STARLINK-30762 (58197)

COSPAR: 2023-167Y | Alt Name: Starlink 30762

Image
STARLINK-30762 Satellite Image
Additional Sources
Launch Details

Launch Date

October 30, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58197

International Designator

2023-167Y

Epoch

Sun, 19 Jul 2026 03:09:06 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

121.40°

Eccentricity

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Argument of Perigee

264.66°

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-30762

Alternative Name

Starlink 30762

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58197U 23167Y   26200.13132345 -.00000789  00000+0 -19127-4 0  9990
2 58197  43.0046 121.3982 0001898 264.6634  95.4001 15.27574288151085

Source: Celestrak

Summary
The satellite named STARLINK-30762 (OBJECT_ID: 2023-167Y) is a Starlink V2M configuration belonging to the Starlink v2 Mini series, launched by SpaceX on October 30, 2023, from Cape Canaveral Air Force Station's 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 weighs 700 kilograms dry and had a launch mass of 730 kilograms. Equipped with Ku/Ka/E-band payload, optical inter-satellite link, and Argon ion thrusters for propulsion, it is powered by solar arrays and batteries. Its primary mission is communication, and it was stabilized on October 31, 2023.

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 6-25-23

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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