CZ-4B R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite CZ-4B R/B at a glance.

Uptime

9451

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.8

Latest

Satellite identification and parameters

Extended collection of information and parameters for CZ-4B R/B.

Object identification

Identified? True

Debris? False

Object name: CZ-4B R/B

International designator: 1999-057C

Object number (NORAD): 25942

Object ID (CCSDS): 25942

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.131 minutes

Inclination: 98.7673 deg

SMA: 7142.877 km

Apoapsis: 833.4 km

Periapsis: 696.083 km

RAAN: 282.7354 deg

Eccentricy: 0.00961216

Argument of periapsis: 4.6967 deg

Mean anomaly: 355.5099 deg

Mean motion: 14.38113062 rev/day

Mean motion (dot): 0.00000417 rev/day2

B* drag term: 0.00014541936 1/REarth

Two-line elements (TLE)

Creation date: Aug. 29, 2025, 2:15 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 28, 2025, 5:53 p.m. UTC

TLE line 0: 0 CZ-4B R/B

TLE line 1: 1 25942U 99057C 25240.74566017 .00000417 00000-0 14542-3 0 9992

TLE line 2: 2 25942 98.7673 282.7354 0096122 4.6967 355.5099 14.38113062353553

Live tracking on map

Real-time ground track for satellite CZ-4B R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object CZ-4B R/B.

Target Orbit TCA Probability of collision Miss distance Type
DMSP 5D-2 F11 DEB SSO 2025-07-06 11:33:10 0.0004947353 118.0 (m) DEBRIS
CZ-6A DEB SSO 2025-06-18 05:43:12 0.0001500403 720.0 (m) DEBRIS
CZ-6A DEB LEO 2025-04-23 04:26:33 0.0002170113 143.0 (m) DEBRIS
CZ-6A DEB SSO 2024-12-22 07:27:30 0.0001147651 937.0 (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-4B R/B 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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