CZ-4C R/B

Satellite information

Favourite Embed

Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

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

Uptime

2617

Days in orbit

Revolutions

≈ 14.9

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.2

Latest

Satellite identification and parameters

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

Object identification

Identified? True

Debris? False

Object name: CZ-4C R/B

International designator: 2018-043B

Object number (NORAD): 43462

Object ID (CCSDS): 43462

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 96.897 minutes

Inclination: 98.2069 deg

SMA: 6988.222 km

Apoapsis: 670.474 km

Periapsis: 549.701 km

RAAN: 240.6897 deg

Eccentricy: 0.0086412

Argument of periapsis: 234.0133 deg

Mean anomaly: 125.3047 deg

Mean motion: 14.86115885 rev/day

Mean motion (dot): 0.00000606 rev/day2

B* drag term: 0.000071741 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 10:56 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 5:54 p.m. UTC

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

TLE line 1: 1 43462U 18043B 25187.74604755 .00000606 00000-0 71741-4 0 9992

TLE line 2: 2 43462 98.2069 240.6897 0086412 234.0133 125.3047 14.86115885387421

Live tracking on map

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

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
CZ-4 DEB SSO 2025-03-01 19:53:11 0.0002980562 549.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-11-02 11:14:02 0.0001609303 338.0 (m) DEBRIS

Associated space launch

Gaofen is a series of civilian Earth observation satellites developed and launched for the China High-definition Earth Observation System (CHEOS), a state-sponsored programme aimed to develop a near-real time, all-weather, global surveillance network consisting of satellite, near-space (stratosphere) airships, and aerial observation platforms. Based on the SAST5000B bus, Gaofen 5 will carry six types of payloads, including visible and short-wave infra hyper-spectral camera, spectral imager, greenhouse gas detector, atmospheric environment infrared detector at very high spectral resolution, differential absorption spectrometer for atmospheric trace gas, and multi-angle polarization detector. The satellite has a designed life of 8 years. It is to be launched atop of a Long March 4C to a 705km Sun Syncronous Orbit (SSO).

CZ-4C R/B was lifted into orbit during the mission ‘Long March 4C | Gaofen 5’, on board a Long March 4C space rocket.

The launch took place on May 8, 2018, 6:28 p.m. from Launch Complex 9.

For more information about the launch, click the button.

Launch to space Long March 4C | Gaofen 5
Long March 4C | Gaofen 5

Agency: N/A

Status: Launch Successful

Launch date: May 8, 2018, 6:28 p.m. UTC

Rocket: Long March 4C

Launch pad: Launch Complex 9

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.