FLOCK 1E-1 (40723)

COSPAR: 1998-067GF | Alt Name: Flock 1e-1
DECAYED

Image
FLOCK 1E-1 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

40723

International Designator

1998-067GF

Decay Date

5/18/2016

Basic Satellite Info

Name

FLOCK 1E-1

Alternative Name

Flock 1e-1

Type

Payload

Status

Decayed

Owner

PLABS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
FLOCK 1E-1, also known as Flock 1e-1, is a CubeSat (3U) satellite manufactured by PLABS and launched on November 20, 1998, from the TYNMC LC40 launch pad using a Falcon 9 vehicle. The satellite measures 0.3 meters in length, has a diameter of 0.1 meters, and spans 0.3 meters. It weighs approximately 4.5 kilograms both at launch and dry mass. Equipped with a PS0, PS1, or PS2 imaging payload known as Dove 0B1A, FLOCK 1E-1 serves a technology mission. The satellite's power supply includes solar cells and batteries, and its shape is described as box+2 pan. Its expected operational lifetime varies from about one year in the International Space Station (ISS) orbit to two to three years in sun-synchronous orbit (SSO).
Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

4.5

Launch Mass

4.5

Shape

Box+2 pan

Radar Cross Section

0.063

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0B1A

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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