CZ-2D R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

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

Uptime

2533

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: 96.547 minutes

Inclination: 97.6189 deg

SMA: 6971.412 km

Apoapsis: 602.788 km

Periapsis: 583.766 km

RAAN: 166.5174 deg

Eccentricy: 0.0013643

Argument of periapsis: 75.5797 deg

Mean anomaly: 284.6935 deg

Mean motion: 14.91494467 rev/day

Mean motion (dot): 0.00004267 rev/day2

B* drag term: 0.00043097 1/REarth

Two-line elements (TLE)

Creation date: May 9, 2025, 2:46 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 8, 2025, 8:13 a.m. UTC

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

TLE line 1: 1 43486U 18048C 25128.34239035 .00004267 00000-0 43097-3 0 9998

TLE line 2: 2 43486 97.6189 166.5174 0013643 75.5797 284.6935 14.91494467374734

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
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 4 (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 4 (SLS-2 / 603)

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

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