ACS3 (59588)

COSPAR: 2024-077B | Alt Name: Advanced Composite Solar Sail System

Image
ACS3 Satellite Image
Launch Details

Launch Date

January 1, 45405

Launch Site

Rocket Lab Launch Complex 1, Māhia, New Zealand

Launch Pad

LC1B

Launch Vehicle

Electron

Orbital Elements

NORAD ID

59588

International Designator

2024-077B

Epoch

Sun, 19 Jul 2026 16:48:18 GMT

Apogee

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Perigee

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Inclination

97.18°

Right Ascension

112.29°

Eccentricity

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Argument of Perigee

31.31°

Period

103.19 min

Mean Motion

13.95 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

ACS3

Alternative Name

Advanced Composite Solar Sail System

Type

Payload

Status

Operational

Owner

NASA Ames Research Center

Country

United States

Constellation

N/A

Related Satellites

Major Events

2024-04-23: Launch; 2024-08-29: Successful deployment of solar sail; 2024-10-25: Detection of slight bend in one boom, mission continues.

Latest TLEs
1 59588U 24077B   26200.70021256  .00003608  00000+0  25000-2 0  9993
2 59588  97.1775 112.2879 0129376  31.3060 329.5729 13.95428126112578

Source: Celestrak

Summary
The ACS3 satellite, also known as the Advanced Composite Solar Sail System, is a CubeSat 12U technology demonstration satellite manufactured by Kongsberg NanoAvionics for NASA Ames Research Center. Launched on April 23, 2024, from Rocket Lab Launch Complex 1 in Māhia, New Zealand, using an Electron launch vehicle, the ACS3 has a length of 0.3 meters, diameter of 0.2 meters, and a span of 12.7 meters when deployed. The satellite's dry mass is 16.1 kg, equal to its launch mass. It uses solar cells and batteries for power and features advanced composite materials in its solar sail propulsion system with carbon fiber reinforced polymer booms coated with polyethylene naphthalate film and metals. The mission objectives include demonstrating the deployment and functionality of a solar sail for future small spacecraft missions. Key events include successful solar sail deployment on August 29, 2024, and detection of a slight bend in one boom on October 25, 2024, with ongoing mission operations continuing as of February 2025. The satellite is equipped with three-axis stabilization and has transmitter frequencies at 401.5 MHz and 2.268 GHz. Its shape is described as a box with a deployed sail, colored silver for the sail and white for the bus section.
Physical Characteristics

Length

0.3

Diameter

0.2

Span

12.7

Dry Mass

16.1

Launch Mass

16.1

Shape

Box with deployed sail

Radar Cross Section

Unknown

Visual Magnitude

2

Color

Silver (sail) and white (bus)

Material Composition

Polyethylene naphthalate film coated with aluminum and chromium; carbon fiber reinforced polymer booms.

Technical Details

Payload

Advanced Composite Solar Sail System

Purpose

Demonstrate the deployment and functionality of a solar sail using composite booms for future small spacecraft missions.

Mission

Technology demonstration of solar sail propulsion using advanced composite materials.

Manufacturer

Kongsberg NanoAvionics

Life Expectancy

Ongoing; mission operations continue as of February 2025.

Bus

CubeSat 12U

Configuration

CubeSat (12U)

Motor

None

Equipment

Solar sail

Power System

Solar cells and batteries

ADCS

Three-axis stabilization

Transmitter Frequency

401.5 MHz, 2.268 GHz

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