FLOCK 2E'-6 (41568)

COSPAR: 1998-067JS | Alt Name: Flock 2e'-6
DECAYED

Image
FLOCK 2E'-6 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

SLC41

Launch Vehicle

Atlas V 401

Orbital Elements

NORAD ID

41568

International Designator

1998-067JS

Decay Date

4/5/2018

Basic Satellite Info

Name

FLOCK 2E'-6

Alternative Name

Flock 2e'-6

Type

Payload

Status

Decayed

Owner

PLAN

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
FLOCK 2E'-6, also known as Flock 2e'-6, is a CubeSat (3U) satellite with dimensions of 0.3 meters in length and diameter, and spans 0.3 meters. It has a dry mass and launch mass of 5 kilograms each. The satellite was launched on November 20, 1998, from the TYSMC SLC41 launch pad using an Atlas V 401 launch vehicle. Manufactured by PLAN, FLOCK 2E'-6's mission is for technology demonstration and it carries a PS0, PS1, or PS2 imaging payload called Dove 0C46. It primarily relies on solar cells and batteries for power supply. The satellite's shape consists of a box with two panels and its reflective surface area (RCS) is 0.089 square meters. Its operational lifetime varies from about one year in ISS orbit to 2-3 years in Sun-Synchronous Orbit (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

0.089

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0C46

Purpose

Technology

Mission

Technology

Manufacturer

PLAN

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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