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

9507

Days in orbit

Revolutions

≈ 14.1

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.2

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: 1999-057M

Object number (NORAD): 26125

Object ID (CCSDS): 26125

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 102.034 minutes

Inclination: 99.2435 deg

SMA: 7233.07 km

Apoapsis: 1029.27 km

Periapsis: 680.601 km

RAAN: 323.3401 deg

Eccentricy: 0.02410242

Argument of periapsis: 224.631 deg

Mean anomaly: 202.9964 deg

Mean motion: 14.11298095 rev/day

Mean motion (dot): 0.00000681 rev/day2

B* drag term: 0.00030822401 1/REarth

Two-line elements (TLE)

Creation date: Oct. 24, 2025, 2:48 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 23, 2025, 11:31 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26125U 99057M 25296.97997220 .00000681 00000-0 30822-3 0 9998

TLE line 2: 2 26125 99.2435 323.3401 0241024 224.6310 202.9964 14.11298095309461

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-2D R/B SSO 2025-02-13 06:27:04 0.000208381 216.0 (m) ROCKET BODY
THOR ABLESTAR DEB LEO 2024-11-13 08:00:54 0.005911705 114.0 (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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