NUVIEW BRAVO (62457)

COSPAR: 2024-252D | Alt Name: NuView Bravo

Image
NUVIEW BRAVO Satellite Image
Launch Details

Launch Date

December 29, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

SLC-40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62457

International Designator

2024-252D

Epoch

Mon, 20 Jul 2026 05:53:28 GMT

Apogee

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Perigee

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Inclination

0.07°

Right Ascension

168.10°

Eccentricity

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Argument of Perigee

337.19°

Period

1436.09 min

Mean Motion

1.00 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

NUVIEW BRAVO

Alternative Name

NuView Bravo

Type

Payload

Status

Operational

Owner

Anuvu

Country

United States

Constellation

Anuvu Constellation

Related Satellites

Major Events

Launched on December 29, 2024, as part of a dedicated Falcon 9 mission carrying four Astranis MicroGEO satellites.

Latest TLEs
1 62457U 24252D   26201.24546909 -.00000217  00000+0  00000+0 0  9998
2 62457   0.0675 168.0997 0001767 337.1854 157.9963 01.00272387  4123

Source: Celestrak

Summary
NUVIEW BRAVO, also known as NuView Bravo, is a high throughput satellite (HTS) manufactured by Astranis and owned by Anuvu. It was launched on December 29, 2024, from Cape Canaveral Space Force Station using a Falcon 9 launch vehicle at SLC-40 pad. The satellite has dimensions of 1.5 meters in length and diameter with a span of 10 meters when its solar arrays are deployed. Weighing 400 kilograms at launch, it is designed to operate for 8 to 10 years, providing high-performance connectivity over North America and the Caribbean. Equipped with software-defined radios (SDRs) and digital channelizers, NUVIEW BRAVO supports in-flight and maritime communications through its Ku-band payload. The satellite is powered by solar arrays and batteries and employs electric propulsion for orbit maintenance. It uses three-axis stabilization for precise orientation control. Constructed from aluminum and composite materials, the spacecraft has a silver color and a box shape with 22-panel solar arrays. NUVIEW BRAVO operates as part of the Anuvu Constellation alongside related satellites like NUVIEW ALPHA and AGILA.
Physical Characteristics

Length

1.5

Diameter

1.5

Span

10

Dry Mass

400

Launch Mass

400

Shape

Box with 22-panel solar arrays

Radar Cross Section

41.175

Visual Magnitude

5

Color

Silver

Material Composition

Aluminum and composite materials

Technical Details

Payload

High Throughput Communications Payload

Purpose

Unknown

Mission

To provide high-performance connectivity over North America and the Caribbean, supporting in-flight and maritime communications.

Manufacturer

Astranis

Life Expectancy

8 to 10 years

Bus

MicroGEO

Configuration

High Throughput Satellite (HTS)

Motor

Electric Propulsion (EP)

Equipment

Equipped with software-defined radios (SDRs) and digital channelizers to optimize on-orbit capacity and power.

Power System

Powered by solar arrays with batteries for energy storage.

ADCS

Three-axis stabilization

Transmitter Frequency

Ku-band

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