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EgyptSat-2

EgyptSat-2, also known as MisrSat-2 or E-Star, was an Egyptian high-resolution optical remote-sensing satellite. It launched from Baikonur on 2014-04-16 aboard Soyuz-U and used the RSC Energia 559GK bus.[1][2]

The optical payload provided panchromatic and multispectral imagery at 1 m panchromatic resolution and 4 m multispectral resolution across a 1400 km swath.[2][3] The spacecraft launched to a 436 x 703 km orbit at 51.6 degrees and later raised its orbit to approximately 720 km via electric-propulsion circularisation.[2][3] The mission ended after losing contact on 2015-04-14.[2][3] Its applications include land-cover change, urban change, and disaster damage assessment.[2]

Full specification

All fields

current statusended
operatorNational Authority for Remote Sensing and Space Sciences
platform559gk-bus
launch vehiclesoyuz-u
Launched2014-04-16
actual end of life2015-04-14
orbit typeLow Earth orbit; launched to about 436 x 703 km, 51.6 deg, later circularised near 720 km
swath km1400
tasking supportedfalse
current geographic priorityEgyptian territory and neighbouring land and maritime areas
Last updated2026-06-21
claim statusagency-sourced
Where this fits, supply chain

Compositional position

this ——— msi-egyptsat-2 payload
this ——— RSC Energia 559GK bus bus
this ——— Land cover change related-topic
this ——— Urban change related-topic
this ——— Disaster damage assessment related-topic
this ——— EgyptSat-1 predecessor
EgyptSat-A ——— this predecessor
Sources
Cite https://eo-atlas.org/missions/egyptsat-2 Markdown twin → Field definitions →