Official name EGYPTSAT 2
Alternative name EgyptSat 2 (MisrSat 2)
Cospar ID 2014-021A
Norad ID 39678
Launch date 2014-04-16
Launch site TTMTR
Launch vehicle Soyuz-U
Country/Organization Egypt
Type application Earth Observation
Operator National Authority for Remote Sensing and Space Sciences
RCS size LARGE
Decay date ON ORBIT
Period (min) 98.97
Inclination (deg) 51.62
Perigee (km) 709
Apogee (km) 710
Eccentricity 0.000704721634954193
Mean motion (revs. per day) 14.5498635950288
Semi-Major axis (km) 7087.635
Raan (deg) 252.3709
Arg of perigee (deg) 64.2239
Shape Hex Cyl + 3 Pan
Mass (kg) 1050
Diameter (m) 0.8
Height (m) 2
Span (m^2) 5
Lifetime 11 years (planned); 1 year (achieved)
Contractors RKK Energiya (prime); OAO Peleng, NIRUP Geoinformatsionnye Sistemy (payload)
Propulsion SPD-70 Xe plasma thrusters
Configuration 559GK bus
Power 3 deployable fixed solar arrays, batteries

EgyptSat 2 (MisrSat 2) is Egypt's second Earth remote-sounding satellite. The satellite is jointly built by Egypt's National Authority for Remote Sensing and Space Sciences together with RKK Energiya in Russia. The imaging payload was developed by OAO Peleng and NIRUP Geoinformatsionnye Sistemy in Belarus.

The satellite is based on RKK Energiya's 559GK bus, which inherits technologies from their USP platform. The satellite features SPD-70 electric engines using Xenon.

EgyptSat-2 has a resolution of 1 m in panchromatic mode and 4 m in multispectral mode. The camera can take both single frame images or stereoscopic images and can operate in push-broom continuous imaging mode or in a cartographic mode.

The satellite was launched on a Soyuz-U booster from Baikonur cosmodrome in April 2014 into an transfer orbit (440 by 720 kilometer, 51.6°) to an unusual non sun-synchronous orbit. It circularized its orbit with its onboard ion engines.

According to industry sources, a dual failure in the flight control system caused a loss of the satellite in April 2015 after only one year in orbit.

Satellite COSPAR Date LS Launch Vehicle Remarks
EGYPTSAT 2 2014-021A 2014-04-16 TTMTR Soyuz-U