HARDWARE / PRODUCTAdded 1 Jul 2026

XDSAT M600

XDLINX Space Labs
XDSAT M600

Micro-satellite platform for payloads up to 300 kg, in-orbit qualified in 2026 with an India-built multispectral optical payload.

Typed specifications7 values

Discloses 0 of 7 fields engineers filter by in this category (category median 3).

Power consumption
1 100 W
product page
Power generation (orbit average)
600 W
product page
Battery capacity
1 100 Wh
product page
Propulsion
included
product page
Payload data downlink rate
500 000 kbps
max · X-band downlink · product page
Radio band
X
product page
Flight heritage
Q4-2024; in-orbit qualified June 2026
product page

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier12 lines, in the manufacturer's own wording
Bus type
M600
Bus os
Antaris SatOS — distributed compute for bus, payload edge and SDR
Payload volume / mass
75-100 kg (up to 300 kg per 2026 mission announcement)
Payloads CAN support
EO Optical, SAR, Siglnt, IoT, Laser
Pointing accuracy & stability / orbit knowledge
±0.002° (1-sigma), 3 axes, 2 Trackers
Power storage
1100 Wh
Solar panels
600 W
Propulsion
Multiple Electric & Chemical Propulsion Systems Available
TT&C, sw update
Secure & Flexible via S-Band SDR & UHF
Data downlink
X-band up to 500 Mbps
Ground control
Public or Private GS with Antaris MC Software
Flight heritage
Q4-2024; in-orbit qualified June 2026

About

XDSAT M600 is the largest micro-satellite platform in XDLINX Space Labs’ XDSAT family, originally specified for 75-100 kg payloads and, following its June 2026 in-orbit qualification, rated to support missions up to 300 kg. It supports EO optical, SAR, SIGINT, IoT and laser payloads on the Antaris SatOS distributed compute stack across bus, payload edge and SDR, with 3-axis pointing accuracy and stability of ±0.002° (1-sigma) using 2 star trackers. Power is supplied by 600 W solar panels with 1100 Wh of storage, with multiple electric and chemical propulsion systems available. TT&C and software updates run securely via S-band SDR and UHF, with X-band downlink up to 500 Mbps, and ground control through public or private ground stations using Antaris mission control software. In June 2026 XDLINX announced in-orbit qualification of the M600 platform together with a multispectral imaging (MSI) optical payload, entirely built in India, with modular architecture supporting Earth observation, defence, maritime intelligence, climate monitoring, communication and infrastructure analytics applications, assembled and tested with partner Ananth Technologies and with more than 20 satellite missions planned over the following two years.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: xdlinx.space ↗

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