Official name DEIMOS 2
Alternative name Deimos-2
Cospar ID 2014-033D
Norad ID 40013
Launch date 2014-06-19
Launch site OREN
Launch vehicle Dnepr
Country/Organization Spain
Type application Earth Observation
Operator Deimos → Urthecast
RCS size LARGE
Decay date ON ORBIT
Period (min) 96.74
Inclination (deg) 97.69
Perigee (km) 601
Apogee (km) 604
Eccentricity 0.0024896265560166
Mean motion (revs. per day) 14.8852594583419
Semi-Major axis (km) 6980.635
Raan (deg) 19.3511
Arg of perigee (deg) 61.0261
Shape Hex Cyl + 3 Pan
Mass (kg) 300
Diameter (m) 1.2
Height (m) 1.3
Span (m^2) 3
Contractors Satrec Initiative (SATRECI)
Equipment EOS-D camera
Propulsion Hall Effect Propulsion System (HEPS)
Configuration SI-300 bus
Power 4 deployable fixed solar arrays, batteries

Deimos 2 is a small Earth observation satellite, which carries a 75-centimeter-resolution imager provided by Satrec Initiative of South Korea. It has a 12-kilometer-diameter swath and be able to swivel 30 degrees off nadir to each side, and 45 degrees in the event of a special order.

Spain?s government-owned Inta performed satellite integration of the 300 kilogram Deimos-2. Deimos? corporate parent, Elecnor of Madrid, has agreed to underwrite much of the 60 million euros in anticipated Deimos-2 costs, a figure that includes the satellite?s construction, launch and insurance. Spain?s Ministry of Industry, Tourism and Trade is picking up 20 percent of Deimos? costs.

Deimos has booked a launch as part of a multi satellite launch aboard Dnepr launch vehicle operated by Kosmotras of Moscow.

Elecnor Deimos Space in June 2015 announced to sell the Deimos Imaging division and the satellites to UrtheCast.

Satellite COSPAR Date LS Launch Vehicle Remarks
DEIMOS 2 2014-033D 2014-06-19 OREN Dnepr with KazEOSat 2, Saudisat 4, TabletSat-Aurora, BugSat 1, AprizeSat 9, AprizeSat 10, UniSat 6, BRITE-CA 1, BRITE-CA 2, Hodoyoshi 3, Hodoyoshi 4, Perseus-M 1, Perseus-M 2, Flock-1c 1, ..., 11, POPSAT-HIP 1, QB50P1, QB50P2, PACE, TigriSat, ANTELSAT, Lemur 1, NanoSatC-Br 1, Duchifat 1, PolyITAN 1, DTUSat 2, AeroCube 6A, AeroCube 6B