CZ-2D DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite CZ-2D DEB at a glance.

Uptime

2703

Days in orbit

Revolutions

≈ 14.9

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.3

Latest

Satellite identification and parameters

Extended collection of information and parameters for CZ-2D DEB.

Object identification

Identified? True

Debris? True

Object name: CZ-2D DEB

International designator: 2018-048E

Object number (NORAD): 43490

Object ID (CCSDS): 43490

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 96.443 minutes

Inclination: 98.2505 deg

SMA: 6966.361 km

Apoapsis: 605.146 km

Periapsis: 571.306 km

RAAN: 87.6087 deg

Eccentricy: 0.00242881

Argument of periapsis: 201.3659 deg

Mean anomaly: 158.6547 deg

Mean motion: 14.93116737 rev/day

Mean motion (dot): 0.00009822 rev/day2

B* drag term: 0.00094196856 1/REarth

Two-line elements (TLE)

Creation date: Oct. 25, 2025, 3:11 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 24, 2025, 9:10 a.m. UTC

TLE line 0: 0 CZ-2D DEB

TLE line 1: 1 43490U 18048E 25297.38222936 .00009822 00000-0 94197-3 0 9995

TLE line 2: 2 43490 98.2505 87.6087 0024288 201.3659 158.6547 14.93116737398959

Live tracking on map

Real-time ground track for satellite CZ-2D DEB.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2024-11-25 06:01:48 0.000304816 316.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-11-10 19:14:56 0.0001250128 506.0 (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. Luojia-1 is a 6U Earth observation cubesat prototype.

CZ-2D DEB 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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