Official name HELLAS-SAT 1 (DFS 3)
Alternative name DFS-Kopernikus 3
Cospar ID 1992-066A
Norad ID 22175
Launch date 1992-10-12
Launch site AFETR
Launch vehicle Delta-7925
Country/Organization Germany
Type application Communication
Operator Deutsche Bundespost Telekom → Deutsche Telekom
RCS size LARGE
Decay date ON ORBIT
Period (min) 1443.94
Inclination (deg) 13.83
Perigee (km) 35926
Apogee (km) 35954
Eccentricity 0.000389538119087368
Mean motion (revs. per day) 0.997271354765433
Semi-Major axis (km) 42318.135
Raan (deg) 12.6382
Arg of perigee (deg) 97.365
Shape Hex Poly + 2 Pan
Mass (kg) 639.25
Height (m) 3.4
Width (m) 1.7
Depth (m) 1.7
Span (m^2) 15.38
Lifetime 10 years
Contractors GESAT (MBB, Dornier, ANT, Siemens, SEL)
Equipment 10 (+5) Ku-band transponders, 1 Ka-band transponder
Propulsion S400
Configuration GESAT-Bus
Power 2 deployable solar arrays, batteries

The DFS series of satellites debuted in 1989 with the third being launched in 1992. Ordered in 1983 and produced by the GESAT consortium of MBB (flight segment prime contractor), Siemens (overall prime contractor), ANT Nachrichtentechnik (payload), Standard Elektrik Lorenz (digital switching equipment), and Dornier Systems (ground control system), DFS spacecraft are smaller than TV-Sat: on-station mass of DFS is 850 kg with a 15.4 m solar array span providing up to 1.5 kW of electrical power.

The communications payload includes ten 14/11-12 GHz transponders with five spares and one experimental 30/20 GHz transponder with one spare. At the end of 1994 DFS 1-3 were stationed at 33.5 degrees E, 28.5 degrees E, and 23.5 degrees E, respectively. Like TV-Sat, the DFS Kopernikus series has been concluded.

DFS 3 was leased to the greek Hellas Sat in 2002 as a stop-gap measure. It was retired in 2003.

Satellite COSPAR Date LS Launch Vehicle Remarks
DFS 1 1989-041B 1989-06-05 FRGUI Ariane-44L H10 with Superbird A
DFS 2 1990-063B 1990-07-24 FRGUI Ariane-44L H10 with TDF 2
HELLAS-SAT 1 (DFS 3) 1992-066A 1992-10-12 AFETR Delta-7925