ODERACS 2B (23472)

COSPAR: 1995-004D | Alt Name: ODERACS 2B
DECAYED

Image
ODERACS 2B Satellite Image
Additional Sources
Launch Details

Launch Date

February 3, 1995

Launch Pad

LC39B

Launch Vehicle

Space Shuttle

Orbital Elements

NORAD ID

23472

International Designator

1995-004D

Decay Date

9/29/1995

Basic Satellite Info

Name

ODERACS 2B

Alternative Name

ODERACS 2B

Type

Payload

Status

Decayed

Owner

JSC

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
ODERACS 2B is a radar calibration satellite launched by JSC on February 3, 1995, from Launch Pad LC39B at AFETR using the Space Shuttle as the launch vehicle. The spacecraft has dimensions of 0.2 meters in length, diameter, and span, with a dry mass of 5 kg. It is equipped with a configuration that includes various-sized spheres and wire dipoles for radar calibration purposes. The satellite was stabilized by February 4, 1995, and does not have any onboard equipment or power systems. Its shape is spherical with a radar cross-section (RCS) of 0.0029 square meters.
Physical Characteristics

Length

0.2

Diameter

0.2

Span

0.2

Dry Mass

5

Launch Mass

5

Shape

Sphere

Radar Cross Section

0.0029

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

ODERACS 4 inch sphere

Purpose

Radar calibration

Mission

Radar calibration

Manufacturer

JSC

Life Expectancy

Unknown

Bus

ODERACS

Configuration

15 cm spheres (#A, B, 2A), 10 cm spheres (#C, D, 2B), 5 cm spheres (#E, F, 2C), 13.3 cm wire dipoles (#2D, 2E), 4.4 cm wire dipoles (#2F)

Motor

None

Equipment

None

Power System

None

ADCS

Unknown

Transmitter Frequency

Unknown

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