GLOBALSTAR M071 (31576)

COSPAR: 2007-020F | Alt Name: Globalstar M071

Image
GLOBALSTAR M071 Satellite Image
Additional Sources
Launch Details

Launch Date

May 29, 2007

Launch Pad

LC31

Launch Vehicle

Soyuz-FG

Orbital Elements

NORAD ID

31576

International Designator

2007-020F

Epoch

Sat, 04 Jul 2026 05:05:28 GMT

Apogee

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Perigee

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Inclination

52.00°

Right Ascension

240.33°

Eccentricity

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Argument of Perigee

165.57°

Period

118.20 min

Mean Motion

12.18 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 M071

Alternative Name

Globalstar M071

Type

Payload

Status

Non-operational

Owner

GLOB

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 31576U 07020F   26185.21213413  .00000027  00000-0  11669-2 0  9994
2 31576  52.0043 240.3254 0001216 165.5738 234.4410 12.18270977541500

Source: Celestrak

Summary
GLOBALSTAR M071 is a communication satellite with the OBJECT_ID 2007-020F and NORAD_CAT_ID 31576. Launched on May 29, 2007, from TYMSC Launch Complex 31 using a Soyuz-FG launch vehicle, it was manufactured by LOR for the US-based company GLOB (Globalstar). The satellite has dimensions of 1.5 meters in length and 0.6 meters in diameter with a span of 12 meters. It had a launch mass of 450 kg and a dry mass of 380 kg, equipped with two deployable solar arrays and batteries for power. Its mission is to provide communication services. The satellite has a box shape with two panels and an RCS value of 2.2995. GLOBALSTAR M071 operates with a motor called LS-400 AOCS and has a configuration similar to the BUS type LS-400. It was designed for a lifetime of 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

2.2995

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globalstar FM71

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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