STARLINK-30969 (58438)

COSPAR: 2023-183B | Alt Name: Starlink 30969

Image
STARLINK-30969 Satellite Image
Additional Sources
Launch Details

Launch Date

November 28, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58438

International Designator

2023-183B

Epoch

Sun, 19 Jul 2026 20:00:34 GMT

Apogee

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Perigee

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Inclination

43.01°

Right Ascension

15.38°

Eccentricity

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Argument of Perigee

275.46°

Period

94.27 min

Mean Motion

15.28 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

STARLINK-30969

Alternative Name

Starlink 30969

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58438U 23183B   26200.83372947  .00003675  00000+0  14298-3 0  9995
2 58438  43.0054  15.3769 0002041 275.4576  84.6043 15.27586619146949

Source: Celestrak

Summary
STARLINK-30969 is a Starlink V2M satellite, configured as a Starlink v2 Mini, launched on November 28, 2023, from LC40 at AFETR using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. The satellite's dry mass is 700 kg, and its launch mass was 730 kg. Equipped with a Ku/Ka/E-band payload and optical inter-satellite link, it uses Argon ion thrusters for propulsion and solar arrays along with batteries for power supply. Operated by SPXS, the primary mission of this satellite is communication within the Starlink Group 6-30-02 constellation.

Starlink is a satellite constellation developed by SpaceX with the aim of providing global broadband internet coverage. Thousands of small satellites are deployed in low Earth orbit (LEO), enabling high-speed internet access even in remote areas. However, the rapid increase in satellites raises concerns about space debris and the potential for collisions, which can lead to further debris creation and endanger other spacecraft. Additionally, the sheer number of Starlink satellites can affect astronomical observations by increasing light pollution. Proper deorbiting plans and international coordination are essential to mitigate these challenges and ensure long-term sustainability in space.
Physical Characteristics

Length

0.3

Diameter

4.1

Span

29

Dry Mass

700

Launch Mass

730

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 6-30-02

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Starlink v2 Mini

Motor

Argon ion thrusters

Equipment

Ku/Ka/E-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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