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

3269

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: 100.207 minutes

Inclination: 98.6279 deg

SMA: 7146.499 km

Apoapsis: 792.231 km

Periapsis: 744.496 km

RAAN: 295.3199 deg

Eccentricy: 0.00333974

Argument of periapsis: 162.1131 deg

Mean anomaly: 198.1239 deg

Mean motion: 14.37019949 rev/day

Mean motion (dot): 0.00000273 rev/day2

B* drag term: 0.0001064122 1/REarth

Two-line elements (TLE)

Creation date: Oct. 23, 2025, 2:46 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 22, 2025, 10:30 p.m. UTC

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

TLE line 1: 1 41858U 16068B 25295.93758898 .00000273 00000-0 10641-3 0 9994

TLE line 2: 2 41858 98.6279 295.3199 0033397 162.1131 198.1239 14.37019949468892

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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