Official name UME 1 (ISS 1)
Alternative name UME 1
Cospar ID 1976-019A
Norad ID 8709
Launch date 1976-02-29
Launch site TNSTA
Launch vehicle N-1
Country/Organization Japan
Type application Research, Ionosphere
Operator NASDA
RCS size LARGE
Decay date ON ORBIT
Period (min) 104.98
Inclination (deg) 69.67
Perigee (km) 987
Apogee (km) 1000
Eccentricity 0.00654252642174132
Mean motion (revs. per day) 13.7168984568489
Semi-Major axis (km) 7371.635
Raan (deg) 223.8697
Arg of perigee (deg) 21.7305
Shape Cyl
Mass (kg) 137.76
Diameter (m) 0.8
Height (m) 0.9
Span (m^2) 0.9
Contractors Mitsubishi Electric Corporation (MELCO)
Power Solar cells, batteries

The ISS (Ionosphere Sounding Satellite) series of satellites was Japan's first ionosphere sounding satellite project. After reaching orbit, they were named Ume.

ISS a or Ume 1 was used to monitor radio waves in the ionosphere and forecast conditions for optimal use of shortwave communications. A power supply system failure caused Ume to malfunction one month after launching.

ISS b or Ume 2 was put into orbit two years later as a replacement. Ume-2 kept gathering observation data even after its 1.5 year mission term. It finished its operation on 23 February 1983, because of deterioration of power generation.

Satellite COSPAR Date LS Launch Vehicle Remarks
UME 1 (ISS 1) 1976-019A 1976-02-29 TNSTA N-1
UME 2 (ISS-B) 1978-018A 1978-02-16 TNSTA N-1