GLOBALSTAR M019 (25677)

COSPAR: 1999-019B | Alt Name: Globalstar M019

Image
GLOBALSTAR M019 Satellite Image
Additional Sources
Launch Details

Launch Date

April 15, 1999

Launch Pad

LC1

Launch Vehicle

Soyuz-U-PVB

Orbital Elements

NORAD ID

25677

International Designator

1999-019B

Epoch

Sat, 04 Jul 2026 04:39:21 GMT

Apogee

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Perigee

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Inclination

51.99°

Right Ascension

93.70°

Eccentricity

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Argument of Perigee

11.73°

Period

118.63 min

Mean Motion

12.14 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 M019

Alternative Name

Globalstar M019

Type

Payload

Status

Non-operational

Owner

GLOBT

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25677U 99019B   26185.19399686 -.00000122  00000-0 -33258-3 0  9999
2 25677  51.9869  93.7041 0002036  11.7317 154.1499 12.13883602231533

Source: Celestrak

Summary
GLOBALSTAR M019, also known as Globalstar M019, is a communication satellite launched on April 15, 1999, from the Tyuratam Site (TYMSC), LC1 launch pad using a Soyuz-U-PVB launch vehicle. It has dimensions of 1.5 meters in length and 0.6 meters in diameter with a span of 12 meters, indicating deployable solar arrays or panels. The satellite was manufactured by LOR for the mission purpose of communication and is owned by GLOBT (Globalstar). It has a dry mass of 380 kg and had a launch mass of 450 kg. Its configuration is described as LS-400, equipped with two deployable solar arrays and batteries for power. The satellite's shape is noted as "Box + 2 Pan," suggesting a box-shaped body with additional panels likely related to its solar array design. The spacecraft has an expected lifetime of 7.5 years and was launched from the US. Its mission involved communication services, utilizing equipment that includes the LS-400 AOCS (Attitude Orbit Control System) for motor control.
Physical Characteristics

Length

1.5

Diameter

0.6

Span

12

Dry Mass

380

Launch Mass

450

Shape

Box + 2 Pan

Radar Cross Section

2.3345

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globalstar FM19

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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