AOBA VELOX-III (41935)

COSPAR: 1998-067KX | Alt Name: AOBA-VeloxIII
DECAYED

Image
AOBA VELOX-III Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

Y2

Launch Vehicle

H-IIB

Orbital Elements

NORAD ID

41935

International Designator

1998-067KX

Decay Date

11/1/2018

Basic Satellite Info

Name

AOBA VELOX-III

Alternative Name

AOBA-VeloxIII

Type

Payload

Status

Decayed

Owner

KYUT/NTU

Country

Japan

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
AOBA VELOX-III is a CubeSat (2U) technology satellite launched on November 20, 1998, from the Tanegashima Space Center using a H-IIB launch vehicle. The spacecraft measures 0.2 meters in length and diameter with a span of 0.2 meters, has a dry mass of 2 kilograms, and was manufactured by KYUT/NTU. It operates on solar cells and batteries for power. The satellite's purpose is technology demonstration, and it has been stable since January 16, 2017, following its launch from pad Y2 with an expected lifetime of 6 months. Its shape is box-like with a radar cross-section (RCS) of 0.088 square meters. The owner and payload name are also AOBA-VeloxIII, indicating it was designed for technology testing purposes by KYUT/NTU.
Physical Characteristics

Length

0.2

Diameter

0.1

Span

0.2

Dry Mass

2

Launch Mass

2

Shape

Box

Radar Cross Section

0.088

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

AOBA-VeloxIII

Purpose

Technology

Mission

Technology

Manufacturer

KYUT/NTU

Life Expectancy

6 months

Bus

Cubesat 2U

Configuration

CubeSat (2U)

Motor

Unknown

Equipment

Unknown

Power System

Solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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