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SUNSAT

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SUNSAT is classified as:


NORAD ID: 25636
Int'l Code: 1999-008C
Perigee: 644.9 km
Apogee: 853.8 km
Inclination: 96.5 °
Period: 99.7 minutes
Semi major axis: 7120 km
RCS: 0.4671 m2 (medium)
Launch date: February 23, 1999
Source: South Africa (SAFR)
Launch site: AIR FORCE WESTERN TEST RANGE (AFWTR)

Uplink (MHz): 436.291
Downlink (MHz): 145.825/2250.000
Beacon (MHz): 145.825
Mode: 9600bps FM
Call sign: SUNSAT-3
Status: Inactive


Sunsat was a micro-satellite built by post-graduate engineering students at the University of Stellenbosch in South Africa. Launched by a Delta II launch vehicle, its payload included NASA experiments, amateur radio communications, a high resolution imager, precision attitude control, and school experiments.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 25636U 99008C   22341.73004667  .00000224  00000-0  63693-4 0  9992
2 25636  96.4528 141.4791 0146737  98.8933 262.8908 14.44939925253211
Source of the keplerian elements: AFSPC