OPTUS B3 (23227)

COSPAR: 1994-055A | Alt Name: Optus B3

Image
OPTUS B3 Satellite Image
Additional Sources
Launch Details

Launch Date

August 27, 1994

Launch Site

XICLF

Launch Pad

LC2

Launch Vehicle

Chang Zheng 2E

Orbital Elements

NORAD ID

23227

International Designator

1994-055A

Epoch

Thu, 02 Jul 2026 15:09:06 GMT

Apogee

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Perigee

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Inclination

12.38°

Right Ascension

30.22°

Eccentricity

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Argument of Perigee

38.70°

Period

1459.04 min

Mean Motion

0.99 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

OPTUS B3

Alternative Name

Optus B3

Type

Payload

Status

Non-operational

Owner

OPT

Country

Australia

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 23227U 94055A   26183.63132660  .00000029  00000-0  00000-0 0  9997
2 23227  12.3823  30.2161 0005995  38.7036 325.3537  0.98695182116076

Source: Celestrak

Summary
OPTUS B3 is a communication satellite launched by OPT on August 27, 1994, from Xichang Satellite Launch Center using a Chang Zheng 2E launch vehicle. The spacecraft measures 2.3 meters in length and diameter with a span of 20.6 meters. It has a dry mass of 1582 kilograms and was equipped with 15 Ku-band transponders, 1 L-band transponder, Ka-band beacon, and laser retroreflector for communication purposes. The satellite's launch mass was 2858 kilograms, and it stabilized on August 28, 1994. Its power system consists of two deployable solar arrays and batteries. It was manufactured by HSES and has a box plus two panel shape with a radar cross-section (RCS) value of 26.3778 square meters. The satellite's intended operational lifetime is ten years, serving communication purposes in Australia.
Physical Characteristics

Length

2.3

Diameter

2.3

Span

20.6

Dry Mass

1582

Launch Mass

2858

Shape

Box + 2 Pan

Radar Cross Section

26.3778

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Optus B3

Purpose

Communication

Mission

Communication

Manufacturer

HSES

Life Expectancy

10 years

Bus

HS-601

Configuration

HS-601

Motor

R-4D-11-300

Equipment

15 Ku-band transponders, 1 L-band tranponder, Ka-band beacon, laser retroreflector

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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