CZ-4 DEB

Satellite information

Favourite Embed

Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite CZ-4 DEB at a glance.

Uptime

9505

Days in orbit

Revolutions

≈ 14.6

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.5

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: 1999-057SF

Object number (NORAD): 35327

Object ID (CCSDS): 35327

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.552 minutes

Inclination: 98.4724 deg

SMA: 7067.574 km

Apoapsis: 743.153 km

Periapsis: 635.725 km

RAAN: 8.6266 deg

Eccentricy: 0.0076001

Argument of periapsis: 149.7657 deg

Mean anomaly: 210.7961 deg

Mean motion: 14.61158121 rev/day

Mean motion (dot): 0.00005735 rev/day2

B* drag term: 0.0011282 1/REarth

Two-line elements (TLE)

Creation date: Oct. 17, 2025, 6:56 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 16, 2025, 10:51 a.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 35327U 99057SF 25289.45223852 .00005735 00000-0 11282-2 0 9993

TLE line 2: 2 35327 98.4724 8.6266 0076001 149.7657 210.7961 14.61158121677711

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
CSTB 1 SSO 2025-09-28 18:25:03 0.0001004864 421.0 (m) PAYLOAD
IRIDIUM 33 DEB LEO 2024-11-19 01:09:45 0.0001859778 101.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-10 11:32:43 0.0001567252 884.0 (m) DEBRIS
THOR BURNER 2 R/B SSO 2024-07-24 06:13:11 0.0003539449 96.0 (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

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.