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

3160

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.6

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: 2016-068B

Object number (NORAD): 41858

Object ID (CCSDS): 41858

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.212 minutes

Inclination: 98.6204 deg

SMA: 7146.706 km

Apoapsis: 792.937 km

Periapsis: 744.205 km

RAAN: 187.0087 deg

Eccentricy: 0.0034094

Argument of periapsis: 123.7608 deg

Mean anomaly: 236.6834 deg

Mean motion: 14.36957322 rev/day

Mean motion (dot): 0.00000164 rev/day2

B* drag term: 0.000069855 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 10:36 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 8:55 p.m. UTC

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

TLE line 1: 1 41858U 16068B 25187.87167379 .00000164 00000-0 69855-4 0 9996

TLE line 2: 2 41858 98.6204 187.0087 0034094 123.7608 236.6834 14.36957322453371

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
NOAA 16 DEB SSO 2025-05-22 00:00:23 0.0001375267 613.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-11 00:42:01 0.0001313752 984.0 (m) DEBRIS
CZ-4 DEB SSO 2025-02-13 06:27:04 0.000208381 216.0 (m) DEBRIS
DMSP 5D-2 F11 DEB SSO 2024-11-15 16:13:38 0.0001073243 288.0 (m) DEBRIS
SL-14 DEB LEO 2024-10-14 21:59:34 0.0001861661 121.0 (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 1-01’, on board a Long March 2D space rocket.

The launch took place on Nov. 11, 2016, 11:14 p.m. from Launch Area 4 (SLS-2 / 603).

For more information about the launch, click the button.

Launch to space Long March 2D | YunHai 1-01
Long March 2D | YunHai 1-01

Agency: N/A

Status: Launch Successful

Launch date: Nov. 11, 2016, 11:14 p.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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