CZ-4B DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite CZ-4B DEB at a glance.

Uptime

8453

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

Latest

Satellite identification and parameters

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

Object identification

Identified? True

Debris? True

Object name: CZ-4B DEB

International designator: 2002-024E

Object number (NORAD): 28438

Object ID (CCSDS): 28438

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.569 minutes

Inclination: 98.6507 deg

SMA: 7116.125 km

Apoapsis: 751.383 km

Periapsis: 724.598 km

RAAN: 193.2248 deg

Eccentricy: 0.001882

Argument of periapsis: 85.8385 deg

Mean anomaly: 274.4957 deg

Mean motion: 14.46230033 rev/day

Mean motion (dot): 0.00003145 rev/day2

B* drag term: 0.00088934 1/REarth

Two-line elements (TLE)

Creation date: July 4, 2025, 6:39 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 4, 2025, 11:14 a.m. UTC

TLE line 0: 0 CZ-4B DEB

TLE line 1: 1 28438U 02024E 25185.46872501 .00003145 00000-0 88934-3 0 9995

TLE line 2: 2 28438 98.6507 193.2248 0018820 85.8385 274.4957 14.46230033203950

Live tracking on map

Real-time ground track for satellite CZ-4B DEB.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-06-05 00:19:26 0.0004433212 18.0 (m) DEBRIS
TSX-5 LEO 2025-04-19 14:26:41 0.0001113728 789.0 (m) PAYLOAD
IRIDIUM 24 LEO 2025-01-10 06:01:44 0.0002007421 747.0 (m) PAYLOAD
SL-8 R/B LEO 2024-12-07 17:40:54 0.0001096118 824.0 (m) ROCKET BODY
SL-8 R/B LEO 2024-06-19 03:30:33 0.0002309824 86.0 (m) ROCKET BODY

Associated space launch

HaiYang abbreviated HY, is a series of marine remote sensing satellites developed and operated by China since 2002. As of June 2020, six satellites were launched and two more are planned. Feng Yun 1D was a polar orbiting meteorological satellite.

CZ-4B DEB was lifted into orbit during the mission ‘Long March 4B | Hai Yang 1 & Feng Yun 1D’, on board a Long March 4B space rocket.

The launch took place on May 15, 2002, 1:50 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 4B | Hai Yang 1 & Feng Yun 1D
Long March 4B | Hai Yang 1 & Feng Yun 1D

Agency: N/A

Status: Launch Successful

Launch date: May 15, 2002, 1:50 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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