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

9399

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.6

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: 1999-057NB

Object number (NORAD): 28071

Object ID (CCSDS): 28071

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 100.398 minutes

Inclination: 98.5916 deg

SMA: 7155.575 km

Apoapsis: 853.536 km

Periapsis: 701.345 km

RAAN: 114.9891 deg

Eccentricy: 0.0106344

Argument of periapsis: 195.2652 deg

Mean anomaly: 231.1017 deg

Mean motion: 14.3428652 rev/day

Mean motion (dot): 0.00000079 rev/day2

B* drag term: 0.000041753 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, 1:19 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 28071U 99057NB 25187.05515257 .00000079 00000-0 41753-4 0 9991

TLE line 2: 2 28071 98.5916 114.9891 0106344 195.2652 231.1017 14.34286520196948

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 2024-10-31 06:50:36 0.0002168168 482.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-08-06 16:05:53 0.000158262 106.0 (m) DEBRIS
DMSP 5D-3 F18 DEB SSO 2024-07-22 15:57:11 0.0001173402 329.0 (m) DEBRIS
CZ-4B R/B SSO 2024-06-24 01:58:51 0.0004148903 95.0 (m) ROCKET BODY

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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