HARDWARE / PRODUCTAdded 9 Jul 2026

Satellite platform SXC6 modification “ADC”

SPUTNIX
Spacecraft up to 10 kg · Nano class (FAA) what this means
Satellite platform SXC6 modification “ADC”

A mid-tier 6U CubeSat platform configuration of the SXC6 family with basic three-axial ADCS, allowing the spacecraft to be oriented in space via redundant subsystems.

Typed specifications28 values

Discloses 5 of 7 fields engineers filter by in this category (category median 3).

Mass
5 kg
product page 12 kg
Envelope (L×W×H)
118.6x228.6x366 mm
product page 118.6x228.6x820 mm
Power consumption
10 W
product page 50 W
Form factor
6U
CubeSat 6U · datasheet p.2
Max payload mass
6 kg
max · max mass of payload, up to (Table 1) · datasheet p.2
Payload volume, U
3 U
3U+ available volume for payload (Table 1) · datasheet p.2
Payload envelope (L × W × H)
85 x 85 x 300
3U+ available volume for payload (Table 1) · datasheet p.2
Power available to payload
8 W
max · available average capacity of payload, up to (Table 1) · datasheet p.2 25 W max · peak (max available capacity of payload, up to; Table 1)
Battery capacity
78 Wh
product page
Attitude control
3-axis stabilised
three-axis w/ reaction wheels, star tracker, magnetometer, an… · datasheet p.2
Pointing accuracy
0.1 °
ADCS accuracy, up to 0.1° (Table 1) · datasheet p.2
Payload data downlink rate
57.6 kbps
product page
Radio band
X
high-speed X-band radio link, included · datasheet p.2 UHF UHF command radio link, included, redundant
Subsystems included
solar arrays
deployable solar panels, included · datasheet p.2 GNSS receiver GPS-receiver, included  |  X-band downlink high-speed X-band radio link, included  |  ADCS three-axis ADCS w/ reaction wheels and star tracker  |  UHF or VHF radio UHF command radio link, included, redundant
Max satellite wet mass
10 kg
mass w/ payload (Table 1 platform comparison, generic SXC6 co… · datasheet p.2
Deployables
hinges for solar wings
deployable solar panels included · datasheet p.2
Deployables (as printed)
Deployable solar panels (included)
datasheet p.2
Satellite class
CubeSat
CubeSat nanosatellite platform line · datasheet p.2
Form factor, U (number)
6 U
CubeSat 6U · datasheet p.2

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 supplier17 lines, in the manufacturer's own wording
Outer dimensions transport mode
118.6x228.6x366 mm
Outer dimensions deployed
118.6x228.6x820 mm
Mass (w/o payload)
5 kg
Maximum mass
12 kg
Battery capacity
78 Wh
Peak power per solar panel
not less than 35 W
Service radio frequency
435-438 or 400-401 MHz
Data rate
2400-57600 bps
ADCS algorithms
B-DOT, sun orientation, nadir, point trace
Sensors
Sun sensors, Angular velocity sensor, Magnetometer
ADCS pointing accuracy sunlit orbit
up to 1 deg
ADCS pointing stability sunlit orbit
up to 0.1 deg
ADCS pointing accuracy eclipse orbit
up to 10 deg
Onboard interface
CAN2.0B, SPUTNIX UniCAN
Average payload power per orbit
10 W
Maximum payload power
50 W
Payload volume
4U

About

The SXC6-ADC modification adds basic three-axial ADCS to the SXC6 platform: redundant power supply with battery and deployable solar panels, redundant UHF transceiver with patch/deployable antennas, redundant electromagnetic damping system, redundant ADCS control unit with sensors, partially redundant reaction wheels unit, and solar sensors. Available upgrades: XTX (X-band transmitter+antenna), GNSS, CAM, MGM, STAR tracker kit.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: sputnix.ru ↗

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