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ASTRA 2E

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ASTRA 2E is classified as:


NORAD ID: 39285
Int'l Code: 2013-056A
Perigee: 35,783.7 km
Apogee: 35,801.7 km
Inclination: 0.1 °
Period: 1,436.0 minutes
Semi major axis: 42163 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   19080.87554906 +.00000125 +00000-0 +00000-0 0  9992
2 39285 000.0864 058.3973 0002129 301.3262 163.0683 01.00275558019957
Source of the keplerian elements: AFSPC