Official name NILESAT 201
Alternative name Nilesat 201
Cospar ID 2010-037A
Norad ID 36830
Launch date 2010-08-04
Launch site FRGUI
Launch vehicle Ariane-5ECA
Country/Organization Egypt
Type application Communication
Operator Nilesat
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.09
Inclination (deg) 0.04
Perigee (km) 35770
Apogee (km) 35803
Eccentricity 0.000461067721068001
Mean motion (revs. per day) 1.00272267058471
Semi-Major axis (km) 42164.635
Raan (deg) 102.3238
Arg of perigee (deg) 328.8465
Shape Box + 2 Pan
Mass (kg) 3200
Height (m) 2.9
Width (m) 1.8
Depth (m) 1.8
Span (m^2) 29.6
Lifetime 15 years
Contractors Thales Alenia Space
Equipment 28 Ku-band transponders, 4 Ka-band transponders
Propulsion S400
Configuration Spacebus-4000B2
Power 2 deployable solar arrays, batteries

Nilesat 201 is an Egyptian geostationary communication satellite operating in Ku- and Ka-bands.

Telecommunications satellite operator Nilesat Co. of Egypt has selected Thales Alenia Space of France and Italy in May 2008 to build the Nilesat 201 satellite, which is scheduled to be launched in early 2010 aboard a European Ariane 5 rocket.

The Nilesat 201 satellite, to be launched into Nilesat's 7 ° West slot, will be a Thales Alenia Space Spacebus-4000B2 platform and is expected to weigh 3,200 kilograms at launch and deliver 5.7 kilowatts of power to the payload. It will carry 28 Ku-band transponders and four transponders in Ka-band for direct-to-home television, radio and data-transmissions in the Middle East and North Africa.

The satellite is expected to retire in 2028. It will be replaced by Nilesat 301.

Satellite COSPAR Date LS Launch Vehicle Remarks
NILESAT 201 2010-037A 2010-08-04 FRGUI Ariane-5ECA with RASCOM-QAF 1R