STARLINK-30133 (56837)

COSPAR: 2023-079Q | Alt Name: Starlink 30133

Image
STARLINK-30133 Satellite Image
Additional Sources
Launch Details

Launch Date

June 4, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

56837

International Designator

2023-079Q

Epoch

Sun, 19 Jul 2026 17:02:33 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

81.07°

Eccentricity

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Argument of Perigee

260.12°

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-30133

Alternative Name

Starlink 30133

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 56837U 23079Q   26200.71011565  .00000245  00000+0  18428-4 0  9993
2 56837  43.0037  81.0711 0001240 260.1196  99.9515 15.27575243173086

Source: Celestrak

Summary
The satellite STARLINK-30133, also known as Starlink 30133, is a member of the Starlink v2 Mini configuration and part of the Starlink Group 6-4-15 payload. Launched on June 4, 2023, from Launch Complex 40 (LC40) at AFETR using a Falcon 9 launch vehicle, it was manufactured by SpaceX (SPXS). The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It operates as a communication satellite equipped with Ku/Ka/E-band payload and an optical inter-satellite link for data transmission. Its propulsion system utilizes Argon ion thrusters, while its power supply consists of solar arrays and batteries. The dry mass is 700 kg, and the launch mass was 730 kg.

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 6-4-15

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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