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

9458

Days in orbit

Revolutions

≈ 14.8

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.3

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: 1999-057CN

Object number (NORAD): 26200

Object ID (CCSDS): 26200

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 97.59 minutes

Inclination: 98.2632 deg

SMA: 7021.486 km

Apoapsis: 674.678 km

Periapsis: 612.024 km

RAAN: 221.023 deg

Eccentricy: 0.0044616

Argument of periapsis: 139.334 deg

Mean anomaly: 221.1214 deg

Mean motion: 14.75567849 rev/day

Mean motion (dot): 0.00007043 rev/day2

B* drag term: 0.0010240522 1/REarth

Two-line elements (TLE)

Creation date: Sept. 4, 2025, 4:29 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 3, 2025, 9:20 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 26200U 99057CN 25246.88946094 .00007043 00000-0 10241-2 0 9991

TLE line 2: 2 26200 98.2632 221.0230 0044616 139.3340 221.1214 14.75567849354254

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
SL-14 R/B LEO 2025-09-04 04:12:46 0.001280762 215.0 (m) ROCKET BODY
GB 2 LEO 2025-03-25 00:59:37 0.0001026018 263.0 (m) PAYLOAD
ELECTRON KICK STAGE R/B LEO 2024-09-27 08:18:57 0.0003041699 584.0 (m) ROCKET BODY
AZUR (GRS A) SSO 2024-09-22 22:39:22 0.0001217719 686.0 (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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