GLOBALSTAR M079 (37188)

COSPAR: 2010-054A | Alt Name: Globalstar M079

Image
GLOBALSTAR M079 Satellite Image
Additional Sources
Launch Details

Launch Date

October 19, 2010

Launch Pad

LC31

Launch Vehicle

Soyuz-2-1A

Orbital Elements

NORAD ID

37188

International Designator

2010-054A

Epoch

Sat, 04 Jul 2026 02:30:20 GMT

Apogee

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Perigee

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Inclination

52.00°

Right Ascension

57.17°

Eccentricity

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Argument of Perigee

58.96°

Period

114.08 min

Mean Motion

12.62 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 M079

Alternative Name

Globalstar M079

Type

Payload

Status

Operational

Owner

GLOB

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 37188U 10054A   26185.10440826 -.00000087  00000-0  91580-4 0  9997
2 37188  52.0045  57.1721 0001039  58.9556 105.6804 12.62266405724684

Source: Celestrak

Summary
GLOBALSTAR M079 is a communication satellite launched on October 19, 2010, from the Taiyuan Satellite Launch Center (TYMSC) using a Soyuz-2-1A launch vehicle. It has a length of 4 meters and a diameter of 2 meters with a span of 12 meters, weighing approximately 715 kg at launch and 500 kg dry mass. Equipped with 16 C-to-S-band transponders and 16 L-to-C-band transponders, it is designed for communication purposes. The satellite features two deployable solar arrays generating a power of 2.4 kW (at beginning of life) and 1.7 kW (at end of life), along with batteries for energy storage. Manufactured by THALR, the satellite uses an LS-400 AOCS motor for attitude control and has a projected lifetime of 15 years.
Physical Characteristics

Length

4

Diameter

2

Span

12

Dry Mass

500

Launch Mass

715

Shape

Trap Cyl + 2 Pan

Radar Cross Section

4.8334

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globalstar-2 FM8

Purpose

Communication

Mission

Communication

Manufacturer

THALR

Life Expectancy

15 years

Bus

Prisma

Configuration

ELiTeBus-1000

Motor

LS-400 AOCS

Equipment

16 C-to-S-band transponders, 16 L-to-C-band transponders

Power System

2 deployable solar arrays, 2.4 kW (bol), 1.7 kW (eol), batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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