View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59949U 26145.39404507 +.00000000 +00000-0 -14572-5 0 00004
2 59949 53.1588 233.1061 0001114 64.8122 295.3012 15.69686215 05
| Epoch (UTC): | 25 May 2026 09:27:25 |
| Eccentricity: | 0.0001114 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 233.1061° |
| argument of perigee: | 64.8122° |
| revolutions per day: | 15.69686215 |
| mean anomaly at epoch: | 295.3012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|