CZ-2D R/B

Satellite information

Favourite Embed

Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite CZ-2D R/B at a glance.

Uptime

2752

Days in orbit

Revolutions

≈ 14.9

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

97.6

Latest

Satellite identification and parameters

Extended collection of information and parameters for CZ-2D R/B.

Object identification

Identified? True

Debris? False

Object name: CZ-2D R/B

International designator: 2018-048C

Object number (NORAD): 43486

Object ID (CCSDS): 43486

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 96.4 minutes

Inclination: 97.5979 deg

SMA: 6964.301 km

Apoapsis: 595.223 km

Periapsis: 577.11 km

RAAN: 18.2238 deg

Eccentricy: 0.00130039

Argument of periapsis: 65.4843 deg

Mean anomaly: 294.7732 deg

Mean motion: 14.93779271 rev/day

Mean motion (dot): 0.00008805 rev/day2

B* drag term: 0.00083384812 1/REarth

Two-line elements (TLE)

Creation date: Dec. 14, 2025, 3:07 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 13, 2025, 9:04 a.m. UTC

TLE line 0: 0 CZ-2D R/B

TLE line 1: 1 43486U 18048C 25347.37790196 .00008805 00000-0 83385-3 0 9990

TLE line 2: 2 43486 97.5979 18.2238 0013004 65.4843 294.7732 14.93779271407404

Live tracking on map

Real-time ground track for satellite CZ-2D R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object CZ-2D R/B.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-07-28 01:04:08 0.0001251622 834.0 (m) DEBRIS
COSMOS 2228 LEO 2025-01-29 06:44:16 0.0002863062 525.0 (m) PAYLOAD

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. Luojia-1 is a 6U Earth observation cubesat prototype.

CZ-2D R/B was lifted into orbit during the mission ‘Long March 2D | Gaofen 6 & Luojia-1’, on board a Long March 2D space rocket.

The launch took place on June 2, 2018, 4:13 a.m. from Launch Area 94 (SLS-2 / 603).

For more information about the launch, click the button.

Launch to space Long March 2D | Gaofen 6 & Luojia-1
Long March 2D | Gaofen 6 & Luojia-1

Agency: N/A

Status: Launch Successful

Launch date: June 2, 2018, 4:13 a.m. UTC

Rocket: Long March 2D

Launch pad: Launch Area 94 (SLS-2 / 603)

Location: Jiuquan 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.