FLOCK 2E'-15 (41764)

COSPAR: 1998-067KL | Alt Name: Flock 2e'-15
DECAYED

Image
FLOCK 2E'-15 Satellite Image
Additional Sources
Launch Details

Launch Date

November 20, 1998

Launch Pad

SLC41

Launch Vehicle

Atlas V 401

Orbital Elements

NORAD ID

41764

International Designator

1998-067KL

Decay Date

11/10/2018

Basic Satellite Info

Name

FLOCK 2E'-15

Alternative Name

Flock 2e'-15

Type

Payload

Status

Decayed

Owner

PLAN

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
FLOCK 2E'-15, also known as Flock 2e'-15, is a CubeSat (3U) satellite manufactured by PLAN and owned by the same entity. It was launched on November 20, 1998, from TYMSC using an Atlas V 401 launch vehicle from SLC41. The satellite has dimensions of 0.3 meters in length, 0.1 meters in diameter, and a span of 0.3 meters. Its dry mass is 5 kg, the same as its launch mass. It carries a PS0, PS1, or PS2 imaging payload and is powered by solar cells with batteries for energy storage. The satellite's mission is technology-focused and it does not have a motor except in cases like #Flock-3p' which uses FEEP. Its shape consists of a box with two panels, and its RCS (reflectivity) value is 0.0964. The satellite became stable on September 14, 2016, and it operates within the technology domain for a lifetime ranging from about one year in an ISS orbit to 2-3 years in SSO.
Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

5

Launch Mass

5

Shape

Box+2 pan

Radar Cross Section

0.0964

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 0C54

Purpose

Technology

Mission

Technology

Manufacturer

PLAN

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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