STARLINK-31117 (58776)

COSPAR: 2024-011M | Alt Name: Starlink 31117

Image
STARLINK-31117 Satellite Image
Additional Sources
Launch Details

Launch Date

January 14, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58776

International Designator

2024-011M

Epoch

Mon, 20 Jul 2026 04:33:37 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

118.43°

Eccentricity

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Argument of Perigee

74.30°

Period

94.10 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-31117

Alternative Name

Starlink 31117

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58776U 24011M   26201.19001613  .00004557  00000+0  16574-3 0  9999
2 58776  53.1591 118.4341 0001289  74.2991 285.8152 15.30231398140554

Source: Celestrak

Summary
STARLINK-31117 is a communication satellite, also known as Starlink 31117, belonging to the Starlink Group 7-10-12 payload and operating under the configuration of Starlink v2 Mini. Launched on January 14, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle, it has dimensions including a length of 0.3 meters, diameter of 4.1 meters, and span of 29 meters. The satellite's dry mass is 700 kg with a launch mass of 730 kg, and its equipment includes Ku/Ka/E-band payload and optical inter-satellite link capabilities. It utilizes solar arrays and batteries for power, Argon ion thrusters as motors, and operates under the ownership of SPXS (SpaceX) in the United States.

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 7-10-12

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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