Official name ECHOSTAR 2
Alternative name EchoStar 2
Cospar ID 1996-055A
Norad ID 24313
Launch date 1996-09-11
Launch site FRGUI
Launch vehicle Ariane-42P H10-3
Country/Organization USA
Type application Communication (Direct Broadcasting)
Operator Dish Network Corporation (EchoStar)
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.26
Inclination (deg) 11.35
Perigee (km) 35739
Apogee (km) 35840
Eccentricity 0.00141102837424384
Mean motion (revs. per day) 1.00260398535084
Semi-Major axis (km) 42167.635
Raan (deg) 34.5416
Arg of perigee (deg) 78.0018
Shape Box + 2 Pan
Mass (kg) 1694.75
Height (m) 2.49
Width (m) 2.79
Depth (m) 2.79
Span (m^2) 23.88
Contractors Lockheed Martin
Equipment 16 Ku-band transponders
Propulsion 2 × LEROS-1b
Configuration AS-7000
Power 2 deployable solar arrays, batteries

EchoStar 1 is an American geostationary communications spacecraft that was launched by a CZ-2E with EPKM upper stage rocket from Xichang Center in Sichuan province, PRC. The 3288 kg spacecraft carries 16 Ku-band transponders to enable direct broadcast communications and television channels through 0.5 meter dishes on the ground in the American continents.

EchoStar 2 is mostly identical to its sister craft.

Satellite COSPAR Date LS Launch Vehicle Remarks
ECHOSTAR 1 1995-073A 1995-12-28 XSC CZ-2E [EPKM]
ECHOSTAR 2 1996-055A 1996-09-11 FRGUI Ariane-42P H10-3