SDX02 (62460)

COSPAR: 2024-253B | Alt Name: SPADEX-B

Image
SDX02 Satellite Image
Launch Details

Launch Date

December 30, 2024

Launch Site

Satish Dhawan Space Centre

Launch Pad

First Launch Pad

Launch Vehicle

PSLV-C60

Orbital Elements

NORAD ID

62460

International Designator

2024-253B

Epoch

Sun, 19 Jul 2026 20:25:45 GMT

Apogee

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Perigee

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Inclination

54.99°

Right Ascension

193.11°

Eccentricity

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Argument of Perigee

28.06°

Period

91.43 min

Mean Motion

15.75 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

SDX02

Alternative Name

SPADEX-B

Type

Payload

Status

Operational

Owner

ISRO

Country

India

Constellation

N/A

Related Satellites

Major Events

Successful docking with SDX01 on January 16, 2025.

Latest TLEs
1 62460U 24253B   26200.85122498  .00048281  00000+0  32020-3 0  9995
2 62460  54.9931 193.1102 0006000  28.0619 332.0747 15.75052894 87669

Source: Celestrak

Summary
SDX02, also known as SPADEX-B, is a microsatellite designed and manufactured by Ananth Technologies under ISRO's guidance. Launched on December 30, 2024, from the Satish Dhawan Space Centre using PSLV-C60, it has dimensions of 1 meter in length, 0.5 meters in diameter, and a span of 2.5 meters when its solar arrays are deployed. The satellite weighs 220 kilograms at launch and operates with two deployable solar arrays and batteries for power supply. It is equipped with a Radiation Monitor (RadMon) payload to measure radiation dose encountered in space. The mission objectives include demonstrating autonomous rendezvous and docking capabilities, validating power transfer between docked spacecraft, and operating scientific payloads post-undocking. SDX02 achieved successful docking with SDX01 on January 16, 2025. The satellite is stabilized by a three-axis system and has an aluminum and composite material construction. It is designed for a mission duration of two years.
Physical Characteristics

Length

1

Diameter

0.5

Span

2.5

Dry Mass

180

Launch Mass

220

Shape

Box with two solar panels

Radar Cross Section

0.1

Visual Magnitude

5.5

Color

Silver

Material Composition

Aluminum and composite materials

Technical Details

Payload

Radiation Monitor (RadMon) payload

Purpose

Technology, docking

Mission

To demonstrate autonomous rendezvous and docking capabilities, validate power transfer between docked spacecraft, and operate scientific payloads post-undocking.

Manufacturer

Ananth Technologies under ISRO guidance

Life Expectancy

Designed for a mission duration of two years, operating payloads post-undocking.

Bus

SPADEX

Configuration

Microsatellite-SSB (SSB-2)

Motor

N/A

Equipment

Radiation Monitor (RadMon) payload to measure radiation dose encountered in space.

Power System

2 deployable solar arrays, batteries

ADCS

Three-axis stabilization

Transmitter Frequency

Unknown

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