View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40338U 26145.61166912 +.00000000 +00000-0 +13817-3 0 00004
2 40338 63.3897 8.9494 0364651 9.0596 351.6777 13.45412232 07
| Epoch (UTC): | 25 May 2026 14:40:48 |
| Eccentricity: | 0.0364651 |
| inclination: | 63.3897° |
| perigee height: | 817 km |
| apogee height: | 1361 km |
| right ascension of ascending node: | 8.9494° |
| argument of perigee: | 9.0596° |
| revolutions per day: | 13.45412232 |
| mean anomaly at epoch: | 351.6777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|