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SUNSAT

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SUNSAT is classified as:


NORAD ID: 25636
Int'l Code: 1999-008C
Perigee: 645.9 km
Apogee: 856.0 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)

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   15185.76909199  .00000152  00000-0  46124-4 0  9997
2 25636 096.4641 233.9104 0147548 065.8802 067.8195 14.44456502861785

Source of the keplerian elements: AFSPC

N2YO: 184