NEONSAT-1 (59587)

COSPAR: 2024-077A | Alt Name: New-space Earth Observation Satellite-1

Image
NEONSAT-1 Satellite Image
Launch Details

Launch Date

January 1, 45405

Launch Site

Rocket Lab Launch Complex 1, Mahia, New Zealand

Launch Pad

LC1B

Launch Vehicle

Electron

Orbital Elements

NORAD ID

59587

International Designator

2024-077A

Epoch

Sun, 19 Jul 2026 20:22:05 GMT

Apogee

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Perigee

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Inclination

97.35°

Right Ascension

284.96°

Eccentricity

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Argument of Perigee

271.48°

Period

93.55 min

Mean Motion

15.39 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

NEONSAT-1

Alternative Name

New-space Earth Observation Satellite-1

Type

Payload

Status

Operational

Owner

Korea Advanced Institute of Science and Technology (KAIST)

Country

South Korea

Constellation

NEONSAT Constellation

Related Satellites

Major Events

Successfully launched on April 23, 2024, and established communication with ground stations shortly after deployment.

Latest TLEs
1 59587U 24077A   26200.84867213  .00006793  00000+0  17634-3 0  9991
2 59587  97.3480 284.9558 0006459 271.4783  88.5723 15.39288950124756

Source: Celestrak

Summary
NEONSAT-1, also known as New-space Earth Observation Satellite-1, is a nanosatellite designed by KAIST Satellite Technology Research Center (SaTReC) and owned by Korea Advanced Institute of Science and Technology (KAIST). It was launched on April 23, 2024, from Rocket Lab Launch Complex 1 in Mahia, New Zealand, using the Electron launch vehicle. NEONSAT-1 is box-shaped with deployable solar panels, measuring 1 meter in length, 0.5 meters in diameter, and weighing 100 kilograms at launch. The satellite is equipped with a high-resolution optical camera capable of capturing black-and-white images up to 1 meter resolution and color images up to 4 meters resolution. Its primary mission is Earth observation, focusing on monitoring natural disasters on the Korean Peninsula, providing high-resolution imagery to enhance surveillance capabilities and improve disaster response efforts. NEONSAT-1 operates with a 3-axis stabilization system and S-band/X-band communication systems for telemetry and payload data transmission. It has a planned mission duration of approximately two years and is part of the NEONSAT Constellation, which includes related satellites like NEONSAT-2 to NEONSAT-5.
Physical Characteristics

Length

1

Diameter

0.5

Span

1

Dry Mass

100

Launch Mass

100

Shape

Box-shaped with deployable solar panels.

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Predominantly metallic with solar panel arrays.

Material Composition

Constructed using lightweight aerospace-grade materials.

Technical Details

Payload

High-resolution optical imaging system.

Purpose

To enhance surveillance capabilities and improve responses to natural disasters by providing high-resolution imagery.

Mission

Earth observation with a focus on monitoring natural disasters on the Korean Peninsula.

Manufacturer

KAIST Satellite Technology Research Center (SaTReC)

Life Expectancy

Designed for a mission duration of approximately 2 years.

Bus

Neonsat

Configuration

Nanosatellite

Motor

Unknown

Equipment

High-resolution optical camera capable of capturing black-and-white images with a ground resolution of up to 1 meter and color images up to 4 meters.

Power System

Equipped with deployable solar arrays and batteries to power its systems.

ADCS

3-axis stabilization system.

Transmitter Frequency

S-band for telemetry and X-band for payload data transmission.

Map
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