11-19 01:09:45 0.0001859778 101.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-10 11:32:43 0.0001567252 884.0 (m) DEBRIS
THOR BURNER 2 R/B SSO 2024-07-24 06:13:11 0.0003539449 96.0 (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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