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

9452

Days in orbit

Revolutions

≈ 14.0

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.3

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: 1999-057AV

Object number (NORAD): 26159

Object ID (CCSDS): 26159

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 102.751 minutes

Inclination: 99.3351 deg

SMA: 7266.931 km

Apoapsis: 1105.869 km

Periapsis: 671.723 km

RAAN: 198.1343 deg

Eccentricy: 0.0298714

Argument of periapsis: 82.6477 deg

Mean anomaly: 335.2256 deg

Mean motion: 14.01445495 rev/day

Mean motion (dot): 0.00004015 rev/day2

B* drag term: 0.0018199032 1/REarth

Two-line elements (TLE)

Creation date: Aug. 29, 2025, 2:15 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 28, 2025, 7:44 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26159U 99057AV 25240.82233535 .00004015 00000-0 18199-2 0 9997

TLE line 2: 2 26159 99.3351 198.1343 0298714 82.6477 335.2256 14.01445495287043

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
BPA 1/SL-24 R/B SSO 2024-11-16 11:47:00 0.0001475056 902.0 (m) ROCKET BODY
DELTA 1 DEB SSO 2024-11-13 17:03:31 0.0001931195 708.0 (m) DEBRIS
DELTA 1 DEB SSO 2024-09-26 00:42:43 0.0001932634 246.0 (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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