FLOCK 2E'-2 (41481)

COSPAR: 1998-067JB | Alt Name: Flock 2e'-2
DECAYED

Image
FLOCK 2E'-2 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

SLC41

Launch Vehicle

Atlas V 401

Orbital Elements

NORAD ID

41481

International Designator

1998-067JB

Decay Date

12/1/2017

Basic Satellite Info

Name

FLOCK 2E'-2

Alternative Name

Flock 2e'-2

Type

Payload

Status

Decayed

Owner

PLABS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
FLOCK 2E'-2 is a CubeSat (3U) technology satellite manufactured by PLABS and owned by the same entity. Launched on November 20, 1998, from TYMSC using an Atlas V 401 launch vehicle from SLC41, this US satellite weighs 5 kilograms both dry and at launch. Its dimensions are a length of 0.3 meters, diameter of 0.1 meters, and span of 0.3 meters. The satellite is equipped with PS0, PS1 or PS2 imaging payload under the Dove 0C1B configuration and operates on solar cells with batteries for power storage. It has no motor unless specified as FEEP (#Flock-3p'). Its shape consists of a box with two panels. The expected operational lifetime varies between about one year in ISS orbit to 2-3 years in SSO.
Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

5

Launch Mass

5

Shape

Box+2 pan

Radar Cross Section

0.0944

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0C1B

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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