CENTISPACE-1 S7 (62576)

COSPAR: 2025-007B | Alt Name: Weili Kongjian 01-01

Image
CENTISPACE-1 S7 Satellite Image
Launch Details

Launch Date

January 13, 2025

Launch Site

Yellow Sea Launch Area

Launch Pad

LP4

Launch Vehicle

Jielong-3

Orbital Elements

NORAD ID

62576

International Designator

2025-007B

Epoch

Sun, 19 Jul 2026 21:21:22 GMT

Apogee

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Perigee

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Inclination

54.97°

Right Ascension

177.62°

Eccentricity

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Argument of Perigee

124.81°

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 S7

Alternative Name

Weili Kongjian 01-01

Type

Payload

Status

Operational

Owner

Centispace

Country

China

Constellation

Centispace-1

Related Satellites

Major Events

Launched on January 13, 2025, CENTISPACE-1 S7 successfully entered its designated orbit and commenced operations to enhance GNSS services.

Latest TLEs
1 62576U 25007B   26200.88984691 -.00000107  00000+0  31711-4 0  9998
2 62576  54.9745 177.6176 0013669 124.8083 235.4161 13.80615695 79235

Source: Celestrak

Summary
The CENTISPACE-1 S7 satellite, also known as Weili Kongjian 01-01, is a part of the Centispace-1 LEO constellation, designed to enhance global navigation services through GNSS augmentation signals. Launched on January 13, 2025, from Yellow Sea Launch Area LP4 using the Jielong-3 launch vehicle, it successfully entered its designated orbit and began operations three hours post-launch. The satellite, manufactured by DFH Shenzhen, has a WN-100 bus configuration and is powered by two deployable solar arrays and batteries. It features a laser communication link for data transmission at 2259.68 MHz frequency and operates with a silver-colored aluminum alloy structure shaped as a box equipped with two solar panels. With dimensions of 1 meter in length, 0.5 meters in diameter, and a span of 2 meters, it has a dry mass of 160 kilograms and is designed for a mission duration of approximately five years. It employs three-axis stabilization and has an RCS value of 0.3 with a VMAG of 6.5. This satellite is part of a constellation that includes CENTISPACE-1 S8, S9, and S10, and aims to significantly improve navigation services globally.
Physical Characteristics

Length

1

Diameter

0.5

Span

2

Dry Mass

160

Launch Mass

160

Shape

Box with two solar panels

Radar Cross Section

0.3

Visual Magnitude

6.5

Color

Silver

Material Composition

Aluminum alloy structure

Technical Details

Payload

Navigation augmentation payload

Purpose

Technology ?

Mission

The CENTISPACE-1 S7 satellite is part of a low Earth orbit (LEO) constellation aimed at providing GNSS augmentation signals to enhance global navigation services.

Manufacturer

DFH Shenzhen

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

2259.68 MHz

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