CHUANG XIN 1 (CZ-1)

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite CHUANG XIN 1 (CZ-1) at a glance.

Uptime

8033

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.5

Latest

Satellite identification and parameters

Extended collection of information and parameters for CHUANG XIN 1 (CZ-1).

Object identification

Identified? True

Debris? False

Object name: CHUANG XIN 1 (CZ-1)

International designator: 2003-049B

Object number (NORAD): 28058

Object ID (CCSDS): 28058

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 99.42 minutes

Inclination: 98.5267 deg

SMA: 7109.032 km

Apoapsis: 739.502 km

Periapsis: 722.292 km

RAAN: 182.6449 deg

Eccentricy: 0.0012104

Argument of periapsis: 193.744 deg

Mean anomaly: 166.3425 deg

Mean motion: 14.48395095 rev/day

Mean motion (dot): 0.00000423 rev/day²

B* drag term: 0.00012493708 1/R_Earth

Two-line elements (TLE)

Creation date: Oct. 18, 2025, 2:17 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 17, 2025, 3:29 p.m. UTC

TLE line 0: 0 CHUANG XIN 1 (CZ-1)

TLE line 1: 1 28058U 03049B 25290.64579897 .00000423 00000-0 12494-3 0 9994

TLE line 2: 2 28058 98.5267 182.6449 0012104 193.7440 166.3425 14.48395095161162

Live tracking on map

Real-time ground track for satellite CHUANG XIN 1 (CZ-1).

In-orbit conjunctions

A list of the most updated potential collisions computed for object CHUANG XIN 1 (CZ-1).

Target	Orbit	TCA	Probability of collision	Miss distance	Type
FENGYUN 1C DEB	SSO	2025-06-29 20:37:37	0.0001073317	824.0 (m)	DEBRIS
COSMOS 2251 DEB	LEO	2025-06-06 18:45:15	0.0002515997	196.0 (m)	DEBRIS
COSMOS 2251 DEB	LEO	2025-05-10 18:28:10	0.0001236769	588.0 (m)	DEBRIS
IRIDIUM 33 DEB	LEO	2025-04-18 04:58:53	0.0005659935	160.0 (m)	DEBRIS
NOAA 16 DEB	SSO	2024-12-31 14:21:45	0.001180707	40.0 (m)	DEBRIS

Associated space launch

The satellite is China's first operational civilian remote-sensing satellite, specifically designed for the Chinese Ministry of Land and Resources (MLR).

CHUANG XIN 1 (CZ-1) was lifted into orbit during the mission ‘Long March 4B | Zi Yuan 1-2’, on board a Long March 4B space rocket.

The launch took place on Oct. 21, 2003, 3:16 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Long March 4B | Zi Yuan 1-2

Agency: N/A

Status: Launch Successful

Launch date: Oct. 21, 2003, 3:16 a.m. UTC

Rocket: Long March 4B

Launch pad: Launch Complex 7

Location: Taiyuan Satellite Launch Center, People's Republic of China

...

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Latest news about this satellite

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