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

2220

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.4

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: 2019-063C

Object number (NORAD): 44549

Object ID (CCSDS): 44549

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 100.037 minutes

Inclination: 98.3624 deg

SMA: 7138.41 km

Apoapsis: 789.788 km

Periapsis: 730.763 km

RAAN: 311.6066 deg

Eccentricy: 0.00413436

Argument of periapsis: 122.6214 deg

Mean anomaly: 237.8975 deg

Mean motion: 14.39462967 rev/day

Mean motion (dot): 0.00000885 rev/day2

B* drag term: 0.00029484414 1/REarth

Two-line elements (TLE)

Creation date: Oct. 22, 2025, 5:40 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 22, 2025, 7:59 a.m. UTC

TLE line 0: 0 CZ-2D DEB

TLE line 1: 1 44549U 19063C 25295.33330488 .00000885 00000-0 29484-3 0 9991

TLE line 2: 2 44549 98.3624 311.6066 0041344 122.6214 237.8975 14.39462967318483

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
FENGYUN 1C DEB SSO 2025-10-05 03:56:17 0.0001867702 86.0 (m) DEBRIS
NOAA 16 DEB SSO 2025-05-27 10:46:06 0.0001016021 919.0 (m) DEBRIS
RESURS O1 DEB SSO 2025-03-30 17:42:35 0.005077946 17.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-02-23 00:59:13 0.000212019 99.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-07-16 12:13:36 0.0001170273 88.0 (m) DEBRIS

Associated space launch

The Yunhai-1 satellite is designed for detecting environmental elements in the atmosphere and ocean, the space environment, disaster prevention and reduction, and scientific experimentation. It is made by the Shanghai Institute of Spaceflight Technology.

CZ-2D DEB was lifted into orbit during the mission ‘Long March 2D | Yunhai-1-02’, on board a Long March 2D space rocket.

The launch took place on Sept. 25, 2019, 12:54 a.m. from Launch Area 4 (SLS-2 / 603).

For more information about the launch, click the button.

Launch to space Long March 2D | Yunhai-1-02
Long March 2D | Yunhai-1-02

Agency: N/A

Status: Launch Successful

Launch date: Sept. 25, 2019, 12:54 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

...

Latest news about this satellite

News about space launch
Breakup of China’s Yunhai-1 (02) satellite linked to space debris collision

U.S. space tracking has linked the breakup of Chinese satellite Yunhai-1 (02) to a collision with a small piece of debris from a Russian satellite launch, according to NASA.


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