SPOT 7 (40053)

COSPAR: 2014-034A | Alt Name: SPOT 7

Image
SPOT 7 Satellite Image
Additional Sources
Launch Details

Launch Date

June 30, 2014

Launch Site

SRILR

Launch Pad

FLP

Launch Vehicle

PSLV

Orbital Elements

NORAD ID

40053

International Designator

2014-034A

Epoch

Sat, 04 Jul 2026 07:17:24 GMT

Apogee

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Perigee

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Inclination

98.06°

Right Ascension

247.35°

Eccentricity

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Argument of Perigee

97.04°

Period

98.56 min

Mean Motion

14.61 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 7

Alternative Name

SPOT 7

Type

Payload

Status

Operational

Owner

CNES

Country

France

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 40053U 14034A   26185.30375340  .00000474  00000-0  10587-3 0  9990
2 40053  98.0619 247.3542 0001444  97.0366 263.0999 14.60973495639631

Source: Celestrak

Summary
SPOT 7 is an Earth observation satellite with a NORAD catalog ID of 40053 and an object ID of 2014-034A. It was manufactured by ADSUK for CNES, launched on June 30, 2014, from SRILR using a PSLV launch vehicle. The satellite is based on the AstroSat-500 Mk.2 configuration and has dimensions of 2.7 meters in length, 2 meters in diameter, and spans 7 meters when its solar arrays are deployed. It carries two NAOMI instruments with pan and multispectral resolutions of 2 meters and 8 meters respectively. The satellite's dry mass is 712 kg, which is the same as its launch mass. SPOT 7 utilizes three deployable solar arrays and batteries for power supply and has an expected lifetime of ten years. Its shape consists of a hexagonal cylindrical body with three panoramic sections.
Physical Characteristics

Length

2.7

Diameter

2

Span

7

Dry Mass

712

Launch Mass

712

Shape

Hex cyl+3 pan

Radar Cross Section

3.6769

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

SPOT 7

Purpose

Earth observation

Mission

Earth observation

Manufacturer

ADSUK

Life Expectancy

10 years

Bus

AstroSat-500L

Configuration

AstroSat-500 Mk.2 (AstroBus-L)

Motor

AOCS

Equipment

2 x NAOMI (Pan: 2 m, MS: 8 m)

Power System

3 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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