PRSC-EO1 (62725)

COSPAR: 2025-012A | Alt Name: EO-1

Image
PRSC-EO1 Satellite Image
Launch Details

Launch Date

January 17, 2025

Launch Site

Jiuquan Satellite Launch Centre

Launch Pad

LC43/94

Launch Vehicle

Chang Zheng 2D

Orbital Elements

NORAD ID

62725

International Designator

2025-012A

Epoch

Sun, 19 Jul 2026 19:52:52 GMT

Apogee

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Perigee

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Inclination

97.42°

Right Ascension

272.65°

Eccentricity

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Argument of Perigee

133.36°

Period

94.88 min

Mean Motion

15.18 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

PRSC-EO1

Alternative Name

EO-1

Type

Unknown

Status

Operational

Owner

SUPARCO

Country

Pakistan

Constellation

N/A

Related Satellites

Major Events

Successfully launched on January 17, 2025, from China's Jiuquan Satellite Launch Centre

Latest TLEs
1 62725U 25012A   26200.82839006  .00003307  00000+0  16753-3 0  9995
2 62725  97.4209 272.6476 0007099 133.3602 226.8224 15.17652955 83140

Source: Celestrak

Summary
The PRSC-EO1 satellite is a Pakistani Earth observation satellite designed for resource management, disaster monitoring, and urban planning. It has a mass of 500 kg, measures 2 meters in length and 1.5 meters in diameter, and features a high-resolution optical payload for imaging the Earth's surface. The satellite was launched on January 17, 2025, from China's Jiuquan Satellite Launch Centre using a Chang Zheng 2D launch vehicle. The PRSC-EO1 is equipped with solar panels to provide power for its operations, and uses X-band frequencies for data transmission. Its three-axis stabilization system ensures stable imaging capabilities. The satellite has a designed mission life of five years, during which it will enhance Pakistan's capabilities in natural resource monitoring, disaster management, and urban planning. The PRSC-EO1 is the first indigenous Earth observation satellite built by SUPARCO (Space and Upper Atmosphere Research Commission), Pakistan's space agency. Its successful launch marks an important milestone for Pakistan's space program, with plans to establish a constellation of satellites for various applications in the future.
Physical Characteristics

Length

2

Diameter

1.5

Span

8

Dry Mass

500

Launch Mass

500

Shape

Box with deployable solar panels

Radar Cross Section

0.5

Visual Magnitude

6

Color

White with national insignia

Material Composition

Aluminum alloy structure with composite materials

Technical Details

Payload

Electro-Optical imaging system

Purpose

To enhance capabilities in natural resource monitoring, disaster management, and urban planning

Mission

Earth observation for resource management, disaster monitoring, and urban planning

Manufacturer

SUPARCO

Life Expectancy

Designed for a mission life of 5 years

Bus

PRSC-EO

Configuration

Earth Observation Satellite

Motor

Unknown

Equipment

High-resolution optical payload for Earth observation

Power System

Solar panels providing necessary power for operations

ADCS

Three-axis stabilization

Transmitter Frequency

X-band for data transmission

Map
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