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

2653

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: 96.022 minutes

Inclination: 98.2944 deg

SMA: 6946.074 km

Apoapsis: 577.789 km

Periapsis: 558.089 km

RAAN: 69.1634 deg

Eccentricy: 0.00141811

Argument of periapsis: 84.8769 deg

Mean anomaly: 275.4071 deg

Mean motion: 14.99662863 rev/day

Mean motion (dot): 0.00011899 rev/day2

B* drag term: 0.00096760068 1/REarth

Two-line elements (TLE)

Creation date: Sept. 4, 2025, 4:29 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 3, 2025, 6:34 p.m. UTC

TLE line 0: 0 CZ-2D DEB

TLE line 1: 1 44619U 18048F 25246.77392501 .00011899 00000-0 96760-3 0 9997

TLE line 2: 2 44619 98.2944 69.1634 0014181 84.8769 275.4071 14.99662863388658

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 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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