INMARSAT 5-F2

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INMARSAT 5-F2 is classified as:

Geostationary

NORAD ID: 40384

Int'l Code: 2015-005A

Perigee: 35,792.6 km

Apogee: 35,795.0 km

Inclination: 0.0 °

Period: 1,436.1 minutes

Semi major axis: 42164 km

RCS: Unknown

Launch date: February 1, 2015
Source: International Mobile Satellite Organization (INMARSAT) (IM)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

INMARSAT 5 F2 was built in El Segundo, California, by Boeing Satellite Systems International, and it carries its own chemical and electric propulsion system to maneuver into a circular orbit 22,300 miles (35,888 km) over the equator in the coming weeks, where Inmarsat will complete testing of the platform and begin using it for commercial service. The satellite is about the size of a London double-decker bus, and it will extend power-generating solar panels to a span of 111 feet (33.8 m).

1 40384U 15005A   25199.40283027 -.00000279  00000-0  00000-0 0  9991
2 40384   0.0146  45.4503 0000292 341.2040 359.8196  1.00271591 37647

Source of the keplerian elements: AFSPC