NAVSTAR 83 (USA 440) (62339)

COSPAR: 2024-242A | Alt Name: GPS III SV07

Image
NAVSTAR 83 (USA 440) Satellite Image
Launch Details

Launch Date

December 16, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

SLC-40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62339

International Designator

2024-242A

Epoch

Sun, 19 Jul 2026 17:19:15 GMT

Apogee

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Perigee

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Inclination

54.83°

Right Ascension

332.86°

Eccentricity

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Argument of Perigee

4.35°

Period

717.95 min

Mean Motion

2.01 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

NAVSTAR 83 (USA 440)

Alternative Name

GPS III SV07

Type

Payload

Status

Operational

Owner

United States Space Force

Country

United States

Constellation

GPS

Related Satellites

Major Events

Launched on December 16, 2024, as part of the Rapid Response Trailblazer program to demonstrate expedited launch capabilities.

Latest TLEs
1 62339U 24242A   26200.72170845 -.00000109  00000+0  00000+0 0  9990
2 62339  54.8338 332.8621 0017996   4.3540 337.1791 02.00572353 11908

Source: Celestrak

Summary
NAVSTAR 83 (USA 440), also known as GPS III SV07, is a navigation satellite built by Lockheed Martin and launched on December 16, 2024, from Cape Canaveral Space Force Station using a Falcon 9 launch vehicle. It measures 3.4 meters in length with a diameter of 1.8 meters and a span of 14 meters due to its deployable solar arrays. The satellite has a dry mass of 2,160 kilograms and was launched with a total mass of 4,352 kilograms. Equipped with advanced navigation payloads including L1C civil signal compatibility and M-code for military use, it provides enhanced global positioning and timing services to both civilian and military users. The satellite is stabilized using three-axis stabilization and is powered by two deployable solar arrays and batteries. It operates on frequencies of L1 (1575.42 MHz), L2 (1227.60 MHz), and L5 (1176.45 MHz). NAVSTAR 83 has a designed lifetime of 15 years and is part of the GPS constellation, with similar satellites including GPS III SV01 through SV06.
Physical Characteristics

Length

3.4

Diameter

1.8

Span

14

Dry Mass

2160

Launch Mass

4352

Shape

Box with two solar panel arrays

Radar Cross Section

0.5

Visual Magnitude

5.5

Color

Silver and white

Material Composition

Aluminum and composite materials

Technical Details

Payload

Navigation payload with L1C and M-code signals

Purpose

Provides enhanced global positioning and timing services for military and civilian users

Mission

Navigation

Manufacturer

Lockheed Martin

Life Expectancy

15 years

Bus

A2100

Configuration

A2100A

Motor

LEROS-1c

Equipment

The satellite is equipped with advanced navigation payloads, including the new L1C civil signal compatible with international global navigation satellite systems, and M-code for improved anti-jamming and secure military communications.

Power System

Two deployable solar arrays, batteries

ADCS

Three-axis stabilization

Transmitter Frequency

L1 (1575.42 MHz), L2 (1227.60 MHz), L5 (1176.45 MHz)

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