PREFIRE-1 (59965)

COSPAR: 2024-108A | Alt Name: PREFIRE 1

Image
PREFIRE-1 Satellite Image
Launch Details

Launch Date

January 1, 45448

Launch Site

Rocket Lab Launch Complex 1, Māhia, New Zealand

Launch Pad

Pad B

Launch Vehicle

Electron

Orbital Elements

NORAD ID

59965

International Designator

2024-108A

Epoch

Sun, 19 Jul 2026 09:02:03 GMT

Apogee

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Perigee

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Inclination

97.54°

Right Ascension

355.32°

Eccentricity

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Argument of Perigee

125.06°

Period

94.49 min

Mean Motion

15.24 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

PREFIRE-1

Alternative Name

PREFIRE 1

Type

Payload

Status

Operational

Owner

NASA

Country

United States

Constellation

N/A

Related Satellites

Major Events

Launch on June 5, 2024; commencement of data collection shortly thereafter.

Latest TLEs
1 59965U 24108A   26200.37643186  .00002457  00000+0  10440-3 0  9996
2 59965  97.5351 355.3152 0012583 125.0567 235.1852 15.23968209117498

Source: Celestrak

Summary
PREFIRE-1 is a 6U CubeSat satellite launched by NASA on June 5, 2024, from Rocket Lab Launch Complex 1 in Māhia, New Zealand, using an Electron launch vehicle. The spacecraft measures 0.3 meters in length with a dry mass of 3 kilograms and features three-axis stabilization for its operations. Equipped with a Thermal InfraRed Spectrometer (TIRS), it aims to measure far-infrared radiation from Earth's polar regions to improve understanding of Arctic warming, sea ice loss, and ice-sheet melting. The mission is designed to operate for approximately one year, covering one seasonal cycle. PREFIRE-1 was manufactured by NASA Jet Propulsion Laboratory (JPL) and is part of the Polar Radiant Energy in the Far InfraRed Experiment (PREFIRE). It provides climate models with enhanced data on Earth's energy budget through far-infrared emissions from polar regions, contributing significantly to climate predictions and monitoring.
Physical Characteristics

Length

0.3

Diameter

0.2

Span

12.7

Dry Mass

3

Launch Mass

10

Shape

Rectangular

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Thermal InfraRed Spectrometer (TIRS)

Purpose

To study the Earth's energy budget by measuring far-infrared emissions from polar regions, enhancing climate models and predictions.

Mission

The Polar Radiant Energy in the Far InfraRed Experiment (PREFIRE) aims to measure far-infrared radiation emitted from Earth's polar regions to improve understanding of Arctic warming, sea ice loss, and ice-sheet melting.

Manufacturer

NASA Jet Propulsion Laboratory (JPL)

Life Expectancy

The mission is designed to operate for approximately one year, covering one seasonal cycle.

Bus

6U CubeSat

Configuration

Unknown

Motor

Unknown

Equipment

Thermal InfraRed Spectrometer (TIRS), a pushbroom spectrometer with 64 channels measuring mid- and far-infrared radiation from approximately 5 to 54 µm.

Power System

Approximately 4.5 W

ADCS

Three-axis stabilization

Transmitter Frequency

Unknown

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