EUTELSAT 1-F2 (ECS 2) (15158)

COSPAR: 1984-081A | Alt Name: ECS 2

Image
EUTELSAT 1-F2 (ECS 2) Satellite Image
Additional Sources
Launch Details

Launch Date

August 4, 1984

Launch Site

FRGUI

Launch Pad

ELA1

Launch Vehicle

Ariane 3

Orbital Elements

NORAD ID

15158

International Designator

1984-081A

Epoch

Sat, 04 Jul 2026 03:39:08 GMT

Apogee

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Perigee

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Inclination

12.48°

Right Ascension

332.82°

Eccentricity

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Argument of Perigee

225.24°

Period

1457.51 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

EUTELSAT 1-F2 (ECS 2)

Alternative Name

ECS 2

Type

Payload

Status

Non-operational

Owner

EUTEL

Country

EUTELSAT

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 15158U 84081A   26185.15217707 -.00000160  00000-0  00000-0 0  9991
2 15158  12.4754 332.8238 0009544 225.2358 145.6820  0.98798915117431

Source: Celestrak

Summary
EUTELSAT 1-F2 (ECS 2) is a communication satellite with the NORAD identifier 15158 and OBJECT_ID of 1984-081A, launched on August 4, 1984, from ELA1 at Kourou, French Guiana using an Ariane 3 launch vehicle. The satellite has dimensions of 2.4 meters in length, a diameter of 2.2 meters, and spans up to 13.8 meters. It is equipped with either 10 (+2) or 12 (+2) Ku-band transponders depending on the unit, and powered by two deployable solar arrays and batteries. ECS 2 has a dry mass of 450 kg and launched at a weight of 567 kg. The satellite's design includes a Box + 2 Pan shape with an RCS of 5.0118 square meters. It was manufactured by BAES for EUTEL, the owner operator, with a mission to provide communication services. Its intended lifetime was 7 years and it operates under the ECS-Bus configuration.
Physical Characteristics

Length

2.4

Diameter

2.2

Span

13.8

Dry Mass

450

Launch Mass

567

Shape

Box + 2 Pan

Radar Cross Section

5.0118

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

ECS 2

Purpose

Communication

Mission

Communication

Manufacturer

BAES

Life Expectancy

7 years

Bus

ECS

Configuration

ECS-Bus

Motor

Mage 2

Equipment

10 (+2) Ku-band transponders (#1); 12 (+2) Ku-band transponders (# 2-5)

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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