FLOCK 1E-4 (40724)

COSPAR: 1998-067GG | Alt Name: Flock 1e-4
DECAYED

Image
FLOCK 1E-4 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

40724

International Designator

1998-067GG

Decay Date

6/24/2016

Basic Satellite Info

Name

FLOCK 1E-4

Alternative Name

Flock 1e-4

Type

Payload

Status

Decayed

Owner

PLABS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
FLOCK 1E-4 is a CubeSat (3U) satellite built by PLABS for technology demonstration purposes and owned by the same entity. It was launched on November 20, 1998, from the TYMSC launch site using Falcon 9 as the launch vehicle. The satellite measures 0.3 meters in length with a diameter of 0.1 meters and has a span of 0.3 meters. Its dry mass is 4.5 kg, which is also its launch mass. Equipped with either PS0, PS1, or PS2 imaging payload known as Dove 0C06, it relies on solar cells and batteries for power. FLOCK 1E-4 has a shape described as Box+2 pan and an RCS (Reflectivity Cross Section) of 0.063 square meters. The satellite's operational lifetime is approximately one year when in ISS orbit and two to three years in SSO (Sun-Synchronous Orbit).
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 0C06

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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