GLOBALSTAR M006 (25307)

COSPAR: 1998-023B | Alt Name: Globalstar M006

Image
GLOBALSTAR M006 Satellite Image
Additional Sources
Launch Details

Launch Date

April 24, 1998

Launch Pad

LC17A

Launch Vehicle

Delta 7420-10C

Orbital Elements

NORAD ID

25307

International Designator

1998-023B

Epoch

Fri, 03 Jul 2026 21:10:28 GMT

Apogee

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Perigee

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Inclination

52.00°

Right Ascension

345.10°

Eccentricity

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Argument of Perigee

85.64°

Period

124.33 min

Mean Motion

11.58 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 M006

Alternative Name

Globalstar M006

Type

Payload

Status

Non-operational

Owner

GLOBT

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25307U 98023B   26184.88227638 -.00000104  00000-0 -57027-3 0  9995
2 25307  51.9961 345.0988 0004387  85.6434  81.6639 11.58169972261055

Source: Celestrak

Summary
GLOBALSTAR M006, also known as Globalstar M006, is a communication satellite identified by NORAD CAT ID 25307 and OBJECT ID 1998-023B. Launched on April 24, 1998, from the Cape Canaveral Air Force Station LC17A launch pad using a Delta 7420-10C launch vehicle, this satellite has a configuration of LS-400 and was manufactured by LOR for the United States. The spacecraft measures 1.5 meters in length with a diameter of 0.6 meters and a span of 12 meters when its solar arrays are deployed. It had a dry mass of 380 kilograms and a launch mass of 450 kilograms, equipped with deployable solar arrays and batteries for power. The satellite's shape is described as a box with two panels and has a reflective cross-section (RCS) area of 2.4068 square meters. It was designed to operate in orbit for approximately 7.5 years.
Physical Characteristics

Length

1.5

Diameter

0.6

Span

12

Dry Mass

380

Launch Mass

450

Shape

Box + 2 Pan

Radar Cross Section

2.4068

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globalstar FM06

Purpose

Communication

Mission

Communication

Manufacturer

LOR

Life Expectancy

7.5 years

Bus

LS-400

Configuration

LS-400

Motor

?

Equipment

?

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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