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SUNSAT

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SUNSAT is classified as:


NORAD ID: 25636
Int'l Code: 1999-008C
Perigee: 647.1 km
Apogee: 854.9 km
Inclination: 96.5 °
Period: 99.7 minutes
Semi major axis: 7122 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   15147.73456870  .00000121  00000-0  38695-4 0  9995
2 25636 096.4672 204.9302 0145892 185.5033 288.7297 14.44439428856298

Source of the keplerian elements: AFSPC

N2YO: 306