CENTISPACE-1 S8 (62577)

COSPAR: 2025-007C | Alt Name: Weili Kongjian 01-02

Image
CENTISPACE-1 S8 Satellite Image
Launch Details

Launch Date

January 13, 2025

Launch Site

Yellow Sea Launch Area (YSLA)

Launch Pad

LP4

Launch Vehicle

Jielong-3

Orbital Elements

NORAD ID

62577

International Designator

2025-007C

Epoch

Sun, 19 Jul 2026 19:16:03 GMT

Apogee

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Perigee

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Inclination

54.98°

Right Ascension

177.52°

Eccentricity

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Argument of Perigee

178.94°

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 S8

Alternative Name

Weili Kongjian 01-02

Type

Payload

Status

Operational

Owner

Beijing Future Navigation Technology Co., Ltd.

Country

China

Constellation

CentiSpace

Related Satellites

Major Events

Launched on January 13, 2025, CENTISPACE-1 S8 successfully entered its planned orbit and commenced operations to enhance GNSS services.

Latest TLEs
1 62577U 25007C   26200.80281529 -.00000128  00000+0  11647-4 0  9990
2 62577  54.9832 177.5240 0013784 178.9385 181.1603 13.80618219 79230

Source: Celestrak

Summary
The CENTISPACE-1 S8 satellite, also known as Weili Kongjian 01-02, was launched on January 13, 2025, from the Yellow Sea Launch Area (YSLA) using a Jielong-3 launch vehicle. It is part of the CentiSpace constellation and aims to enhance global navigation accuracy through GNSS augmentation services. The satellite has dimensions of 1 meter in length, 0.5 meters in diameter, and a span of 2 meters, with a dry mass of 160 kg. Equipped with two deployable solar arrays and batteries for power supply, it is designed to operate for approximately five years. It features three-axis stabilization, an aluminum alloy structure with composite materials, and is painted silver. The satellite includes a navigation augmentation payload and laser communication link, transmitting at frequencies of 1575.42 MHz and 1227.60 MHz. Its shape is a box with two solar panels, and it has a radar cross-section (RCS) of 0.1 square meters. The satellite was manufactured by DFHS and owned by Beijing Future Navigation Technology Co., Ltd.
Physical Characteristics

Length

1

Diameter

0.5

Span

2

Dry Mass

160

Launch Mass

160

Shape

Box with two solar panels

Radar Cross Section

0.1

Visual Magnitude

6.5

Color

Silver

Material Composition

Aluminum alloy structure with composite materials.

Technical Details

Payload

Navigation augmentation payload

Purpose

Technology ?

Mission

The CENTISPACE-1 S8 satellite is part of the CentiSpace constellation, aimed at providing GNSS augmentation services to enhance global navigation accuracy.

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 systems.

ADCS

Three-axis stabilization

Transmitter Frequency

1575.42 MHz, 1227.60 MHz

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