STARLINK-3608 (51776)

COSPAR: 2022-017J | Alt Name: Starlink 3608

Image
STARLINK-3608 Satellite Image
Additional Sources
Launch Details

Launch Date

February 25, 2022

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

51776

International Designator

2022-017J

Epoch

Mon, 20 Jul 2026 08:00:01 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

102.37°

Eccentricity

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Argument of Perigee

37.97°

Period

94.41 min

Mean Motion

15.25 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-3608

Alternative Name

Starlink 3608

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 51776U 22017J   26201.33335647  .00010971  00000+0  44230-3 0  9996
2 51776  53.1587 102.3717 0001055  37.9653  98.7298 15.25338860  5809

Source: Celestrak

Summary
The satellite named STARLINK-3608 (OBJECT_ID: 2022-017J) is a Starlink communication satellite launched on February 25, 2022, from the AFWTR site at SLC4E using a Falcon 9 launch vehicle. It has dimensions of 0.2 meters in length and 2.8 meters in diameter with a span of 9 meters. The satellite weighs 275 kilograms dry and was launched with a mass of 297 kilograms. Equipped with Ku/Ka-band payload and optical inter-satellite link, it also features krypton ion thrusters for propulsion. Power is supplied by solar arrays and batteries. The manufacturer and owner are SpaceX (SPXS).

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 4-11-09

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

Map
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