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SUNSAT

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SUNSAT is classified as:


NORAD ID: 25636
Int'l Code: 1999-008C
Perigee: 645.7 km
Apogee: 855.8 km
Inclination: 96.4 °
Period: 99.7 minutes
Semi major axis: 7121 km
RCS: 0.4671 m2 (medium)
Launch date: February 23, 1999
Source: South Africa (SAFR)
Launch site: AIR FORCE WESTERN TEST RANGE (AFWTR)

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   16041.92576189 +.00000118 +00000-0 +37318-4 0  9993
2 25636 096.4494 042.0928 0147539 084.0578 277.7412 14.4452359089343
Source of the keplerian elements: AFSPC

N2YO: 886