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

2049

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: 99.962 minutes

Inclination: 98.2951 deg

SMA: 7134.806 km

Apoapsis: 761.094 km

Periapsis: 752.247 km

RAAN: 86.8804 deg

Eccentricy: 0.00062

Argument of periapsis: 312.3661 deg

Mean anomaly: 47.7003 deg

Mean motion: 14.40553949 rev/day

Mean motion (dot): 0.00000438 rev/day2

B* drag term: 0.00015071 1/REarth

Two-line elements (TLE)

Creation date: May 5, 2025, 2:11 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 4, 2025, 10:05 p.m. UTC

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

TLE line 1: 1 44548U 19063B 25124.92053415 .00000438 00000-0 15071-3 0 9999

TLE line 2: 2 44548 98.2951 86.8804 0006200 312.3661 47.7003 14.40553949294779

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
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
PSLV R/B SSO 2024-08-15 20:02:50 0.0001583635 662.0 (m) ROCKET BODY

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 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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