FLOCK 4V-25 (46812)

COSPAR: 2020-061BP | Alt Name: Flock 4v-25
DECAYED

Image
FLOCK 4V-25 Satellite Image
Additional Sources
Launch Details

Launch Date

September 3, 2020

Launch Site

FRGUI

Launch Pad

ZLV

Launch Vehicle

Vega

Orbital Elements

NORAD ID

46812

International Designator

2020-061BP

Decay Date

3/3/2024

Basic Satellite Info

Name

FLOCK 4V-25

Alternative Name

Flock 4v-25

Type

Payload

Status

Decayed

Owner

PLAN

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
FLOCK 4V-25, also known as Flock 4v-25, is a CubeSat (3U) technology satellite manufactured by PLAN and owned by the same entity. It was launched on September 3, 2020, from the FRGUI site using the Vega launch vehicle at ZLV pad. 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 5.7 kilograms, which is identical to its launch mass. It is equipped with a Dove 240c payload that includes PS0, PS1 or PS2 imaging equipment. Power comes from solar cells and batteries. FLOCK 4V-25's shape consists of a box with two panels and it has no motor, except for those in the #Flock-3p' variant which use FEEP (Field-Emission Electric Propulsion). The satellite is expected to operate for about one year in an International Space Station orbit or between 2 to 3 years in Sun-Synchronous Orbit (SSO).
Physical Characteristics

Length

0.3

Diameter

0.1

Span

0.3

Dry Mass

5.7

Launch Mass

5.7

Shape

Box+2 pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Dove 240c

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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