FLOCK 1E-2 (40722)

COSPAR: 1998-067GE | Alt Name: Flock 1e-2
DECAYED

Image
FLOCK 1E-2 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

40722

International Designator

1998-067GE

Decay Date

3/5/2016

Basic Satellite Info

Name

FLOCK 1E-2

Alternative Name

Flock 1e-2

Type

Payload

Status

Decayed

Owner

PLABS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
The satellite FLOCK 1E-2 (OBJECT_ID: 1998-067GE) is a CubeSat (3U) configuration manufactured by PLABS in the US, designed primarily for technology demonstration purposes. It was launched on November 20, 1998, from Launch Pad LC40 at TYMSC using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters length and span with a diameter of 0.1 meters, and it weighs approximately 4.5 kg both at launch and dry mass. FLOCK 1E-2 is equipped with PS0, PS1 or PS2 imaging payload under the name Dove 0B10. It has solar cells for power generation alongside batteries. The satellite's shape consists of a box with two panels and its expected lifetime ranges from about one year in an ISS orbit to 2-3 years in Sun-Synchronous Orbit (SSO).
Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

4.5

Launch Mass

4.5

Shape

Box+2 pan

Radar Cross Section

0.075

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0B10

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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