FLOCK 1E-9 (40736)

COSPAR: 1998-067GN | Alt Name: Flock 1e-9
DECAYED

Image
FLOCK 1E-9 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

40736

International Designator

1998-067GN

Decay Date

2/8/2016

Basic Satellite Info

Name

FLOCK 1E-9

Alternative Name

Flock 1e-9

Type

Payload

Status

Decayed

Owner

PLABS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
FLOCK 1E-9, also known as Flock 1e-9, is a CubeSat (3U) technology satellite manufactured by PLABS and owned by the same entity. It was launched on November 20, 1998, from TYMSC LC40 using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length, 0.1 meter in diameter, and spans 0.3 meters with its solar panels deployed. With a dry mass of 4.5 kilograms and a launch mass of the same weight, it is equipped with PS0, PS1, or PS2 imaging payloads (Dove 0B1F) for technology demonstration purposes. Its operational lifetime ranges from about one year in an ISS orbit to two to three years in Sun-Synchronous Orbit (SSO). Power generation relies on solar cells and batteries, and its shape is described as a box with two panels. The satellite's radar cross-section (RCS) is 0.041 square meters.
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

0.041

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0B1F

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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