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SUNSAT is classified as:

NORAD ID: 25636
Int'l Code: 1999-008C
Perigee: 647.0 km
Apogee: 854.1 km
Inclination: 96.5 °
Period: 99.7 minutes
Semi major axis: 7121 km
RCS: 0.4671 m2 (medium)
Launch date: February 23, 1999
Source: South Africa (SAFR)
Uplink (MHz): 436.291
Downlink (MHz): 145.825
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   16299.39343861  .00000113  00000-0  36839-4 0  9990
2 25636  96.4775 238.1769 0145424 347.9524  11.8207 14.44580578930874
Source of the keplerian elements: AFSPC