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SES 7 (PROTOSTAR 2)

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SES 7 (PROTOSTAR 2) is classified as:


NORAD ID: 34941
Int'l Code: 2009-027A
Perigee: 35,786.0 km
Apogee: 35,801.1 km
Inclination: 0.1 °
Period: 1,436.1 minutes
Semi major axis: 42164 km
RCS: 7.9433 m2 (large)
Launch date: May 16, 2009
Source: SOCIETE EUROPEENNE DES SATELLITES (SES)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

The 8,609-pound [3,905-kg] ProtoStar 2 satellite carries its own propulsion system to reach a final geosynchronous orbit 22,300 miles [35,900 km] over the equator. The spacecraft will be positioned in a slot at 107.7 degrees east longitude in the geosynchronous belt, allowing it to reach customers in Indonesia, India, the Philippines and Taiwan. ProtoStar 2, also called IndoStar 2, is outfitted with 13 S-band and 27 Ku-band transponders on a Boeing 601HP satellite platform designed to last at least 15 years.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 34941U 09027A   18292.55033929 -.00000352 +00000-0 +00000-0 0  9998
2 34941 000.0899 091.9714 0001792 141.9563 100.4637 01.00272436034584
Source of the keplerian elements: AFSPC