CZ-2D R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite CZ-2D R/B at a glance.

Uptime

2272

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.3

Latest

Satellite identification and parameters

Extended collection of information and parameters for CZ-2D R/B.

Object identification

Identified? True

Debris? False

Object name: CZ-2D R/B

International designator: 2019-063B

Object number (NORAD): 44548

Object ID (CCSDS): 44548

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.95 minutes

Inclination: 98.3257 deg

SMA: 7134.27 km

Apoapsis: 761.363 km

Periapsis: 750.907 km

RAAN: 301.4671 deg

Eccentricy: 0.0007328

Argument of periapsis: 8.711 deg

Mean anomaly: 351.4205 deg

Mean motion: 14.40716159 rev/day

Mean motion (dot): 0.000005 rev/day2

B* drag term: 0.00016986 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 7:16 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 11, 2025, 8:33 p.m. UTC

TLE line 0: 0 CZ-2D R/B

TLE line 1: 1 44548U 19063B 25345.85651992 .00000500 00000-0 16986-3 0 9996

TLE line 2: 2 44548 98.3257 301.4671 0007328 8.7110 351.4205 14.40716159326582

Live tracking on map

Real-time ground track for satellite CZ-2D R/B.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB SSO 2025-11-21 04:13:54 0.0001087587 468.0 (m) DEBRIS
SL-16 DEB LEO 2024-11-29 21:23:11 0.0001020783 196.0 (m) DEBRIS
CZ-6A DEB SSO 2024-10-27 13:48:15 0.0003497199 817.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-10-26 06:17:47 0.0002123517 447.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-09-09 20:51:54 0.0001560733 405.0 (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 R/B 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 94 (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 94 (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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