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ASTRA 2E

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ASTRA 2E is classified as:


NORAD ID: 39285
Int'l Code: 2013-056A
Perigee: 35,782.2 km
Apogee: 35,805.6 km
Inclination: 0.1 °
Period: 1,436.1 minutes
Semi major axis: 42164 km
RCS: Unknown
Launch date: September 29, 2013
Source: SOCIETE EUROPEENNE DES SATELLITES (SES)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

ASTRA 2E, built by Astrium Satellites in France and based on the Eurostar E3000 platform, is designed to beam next-generation broadcast, direct-to-home and broadband services over Europe, the Middle East and Africa for a 15-year mission. It carries 60 Ku-band and four wideband Ka-band transponders to do the job.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 39285U 13056A   17086.40694804 +.00000136 +00000-0 +00000-0 0  9999
2 39285 000.0886 055.3992 0002773 305.9382 358.6580 01.00271281012812
Source of the keplerian elements: AFSPC