View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40967U 26072.41720606 +.00000000 +00000-0 +36306-3 0 00003
2 40967 64.7750 216.4686 0128798 94.4174 267.1665 14.90389712 01
| Epoch (UTC): | 13 March 2026 10:00:46 |
| Eccentricity: | 0.0128798 |
| inclination: | 64.7750° |
| perigee height: | 507 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 216.4686° |
| argument of perigee: | 94.4174° |
| revolutions per day: | 14.90389712 |
| mean anomaly at epoch: | 267.1665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|