Official name EXPRESS AM-2
Alternative name Ekspress-AM 2
Cospar ID 2005-010A
Norad ID 28629
Launch date 2005-03-29
Launch site TTMTR
Launch vehicle Proton-K Blok-DM-2M
Country/Organization Russia
Type application Communication
Operator RSCC (Kosmicheskiya Svyaz)
RCS size LARGE
Decay date ON ORBIT
Period (min) 1453.94
Inclination (deg) 7.92
Perigee (km) 36047
Apogee (km) 36224
Eccentricity 0.00244911513608501
Mean motion (revs. per day) 0.990412259102852
Semi-Major axis (km) 42513.635
Raan (deg) 62.5295
Arg of perigee (deg) 76.2964
Shape Cyl + 2 Pan
Mass (kg) 2542
Diameter (m) 2
Height (m) 2
Span (m^2) 27
Lifetime 12 years
Contractors NPO Prikladnoi Mekhaniki (NPO PM) (Bus), Alcatel (Payload)
Equipment 4 Ku-band (140 W), 8 Ku-Band (101 W), 4 C-band (100 W), 1 C-band (100 W), 11 C-band (60 W), 1 L-band (30 W) transponders
Propulsion 8 × SPT-100 Stationary Plasma Thrusters
Configuration MSS-2500-GSO (MSS-767)
Power 2 deployable solar arrays, batteries

The Ekspress-AM 2 and 3 series are communications satellites for Russian domestic communication services. The lifetime of the spacecraft has been increased to 12 years. While the spacecraft itself is built by Russian RSCC (Kosmicheskiya Svyaz), the communication payloads are built by Alcatel.

The satellite was retired in 2016 and was moved into a graveyard orbit above the geostationary belt.

Satellite COSPAR Date LS Launch Vehicle Remarks
EXPRESS AM-2 2005-010A 2005-03-29 TTMTR Proton-K Blok-DM-2M
EXPRESS AM-3 2005-023A 2005-06-24 TTMTR Proton-K Blok-DM-2