MEMS 1 & 2 |
USA |
Designation | 26080 / 00004H |
Launch date | 27 Jan 2000 - 03:03 UT |
Launch site | Va, SLC-8 |
Launch vehicle | Minotaur (#1) |
Mission | Technology, intersatellite communications experiment |
Earth orbit on Feb 08, 2000: | |
Perigee / Apogee | 749 x 800 km |
Eccentricity | 0.004 |
Inclination | 100.23 deg |
Period | 100.33 min |
Prime contractor | - |
Platform | OPAL satellite |
Mass at launch | 2 x 0.25 kg |
Mass in orbit | |
Dimension | 10 x 7.5 x 2.5 cm |
Solar array | none |
Stabilization | none |
DC power | |
Design lifetime |