ASTRA 2E

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ASTRA 2E is classified as:

Geostationary
TV

NORAD ID: 39285

Int'l Code: 2013-056A

Perigee: 35,781.2 km

Apogee: 35,805.0 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.

1 39285U 13056A   25289.91824779  .00000139  00000-0  00000-0 0  9998
2 39285   0.0760 318.1950 0002826 244.8927 181.6987  1.00274095 43974

Source of the keplerian elements: AFSPC