STARLINK-30812 (58168)

COSPAR: 2023-166U | Alt Name: Starlink 30812

Image
STARLINK-30812 Satellite Image
Additional Sources
Launch Details

Launch Date

October 29, 2023

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58168

International Designator

2023-166U

Epoch

Sun, 19 Jul 2026 18:17:03 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

325.91°

Eccentricity

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Argument of Perigee

84.76°

Period

94.11 min

Mean Motion

15.30 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-30812

Alternative Name

Starlink 30812

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58168U 23166U   26200.76184314  .00000775  00000+0  38283-4 0  9996
2 58168  53.1590 325.9070 0001231  84.7586 275.3556 15.30201727153251

Source: Celestrak

Summary
STARLINK-30812 is a Starlink v2 Mini satellite (OBJECT_ID: 2023-166U) launched on October 29, 2023, from Space Launch Complex 4E at AFWTR using a Falcon 9 launch vehicle. The spacecraft measures 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters. It weighs 700 kilograms dry and was launched with a mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and optical inter-satellite link, the satellite uses Argon ion thrusters for propulsion and solar arrays along with batteries for power generation. Manufactured by SPXS, STARLINK-30812 is owned by SpaceX and operates in a communication mission as part of the Starlink Group 7-6-19 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 7-6-19

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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