Meteor-3M 1 |
CIS |
Spacecraft n°: |
CIS satellite n°: |
| Designation | 27001 / 01056A |
| Launch date | 10 Dec 2001 - 17:18:57 UT |
| Launch site | B, LC45/1 |
| Launch vehicle | Zenit-2 (S/N 19L - 1381573091) |
| Mission | Weather |
| Sun-Synchronous LEO orbit: | |
| Perigee / Apogee | 996 x 1015 km |
| Eccentricity | 1.29E-03 |
| Inclination | 99.5 deg |
| Period | 105.24 min |
| Prime contractor | Elektromekhanika Research Institute (VNIIEM) |
| Platform | |
| Operator | |
| Mass at launch | 2500 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| DC power | 1000 W |
| Design lifetime | 3 yrs |