SPOT 2 (20436)

COSPAR: 1990-005A | Alt Name: SPOT 2

Image
SPOT 2 Satellite Image
Additional Sources
Launch Details

Launch Date

January 22, 1990

Launch Site

FRGUI

Launch Pad

ELA2

Launch Vehicle

Ariane 40

Orbital Elements

NORAD ID

20436

International Designator

1990-005A

Epoch

Sat, 04 Jul 2026 03:25:26 GMT

Apogee

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Perigee

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Inclination

98.72°

Right Ascension

343.52°

Eccentricity

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Argument of Perigee

35.15°

Period

97.70 min

Mean Motion

14.74 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

SPOT 2

Alternative Name

SPOT 2

Type

Payload

Status

Non-operational

Owner

CNES

Country

France

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 20436U 90005A   26185.14266686  .00000708  00000-0  10334-3 0  9999
2 20436  98.7154 343.5172 0129366  35.1549 325.8108 14.73928888917822

Source: Celestrak

Summary
SPOT 2 was an Earth observation satellite launched by CNES on January 22, 1990, from Guiana Space Centre using Ariane 40 as the launch vehicle. It had dimensions of 4.5 meters in length and a diameter of 2 meters, with a span of 8.2 meters. The satellite's dry mass was 1750 kg, and it weighed 1900 kg at launch. Equipped with a deployable solar array and batteries for power, SPOT 2 featured two HRV imagers as its primary payload for Earth observation purposes. Designed to have a lifetime of 3 years, the satellite operated using an AOCS system for attitude control. The spacecraft was part of the SPOT constellation manufactured by MMST, with a box plus panel shape and a radar cross-section (RCS) of 6.217 m².
Physical Characteristics

Length

4.5

Diameter

2

Span

8.2

Dry Mass

1750

Launch Mass

1900

Shape

Box + Pan

Radar Cross Section

6.217

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

SPOT 2

Purpose

Earth observation

Mission

Earth observation

Manufacturer

MMST

Life Expectancy

3 years (design)

Bus

SPOT

Configuration

SPOT Mk.1

Motor

SPOT AOCS

Equipment

2 HRV imager

Power System

Deployable solar array, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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