STARLINK-3312 (50850)

COSPAR: 2022-001AZ | Alt Name: Starlink 3312

Image
STARLINK-3312 Satellite Image
Additional Sources
Launch Details

Launch Date

January 6, 2022

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

50850

International Designator

2022-001AZ

Epoch

Sun, 19 Jul 2026 10:35:52 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

265.47°

Eccentricity

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Argument of Perigee

56.46°

Period

94.57 min

Mean Motion

15.23 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-3312

Alternative Name

Starlink 3312

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 50850U 22001AZ  26200.44157826  .00007269  00000+0  32242-3 0  9999
2 50850  53.1605 265.4692 0001474  56.4583 303.6555 15.22620161251282

Source: Celestrak

Summary
The STARLINK-3312 satellite, also known as Starlink 3312, is part of the Starlink constellation owned by SPXS (SpaceX). It was launched on January 6, 2022, from LC39A at AFETR using a Falcon 9 launch vehicle. This communication satellite has dimensions of 0.2 meters in length and 2.8 meters in diameter with a span of 9 meters. The satellite carries a Ku/Ka-band payload along with an optical inter-satellite link and is powered by solar arrays and batteries. It weighs approximately 275 kg dry, with a launch mass of 297 kg. Equipped with Krypton ion thrusters for maneuvering, STARLINK-3312's mission is to provide communication services as part of the Starlink Group 4-5-48 constellation segment.

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

0.2

Diameter

2.8

Span

9

Dry Mass

275

Launch Mass

297

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 4-5-48

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink

Configuration

Unknown

Motor

Krypton ion thrusters

Equipment

Ku/Ka-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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