Thuraya 4-NGS (62483)

COSPAR: 2025-001A | Alt Name: Thuraya 4 Next Generation Satellite

Image
Thuraya 4-NGS Satellite Image
Launch Details

Launch Date

January 4, 2025

Launch Site

Cape Canaveral Space Force Station

Launch Pad

SLC-40

Launch Vehicle

Falcon 9 Block 5

Orbital Elements

NORAD ID

62483

International Designator

2025-001A

Epoch

Sun, 19 Jul 2026 20:13:50 GMT

Apogee

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Perigee

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Inclination

0.02°

Right Ascension

76.11°

Eccentricity

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Argument of Perigee

335.73°

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

Thuraya 4-NGS

Alternative Name

Thuraya 4 Next Generation Satellite

Type

Payload

Status

Operational

Owner

Space42

Country

United Arab Emirates

Constellation

Thuraya

Related Satellites

Major Events

Launched on January 4, 2025, Thuraya 4-NGS is expected to commence operational services after reaching its designated geostationary orbit and completing in-orbit testing.

Latest TLEs
1 62483U 25001A   26200.84294183  .00000136  00000+0  00000+0 0  9998
2 62483   0.0201  76.1083 0000031 335.7287 233.5563 01.00272319  4503

Source: Celestrak

Summary
Thuraya 4-NGS (2025-001A) is a geostationary satellite designed for advanced mobile satellite communication services, launched on January 4, 2025, from Cape Canaveral Space Force Station's SLC-40 launch pad using a Falcon 9 Block 5 rocket. Operated by Space42 and manufactured by Airbus Defence and Space, it is part of the Thuraya constellation and is based on the Eurostar NEO bus configuration. The satellite measures 8 meters in length with a diameter of 3 meters and spans up to 40 meters when its solar arrays are deployed. It has a dry mass of 5,000 kg and is equipped with high-capacity L-band transponders and a 12-meter L-band antenna, capable of handling up to 3,200 communication channels with dynamic power allocation across multiple spot beams. Thuraya 4-NGS features two deployable solar arrays generating approximately 20 kW of power, supported by rechargeable batteries. It is equipped with a PPS-5000 electric propulsion system and employs 3-axis stabilization using reaction wheels and star trackers for precise orbit control. The satellite’s equipment includes an advanced onboard processing unit to support secure voice, data, and video transmission services. Constructed primarily from lightweight aluminum and composite materials, the spacecraft has a box-shaped main body with large deployable antenna and solar arrays. Its design is intended to provide enhanced mobile satellite services across multiple regions for over 15 years.
Physical Characteristics

Length

8

Diameter

3

Span

40

Dry Mass

5000

Launch Mass

5000

Shape

Box-shaped main body with large deployable antenna and solar arrays

Radar Cross Section

Unknown

Visual Magnitude

Estimated at 8.0 based on size and reflectivity

Color

Predominantly white with company logos and markings

Material Composition

Constructed using lightweight aluminum and composite materials for the main structure, with a large mesh reflector for the antenna.

Technical Details

Payload

High-capacity L-band transponders

Purpose

Communication

Mission

To provide advanced mobile satellite communication services, including secure voice, data, and video transmission, supporting various sectors such as defense, government, and enterprise.

Manufacturer

Airbus Defence and Space

Life Expectancy

Designed for a mission life of over 15 years, providing enhanced mobile satellite services across multiple regions.

Bus

Eurostar NEO

Configuration

Eurostar-Neo

Motor

PPS-5000 electric propulsion system

Equipment

12-meter L-band antenna, advanced onboard processing unit capable of handling up to 3,200 communication channels with dynamic power allocation across multiple spot beams.

Power System

Two deployable solar arrays generating approximately 20 kW of power, supported by rechargeable batteries.

ADCS

3-axis stabilized using reaction wheels and star trackers

Transmitter Frequency

L-band frequencies for mobile communication services

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