FLOCK 2B-2 (40951)

COSPAR: 1998-067HC | Alt Name: Flock 2b-2

DECAYED

Image

Additional Sources

Launch Details

Launch Date

November 20, 1998

Launch Site

Tyuratam Missile and Space Complex

Launch Pad

Launch Vehicle

H-IIB

Orbital Elements

NORAD ID

40951

International Designator

1998-067HC

Decay Date

10/2/2016

Basic Satellite Info

Name

FLOCK 2B-2

Alternative Name

Flock 2b-2

Type

Payload

Status

Decayed

Owner

PLABS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary

The FLOCK 2B-2 satellite, also known as Flock 2b-2, is a CubeSat (3U) technology mission satellite manufactured by PLABS and owned by the same entity. It was launched on November 20, 1998, from TYMSC Launch Site Y2 using an H-IIB launch vehicle. The satellite has dimensions of 0.3 meters in length and diameter, with a span of 0.3 meters. Weighing approximately 5 kilograms at launch, it carries a PS0, PS1 or PS2 imaging payload named Dove 0C18. Its power is derived from solar cells and batteries. The satellite has a calculated RCS of 0.079 and is shaped as a box with two panels. It was stabilized by October 6, 2015, after its launch. The expected lifetime varies between about one year for an ISS orbit or 2-3 years for SSO (Sun-Synchronous Orbit).

Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

Launch Mass

Shape

Box+2 pan

Radar Cross Section

0.079

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0C18

Purpose

Technology

Mission

Technology

Manufacturer

PLABS

Life Expectancy

~ 1 year (ISS orbit); 2-3 years (SSO)

Bus

Cubesat 3U

Configuration

CubeSat (3U)

Motor

None (most); FEEP (#Flock-3p')

Equipment

PS0, PS1 or PS2 imaging payload

Power System

Solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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