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

9558

Days in orbit

Revolutions

≈ 14.6

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: 1999-057AR

Object number (NORAD): 26155

Object ID (CCSDS): 26155

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.522 minutes

Inclination: 98.5643 deg

SMA: 7066.153 km

Apoapsis: 776.412 km

Periapsis: 599.623 km

RAAN: 39.6756 deg

Eccentricy: 0.01250959

Argument of periapsis: 354.5039 deg

Mean anomaly: 34.9375 deg

Mean motion: 14.61598976 rev/day

Mean motion (dot): 0.0001356 rev/day2

B* drag term: 0.0024466347 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 2:36 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26155U 99057AR 25346.10849492 .00013560 00000-0 24466-2 0 9995

TLE line 2: 2 26155 98.5643 39.6756 0125096 354.5039 34.9375 14.61598976342055

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
IRIDIUM 38 LEO 2025-06-30 07:42:05 0.000344672 619.0 (m) PAYLOAD
TAURUS R/B LEO 2025-06-26 16:48:26 0.0001318881 78.0 (m) ROCKET BODY
UWE-1 SSO 2025-03-02 12:52:39 0.0001339755 558.0 (m) PAYLOAD
CZ-6A DEB LEO 2024-12-20 08:36:52 0.0004320087 268.0 (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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