FLOCK 4BE-26 (60484)

COSPAR: 2024-149S | Alt Name: Flock 4be-26

Image
FLOCK 4BE-26 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

60484

International Designator

2024-149S

Epoch

Sun, 19 Jul 2026 19:06:59 GMT

Apogee

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Perigee

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Inclination

97.36°

Right Ascension

288.70°

Eccentricity

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Argument of Perigee

206.56°

Period

91.19 min

Mean Motion

15.79 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-26

Alternative Name

Flock 4be-26

Type

Payload

Status

Partially operational

Owner

PLAN

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60484U 24149S   26200.79652448  .00174787  00000+0  96789-3 0  9992
2 60484  97.3603 288.7047 0003789 206.5603 153.5471 15.79079692107590

Source: Celestrak

Summary
The satellite FLOCK 4BE-26 (OBJECT_ID: 2024-149S) is a CubeSat (3U) technology demonstration satellite manufactured by PLAN in the US. It was launched on August 16, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite measures 0.3 meters in length and has a diameter of 0.1 meters with a span of 0.3 meters. Its dry mass is 5.7 kg, which is also its launch mass. It is equipped with a PS0, PS1 or PS2 imaging payload (Dove 24f0) for technology purposes. Power is provided by solar cells and batteries. The satellite's shape is described as Box+2 pan and it has no motor or RCS system noted. Its expected lifetime ranges from approximately one year in the ISS orbit to two to three 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 24f0

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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