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

2752

Days in orbit

Revolutions

≈ 15.0

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: 2018-048F

Object number (NORAD): 44619

Object ID (CCSDS): 44619

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 95.892 minutes

Inclination: 98.3045 deg

SMA: 6939.818 km

Apoapsis: 571.499 km

Periapsis: 551.867 km

RAAN: 175.3501 deg

Eccentricy: 0.00141443

Argument of periapsis: 114.1865 deg

Mean anomaly: 246.0838 deg

Mean motion: 15.01691289 rev/day

Mean motion (dot): 0.00011005 rev/day2

B* drag term: 0.00084922301 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 6:13 a.m. UTC

TLE line 0: 0 CZ-2D DEB

TLE line 1: 1 44619U 18048F 25346.25936784 .00011005 00000-0 84922-3 0 9994

TLE line 2: 2 44619 98.3045 175.3501 0014144 114.1865 246.0838 15.01691289403579

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
TIROS 5 LEO 2025-05-29 19:10:32 0.000254684 454.0 (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 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 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

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