STARLINK-30820 (58190)

COSPAR: 2023-167R | Alt Name: Starlink 30820

Image
STARLINK-30820 Satellite Image
Additional Sources
Launch Details

Launch Date

October 30, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58190

International Designator

2023-167R

Epoch

Sun, 19 Jul 2026 03:29:15 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

120.65°

Eccentricity

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Argument of Perigee

255.75°

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-30820

Alternative Name

Starlink 30820

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58190U 23167R   26200.14531704  .00000485  00000+0  27146-4 0  9997
2 58190  43.0019 120.6544 0000692 255.7453 104.3322 15.27578868151090

Source: Celestrak

Summary
The satellite STARLINK-30820, also known as Starlink 30820, is a communication satellite belonging to the Starlink v2 Mini configuration. Launched on October 30, 2023 from Launch Complex 40 at Cape Canaveral Air Force Station using a Falcon 9 launch vehicle, this satellite has a bus type of Starlink V2M and measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. It was manufactured by SpaceX (SPXS) and is owned by the same entity. The dry mass of the satellite is 700 kilograms, while its launch mass was 730 kilograms. Equipped with Argon ion thrusters for propulsion and solar arrays along with batteries for power generation, it features a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. The shape of the satellite is described as "Box + pan" without specific color details or RCS values provided.

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 6-25-16

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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