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

9343

Days in orbit

Revolutions

≈ 14.8

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: 1999-057EY

Object number (NORAD): 26262

Object ID (CCSDS): 26262

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 97.627 minutes

Inclination: 98.35 deg

SMA: 7023.286 km

Apoapsis: 675.315 km

Periapsis: 614.987 km

RAAN: 213.1664 deg

Eccentricy: 0.0042948

Argument of periapsis: 346.4119 deg

Mean anomaly: 132.9194 deg

Mean motion: 14.75000699 rev/day

Mean motion (dot): 0.00007592 rev/day2

B* drag term: 0.0011193 1/REarth

Two-line elements (TLE)

Creation date: May 12, 2025, 10:16 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 12, 2025, 5:21 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26262U 99057EY 25132.72332997 .00007592 00000-0 11193-2 0 9993

TLE line 2: 2 26262 98.3500 213.1664 0042948 346.4119 132.9194 14.75000699328624

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-4C R/B SSO 2025-03-01 19:53:11 0.0002980562 549.0 (m) ROCKET BODY
CZ-6A DEB LEO 2025-02-21 11:23:23 0.0002687704 510.0 (m) DEBRIS
CZ-2C R/B SSO 2024-12-19 17:47:58 0.0001777668 71.0 (m) ROCKET BODY
CZ-6A DEB LEO 2024-09-28 14:21:14 0.0001709324 439.0 (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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