GLOBALSTAR M024 (25883)

COSPAR: 1999-043A | Alt Name: Globalstar M024

Image
GLOBALSTAR M024 Satellite Image
Additional Sources
Launch Details

Launch Date

August 17, 1999

Launch Pad

SLC17B

Launch Vehicle

Delta 7420-10C

Orbital Elements

NORAD ID

25883

International Designator

1999-043A

Epoch

Sat, 04 Jul 2026 03:09:38 GMT

Apogee

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Perigee

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Inclination

52.00°

Right Ascension

238.82°

Eccentricity

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Argument of Perigee

359.37°

Period

129.71 min

Mean Motion

11.10 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

GLOBALSTAR M024

Alternative Name

Globalstar M024

Type

Payload

Status

Non-operational

Owner

GLOBT

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25883U 99043A   26185.13170098  .00000019  00000-0  29576-2 0  9993
2 25883  51.9993 238.8199 0001017 359.3689  12.5819 11.10171896157280

Source: Celestrak

Summary
GLOBALSTAR M024 (also known as Globalstar M024) is a communication satellite with the NORAD Catalog ID 25883 and OBJECT_ID 1999-043A. Manufactured by LOR, it was launched on August 17, 1999, from Cape Canaveral Air Force Station (AFETR), using Delta 7420-10C as the launch vehicle from SLC17B pad. The satellite is configured with a LS-400 system and is owned by GLOBT. It has dimensions of 1.5 meters in length, 0.6 meters in diameter, and a span of 12 meters. Its dry mass is 380 kg, and it had an initial launch mass of 450 kg. The satellite is powered by two deployable solar arrays and batteries. It has a mission lifetime of 7.5 years and its purpose is communication. The satellite's shape consists of a box with two panels, and it features the LS-400 AOCS motor for attitude control. Its radar cross-section (RCS) is 2.3881 square meters. The payload carried is Globalstar FM24.
Physical Characteristics

Length

1.5

Diameter

0.6

Span

12

Dry Mass

380

Launch Mass

450

Shape

Box + 2 Pan

Radar Cross Section

2.3881

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globalstar FM24

Purpose

Communication

Mission

Communication

Manufacturer

LOR

Life Expectancy

7.5 years

Bus

LS-400

Configuration

LS-400

Motor

LS-400 AOCS

Equipment

?

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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