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

9341

Days in orbit

Revolutions

≈ 14.6

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.4

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: 1999-057MM

Object number (NORAD): 27492

Object ID (CCSDS): 27492

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.78 minutes

Inclination: 98.4354 deg

SMA: 7078.459 km

Apoapsis: 758.126 km

Periapsis: 642.521 km

RAAN: 176.7852 deg

Eccentricy: 0.008166

Argument of periapsis: 190.0017 deg

Mean anomaly: 169.9559 deg

Mean motion: 14.57789155 rev/day

Mean motion (dot): 0.00004542 rev/day2

B* drag term: 0.00095913 1/REarth

Two-line elements (TLE)

Creation date: May 10, 2025, 5:27 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 9, 2025, 8:26 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 27492U 99057MM 25129.85173385 .00004542 00000-0 95913-3 0 9998

TLE line 2: 2 27492 98.4354 176.7852 0081660 190.0017 169.9559 14.57789155264585

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 2025-02-18 02:00:57 0.0001094587 426.0 (m) DEBRIS
PICOSAT 5 SSO 2025-01-06 08:14:34 0.00010682 326.0 (m) PAYLOAD
IRIDIUM 33 DEB LEO 2024-11-14 10:04:19 0.0001887771 50.0 (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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