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ExseedSat-1 Amateur Radio CubeSat (VO-96)

Satellize
ExseedSat-1 Amateur Radio CubeSat (VO-96)

ExseedSat-1 (OSCAR designation VO-96 / VUsat-OSCAR 96) is India’s first privately built and operated satellite, launched December 3, 2018 aboard a SpaceX Falcon 9 (SSO-A rideshare mission) from Vandenberg AFB into a polar sun-synchronous orbit at approximately 600 km altitude. Built by a team of 8 scientists from Exseed Space (now Satellize) in approximately 4 […]

Key figurescomparable across the catalogue

Mass
1 kg
Power
2.8 W

Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.

As published by the supplier

Form factor
1U CubeSat (10 × 10 × 10 cm)
Mass
~1 kg
Material
Aluminium alloy
Orbit
Polar SSO, ~600 km altitude
Launch date
December 3, 2018
Launch vehicle
SpaceX Falcon 9 v1.2 Block 5 (SSO-A mission)
OSCAR designation
VO-96 (VUsat-OSCAR 96)
Beacon frequency
145.900 MHz FM
Payload
UHF/VHF NBFM amateur radio transponder; APRS digipeater; CW beacon (Morse 'V' + RTTY telemetry)
Solar power
~2.8 W average from solar cells
TX power
0.5 W or 1 W (selectable)
CTCSS squelch
67 Hz
Estimated lifetime
2–5 years (battery-dependent)
Build cost
~₹2 crore (~$240,000 USD)
Build time
~4 months, team of 8

About

ExseedSat-1 (OSCAR designation VO-96 / VUsat-OSCAR 96) is India’s first privately built and operated satellite, launched December 3, 2018 aboard a SpaceX Falcon 9 (SSO-A rideshare mission) from Vandenberg AFB into a polar sun-synchronous orbit at approximately 600 km altitude. Built by a team of 8 scientists from Exseed Space (now Satellize) in approximately 4 months at a cost of roughly ₹2 crore (~$240,000 USD), the satellite is a 1U CubeSat (10 × 10 × 10 cm, ~1 kg) constructed from aluminium alloy and equipped with a multifunction UHF/VHF amateur radio transponder payload. ExseedSat-1 serves the global ham radio community by providing an FM-mode transponder, an APRS digipeater (VHF downlink on 145.900 MHz), and a CW (Morse code) beacon — transmitting ‘V’ in Morse followed by radio teletype (RTTY) telemetry every minute. Solar cells provide average 2.8 W power with selectable transmit power of 0.5 W or 1 W. ExseedSat-1 is intended to provide backup emergency communications capability when conventional terrestrial infrastructure fails. As India’s first private satellite, it demonstrated that a small team with limited resources could build and operate a functioning spacecraft — proving the commercial viability of low-cost CubeSat manufacturing in India and laying the groundwork for Satellize’s broader nanosatellite platform offering.

Documentation

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

Source: www.satellize.com ↗

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