FLOCK 2E-2 (41484)

COSPAR: 1998-067JE | 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

41484

International Designator

1998-067JE

Decay Date

1/23/2018

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, also known as Flock 2e-2, is a CubeSat (3U) satellite manufactured by PLABS and launched on November 20, 1998, from the TYSMC launch site using an Atlas V 401 vehicle. It has dimensions of 0.3 meters in length and span with a diameter of 0.1 meters, weighing 5 kilograms at launch and dry mass. The satellite is equipped with PS0, PS1 or PS2 imaging payload and powered by solar cells along with batteries. Its primary mission is for technology purposes. It was stabilized on May 17, 2016, and its expected lifetime ranges from about one year in ISS orbit to two to three years in a Sun-Synchronous Orbit (SSO). The satellite's shape is described as "Box+2 pan" with an RCS of 0.0589 and ownership by PLABS. Its payload is identified as Dove 0C78, and it carries no motor except for the FEEP variant in #Flock-3p'.
Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

5

Launch Mass

5

Shape

Box+2 pan

Radar Cross Section

0.0589

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0C78

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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