STARLINK-32630 (62047)

COSPAR: 2024-216R | Alt Name: Starlink 32630

Image
STARLINK-32630 Satellite Image
Additional Sources
Launch Details

Launch Date

November 21, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62047

International Designator

2024-216R

Epoch

Sun, 19 Jul 2026 09:20:48 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

239.79°

Eccentricity

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Argument of Perigee

276.49°

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-32630

Alternative Name

Starlink 32630

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62047U 24216R   26200.38945233  .00009848  00000+0  36736-3 0  9997
2 62047  42.9971 239.7949 0002403 276.4868  83.5710 15.27537598 93936

Source: Celestrak

Summary
The satellite designated STARLINK-32630 (OBJECT_ID: 2024-216R) is a Starlink v2 Mini spacecraft built by SPXS for communication purposes. It was launched on November 21, 2024, from LC40 at AFETR 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. Its dry mass is 700 kg and it had a launch mass of 730 kg. It is equipped with Ku/Ka/E-band payload, optical inter-satellite link, and Argon ion thrusters for propulsion. The satellite's power system includes solar arrays and batteries.

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 6-66-16

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

Map
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