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

9337

Days in orbit

Revolutions

≈ 14.1

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.1

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: 1999-057SA

Object number (NORAD): 35322

Object ID (CCSDS): 35322

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 101.834 minutes

Inclination: 99.1338 deg

SMA: 7223.62 km

Apoapsis: 988.148 km

Periapsis: 702.823 km

RAAN: 152.399 deg

Eccentricy: 0.0197495

Argument of periapsis: 185.8514 deg

Mean anomaly: 174.0349 deg

Mean motion: 14.14068294 rev/day

Mean motion (dot): 0.00000877 rev/day2

B* drag term: 0.00040307 1/REarth

Two-line elements (TLE)

Creation date: April 27, 2025, 6:35 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: April 27, 2025, 8:22 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 35322U 99057SA 25117.34861844 .00000877 00000-0 40307-3 0 9998

TLE line 2: 2 35322 99.1338 152.3990 0197495 185.8514 174.0349 14.14068294612394

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
FENGYUN 1C DEB SSO 2025-04-24 04:40:10 0.0008830125 26.0 (m) DEBRIS
DELTA 1 DEB SSO 2024-11-11 09:26:12 0.0001482895 866.0 (m) DEBRIS
DELTA 1 R/B SSO 2024-10-03 09:20:05 0.0001042384 268.0 (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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