Official name LUCH 5B
Alternative name Luch 5B
Cospar ID 2012-061A
Norad ID 38977
Launch date 2012-11-02
Launch site TTMTR
Launch vehicle Proton-M Briz-M (Ph.3)
Country/Organization Russia
Type application Communication, data relay
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.1
Inclination (deg) 9.64
Perigee (km) 35777
Apogee (km) 35796
Eccentricity 0.000265463233342182
Mean motion (revs. per day) 1.00271568832254
Semi-Major axis (km) 42164.635
Raan (deg) 53.6178
Arg of perigee (deg) 124.5642
Shape Box + 2 Pan
Mass (kg) 1282
Height (m) 6
Width (m) 2
Depth (m) 2
Span (m^2) 20.8
Lifetime 10 years
Contractors ISS Reshetnev (ex NPO Prikladnoi Mekhaniki, NPO PM)
Equipment ?
Propulsion ?
Configuration Ekspress-1000AM (3-Axis stabilized, 2 solar arrays)
Power 2 deployable solar arrays, batteries

The Luch-5 are the Russian follow-on relay satellites, which replace the Luch (Altair) and Luch-2 (Gelios) satellites. Two satellites named Luch 5A and Luch 5B were procured for launches in 2010 and 2011. The smaller satellites are based on the Ekspress-1000 bus and were launched with a co-passenger on Proton-M Briz-M boosters.

S- and Ku-band data relay channels of each satellite will be linked with receive/transmit points via satellite communications links.

Each data relay satellite is capable of orienting its high-precision antennas towards low-flying space objects so as to ?catch? and ?track? them along their trajectories. Moreover, each of the two user antennas is capable of tracking its ?own? low-flying space object. One antenna will operate in the Ku-band, the other ? in the S-band, with the Ku-band channel capacity at 150 Mbit/s and the S-band channel capacity at up to 5 Mbit/s.

The satellite carries also a payload to send differential correction signals for the GLONASS satellite navigation system. Additionally, the Luch-5B spacecraft carries a laser-communication device.

Satellite COSPAR Date LS Launch Vehicle Remarks
LUCH 5B 2012-061A 2012-11-02 TTMTR Proton-M Briz-M (Ph.3) with Yamal 300K