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

9345

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

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: 1999-057NF

Object number (NORAD): 28075

Object ID (CCSDS): 28075

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.838 minutes

Inclination: 98.6697 deg

SMA: 7128.945 km

Apoapsis: 819.226 km

Periapsis: 682.394 km

RAAN: 185.7104 deg

Eccentricy: 0.0095969

Argument of periapsis: 310.4175 deg

Mean anomaly: 48.867 deg

Mean motion: 14.42330809 rev/day

Mean motion (dot): 0.00001016 rev/day2

B* drag term: 0.00030543 1/REarth

Two-line elements (TLE)

Creation date: May 12, 2025, 7:41 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 12, 2025, 2:30 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 28075U 99057NF 25132.10420553 .00001016 00000-0 30543-3 0 9991

TLE line 2: 2 28075 98.6697 185.7104 0095969 310.4175 48.8670 14.42330809676358

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
OV3-3 LEO 2025-04-18 17:09:42 0.003714901 36.0 (m) PAYLOAD

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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