Article · Wikipedia archive · Last revised Jun 16, 2026

EOS 02

EOS-02 was an Indian Earth observation microsatellite developed by ISRO as a test payload on the maiden launch of the Small Satellite Launch Vehicle (SSLV). EOS-02 was based on Microsat-TD. The objective behind EOS-02 was to realize and fly an experimental imaging satellite with short turnaround time to showcase launch on demand capability.

Last revised
Jun 16, 2026
Read time
≈ 2 min
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449 w
Citations
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Source
EOS-02
NamesEOS-02 / Microsat-2A
Mission typeEarth observation
OperatorISRO
Websitehttps://www.isro.gov.in/
Mission duration55 minutes
Orbits completed<1
Spacecraft properties
SpacecraftEOS-02
ManufacturerISRO
Launch mass135 kg
Start of mission
Launch date03:48 UTC, 7 August 2022
RocketSmall Satellite Launch Vehicle
Launch siteSatish Dhawan Space Centre, First launch Pad (FLP)
ContractorISRO
End of mission
Decay date7 August 2022 04:43 UTC
Orbital parameters
RegimeLow Earth (intended)
Transatmospheric (achieved)
Periapsis altitude76 km (47 mi)
Apoapsis altitude356 (221 mi)
Inclination37.2

EOS-02 (formerly known as Microsat-2A) was an Indian Earth observation microsatellite developed by ISRO as a test payload on the maiden launch of the Small Satellite Launch Vehicle (SSLV).1 EOS-02 was based on Microsat-TD. The objective behind EOS-02 was to realize and fly an experimental imaging satellite with short turnaround time to showcase launch on demand capability.2

It was intended to be used for cartographic applications at a cadastral level, urban and rural management, coastal land use and regulation, utilities mapping, development and various other GIS applications. The satellite carried two payloads: a mid-wavelength and a long-wavelength infared camera with a 6m resolution.3

Launch

EOS-02 was launched on Small Satellite Launch Vehicle's maiden flight SSLV-D1 at 03:48 UTC / 09:18 IST on 7 August 2022,45 but due to the final VTM stage failure, the rocket entered a transatmospheric orbit of 356 km × 76 km (221 mi × 47 mi) instead of the planned circular 356 km (221 mi) circular orbit. As a result, both satellites onboard (EOS-02 and AzaadiSAT) were destroyed during reentry.6

References

References