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ASTRA 2E

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ASTRA 2E is classified as:


NORAD ID: 39285
Int'l Code: 2013-056A
Perigee: 35,784.6 km
Apogee: 35,802.1 km
Inclination: 0.0 °
Period: 1,436.1 minutes
Semi major axis: 42164 km
RCS: Unknown
Launch date: September 29, 2013
Source: SOCIETE EUROPEENNE DES SATELLITES (SES)

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   15188.24672691  .00000136  00000-0  10000-3 0  9996
2 39285 000.0461 341.6496 0002079 135.8957 284.5169 01.00273158  6502

Source of the keplerian elements: AFSPC

N2YO: 280