
Japan's first ionoshere sounding satellite was named Ume. It was used to monitor radio waves in the ionosphere and forecast conditions for optimal use of shortwave communications.
Ume-2 was put into orbit two years later - a power supply system failure caused Ume to malfunction one month after launching.
Ume-2 kept gathering obserration data even after its 1.5 year mission term. And it finished its operation on February 23,1983,because of deterioration of power generation.
| UME (ISS) | Launch Date | 2/29/1976 |
|---|---|---|
| Launch Vehicle | N-I Launch Vehicle (N2F) | |
| Launch Site | Tanegashima Space Center | |
| Weight | 139kg | |
| UME-2 (ISS-b) | Launch Date | 2/16/1978 |
| Launch Vehicle | N-I Launch Vehicle (N4F) | |
| Launch Site | Tanegashima Space Center | |
| Weight | 141kg | |
| Orbit | 1000km(alt)circular/70 inclination/105 min. period | |
| Dimensions | Cylindrical, D:94cm | |