GLOBALSTAR M047 (25772)

COSPAR: 1999-031C | Alt Name: Globalstar M047

Image
GLOBALSTAR M047 Satellite Image
Additional Sources
Launch Details

Launch Date

June 10, 1999

Launch Pad

SLC17B

Launch Vehicle

Delta 7420-10C

Orbital Elements

NORAD ID

25772

International Designator

1999-031C

Epoch

Fri, 03 Jul 2026 21:39:01 GMT

Apogee

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Perigee

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Inclination

51.98°

Right Ascension

9.44°

Eccentricity

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Argument of Perigee

195.96°

Period

127.22 min

Mean Motion

11.32 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 M047

Alternative Name

Globalstar M047

Type

Payload

Status

Non-operational

Owner

GLOBT

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25772U 99031C   26184.90210246 -.00000066  00000-0  84978-4 0  9993
2 25772  51.9849   9.4381 0016092 195.9610 164.0691 11.31933988514334

Source: Celestrak

Summary
GLOBALSTAR M047 is a communication satellite with the NORAD catalog ID 25772 and object identifier 1999-031C. Launched on June 10, 1999, from Cape Canaveral Air Force Station's SLC17B launch pad aboard a Delta 7420-10C launch vehicle, the satellite was built by LOR and is owned by GLOBT (Globalstar). It measures 1.5 meters in length with a diameter of 0.6 meters and a span of 12 meters when its deployable solar arrays are extended. The satellite has a dry mass of 380 kg and weighed 450 kg at launch, equipped with batteries for power storage. Its mission is to provide communication services as part of the Globalstar constellation. The motor system used for attitude control is LS-400 AOCS. The RCS value is 2.5521, indicating its reflective surface characteristics.
Physical Characteristics

Length

1.5

Diameter

0.6

Span

12

Dry Mass

380

Launch Mass

450

Shape

Box + 2 Pan

Radar Cross Section

2.5521

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Globalstar FM47

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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