GLOBALSTAR M058 (25907)

COSPAR: 1999-049A | Alt Name: Globalstar M058

Image
GLOBALSTAR M058 Satellite Image
Additional Sources
Launch Details

Launch Date

September 22, 1999

Launch Pad

LC1

Launch Vehicle

Soyuz-U-PVB

Orbital Elements

NORAD ID

25907

International Designator

1999-049A

Epoch

Sat, 04 Jul 2026 05:11:10 GMT

Apogee

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Perigee

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Inclination

51.99°

Right Ascension

169.04°

Eccentricity

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Argument of Perigee

292.70°

Period

120.68 min

Mean Motion

11.93 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 M058

Alternative Name

Globalstar M058

Type

Payload

Status

Non-operational

Owner

GLOBT

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25907U 99049A   26185.21608830 -.00000078  00000-0  79720-4 0  9999
2 25907  51.9907 169.0399 0002840 292.6983  67.3551 11.93214411587145

Source: Celestrak

Summary
GLOBALSTAR M058 is a communication satellite, also known as Globalstar FM58, with the OBJECT_ID 1999-049A and NORAD_CAT_ID 25907. It was manufactured by LOR for GLOBT (Globalstar) and launched on September 22, 1999, from TYMSC LC1 using a Soyuz-U-PVB launch vehicle. The satellite measures 1.5 meters in length with a diameter of 0.6 meters and has a span of 12 meters due to its deployable solar arrays. It has a dry mass of 380 kg and a launch mass of 450 kg, equipped with batteries for power storage alongside the solar arrays. Its shape is described as Box + 2 Pan with an RCS (Radar Cross Section) value of 2.1977. The satellite was operational for approximately 7.5 years, serving communication purposes through its AOCS (Attitude and Orbit Control System).
Physical Characteristics

Length

1.5

Diameter

0.6

Span

12

Dry Mass

380

Launch Mass

450

Shape

Box + 2 Pan

Radar Cross Section

2.1977

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globalstar FM58

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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