INTELSAT 501 (12474)

COSPAR: 1981-050A | Alt Name: INTELSAT 501

Image
INTELSAT 501 Satellite Image
Additional Sources
Launch Details

Launch Date

May 23, 1981

Launch Pad

LC36B

Launch Vehicle

Atlas SLV-3D Centaur

Orbital Elements

NORAD ID

12474

International Designator

1981-050A

Epoch

Sat, 04 Jul 2026 05:12:41 GMT

Apogee

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Perigee

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Inclination

10.95°

Right Ascension

324.58°

Eccentricity

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Argument of Perigee

271.01°

Period

1456.70 min

Mean Motion

0.99 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

INTELSAT 501

Alternative Name

INTELSAT 501

Type

Payload

Status

Non-operational

Owner

INTEL

Country

INTELSAT

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 12474U 81050A   26185.21714398 -.00000229  00000-0  00000-0 0  9993
2 12474  10.9478 324.5832 0002807 271.0111  99.3562  0.98853555137841

Source: Celestrak

Summary
INTELSAT 501 is a communication satellite, also known as INTELSAT V F1, launched on May 23, 1981, from LC36B at the Air Force Eastern Test Range using an Atlas SLV-3D Centaur launch vehicle. It has dimensions of 6.4 meters in length and a diameter of 2 meters with a span of 15.9 meters when its solar arrays are deployed. The satellite is equipped with 21 C-band transponders and 4 Ku-band transponders, providing communication services with a dry mass of 775 kilograms and a launch mass of 945 kilograms. It was manufactured by FORDA and has a power system consisting of two deployable solar arrays and batteries. The satellite's design includes a box shape with two panels and it uses a Star 37F motor for its operations, operating for approximately 7 years post-launch.
Physical Characteristics

Length

6.4

Diameter

2

Span

15.9

Dry Mass

775

Launch Mass

945

Shape

Box + 2 Pan

Radar Cross Section

3.981

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

INTELSAT V F1

Purpose

Communication

Mission

Communication

Manufacturer

FORDA

Life Expectancy

7 years

Bus

FS INTELSAT 5

Configuration

Intelsat-5 bus

Motor

Star 37F

Equipment

21 C-band transponders, 4 Ku-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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