Official name FREJA
Alternative name Freja
Cospar ID 1992-064A
Norad ID 22161
Launch date 1992-10-06
Launch site JSC
Launch vehicle CZ-2C
Country/Organization Sweden
Type application Research, magnetospheric
Operator SSC
RCS size LARGE
Decay date ON ORBIT
Period (min) 108.12
Inclination (deg) 62.98
Perigee (km) 545
Apogee (km) 1735
Eccentricity 0.521929824561403
Mean motion (revs. per day) 13.3185349611543
Semi-Major axis (km) 7518.135
Raan (deg) 64.301
Arg of perigee (deg) 171.996
Shape Trunc Cone + 2 Ant
Mass (kg) 257
Height (m) 0.5
Width (m) 2.2
Depth (m) 22
Span (m^2) 22
Lifetime 2.5 years
Contractors SSC
Propulsion Star-13A (PKM), Star-6 (AKM)
Power Solar cells, batteries

The Freja magnetospheric research satellite was launched on 6 October 1992 as a "piggyback" payload on a Long March 2C (CZ-2C) rocket from the Jiuquan Satellite Launch Center in China. The satellite is in an orbit between 601 and 1756 km at 63o inclination. Freja is a sun-pointing spinner with a 2.2 m diameter and 214 kg dry mass.

The Swedish Space Corporation is the Prime Contractor to the Swedish National Space Board (SNSB). Freja images the aurora and measures particles and fields in the upper ionosphere and lower magnetosphere. Swedish, German, Canadian and U.S. instruments are flown on the satellite.

The total cost of the Freja program including satellite, launch, ground system and 2.5 years of operation, but excl. experiments was $19 million (FY95). The satellite has been in operation for more than 1000 days.

Satellite COSPAR Date LS Launch Vehicle Remarks
FREJA 1992-064A 1992-10-06 JSC CZ-2C with FSW-2 4