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EGYPTSAT 2

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EGYPTSAT 2 is classified as:


NORAD ID: 39678
Int'l Code: 2014-021A
Perigee: 718.6 km
Apogee: 720.1 km
Inclination: 51.6 °
Period: 99.0 minutes
Semi major axis: 7090 km
RCS: Unknown
Launch date: April 16, 2014
Source: Egypt (EGYP)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

EGYPTSAT 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. EGYPTSAT 2 is based on RKK Energiya's 559GK bus, which inherits technologies from their USP platform. The satellite reportedly features 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.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE): 
1 39678U 14021A   19047.38252902 -.00000133  00000-0  10607-4 0  9999
2 39678  51.6216  99.7646 0001040 101.3781 258.7270 14.54133974257267
Source of the keplerian elements: AFSPC