ASTRA 2A (25462)

COSPAR: 1998-050A | Alt Name: Astra 2A

Image
ASTRA 2A Satellite Image
Additional Sources
Launch Details

Launch Date

August 30, 1998

Launch Pad

LC81/23

Launch Vehicle

Proton-K/DM-2M

Orbital Elements

NORAD ID

25462

International Designator

1998-050A

Epoch

Sat, 04 Jul 2026 05:35:24 GMT

Apogee

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Perigee

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Inclination

7.14°

Right Ascension

68.82°

Eccentricity

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Argument of Perigee

64.61°

Period

1459.57 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

ASTRA 2A

Alternative Name

Astra 2A

Type

Payload

Status

Non-operational

Owner

SES

Country

Luxembourg

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25462U 98050A   26185.23291740  .00000046  00000-0  00000-0 0  9991
2 25462   7.1447  68.8228 0024799  64.6088 287.1371  0.98659371 46435

Source: Celestrak

Summary
ASTRA 2A is a communication satellite operated by SES for direct broadcasting purposes. Launched on August 30, 1998, from Tyuratam Site (TYMSC) using the Proton-K/DM-2M launch vehicle from Launch Pad LC81/23, it has a design lifetime of 15 years. The satellite is based on the HS-601HP / BSS-601HP bus manufactured by HSES and equipped with 32 Ku-band transponders (all) and 2 Ka-band transponders (only #1H). It measures 4 meters in length, 3.2 meters in diameter, and has a span of 26.2 meters. Its dry mass is 1950 kilograms, while its launch mass was 3550 kilograms. The satellite powers itself with two deployable solar arrays and batteries.
Physical Characteristics

Length

4

Diameter

3.2

Span

26.2

Dry Mass

1950

Launch Mass

3550

Shape

Box + 2 Pan

Radar Cross Section

18.8958

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Astra 2A

Purpose

Communication (Direct Broadcasting)

Mission

Communication (Direct Broadcasting)

Manufacturer

HSES

Life Expectancy

15 years

Bus

HS-601HP

Configuration

HS-601HP / BSS-601HP

Motor

X/R-4D11-300

Equipment

32 Ku-band transponders (all), 2 Ka-band transponders (only #1H)

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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