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

≈ 14.7

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.4

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: 1999-057HV

Object number (NORAD): 26336

Object ID (CCSDS): 26336

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 97.884 minutes

Inclination: 98.3863 deg

SMA: 7035.58 km

Apoapsis: 694.681 km

Periapsis: 620.209 km

RAAN: 235.8206 deg

Eccentricy: 0.0052925

Argument of periapsis: 200.2017 deg

Mean anomaly: 159.7095 deg

Mean motion: 14.71136215 rev/day

Mean motion (dot): 0.00003828 rev/day2

B* drag term: 0.00061737 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, 2:36 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26336U 99057HV 25187.60878727 .00003828 00000-0 61737-3 0 9996

TLE line 2: 2 26336 98.3863 235.8206 0052925 200.2017 159.7095 14.71136215334861

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
LIBERTAD 1 SSO 2025-06-04 05:59:29 0.0001937718 254.0 (m) PAYLOAD
IRIDIUM 33 DEB LEO 2024-11-14 04:10:15 0.001598008 101.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-09-25 17:09:00 0.0004822446 135.0 (m) DEBRIS
CZ-4 DEB SSO 2024-06-25 08:12:20 0.00021541 225.0 (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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