STARLINK-33549 (62289)

COSPAR: 2024-237Y | Alt Name: Starlink 33549

Image
STARLINK-33549 Satellite Image
Additional Sources
Launch Details

Launch Date

December 8, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62289

International Designator

2024-237Y

Epoch

Sun, 19 Jul 2026 15:57:01 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

191.22°

Eccentricity

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Argument of Perigee

281.07°

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-33549

Alternative Name

Starlink 33549

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62289U 24237Y   26200.66459830  .00008714  00000+0  32567-3 0  9991
2 62289  43.0005 191.2179 0002407 281.0703  78.9877 15.27593319 91376

Source: Celestrak

Summary
The satellite STARLINK-33549 (OBJECT_ID: 2024-237Y) is a Starlink V2MO spacecraft launched by SpaceX on December 8, 2024, from the Cape Canaveral Space Force Station Launch Complex 40 using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters, indicating the presence of deployable structures such as solar panels or antennas. It weighs approximately 500 kilograms dry mass and had a launch mass of 530 kilograms. The satellite's shape is described as "Box + pan." It belongs to the Starlink Group 12-5-23 payload, aimed at enhancing SpaceX's internet connectivity 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

500

Launch Mass

530

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 12-5-23

Purpose

Unknown

Mission

Unknown

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2MO

Configuration

Unknown

Motor

Unknown

Equipment

Unknown

Power System

Unknown

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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