FLOCK 4Q-28 (58280)

COSPAR: 2023-174AA | Alt Name: Flock 4q-28

Image
FLOCK 4Q-28 Satellite Image
Additional Sources
Launch Details

Launch Date

November 11, 2023

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58280

International Designator

2023-174AA

Epoch

Sun, 19 Jul 2026 18:41:11 GMT

Apogee

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Perigee

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Inclination

97.39°

Right Ascension

293.09°

Eccentricity

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Argument of Perigee

49.03°

Period

92.49 min

Mean Motion

15.57 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 4Q-28

Alternative Name

Flock 4q-28

Type

Payload

Status

Operational

Owner

PLAN

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58280U 23174AA  26200.77860257  .00017833  00000+0  24889-3 0  9997
2 58280  97.3874 293.0930 0004380  49.0281 311.1352 15.56935935150810

Source: Celestrak

Summary
FLOCK 4Q-28, also known as Flock 4q-28, is a CubeSat (3U) technology satellite launched on November 11, 2023, 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. It is owned by PLAN and manufactured by PLAN as well. The dry mass and launch mass are both 5.7 kg, equipped with solar cells and batteries for power generation. Its primary payload is the Dove 24f6 imaging system capable of PS0, PS1, or PS2 imaging. The satellite's mission life expectancy is approximately one year when in ISS orbit and two to three years in Sun-Synchronous Orbit (SSO). The shape of FLOCK 4Q-28 is described as a box with two panels.
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 24f6

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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