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

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

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: 1999-057U

Object number (NORAD): 26132

Object ID (CCSDS): 26132

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.227 minutes

Inclination: 98.657 deg

SMA: 7099.807 km

Apoapsis: 798.245 km

Periapsis: 645.1 km

RAAN: 265.7713 deg

Eccentricy: 0.0107851

Argument of periapsis: 250.9467 deg

Mean anomaly: 177.0968 deg

Mean motion: 14.51218854 rev/day

Mean motion (dot): 0.00003635 rev/day2

B* drag term: 0.00086066 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, 11:34 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26132U 99057U 25187.48210744 .00003635 00000-0 86066-3 0 9993

TLE line 2: 2 26132 98.6570 265.7713 0107851 250.9467 177.0968 14.51218854317678

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 2025-06-25 17:19:04 0.0001305701 52.0 (m) DEBRIS
CZ-6A DEB LEO 2025-03-07 14:30:42 0.0001120212 191.0 (m) DEBRIS
OSCAR 18 (WEBERSAT) SSO 2025-01-21 00:11:17 0.0009219332 131.0 (m) PAYLOAD
COSMOS 1275 DEB LEO 2024-10-26 09:36:08 0.0005714807 25.0 (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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