ASTRA 1C (22653)

COSPAR: 1993-031A | Alt Name: Astra 1C

Image
ASTRA 1C Satellite Image
Additional Sources
Launch Details

Launch Date

May 12, 1993

Launch Site

FRGUI

Launch Pad

ELA2

Launch Vehicle

Ariane 42L

Orbital Elements

NORAD ID

22653

International Designator

1993-031A

Epoch

Fri, 03 Jul 2026 18:14:31 GMT

Apogee

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Perigee

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Inclination

12.87°

Right Ascension

25.46°

Eccentricity

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Argument of Perigee

34.04°

Period

1456.85 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 1C

Alternative Name

Astra 1C

Type

Payload

Status

Non-operational

Owner

SES

Country

Luxembourg

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 22653U 93031A   26184.76009024 -.00000149  00000-0  00000-0 0  9998
2 22653  12.8747  25.4650 0005107  34.0358 322.2162  0.98843089 51257

Source: Celestrak

Summary
ASTRA 1C is a communication satellite manufactured by HSES and owned by SES. It was launched on May 12, 1993, from ELA2 at the Guiana Space Centre using an Ariane 42L launch vehicle. The spacecraft has dimensions of 4.3 meters in length, 2.7 meters in diameter, and a span of 21 meters due to its solar arrays. It was equipped with 24 Ku-band transponders for direct broadcasting services and powered by two deployable solar arrays and batteries. ASTRA 1C had a launch mass of 2790 kg and a dry mass of 1180 kg, with an expected lifetime of 12 years. Its shape is described as a box with two panels, and it has a radar cross-section (RCS) value of 14.13 square meters. The satellite's configuration and bus type are both HS-601, indicating its design for communication purposes.
Physical Characteristics

Length

4.3

Diameter

2.7

Span

21

Dry Mass

1180

Launch Mass

2790

Shape

Box + 2 Pan

Radar Cross Section

14.13

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Astra 1C

Purpose

Communication (Direct Broadcasting)

Mission

Communication (Direct Broadcasting)

Manufacturer

HSES

Life Expectancy

12 years

Bus

HS-601

Configuration

HS-601

Motor

R-4D-11

Equipment

24 Ku-band transponders

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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