CBERS 2

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite CBERS 2 at a glance.

Uptime

8033

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

Latest

Satellite identification and parameters

Extended collection of information and parameters for CBERS 2.

Object identification

Identified? True

Debris? False

Object name: CBERS 2

International designator: 2003-049A

Object number (NORAD): 28057

Object ID (CCSDS): 28057

Country: PEOPLES REPUBLIC OF CHINA/BRAZIL (CHBZ)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.237 minutes

Inclination: 98.7215 deg

SMA: 7147.909 km

Apoapsis: 770.974 km

Periapsis: 768.574 km

RAAN: 254.1299 deg

Eccentricy: 0.00016794

Argument of periapsis: 111.8134 deg

Mean anomaly: 248.323 deg

Mean motion: 14.36594645 rev/day

Mean motion (dot): 0.00000382 rev/day2

B* drag term: 0.00014542694 1/REarth

Two-line elements (TLE)

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

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 17, 2025, 9:31 p.m. UTC

TLE line 0: 0 CBERS 2

TLE line 1: 1 28057U 03049A 25290.89686048 .00000382 00000-0 14543-3 0 9998

TLE line 2: 2 28057 98.7215 254.1299 0001679 111.8134 248.3230 14.36594645152399

Live tracking on map

Real-time ground track for satellite CBERS 2.

In-orbit conjunctions

A list of the most updated potential collisions computed for object CBERS 2.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 1503 LEO 2025-06-26 23:20:30 0.000138195 182.0 (m) PAYLOAD
COSMOS 1375 DEB LEO 2025-02-07 01:35:02 0.001411037 141.0 (m) DEBRIS
SL-16 DEB LEO 2024-10-15 12:29:12 0.0001407078 398.0 (m) DEBRIS
IRIDIUM 33 DEB LEO 2024-06-26 12:50:04 0.0003141559 470.0 (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).

CBERS 2 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.

Launch to space Long March 4B | Zi Yuan 1-2
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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