STARLINK-30782 (58137)

COSPAR: 2023-162V | Alt Name: Starlink 30782

Image
STARLINK-30782 Satellite Image
Additional Sources
Launch Details

Launch Date

October 22, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58137

International Designator

2023-162V

Epoch

Sun, 19 Jul 2026 04:06:25 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

110.10°

Eccentricity

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Argument of Perigee

264.56°

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-30782

Alternative Name

Starlink 30782

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58137U 23162V   26200.17112443  .00000041  00000+0  11007-4 0  9998
2 58137  43.0016 110.1018 0001083 264.5618  95.5110 15.27572991152418

Source: Celestrak

Summary
The Starlink-30782 satellite, identified by NORAD as CAT ID 58137 and OBJECT_ID 2023-162V, is a Starlink v2 Mini configuration manufactured by SpaceX (SPXS). Launched on October 22, 2023, from Cape Canaveral Air Force Station Launch Complex 40 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. It is equipped with Ku/Ka/E-band payload capabilities, an optical inter-satellite link, Argon ion thrusters for propulsion, solar arrays for power generation, and batteries as backup power sources. Its primary mission is communication.

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 6-24-20

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

Map
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