View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62011U 26145.35733568 +.00000000 +00000-0 +14319-2 0 00001
2 62011 53.1575 23.5430 0000910 62.4801 297.6309 15.69781856 08
| Epoch (UTC): | 25 May 2026 08:34:33 |
| Eccentricity: | 0.0000910 |
| inclination: | 53.1575° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 23.5430° |
| argument of perigee: | 62.4801° |
| revolutions per day: | 15.69781856 |
| mean anomaly at epoch: | 297.6309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|