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

≈ 14.7

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.1

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: 1999-057CG

Object number (NORAD): 26194

Object ID (CCSDS): 26194

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.007 minutes

Inclination: 98.1308 deg

SMA: 7041.491 km

Apoapsis: 694.311 km

Periapsis: 632.4 km

RAAN: 81.9375 deg

Eccentricy: 0.0043961

Argument of periapsis: 179.4223 deg

Mean anomaly: 304.1698 deg

Mean motion: 14.69284387 rev/day

Mean motion (dot): 0.00002692 rev/day2

B* drag term: 0.00045825 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, 10:23 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26194U 99057CG 25127.43286309 .00002692 00000-0 45825-3 0 9990

TLE line 2: 2 26194 98.1308 81.9375 0043961 179.4223 304.1698 14.69284387585288

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
COSMOS 192 LEO 2024-10-23 16:52:35 0.0001522014 417.0 (m) PAYLOAD
COSMOS 2251 DEB LEO 2024-08-02 17:27:47 0.0001548923 128.0 (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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