ASTRA 1F (23842)

COSPAR: 1996-021A | Alt Name: Astra 1F

Image

Additional Sources

Launch Details

Launch Date

April 8, 1996

Launch Site

Tyuratam Missile and Space Complex

Launch Pad

LC81/23

Launch Vehicle

Proton-K/DM-2M

Orbital Elements

NORAD ID

23842

International Designator

1996-021A

Epoch

Fri, 03 Jul 2026 22:37:48 GMT

Apogee

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Perigee

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Inclination

5.46°

Right Ascension

73.67°

Eccentricity

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Argument of Perigee

102.35°

Period

1452.77 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 1F

Alternative Name

Astra 1F

Type

Payload

Status

Non-operational

Owner

SES

Country

Luxembourg

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 23842U 96021A   26184.94292769  .00000012  00000-0  00000-0 0  9999

2 23842   5.4632  73.6699 0003105 102.3469 115.0621  0.99120777 52268

Source: Celestrak

Summary

ASTRA 1F is a communication satellite (Direct Broadcasting) with a NORAD catalog ID of 23842 and an object ID of 1996-021A. It was launched on April 8, 1996, from the TYMSC launch site using a Proton-K/DM-2M launch vehicle. The satellite has dimensions of 4 meters in length, 3 meters in diameter, and a span of 26 meters. Its dry mass is 1,600 kilograms with a total launch mass of 3,010 kilograms. Equipped with 24 Ku-band transponders (#1E) and 30 Ku-band transponders (#1F), it uses two deployable solar arrays for power generation along with batteries. Manufactured by HSES, the satellite's design is based on the HS-601 bus configuration. It was owned by SES and stabilized in orbit one day after launch on April 9, 1996. The mission of ASTRA 1F aimed to provide communication services for direct broadcasting with an expected lifetime of 15 years.

Physical Characteristics

Length

Diameter

Span

Dry Mass

1600

Launch Mass

3010

Shape

Box + 2 Pan

Radar Cross Section

3.3814

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Astra 1F

Purpose

Communication (Direct Broadcasting)

Mission

Communication (Direct Broadcasting)

Manufacturer

HSES

Life Expectancy

15 years

Bus

HS-601

Configuration

HS-601

Motor

R-4D-11-300

Equipment

24 Ku-band transponders (#1E); 30 Ku-band transponders (#1F)

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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