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

2988

Days in orbit

Revolutions

≈ 15.0

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

97.5

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: 2017-060B

Object number (NORAD): 44609

Object ID (CCSDS): 44609

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 96.108 minutes

Inclination: 97.549 deg

SMA: 6950.253 km

Apoapsis: 593.789 km

Periapsis: 550.447 km

RAAN: 6.6124 deg

Eccentricy: 0.00311803

Argument of periapsis: 212.7346 deg

Mean anomaly: 147.1946 deg

Mean motion: 14.98310454 rev/day

Mean motion (dot): 0.00010928 rev/day2

B* drag term: 0.00091297004 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, 8:16 a.m. UTC

TLE line 0: 0 CZ-2D DEB

TLE line 1: 1 44609U 17060B 25347.34450785 .00010928 00000-0 91297-3 0 9995

TLE line 2: 2 44609 97.5490 6.6124 0031180 212.7346 147.1946 14.98310454437337

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
SL-14 R/B LEO 2024-09-27 20:24:14 0.002615257 253.0 (m) ROCKET BODY
GP-B LEO 2024-08-10 09:16:30 0.0003031203 290.0 (m) PAYLOAD

Associated space launch

VRSS-2 is the second Venezuelan remote sensing satellite. Spacecraft was built by China. Weighing about 1000 kg, it is to operate in sun-synchronous orbit at an altitude of 645 kilometres, providing services in traffic management, disaster warning and prevention, tracking agriculture and land use.

CZ-2D DEB was lifted into orbit during the mission ‘Long March 2D | VRSS-2 (Antonio José de Sucre)’, on board a Long March 2D space rocket.

The launch took place on Oct. 9, 2017, 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 | VRSS-2 (Antonio José de Sucre)
Long March 2D | VRSS-2 (Antonio José de Sucre)

Agency: N/A

Status: Launch Successful

Launch date: Oct. 9, 2017, 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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