CBERS 2B (32062)

COSPAR: 2007-042A | Alt Name: Zi Yuan 1-02B

Image
CBERS 2B Satellite Image
Additional Sources
Launch Details

Launch Date

September 19, 2007

Launch Site

TAISC

Launch Pad

LC7

Launch Vehicle

Chang Zheng 4B

Orbital Elements

NORAD ID

32062

International Designator

2007-042A

Epoch

Sat, 04 Jul 2026 02:23:35 GMT

Apogee

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Perigee

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Inclination

98.39°

Right Ascension

129.45°

Eccentricity

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Argument of Perigee

284.70°

Period

99.90 min

Mean Motion

14.41 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot
3D Visualization
Basic Satellite Info

Name

CBERS 2B

Alternative Name

Zi Yuan 1-02B

Type

Payload

Status

Non-operational

Owner

ZZWYZ/INPE

Country

China

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 32062U 07042A   26185.09971267  .00000270  00000-0  96118-4 0  9997
2 32062  98.3927 129.4546 0029754 284.7038  85.5945 14.41484874987121

Source: Celestrak

Summary
CBERS 2B (also known as Zi Yuan 1-02B) is an Earth observation satellite with a NORAD catalog ID of 32062 and object ID of 2007-042A. It was launched on September 19, 2007, from the Taiyuan Satellite Launch Center (TAISC) using a Chang Zheng 4B launch vehicle from launch pad LC7. The satellite operates with a Phoenix-Eye-1 bus configuration and has dimensions of 1.8 meters in length, 2 meters in diameter, and a span of 9 meters. It carries equipment including CCD, WFI, IRMSS (#01, 02), and HRC (#02B) sensors for Earth observation purposes. The satellite's dry mass is 1400 kg with a launch mass of 1450 kg. Its power system consists of deployable solar arrays and batteries. CBERS 2B has an expected operational lifetime of two years and was manufactured by CAST/INPE under the ownership of ZZWYZ/INPE. The mission is dedicated to Earth observation, utilizing an AOCS 20N motor for attitude control. Its shape can be described as a box with a pan configuration, and it has a radar cross-section (RCS) of 2.512 square meters.
Physical Characteristics

Length

1.8

Diameter

2

Span

9

Dry Mass

1400

Launch Mass

1450

Shape

Box + Pan

Radar Cross Section

2.512

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

ZY-1 02B

Purpose

Earth Observation

Mission

Earth Observation

Manufacturer

CAST/INPE

Life Expectancy

2 years

Bus

ZY

Configuration

Phoenix-Eye-1 bus

Motor

AOCS 20N

Equipment

CCD, WFI, IRMSS (#01, 02), HRC (#02B)

Power System

Deployable solar array, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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