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

9338

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.6

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: 1999-057KT

Object number (NORAD): 26446

Object ID (CCSDS): 26446

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.498 minutes

Inclination: 98.5984 deg

SMA: 7112.742 km

Apoapsis: 801.522 km

Periapsis: 667.693 km

RAAN: 188.6053 deg

Eccentricy: 0.0094077

Argument of periapsis: 267.473 deg

Mean anomaly: 91.569 deg

Mean motion: 14.47261995 rev/day

Mean motion (dot): 0.00001911 rev/day2

B* drag term: 0.00050755 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 10:11 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26446U 99057KT 25127.42458062 .00001911 00000-0 50755-3 0 9997

TLE line 2: 2 26446 98.5984 188.6053 0094077 267.4730 91.5690 14.47261995312323

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
CZ-6A DEB LEO 2025-03-18 21:54:18 0.0002431779 45.0 (m) DEBRIS
CZ-6A DEB LEO 2024-12-28 16:44:55 0.0001075685 317.0 (m) DEBRIS
PEGASUS DEB LEO 2024-11-11 04:42:34 0.005587966 36.0 (m) DEBRIS
THORAD AGENA D DEB LEO 2024-08-02 03:52:22 0.0001362263 100.0 (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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