GLOBALSTAR M075 (37192)

COSPAR: 2010-054E | Alt Name: Globalstar M075

Image
GLOBALSTAR M075 Satellite Image
Additional Sources
Launch Details

Launch Date

October 19, 2010

Launch Pad

LC31

Launch Vehicle

Soyuz-2-1A

Orbital Elements

NORAD ID

37192

International Designator

2010-054E

Epoch

Sat, 04 Jul 2026 06:00:34 GMT

Apogee

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Perigee

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Inclination

51.99°

Right Ascension

98.24°

Eccentricity

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Argument of Perigee

47.28°

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 M075

Alternative Name

Globalstar M075

Type

Payload

Status

Operational

Owner

GLOB

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 37192U 10054E   26185.25040164 -.00000065  00000-0  21757-3 0  9993
2 37192  51.9943  98.2389 0000558  47.2767 121.4240 12.62267685724096

Source: Celestrak

Summary
GLOBALSTAR M075, also known as Globalstar M075, is a communication satellite with NORAD catalog ID 37192 and object ID 2010-054E. It was manufactured by THALR for the US owner GLOB (Globalstar) and launched on October 19, 2010, from TYMSC LC31 using a Soyuz-2-1A launch vehicle. The satellite has dimensions of 4 meters in length, 2 meters in diameter, and spans 12 meters with its solar arrays deployed. It weighs 715 kg at launch and 500 kg dry, equipped with 2 deployable solar arrays providing up to 2.4 kW (bol) or 1.7 kW (eol), along with batteries for power storage. The satellite features the ELiTeBus-1000 configuration and is part of the Prisma bus family. It carries a communication payload including 16 C-to-S-band transponders and 16 L-to-C-band transponders, designed to support Globalstar-2 FM4 mission objectives. GLOBALSTAR M075 has an expected operational lifetime of 15 years and uses an LS-400 AOCS motor for attitude control. The satellite's shape is described as a trap cylinder with two panels and has a surface area (RCS) of 4.7436 square meters.
Physical Characteristics

Length

4

Diameter

2

Span

12

Dry Mass

500

Launch Mass

715

Shape

Trap Cyl + 2 Pan

Radar Cross Section

4.7436

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globalstar-2 FM4

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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