FLOCK 1-6 (39519)

COSPAR: 1998-067DM | Alt Name: Flock 1-06
DECAYED

Image
FLOCK 1-6 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

Pad 0A

Launch Vehicle

Antares 120

Orbital Elements

NORAD ID

39519

International Designator

1998-067DM

Decay Date

6/15/2014

Basic Satellite Info

Name

FLOCK 1-6

Alternative Name

Flock 1-06

Type

Payload

Status

Decayed

Owner

PLABS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
The FLOCK 1-6 satellite, also known as Flock 1-06, is a CubeSat (3U) technology demonstration satellite owned and manufactured by Planet Labs (PLABS). Launched on November 20, 1998, from the Mid-Atlantic Regional Spaceport Complex (TYMSC), Pad 0A, it uses an Antares 120 launch vehicle. The satellite measures 0.3 meters in length with a diameter of 0.1 meters and a span of 0.3 meters. It has a dry mass of 4.25 kg and carries either PS0, PS1, or PS2 imaging payloads. FLOCK 1-6 is equipped with solar cells and batteries for power supply and was stabilized by February 13, 2014. Its mission focuses on technology demonstration, and its operational lifetime ranges from about a year in the International Space Station (ISS) orbit to 2-3 years in sun-synchronous orbit (SSO).
Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

4.25

Launch Mass

4.25

Shape

Box+2 pan

Radar Cross Section

0.0582

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0735

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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