CZ-4C R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

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

Uptime

1107

Days in orbit

Revolutions

≈ 15.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.0

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: 2022-069B

Object number (NORAD): 52913

Object ID (CCSDS): 52913

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 94.371 minutes

Inclination: 97.959 deg

SMA: 6866.26 km

Apoapsis: 522.482 km

Periapsis: 453.768 km

RAAN: 140.2089 deg

Eccentricy: 0.0050038

Argument of periapsis: 221.5465 deg

Mean anomaly: 138.1964 deg

Mean motion: 15.25887056 rev/day

Mean motion (dot): 0.0000482 rev/day2

B* drag term: 0.00018475 1/REarth

Two-line elements (TLE)

Creation date: July 8, 2025, 2:27 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 7, 2025, 8:27 p.m. UTC

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

TLE line 1: 1 52913U 22069B 25188.85277002 .00004820 00000-0 18475-3 0 9996

TLE line 2: 2 52913 97.9590 140.2089 0050038 221.5465 138.1964 15.25887056167380

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
SL-3 R/B LEO 2025-02-25 11:09:37 0.0001161892 401.0 (m) ROCKET BODY
PEGASUS DEB LEO 2024-08-23 13:31:28 0.0001827931 950.0 (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.

CZ-4C R/B was lifted into orbit during the mission ‘Long March 4C | Gaofen-12-03’, on board a Long March 4C space rocket.

The launch took place on June 27, 2022, 3:46 p.m. from Launch Area 4 (SLS-2 / 603).

For more information about the launch, click the button.

Launch to space Long March 4C | Gaofen-12-03
Long March 4C | Gaofen-12-03

Agency: N/A

Status: Launch Successful

Launch date: June 27, 2022, 3:46 p.m. UTC

Rocket: Long March 4C

Launch pad: Launch Area 4 (SLS-2 / 603)

Location: Jiuquan Satellite Launch Center, People's Republic of China

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