View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65905U 26145.36850095 +.00000000 +00000-0 +69102-3 0 00003
2 65905 53.1608 15.2079 0001857 101.4886 258.6324 15.30201932 09
| Epoch (UTC): | 25 May 2026 08:50:38 |
| Eccentricity: | 0.0001857 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 15.2079° |
| argument of perigee: | 101.4886° |
| revolutions per day: | 15.30201932 |
| mean anomaly at epoch: | 258.6324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|