CENTISPACE-1 S14 (62583)

COSPAR: 2025-007J | Alt Name: Weili Kongjian 01-08

Image
CENTISPACE-1 S14 Satellite Image
Launch Details

Launch Date

January 13, 2025

Launch Site

YSLA

Launch Pad

LP4

Launch Vehicle

Jielong-3

Orbital Elements

NORAD ID

62583

International Designator

2025-007J

Epoch

Sun, 19 Jul 2026 18:55:25 GMT

Apogee

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Perigee

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Inclination

54.98°

Right Ascension

178.59°

Eccentricity

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Argument of Perigee

148.73°

Period

104.30 min

Mean Motion

13.81 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

CENTISPACE-1 S14

Alternative Name

Weili Kongjian 01-08

Type

Payload

Status

Operational

Owner

Beijing Future Navigation Technology Co., Ltd.

Country

China

Constellation

CentiSpace-1

Related Satellites

Major Events

Launched on January 13, 2025, aboard a Jielong-3 rocket from YSLA. Successfully entered its planned orbit and commenced operations to enhance GNSS services.

Latest TLEs
1 62583U 25007J   26200.78849096 -.00000116  00000+0  23261-4 0  9995
2 62583  54.9823 178.5881 0011708 148.7293 211.4362 13.80615413 79216

Source: Celestrak

Summary
The CentiSpace-1 S14 satellite, also known as Weili Kongjian 01-08, is a low Earth orbit (LEO) satellite designed to enhance Global Navigation Satellite System (GNSS) services by providing GNSS augmentation signals for improved accuracy and integrity. Launched on January 13, 2025, from YSLA using the Jielong-3 rocket, it has a bus configuration of WN-100 and is operated by Beijing Future Navigation Technology Co., Ltd. The satellite measures 1 meter in length with a diameter of 0.5 meters and spans 2 meters when its solar arrays are deployed. It weighs 160 kilograms both at launch and dry mass, featuring a white box-shaped structure with composite materials for specific components and aluminum alloy for the main structure. Equipped with a navigation augmentation payload and laser communication link, it communicates using L-band and S-band frequencies. The satellite employs three-axis stabilization and solar power from two deployable arrays to sustain its operations. Its mission is designed to last approximately 5 years, enhancing GNSS services as part of the CentiSpace-1 constellation.
Physical Characteristics

Length

1

Diameter

0.5

Span

2

Dry Mass

160

Launch Mass

160

Shape

Box-shaped with two deployable solar panels.

Radar Cross Section

0.5

Visual Magnitude

5

Color

White

Material Composition

Aluminum alloy structure with composite materials for specific components.

Technical Details

Payload

Navigation augmentation payload

Purpose

Technology ?

Mission

The CentiSpace-1 S14 satellite is part of a low Earth orbit (LEO) constellation aimed at enhancing Global Navigation Satellite System (GNSS) services. It focuses on providing GNSS augmentation signals to improve positioning accuracy and integrity.

Manufacturer

DFHS

Life Expectancy

Designed for a mission duration of approximately 5 years.

Bus

WK01

Configuration

WN-100 bus

Motor

Unknown

Equipment

Laser communication link

Power System

Equipped with two deployable solar arrays and batteries to power its onboard systems.

ADCS

Three-axis stabilization

Transmitter Frequency

L-band and S-band frequencies for navigation augmentation and communication.

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