FLOCK 4BE-3 (60561)

COSPAR: 2024-149CX | Alt Name: Flock 4be-3

Image
FLOCK 4BE-3 Satellite Image
Additional Sources
Launch Details

Launch Date

August 16, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60561

International Designator

2024-149CX

Epoch

Sun, 19 Jul 2026 18:52:54 GMT

Apogee

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Perigee

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Inclination

97.37°

Right Ascension

285.03°

Eccentricity

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Argument of Perigee

155.49°

Period

93.36 min

Mean Motion

15.42 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot
3D Visualization
Basic Satellite Info

Name

FLOCK 4BE-3

Alternative Name

Flock 4be-3

Type

Payload

Status

Operational

Owner

PLAN

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60561U 24149CX  26200.78673810  .00010434  00000+0  24270-3 0  9997
2 60561  97.3685 285.0320 0005331 155.4929 204.6573 15.42489838107361

Source: Celestrak

Summary
The FLOCK 4BE-3 satellite, also known as Flock 4be-3, is a CubeSat (3U) configuration developed by PLAN and owned by the same entity. It was launched on August 16, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. The spacecraft measures 0.3 meters in length with a diameter of 0.1 meters and spans 0.3 meters. Its dry mass is 5.7 kg, which is the same as its launch mass. FLOCK 4BE-3 is equipped with PS0, PS1 or PS2 imaging payload technology and utilizes Dove 2500 payload for Earth observation. The satellite's power comes from solar cells and batteries. It has a box shape with two panels and no motor except for FEEP models in the #Flock-3p series. Its mission is primarily technological, focusing on space-based imaging capabilities. The expected operational lifetime of this satellite ranges from one year when operating 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

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 2500

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

Map
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