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

≈ 14.1

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.1

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: 1999-057E

Object number (NORAD): 26118

Object ID (CCSDS): 26118

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 102.046 minutes

Inclination: 99.1467 deg

SMA: 7233.64 km

Apoapsis: 1058.696 km

Periapsis: 652.313 km

RAAN: 234.6243 deg

Eccentricy: 0.0280898

Argument of periapsis: 233.9323 deg

Mean anomaly: 123.5532 deg

Mean motion: 14.1113141 rev/day

Mean motion (dot): 0.00001648 rev/day2

B* drag term: 0.0006517 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, 1:31 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26118U 99057E 25187.56357459 .00001648 00000-0 65170-3 0 9996

TLE line 2: 2 26118 99.1467 234.6243 0280898 233.9323 123.5532 14.11131410293046

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
PEGASUS DEB LEO 2025-02-08 22:58:21 0.001504112 31.0 (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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