EGYPTSAT-A (MISRSAT-A) (44047)

COSPAR: 2019-008A | Alt Name: MisrSat A

Image
EGYPTSAT-A (MISRSAT-A) Satellite Image
Additional Sources
Launch Details

Launch Date

February 21, 2019

Launch Pad

LC31

Launch Vehicle

Soyuz-2-1B

Orbital Elements

NORAD ID

44047

International Designator

2019-008A

Epoch

Sat, 04 Jul 2026 08:05:52 GMT

Apogee

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Perigee

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Inclination

98.02°

Right Ascension

249.87°

Eccentricity

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Argument of Perigee

98.36°

Period

97.80 min

Mean Motion

14.72 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

EGYPTSAT-A (MISRSAT-A)

Alternative Name

MisrSat A

Type

Payload

Status

Operational

Owner

EGYSA

Country

Egypt

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 44047U 19008A   26185.33740920  .00000377  00000-0  67434-4 0  9992
2 44047  98.0185 249.8686 0001622  98.3590 261.7801 14.72325989395765

Source: Celestrak

Summary
EGYPTSAT-A (MISRSAT-A), also known as MisrSat A, is an Earth Observation satellite designed and operated by EGYSA using the 559GK bus configuration. Launched on February 21, 2019, from the TYSMC LC31 launch pad with a Soyuz-2-1B vehicle, this satellite has a dry mass of 1050 kg and is powered by three deployable fixed solar arrays along with batteries. The satellite's dimensions are 0.5 meters in length and diameter, and it spans 2 meters. Equipped with SPT-70 Xe plasma thrusters for propulsion, EGYPTSAT-A has a projected lifetime of 11 years. Manufactured by YUZHUA, the satellite is used primarily for Earth observation missions and follows a box shape augmented with four panoramic cameras and antennas.
Physical Characteristics

Length

0.5

Diameter

0.5

Span

2

Dry Mass

1050

Launch Mass

1050

Shape

Box + 4 Pan + Ant

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Egyptsat A No. 2

Purpose

Earth Observation

Mission

Earth Observation

Manufacturer

YUZHUA

Life Expectancy

11 years

Bus

Egyptsat

Configuration

559GK bus

Motor

SPT-70 Xe plasma thrusters

Equipment

Unknown

Power System

3 deployable fixed solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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