Fox 1C [AMSAT]
Official name AO-95
Alternative name Fox-1Cliff
Cospar ID 2018-099N
Norad ID 43770
Launch date 2018-12-03
Launch site AFWTR
Launch vehicle Falcon-9 v1.2 (Block 5)
Country/Organization USA
Type application Amateur communication, technology
Operator AMSAT, Vanderbilt University, Virginia Tech
RCS size SMALL
Decay date ON ORBIT
Period (min) 94.93
Inclination (deg) 97.49
Perigee (km) 509
Apogee (km) 521
Eccentricity 0.0116504854368932
Mean motion (revs. per day) 15.169071947751
Semi-Major axis (km) 6893.135
Raan (deg) 203.9939
Arg of perigee (deg) 260.2034
Shape Box
Mass (kg) 1
Height (m) 0.1
Width (m) 0.1
Depth (m) 0.1
Span (m^2) 0.1
Contractors AMSAT
Propulsion None
Configuration CubeSat (1U)
Power Solar cells, batteries

Fox-1C is a radio amateur and technology research cubesat developed by AMSAT and hosting several university developed payloads.

Fox-1C is an 1U CubeSat designed to operate in Low Earth Orbit built on the flight spare of Fox 1A. It carries a 2 meter whip antenna and a 70 cm whip antenna.

As affordable launch opportunities for amateur communications satellites become more rare, AMSAT deviced a new strategy: a small cubesat, which hosts both an amateur communications payload as well as a scientific or technological payload, so that the satellite qualifies for launches in sponsored programs like NASA's Educational Launch of Nanosatellites (ELaNa) Program.

Fox-1C will carry a radiation effects experiment developed by the Institute for Space and Defense Electronics (ISDE) at Vanderbilt University, a Virginia Tech camera experiment, and a Pennsylvania State-Erie MEMS gyro experiment.

Fox-1C will also serve as a communications relay for amateurs worldwide via the onboard FM repeater system. The communications and experiment missions will run concurrently. The repeater features a VHF downlink with FM analog voice and FSK data and UHF and L-band uplink.

AMSAT has teamed with Spaceflight Inc. for integration and launch utilizing Spaceflight?s Sherpa system on a Falcon-9 v1.2 (Block 5) launch vehicle to a sun-synchronous orbit in the third quarter of 2015. The mission was the rebooked on the SSO-A cluster launch also on a Falcon-9 v1.2 (Block 5) in late 2017 or early 2018.

Satellite COSPAR Date LS Launch Vehicle Remarks
AO-95 2018-099N 2018-12-03 AFWTR Falcon-9 v1.2 (Block 5) with SkySat 14, 15, Eu:CROPIS, STPSat 5, FalconSat 6, NEXTSat 1, KazSTSAT, eXCITe, SeeMe, ICEYE X2, BlackSky 2, ESEO, Hawk A, B, C, Capella 1, AISTECHSAT 2, CSIM-FD, Hiber 2, ITASAT 1, Landmapper-BC 4, ORS 7A, 7B, Al-Farabi 2, Astrocast 0.1, Audacy 0, BRIO, Centauri 1, Eaglet 1, Enoch, Flock-3s 1, 2, 3, K2SAT, KazSciSat 1, MinXSS 2, Orbital Reflector, RAAF M1, SeaHawk 1, SNUSAT 2, THEA, VESTA, PW-Sat 2, SNUGLITE, VisionCube, RANGE A, B, Elysium-Star 2, ExseedSat 1, Irvine 02, JY1-Sat, KNACKSAT, MOVE 2, SpaceBEE 5, 6, 7, Suomi-100, WeissSat 1, Sirion Pathfinder 2, OrbWeaver 1, 2, SPAWAR-CAL O, OR, R