FLOCK 4BE-9 (60514)

COSPAR: 2024-149AY | Alt Name: Flock 4be-9

Image
FLOCK 4BE-9 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

60514

International Designator

2024-149AY

Epoch

Sun, 19 Jul 2026 19:28:49 GMT

Apogee

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Perigee

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Inclination

97.38°

Right Ascension

285.42°

Eccentricity

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Argument of Perigee

159.17°

Period

93.40 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-9

Alternative Name

Flock 4be-9

Type

Payload

Status

Operational

Owner

PLAN

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60514U 24149AY  26200.81168058  .00011050  00000+0  26366-3 0  9995
2 60514  97.3785 285.4200 0003938 159.1744 200.9664 15.41712161107343

Source: Celestrak

Summary
FLOCK 4BE-9 is a CubeSat (3U) satellite manufactured by PLAN and owned by PLAN, designated for technology purposes. Launched on August 16, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle, it has dimensions of 0.3 meters in length with a span of 0.3 meters and a diameter of 0.1 meters. The satellite's dry mass is 5.7 kilograms, identical to its launch mass, indicating no significant propellant usage. It carries a Dove 250e payload with PS0, PS1, or PS2 imaging capabilities and relies on solar cells for power generation, complemented by batteries for energy storage. Its mission life expectancy ranges from about one year in ISS orbit to 2-3 years in Sun-Synchronous Orbit (SSO). The satellite has a box shape with two panels and no motor is installed except for some Flock-3p' variants using an FEEP propulsion system.
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 250e

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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