FLOCK 1E-3 (40725)

COSPAR: 1998-067GH | Alt Name: Flock 1e-3
DECAYED

Image
FLOCK 1E-3 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

40725

International Designator

1998-067GH

Decay Date

5/29/2016

Basic Satellite Info

Name

FLOCK 1E-3

Alternative Name

Flock 1e-3

Type

Payload

Status

Decayed

Owner

PLABS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
FLOCK 1E-3 is a CubeSat (3U) satellite launched on November 20, 1998, from TYMSC LC40 using a Falcon 9 launch vehicle. It was manufactured by PLABS and has dimensions of 0.3 meters in length and diameter, with a span of 0.3 meters. The satellite weighs 4.5 kilograms at launch and is equipped with PS0, PS1 or PS2 imaging payload technology under the name Dove 0C03. It primarily serves technological purposes and operates on solar cells and batteries for power. The satellite has been stable since July 14, 2015, and its expected lifetime ranges from about one year in an ISS orbit to two to three years in a 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

0.081

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0C03

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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